128
134 1 J 1,1 EMISSION·CONTROL DEVICES FOR CONVENTIONAL INTERNAL COMBUSTION ENGINE DESIGNS AND THEIR IMPLICATIONS FOR OXIDANT CONTROL STRATEGIES by Robert F. Sawyer Professor, Department of Mechanical Engineering University of California Berkeley, California Most of my comments today will be based upon the National Academy of Sciences study which has just recently been completed. There are at least two other people here who have been closely associated with that study, Professor Newhall, University of Wisconsin, recently of Chevron Research, who will be the second speaker, and Dr. Benson of Stanford Research Insti- tute, who was one of the committee members on that study. There has been some confusion about the National Academy of Sciences study, since there have been several recently in the automotive emissions area. The one which appeared in September, 1974, by the Costs/Benefit Panel received a great deal of publicity, some of it somewhat negative. I would encourage you to read all four volumes of that report. It does contain a lot of good information. It did deal with a very fuzzy subject, that of benefits vs. costs of air pollution control and, therefore, was not as precise as some would like. The report which has recently been completed (the volumes were released last week) is called the Report by the Committee on Motor Vehicle Emissions. Because the interest is high, I'll take a moment to tell you how to get a copy. Request the Report by the Committee on Motor Vehicle Emissions by writing to the National Academy of Sciences, specifically the Commission on Sociotechnical Systems, National Research Council, 2101 Constitution Avenue, Washington, DC 20418.

EMISSION·CONTROL DEVICES FOR CONVENTIONAL INTERNAL

  • Upload
    others

  • View
    1

  • Download
    0

Embed Size (px)

Citation preview

134

1 J 11

EMISSIONmiddotCONTROL DEVICES FOR CONVENTIONAL INTERNAL COMBUSTION ENGINE DESIGNS AND THEIR

IMPLICATIONS FOR OXIDANT CONTROL STRATEGIES

by

Robert F Sawyer Professor Department of Mechanical Engineering

University of California Berkeley California

Most of my comments today will be based upon the National Academy of

Sciences study which has just recently been completed There are at least

two other people here who have been closely associated with that study

Professor Newhall University of Wisconsin recently of Chevron Research

who will be the second speaker and Dr Benson of Stanford Research Instishy

tute who was one of the committee members on that study

There has been some confusion about the National Academy of Sciences

study since there have been several recently in the automotive emissions

area The one which appeared in September 1974 by the CostsBenefit

Panel received a great deal of publicity some of it somewhat negative

I would encourage you to read all four volumes of that report It does

contain a lot of good information It did deal with a very fuzzy subject

that of benefits vs costs of air pollution control and therefore was

not as precise as some would like The report which has recently been

completed (the volumes were released last week) is called the Report by

the Committee on Motor Vehicle Emissions Because the interest is high

Ill take a moment to tell you how to get a copy Request the Report by

the Committee on Motor Vehicle Emissions by writing to the National

Academy of Sciences specifically the Commission on Sociotechnical Systems

National Research Council 2101 Constitution Avenue Washington DC 20418

135

Some of you may have received copies already those who contributed to the

study should have received copies by this time

One thing that has become apparent during the first day of this

meeting and was even reflected by the previous speaker is that there

remain a lot of unknowns a lot of questions that seem to me should have

been answered in the last ten years In spite of the uncertainties about

the causeeffect relationships between emission sources and photochemical

smog the decision fortunately has been made to go ahead and control the

smog anyway The general conclusion has been that air pollution is

reduced by reducing the emission of air pollutants and an aggressive

automobile emission control program has been initiated although it has

been delayed several times and the results have not come as rapidly as

one would have hoped With the 1975 automobiles there is indeed a subshy

stantial reduction in hydrocarbon and CO emissions this impact should now

begin to be felt over the next 10 years as these vehicles replace those

already on the road

The costs of these emissions controls are large somewhere between

one and five billion dollars per year The costs are large especially in

comparison with the investment that has been made in fundamental research

to understand the nature of the air pollution problem I would like to

discuss several points First I would like to say a few words on the

background of the automotive engine emissions controls then I would like

to give my assessment of the 1975 California vehicle and its emission

control system--just what its strong points and problems are and finally

I will try to identify what the critical problem areas are now in automotive

emissions controls

I believe it is important to remind you that the automobile engine was

developed over the last 50 years with goals in mind which had nothing to do

136

with air pollution As a consequence we have an automobile engine which

is a low-cost production item has a high power-to-weight ratio has

turned out to be a reliable relatively low maintenance very durable

device and in some cases even the fuel economy is not so bad Then after

the fact it was decided that this engine rhould be made to be low

emitting Therefore it is not too surprising that the approach of the

automobile industry has been to modify thi engine in which they have a

great deal of confidence and know how to build inexpensively as little as

possible The control approaches therefore have been minor modifications

to the engine and have now focused upon processing the exhaust This to

my thinking as an engineer is not a good approach But objectively if

one judges simply on the basis of whether emissions are controlled or not

has worked out quite well I do not think we can be too critical of the

add-on catalyst technology if it works The evidence now suggests that it

is going to work that it is probably cost effective and that the autoshy

mobile industry probably deserves more credit than they are receiving for

the job theyve done in developing the oxidation catalyst for the autoshy

mobile engine What Im saying is the add-on approach is not necessarily

all that bad

Again to give some general perspective on how one might approach

automotive emission controls and how we arrived where we are Id like to

discuss Figure 1 which points out several approaches to controlling

emissions from the automobile engine These are

1) preparation of the air fuel mixture which has received only minor

attention by the auto industry

2) modification of the engine itself the combustion process which

is not very evident in the 1975 automobiles but will be the subject of

Dr Newhalls presentation and

I I

I

137

3) the general field of exhaust treatment where most of the effort

has been placed by the U S auto industry

I would like to emphasize that the first area the whole matter of

mixture control that is either improving the present carburetor or

replacing it with a better mixture control system is perhaps the single

technological area which has been most overlooked by the automobile

industry The engine requires a well meteTed fuel-to-air mixture over a

wide variety of operating conditions that is good cycle-to-cycle and

cylinder-to-cylinder control The present systems simply do not do that

It is also evident that the mixture control system must operate with varying

ambient conditions of pressure and temperature The present systems do not

do that adequately There are promising developments in improvement of

mixture control systems both carbureted and fuel injection which do not

appear to be under really aggressive develJpment by the automobile industry

One should question why this is not occurring

I will skip the area of combustion modification because that really

comes under the new generation of engines The combustion modification is

an important approach and will be discussed by the next speaker

The area of exhaust system treatment the third area is the one about

which youve seen the most We early saw the use of air injection and then

improved air injection with thermal reactors Now were seeing oxidation

catalysts on essentially 100 of the U S cars sold in California There

are yet other possibilities for exhaust treatment for the control of

oxides of nitrogen based upon reduction catalysts or what is known as

threeway catalysts another variation of the reduction catalyst and

possibly also the use of particulate traps as a way of keeping lead in

gasoline if that proves a desirable thing to do (which does not appear to

be the case)

138

What about the 1975 California car Most of you probably have enough

interest in this vehicle that youve tried to figure out just what it does

But in case some of you have not been able to straighten its operation out

let me tell you as best I understand what the 1975 California car is

The cars from Detroit are 100 cataly~t eq11ipped There may be an excepshy[

l

1 tion sneaking through here and there but it looks like it is 100 These

are equipped with oxidation catalysts in a variety of configurations and

sizes the major difference being the pellet system which is used by

General Motors versus the monolith system which has been used by Ford and

Chrysler The pellet system appears to be better than the monolithic ~ l l system but it is not so obvious that there are huge differences between the

aocgtnow The catalysts come in a variety of sizes they are connected to

the engine in different ways sometimes there are two catalysts sometimes

a single catalyst (the single catalyst being on the 4 and 6-cylinder

engines) Some of the 8-cylinder engines have two catalysts some of them

have one catalyst All California cars have all of the exhaust going

through catalysts This is not true of some of the Federal cars in which

some of the exhaust goes through catalysts and some does not

Ninety percent of the California cars probably will have air pumps

Practically all the cars from Detroit have electronic ignition systems

which produce more energetic sparks and more reliable ignition The

exhaust gas recirculation (EGR) systems appear to have been improved

somewhat over 1974 but not as much as one would have hoped There were

some early designs of EGR systems which were fully proportional sophistishy

cated systems These do not appear to have come into final certification

so that there still is room for further improvement of the EGR system

The emissions levels in certification of these vehicles are extremely low

139

(Table I) Just how the automc1bile industry selects the emission levels

at which they tune their vehicles has been of great interest The

hydrocarbon and CO levels in certification (with deterioration factors

applied--so this is the effective emissions of the certification vehicles

at the end of 50000 miles) are approximately one-half the California

standards The oxides of nitrogen emissions are approximately two-thirds

of the California standards This safety factor is put in by the automoshy

bile industry to allow for differences between the certification vehicles

and the production vehicles to ensure that they did not get into a situation

of recall of production vehicles which would be very expensive

There appears to have been a great deal of sophistication developed by

the automobile industry in being able to tune their vehicles to specific

emission levels General Motors appears to have done better tuning than

the other manufacturers This leads to the rather interesting result

that a significant number of the 1975 California vehicles meet the 1977

emission standards (Table II) that is approximately 10 of the U S cars

certified for California already meet the 1977 emission standards This

does not mean to say that the industry could immediately put all of their

production into such vehicles and meet the 1977 emission standards because

of a concern about the safety factor for the certification versus producshy

tion vehicles Thirty-four percent of the foreign vehicles certified for

1975 in California meet the 1977 emission standards The 1977 emission

standards are 041 grn hydrocarbon~ 34 gm carbon monoxid~ and 20 gm

oxides of nitrogen This does confirm that the oxidation catalysts are a

more than adequate technology for meeting the 1977 emission standards and

only minor refinements and adjustments to those systems are required to go

ahead with the 1977 emission standards There are some other arguments

against this optimistic viewpoint and Ill deal with those later

140

There is a great uniformity in the deBigns which the U S manufacturshy

ers have selected for the 1975 California vehicles For those of you who

do not live in California about 80 of thl~ vehicles in the rest of the

country will be catalyst equipped General Motors is going with 100

catalysts apparently to realize the fuel economy benefit of their system

which more than pays for the cost of the catalyst system We have the very

interesting situation that the more stringent 1975 emission standards have

not only reduced the emissions of the 1975 vheicles with respect to the

1973-1974 vehicles but have also reduced the cost of operating the car

and have improved fuel economy The idea that emissions control and fuel

economy and economical operation are always one at odds with the other is

simply not true Compared to the previous years vehicles the more

stringent emissions standards of 1975 have brought improvements to fuel

economy because they forced the introduction of more advanced technology

The fuel savings which have been realized produce a net decrease in operashy

tional costs over the lifetime of the car This is not to say that pollution

control doesnt cost something If you were to compare the 1975 vehicle

with a completely uncontrolled vehicle tht~re would indeed be an incremental

cost associated with the 1975 vehicle

The foreign manufacturers have demonstrated a greater variety of

approaches in meeting the 1975 California standards but again they are

producing mostly catalyst equipped vehicles There is a widespread use of

fuel injection by the foreign manufacturers especially the Europeans

apparently because this is the easiest appmiddotroach for them and they realize

that only a fraction of their production comes to the United States

Volkswagen for example apparently has gone to 100 fuel injection on its

air cooled engines to be sold in California Mazda will continue to sell

141

rotary engine vehicles and thereby be the only rotary engine vehicle

manufacturer and marketer in the United States General Motorsgt elimination

of therotary engine stated for reasons of emissions is probably more

influenced by problems with fml economy although the two are a bit

difficult to separate Mazda is meeting the 1975 emissions standards and

in fact can meet the 1977 emission standards It has not solved its fuel

economy difficulties on the 1975 cars they will do better in 1976 All

evidence points to a fuel economy penalty for the rotary engine Nonetheshy

less we do have this option available because of the Japanese Also the

foreign manufacturers are providing us with a small number of diesel

engine cars These are of great interest because of definite fuel economy

advantages The diesel engine vehicles also meet the 1977 emissions

standards right now Also in J975 well 3ee the CVCC engine marketed by

Honda

The costs of the 1975 vehicles over tae lifetime of the vehicle are

definitely lower than the costs of the 197~ vehicles The National Academy

of Sciences estimate averaged over all vehicles is that in comparison to

the 1970 vehicles the lifetime cost of emission control system including

maintenance and fuel economy costs is aboJt $250 per vehicle greater in

1975 than 1970 Since the 1974 vehicles w2re about $500 more expensive

there has been a net saving in going from 1974 to 1975 I think the

conclusion we should draw for 1975 is that the auto industry has done a

pretty good job in meeting these standards This is something which they

said they couldnt do a few years ago something which they said that if

they could do it would be much more expewdve than it has turned out to

be

The same technology can be applied to 1977 models with no technological

difficulty and only slight refinements of the systems The fuel economy

142

penalties as estimated by the National Academy of Sciences are small 3

or less in going to the 1977 standards This estimate does assume further

advancements by the auto industry to improve fuel economy--primarily

improved exhaust gas recirculation systems It is unfortunate that this

issue of fuel economy has become so mixed up with the air pollution question

because the two are only slightly related If one is really concerned about

fuel economy and there isnt too much evidence that the auto industry or

the American public really is too concerned right now there is only one

way to have a drastic effect on fuel economy and that is to decrease the

vehicle weight Until that is done with gains on the order of 50 or

more to worry about 3 or 5 differences in fuel economy related to emission

control systems is simply to focus upon the wrong issue

Now what are the problem areas What remains to be done The

problems certainly arent over with the introduction of the 1975 vehicles

Problem Area Number One Field performance What is going to happen

to these vehicles when they get into actual service Past experience with

the 1971 through 1973 vehicles has been rather poor in that EPA and

California surveillance data show that these vehicles are not meeting the

standards Many of them did not meet the standards when they were new

The situation in general is getting worse at least for CO and hydrocarbons

that is with time the emission levels of CO and hydrocarbons for the 1971 I through 1973 vehicles is degrading There is no in-service experience of

this sort with the 1975 vehicles yet The certification data look quite I promising but the test procedures especially for durability are not ithe same as what occurs in actual use It is generally stated that the

1actual use situation for the catalysts will be more severe than the EPA

test procedure A larger number of cold starts are involved in actual use

than in the EPA test procedure and thermal cycling will probably have an

143

adverse effect on the lifetime of the cata]_yst This is not so obvious

It is also likely that the higher temperature duty cycle in actual use will

improve the performance of the catalyst in that it will help to regenerate

the catalyst through the removal of contaminants as long as one does not

get into an overheat situation The National Academy of Sciences estimate

was that the number of catalyst failures tn the first 50000 miles would

be on the order of about 7 Thats a very difficult number to estimate in

the absence of any real data A 7 failure still leaves a net gain in

emissions control even if nothing is done about this failure This points

to the problem of what happens after 50000 miles The EPA certification

procedure and control program only addresses the first 50000 miles The

second 50000 miles or slightly less for the average car is the responsishy

bility of the states Unfortunately then~ seems to be very little progress

in the area of mandatory inspection and ma-Lntenance--very little thought

being given to whether the replacement ofthe catalyst at 50000 miles

if it has failed is going to be required and how that is going to be

brought about The area of field performance remains a major problem

area one which obviously needs to be monitored as the California Air

Resources Board has been doing in the past but probably even more carefully

because the unknowns are higher with the catalyst systems

Problem Area Number Two Evaporative hydrocarbons from automobiles

It was identified at least 18 months ago that the evaporative emission

control systems are not working that the evaporative emissions are on the

order of 10 times greater than generally thought In the Los Angeles

area cars which are supposed to be under good evaporative emissions

controls are emitting approximately 19 grams per mile of hydrocarbons

through evaporation This apparently has to do with the test procedure used

144

The EPA is pursuing this The California Air Resources Board does have some

consideration going on for this but it appears that the level of activity

in resolving this problem is simply not adequate If we are to go ahead

to 04 of a gram per mile exhaust emissions standards for hydrocarbons

then it just doesnt make sense to let 19 grams per mile equivalent escape

through evaporative sources

Problem Area Number Three What about the secondary effects of the

catalyst control systems Specifically this is the sulfate emissions

problem and I really do not know the answer to that Our appraisal is

that it is not going to be an immediate problem so we can find out what

the problem is in time to solve it The way to solve it now since the

automobile industry is committed to catalysts and it is unreasonable

to expect that they will reverse that technology in any short period of

time is take the sulfur out of the gasoline The cost of removing sulfur

from gasoline is apparently less than one cent per gallon Therefore if

it becomes necessary to be concerned with sulfate emissions the way to

meet the problem is to take the sulfur out of gasoline Obviously sulfate

emissions need to be monitored very carefully to see what happens The

final appraisal is certainly not now available Another secondary effect

of the catalysts is the introduction of significant quantities of platinum

into an environment where it hasnt existed before Not only through

exhaust emissions which appear to be small but also through the disposal

problem of the catalytic reactors Since the quantity of platinum involved

is quite small the argument is sometimes used that platinum does not

represent much of a problem The fact that the amount of platinum in the

catalyst is so small may also mean that its not economical to recover it

This is probably unfortunate because then the disposal of these catalysts

l Jj

145

I becomes important I will not speak to the medical issues because

am not qualified The evidence is that theuro~ platinum will be emitted in a

form which does not enter into biological cycles--but this is no assurance

that it couldnt later be transformed in such a form What is obviously

needed is a very careful monitoring program which hopefully was started

before the catalysts were put into service If it wasnt then it should

be started today

Problem Area Number Four NO control The big problem with NO X X

control is that nobody seems to know or to be willing to establish what

the emission control level should be It is essential that this be tied

down rapidly and that it be fixed for a reiatively long period of time

because the NO level is going to have a VE~ry important ef feet upon the X

development of advanced engine technology The 20 gm level has been

attained in California with some loss of fuel economy through the use of

EGR and it is not unreasonable in our estimation to go to 15 grams per

mile with very little loss in fuel economy To go to 04 gram per mile

with present technology requires the use of one of two catalytic systems

either the reduction catalyst in tandem with the oxidation catalyst or what

is known as the three-way catalyst Both of these systems require technoshy

logical gains The state of development appears to be roughly that of the

oxidation catalyst two years ago The auto industry will probably say

that it is not quite that advanced but that if it were required to go to

04 gram per mile in 1978 that it could be done With the catalyst systems

the fuel economy penalties would not be great in fact the improvement to

the engine which would be required to make the system work would again

probably even allow a slight improvement in fuel economy What the 04

gram per mile NO catalyst system would appear to do however is to X

146

eliminate the possibility of the introduction of stratified charge engines

both the CVCC and the direction injection system and also diesel engines

It is in the context of the advantages of these advanced engines to meet

emission standards with improved fuel economy that one should be very

cautious about the 04 grammile oxides of nitrogen standards for automoshy

biles My own personal opinion is that the number should not be that

stringent that a number of 1 or 15 gm is appropriate Such a level

would require advancements but would not incur great penalties

Other items which I view as problem areas are less technically

involved and therefore require fewer comments

bull Nonregulated pollutants--again thls is a matter of keeping track

of particulates aldehydes hydrocarbon composition to make

certain that important pollutants ire not being overlooked or

that emission control systems are not increasing the output of

some of these pollutants

bull Fuel economy The pressures of fuel economy are going to be used

as arguments against going ahead wlth emissions control Mostly

these two can be resolved simultaneously We should simply ask

the automobile industry to work harder at this

bull Final problem area New fuels Again it does not appear that

the introduction of new fuels will come about as an emissions

control approach but that they may be introduced because of the

changing fuel availability patterns and the energy crisis These

fuels should be watched carefully for their impact upon emissions

This does middotappear to be an area in which a great deal of study is

going on at the present time It is one problem area perhaps in

which the amount of wprk being done is adequate to the problem

which is involved

147

In sunnnary then the appraisal of the 1975 systems is that they are

a big advancement they will be a lot better than most of us thought and

that we should give the automobile industry credit for the job theyve

done in coming up with their emissions control systems

With that boost for the auto industry which Im very unaccustomed

to Ill entertain your questions

-------=-~ ~~~ U- ~a1

~_~a--~-~ -J~ ~ -~r- _ --=~-- -___ja--~ __1~~ ~-~----=

AIR

1-4 FUEL----1

I I ENGINE

I II

_________ EXHAUST SYSTEM I bull EXHAUST

I I I

+ MIXTURE CONTROL COMBUSTION MODIFICATION EXHAUST TREATMENT

FuelAir Metering Ignition Air Jnjection FuelAir Mixing Chamber Geometry Thermal Reactor Fuel Vaporization Spark Timing Oxidation Catalyst Mixture Distribution Staged Combustion Reduction Catalyst Fuel Characteristics Ex tern almiddot Combustion Three Way Catalyst Exhaust Gas Redrculation Particulate Trap

FIGURE 1 Approaches to the Control of Engine Emissions

~ i 00

149

TABLE I

Average Emissions of 1975 Certification Vehicles (As Corrected Using the 50000-Mile Deterioration Factor)

Emissions in gmi Fraction of Standard HC CO NO HC CO NO

Federal 1975 X X

AMC 065 67 25 043 045 080

Chrysler 074 77 25 049 051 082

Ford 081 92 24 054 061 078

GM 083 80 23 055 053 074

Weighted Average 080 82 24 053 055 076

California 1975

AMC 042 49 17 047 054 087

Chrysler 048 61 16 053 067 082

Ford 052 56 13 058 062 067

GM 065 55 16 0 72 061 082

Weighted Average 058 56 16 064 062 078

kWeighted average assumes the following market shares AMC 3 Chrysler 16 Ford 27 and GM 54

150

TABLE II

Total Number of Vehicles Certified for California 1975 Standard and the Number (and percentage) of These Able to Meet

Certain More Stringent Standards

Calif 1975 Federal 1977 Hypothesized Hypothes ized 099020 04J420 049020 093420

i ~

Manufacturer no () no () no () no ()

AMC 16 (100) 1 ( 6) ti ( 38) 3 (19)

Chrysler 21 (100) 2 ( 9) ( 33) 0 ( O)

Ford 26 (100) 4 (15) -middot ( 15) 5 (19)

l GM 46 (100) 1 ( 2) -1 ( 9) 5 (11)

Foreign 62 (100) 21 (34) 3H (61) 28 (45)

1J

f

-l

151

CURRENT STATUS OF ALTERNATIVE AUTOM)BIIE ENGINE TECHNOLCXY

by

Henry K Newhall Project Leader Fuels Division

Chevron Research CanpanyRicbmmd California

I

iH1middot

10 1ntroduction and General Background

I

11 General

The term stratified ct1arge englne has been used for many

years in connection with a variety of unconventional engine

combustion systems Common to nearly all such systems is

the combustion of fuel-air mixtures havlng a significant

gradation or stratification in fuel- concentration within the

engine combustion chamber Henee the term nstratifled charge

Historically the objective of stratified charge engine designs

has been to permit spark ignition engine operation with average

or overall fuel-air ratios lean beyond the ignition limits of

conventional combustion systems The advantages of this type

of operation will be enumerated shortly Attempts at achieving

this objective date back to the first or second decade of this

century 1

More recently the stratified charge engine has been recognized

as a potential means for control of vehicle pollutant emissions

with minimum loss of fuel economy As a consequence the

various stratified charge concepts have been the focus of

renewed interest

152

12 Advantages and Disadvantages of Lean Mixture Operation

Fuel-lean combustion as achieved in a number of the stratified

charge engine designs receiving current attention has both

advantages and disadvantages wnen considered from the comshy

bined standpoints of emissionsmiddot control vehicle performance

and fuel economy

Advantages of lean mixture operation include the following

Excess oxygen contained in lean mixture combustion

gases helps to promote complete oxidation of hydroshy

carbons (HG) and carbon monoxide (CO) both in the

engine cylinder and in the exhaust system

Lean mixture combustion results in reduced peak

engine cycle temperatures and can therefore yield

lowered nitrogen oxide (NOx) emissions

Thermodynamic properties of lean mixture combustion

products are favorable from the standpoint of engine

cycle thermal efficiency (reduced extent cf dissociashy

tion and higher effective specific heats ratio)

Lean mixture operation caG reduce or eliminate the

need for air throttling as a means of engine load

control The consequent reduction in pumping losses

can result in significantly improved part load fuel

economy

153

Disadvantages of lean mixture operation include the following

Relatively low combustion gas temperatures during

the engine cycle expansion and exhaust processes

are inherent i~ lean mixture operation As a conseshy

quence hydrocarbon oxidation reactions are retarded

and unburned hydrocarbon exhaust emissions can be

excessive

Engine modifications aimed at raising exhaust temperashy

i tures for improved HC emissions control (retarded middot~

ignition timing lowered compression ratlo protrtacted combustion) necessarily impair engine fuel economy1 I

1j bull If lean mixture operation is to be maintained over ~

the entire engine load range maximum power output t l and hence vehicle performance are significantly

impaired

Lean mixture exhaust gases are not amenable to treatshy

ment by existing reducing catalysts for NOx emissions

control

Lean mixture combustion if not carefully controlled

can result in formation of undesirable odorant

materials that appear ln significant concentrations

in the engine exhaust Diesel exhaust odor is typical

of this problem and is thought to derive from lean mixshy

ture regions of the combustion chamber

154

Measures required for control of NOx emissions

to low levels (as example EGR) can accentuate

the above HC and odorant emissions problems

Successful developmentmiddotor the several stratified charge

engine designs now receiving serious attention will depend

very much on the balance that can be achieved among the

foregoing favorable and unfavorable features of lean comshy

bustion This balance will of course depend ultimately on

the standards or goals that are set for emissions control

fuel economy vehicle performance and cost Of particular

importance are the relationships between three factors -

UBHC emissions NOx emissions and fuel economy

13 Stratified Charge Engine Concepts

Charge stratification permitting lean mixture operation has

been achieved in a number of ways using differing concepts

and design configurations

Irrespective of the means used for achieving charge stratifishy

cation two distinct types of combustion process can be idenshy

tified One approach involves ignition of a small and

localized quantity of flammable mixture which in turn serves

to ignite a much larger quantity of adjoining or sur~rounding

fuel-lean mixture - too lean for ignition under normal cirshy

cumstances Requisite m1xture stratification has been achieved

155

in several different ways rangiDg from use of fuel injection

djrectly into open combustion chambers to use of dual

combustion chambers divided physically into rich and lean

mixture regions Under most operating conditions the

overall or average fuel-air ratio is fuel-lean and the

advantages enumerated above for lean operation can be realized

A second approach involves timed staging of the combustion

process An initial rich mj_xture stage in which major comshy

bustion reactions are completed is followed by rapid mixing

of rich mixture combustion products with an excess of air

Mixing and the resultant temperature reduction can in

principle occur so rapidly that minimum opportunity for NO

formation exists and as a consequence NOx emissions are

low Sufficient excess air is made available to encourage

complete oxidation of hydrocarbons and CO in the engine

cylinder and exhaust system The staged combustion concept

has been specifically exploited 1n so-called divided-chamber

or large volume prechamber engine designs But lt will be

seen that staging is also inherent to some degree in other

types of stratified charge engines

The foregoing would indicate that stratified charge engines

can be categorized either as lean burn engines or staged

combustion engines In reality the division between conshy

cepts is not so clear cut Many engines encompass features

of both concepts

156

14 Scope of This Report

During the past several years a large number of engine designs

falling into the broad category of stratified charge engines

have been proposed Many of these have been evaluated by comshy

petent organizations and have been found lacking in one or a

number of important areas A much smaller number of stratified

charge engine designs have shown promise for improved emissions

control and fuel economy with acceptable performance durashy

bility and production feasibility These are currently

receiving intensive research andor development efforts by

major organizations - both domestic and foreign

The purpose of this report is not to enumerate and describe the

many variations of stratified charge engine design that have

been proposed in recent years Rather it is intended to focus

on those engines that are receiving serious development efforts

and for which a reasonably Jarge and sound body of experimental

data has evolved It is hoped that this approach will lead to

a reliable appraisal of the potential for stratified charge

engine systems

20 Open-Chamber Stratified Charge Engines

21 General

From the standpoint of mechanical design stratified charge

engines can be conveniently divided into two types open-chamber

and dual-chamber The open-chamber stratjfied charge engine

has a long history of research lnterest Those crigines

157

reaching the most advanced stages of development are probably

the Ford-programmed c~mbustion process (PROC0) 2 3 and Texacos

controlled combustion process (TCCS) 4 5 Both engines employ a

combination of inlet aar swirl and direct timed combustion

chamber fuel injection to achieve a local fuel-rich ignitable

mixture near the point of ignition _For both engines the overshy

all mixture ratio under most operating conditions is fuel lean

Aside from these general design features that are common to

the two engiries details of their respective engine_cycle proshy

cesses are quite different and these differences reflect

strongly in comparisons of engine performance and emissions

characteristics

22 The Ford PROCO Engin~

221 Description

The Ford PROCO engine is an outgrowth of a stratified charge

development program initiated by Ford in the late 1950s The

development objective at that time was an engine having dieselshy

like fuel economy but with performance noise levels and

driveability comparable to those of conventional engines In

the 1960s objectives were broadened to include exhaust

emissions control

A recent developmental version of the PROCO engine is shown in

Figure 2-1 Fuel is injected directly into the combustion chamber

during the compression stroke resulting in vaporjzation and

formation of a rich mixture cloud or kernel in the immediate

158

vicinity of the spark plug(s) A flame initiated in this rich

mixture region propagates outwardly to the increasingly fuelshy

lean regions of the chamber At the same time high air swirl

velocities resulting from special orientation of the air inlet

system help to promote rapid mixing of fuel-rich combustion

products with excess air contained in the lean region Air

swirl is augmented by the squ1sh action of the piston as it

approaches the combustion chamber roof at the end of the comshy

pression stroke The effect of rapid mixing can be viewed as

promoting a second stage of cori1bustion in which rlch mixture

zone products mix with air contained in lean regions Charge

stratification permits operation with very lean fuel-air mixshy

tures with attendent fuel economy and emissj_ons advantages In

addition charge stratification and direct fuel injection pershy

mit use of high compression ratios with gasolines of moderate

octane quality - again giving a substantial fuel economy

advantage

Present engine operation includes enrichment under maximum

power demand conditions to mixture ratios richer than

stoichiometric Performance therefore closely matches

that of conventionally powered vehicles

Nearly all PROCO development plans at the present time include

use of oxidizing catalysts for HC emissions control For a

given HC emissions standard oxidizing catalyts permit use

of leaner air-fuel ratios (lower exhaust temperatures)

1

l

159

together with fuel injection and ignition timing charactershy

istics optimized for improved fuel economy

222 Emissions and Fuel Economy

Figure 2-2 is a plot of PROCO vehicle fuel economy versus NOx

emissions based or1 the Federal CVS-CH test procedure Also

included are corresponding HC and CO emissions levels Only

the most recent test data have been plotted since these are

most representative of current program directions and also

reflect most accurately current emphasis on improved vehicle

fuel economy 6 7 For comparison purposes average fuel

economies for 1974 production vehicles weighing 4500 pounds

and 5000 pounds have been plotted~ (The CVS-C values

reported in Reference 8 have been adjusted by 5 to obtain

estimated CVS-CH values)

Data points to the left on Figure 2-2 at the o4 gmile

NOx level represent efforts to achieve statutory 1977

emissions levels 6 While the NOx target of o4 gmile was

met the requisite use of exhaust gas recirculation (EGR)

resulted in HC emissions above the statutory level

A redefined NOx target of 2 gn1ile has resulted in the recent

data points appearing in the upper right hand region of

Figure 2-2 7 The HC and CO emissions values listed are

without exhaust oxidation catalysts Assuming catalyst middotl

conversion efficiencies of 50-60 at the end of 50000 miles

of operation HC and CO levels will approach but not meet

160

statutory levels It is clear that excellent fuel economies

have been obtained at the indlcated levels of emissions

control - some 40 to 45 improved re1at1ve to 1974 produc-

tj_on vehicle averages for the same weight class

The cross-hatched horizontal band appearing across the upper

part of Figure 2-2 represents the reductions in NOx emissions

achieveble with use of EGR if HC emissions are unrestricted

The statutory 04 gmile level can apparently be achieved

with this engine with little or no loss of fuel economy but

with significant increases in HC emissions The HC increase

is ascribed to the quenching effect of EGR in lean-middotmixture

regions of the combustion chamber

223 Fuel Requirements

Current PROCO engines operated v1ith 11 1 compression ratio

yield a significant fuel economy advantage over conventional

production engines at current compression ratios According

to Ford engineers the PROCO engine at this compression

ratio j_s satisfied by typical fu1J-boi1ing commercial gasoshy

lines of 91 RON rating Conventional engines are limited to

compression ratios of about 81 and possibly less for

operation on similar fuels

Results of preliminary experiments indicate that the PROCO

engine may be less sensitive to fuel volatility than convenshy

tional engines - m1 important ff1ctor in flextb1 llty from the

standpoint of the fuel supplier

161

224 Present Status

Present development objectives are two-fold

Develop calibrations for alternate emissions target

levels carefully defining the fueleconofuy pbtenshy

tial associated with each level of emissions control

Convert engine and auxiliary systems to designs

feasible for high volume production

23 The Texaco TCCS Stratified Charge Engine

231 General Description

Like the Ford PROCO engine Texacos TCCS system involves_

coordinated air swirl and direct combustion chamber fuel

injection to achieve charge stratification Inlet portshy

induced cylinder air swirl rates typically approach ten times

the rotational engine speed A sectional view of the TCCS

combustion chamber is shown in Figure 2-3

Unlike the PROCO engine fuel injection in the TCCS engine

begins very late in the compression stroke - just before th~

desired time of ignition As shown in Figure 2-4 the first

portion of fuel injected is immediately swept by the swirling

air into the spark plug region where ignition occurs and a

flame front is established The continuing stream of injected

fuel mixes with swirling air and is swept into the flame

region In many respects the Texaco process resembles the

162

spray burning typical of dj_esel combustion ~r1th the difshy

ference that ignition is achieved by energy from an elec-

tric spark rather than by high compression temperatures

The Texaco engine like the diesel engine does not have a

significant fuel octane requirement Further use of positive

spark ignition obviates fuel I

cetane requirements character-

istic of diesel engines The resultant flexibility of the

TCCS engine regarding fuel requirements is a si~1ificant

attribute

In contrast to the TCCS system Fords PROCO system employs

relatively early injection vaporization and mixing of fuel

with air The combustion process more closely resembles the

premixed flame propagation typical of conventional gasoline

engines The PROCO engine therefore has a definite fuel

octane requirement and cannot be considered a multifuel

system

The TCCS engine operates with hi__gh compression ratios and

with little or no inlet air throttling except at idle conshy

ditions As a consequence fuel economy is excellent--both

at full load and under part load operating conditions

232 Exhaust Emissions and Fuel Economv

Low exhaust temperatures characteristlc of the TCCS system

have necessitated use of exhaust oxidation catalysts for

control of HC emissions to low lf~Vels A11 recent development

163

programs have therefore included use of exhaust oxidation

catalysts and most of the data reported here r~present tests

with catalysts installed or with engines tuned for use with

catalysts

Figures 2-5 and 2-6 present fuel economy data at several

exhaust emissions levels for two vehicles--a US Army M-151

vehicle with naturally aspirated 4-cylinder TCCS conversion

and a Plymouth Cricket with turbocharged 4-cylinder TCCS

engine 9 10 1urbocharging has been used to advantage to

increase maximum power output Also plotted in these figures

I are average fuel economies for 1974 production vehicles of

similar weight 8

I When optimized for maximum fuel economy the rrccs vehicles

can meet NOx levels of about 2 gmile It should be noted

that these are relatively lightueight vehicles and that

increasing vehicle weight to the 4000-5000 pound level could

result in significantly increased NOx emissions Figur~s 2-5

and 2-6 both show that engine modifications for reduced NOx

levels including retarded combustion timing EGR and increased

exhaust back pressure result in substantial fuel economy

penalties

For the naturally aspirated engine reducing NOx emissions

from the 2 gmile level to O l~ gmile incurred a fuel

economy penalty of 20 Reducing NOx from the tllrbocharged

164

engine from 15 gmile to 04 gmile gave a 25 fuel economy

penalty Fuel economies for both engines appear to decrease

uniformly as NOx emissions are lowered

For the current TCCS systems most of the fuel economy penalty

associated with emissions control can be ascribed to control

of NOx emissions although several of the measures used for

NOx control (retarded cornbusticn timing and increased exhaust

back pressure) also help to reduce HG emissions HC and CO

emissions ari effectively controlled with oxidation catalysts

resulting in relatively minor reductions in engine efficiency

233 TCCS Fuel Reauirements

The TCCS engine is unique among current stratified charge

systems in its multifuel capability Successful operation

with a nuraber of fuels ranging from gasoline to No 2 diesel

Table 2-I

Emissions and Fuel Economy of Turbocharged TCCS Engine-Powered Vehicle 1

Fuel

Emissions gMile 2 Fuel Economy

mng 2HC co NOx

Gasoline

JP-4

100-600

No 2 Diesel

033

026

014

027

104

109

072

J bull l ~

-

061

050

059

060

197

202

213

230

1M-151 vehicle 8 degrees coffibustion retard 16 light load EGR tw0 catalysts (Ref 10)

2 CVS-CH 2750 pounds tnert1a welght

165

l

has been demonstrated Table ~-I lists emissions levels and

fuel economies obtained with a turbocharged TCCS-powered

M-151 vehicle when operated on each of four different fuels 10

These fuels encompass wide ranges in gravity volatjlity

octane number and cetane leve 1 as middotshown in Table 2-II

Table 2-II

Fuel Specifications for TCCS Emissions Tests (Reference 10)

Gravity 0 API Sulfur

OFDistillation~

Gasolj_ne 100-600 JP-4 No 2

Diesel

88 -

86 124 233 342 388

0024 912

-

486 012

110 170 358 544 615

0002 57 356

541 0020

136 230 314 459 505

-middot --

369 0065

390 435 508 562 594

--

lta 9

IBP 10 50 90 EP

TEL gGal Research Octane Cetane No

Generally the emissions levels were little affected by the

wide variations in fuel properties Vehicle fuel economy

varied in proportion to fuel energy content

As stated above the TCCS engine is unique in its multifuel

capability The results of Tables 2-I and 2-II demonshy

strate that the engine has neither 8ign1ficant fuel octane

nor cetane requirements and further that it can tolerate

166

wide variations j_n fuel volati1tty rhe flexibility offered

by this type of system could be of major importance in

future years

234 Durability Performance Production Readiness

Emissions control system durability has been demonstrated by

mileage accumulation tests Ignltion system service is more

severe than for conventional engines due to heterogeneity of

the fuel-air mixture and also to the high compression ratios

involved The ignition system has been the subject of

intensive development and significant progress in system

reliability has been made

A preproduction prototype engine employing the TCCS process is

now being developed by the Hercules Division of White Motors

Corporation under contract to the US Army Tank Automotive

Command Southwest Research Inr)titute will conduct reliability

tests on the White-developed enGines when installed in Military

vehlcles

30 Small Volume Prechambcr Eng1nes (3-Valve Prechamber Engines Jet Ignition Engines Torch Ignition Engines)

31 General

A number of designs achieve charge stratification through

division of the combustion region into two adjacent chambers

The emissions reduction potentiampl for two types of dualshy

chamber engines has been demonstrated F1 rst ~ j n B desJgn

trad1t1on~JJy caJJld the nrreebrnber engine a 2m211 auxil1ary

167

or ignition chamber equipped w1th a spark plug communicates

with the much larger main combustion chamber located in the

space above the piston (Figure 3-1) The prechamber which

typically contains 5-15 of the total combustion volume

is supplied with a small quantity of fuel-rich ignitable

fuel-air mixture while a large quantity of very lean and

normally unignitable mixture is applied to the main chamber

above the piston Expansion of high temperature flame

products from the prechamber leads to ignition and burning

of the lean maj_n chamber fuel-a_r charge Ignitionmiddot and

combustion in the lean main chamber region are promoted both

by the high temperatures of prechamber gases and bythe

mixing that accompanies the jet-like motion of prechamber

products into the main chamber

I jl

I i j

I

Operation with lean overall mixtures tends to limit peak comshy

bustion temperatures thus minimizing the formation of nitric

oxide Further lean mixture combustion products contain

sufficient oxygen for complete oxidation of HC and CO in the

engine cylinder and exhaust system

It should be reemphasized here that a iraditional problem

with lean mixture engines has been low exhaust temperatures

which tend to quench HC oxidation reactions leading to

excessive emissions

Control of HC emissions to low levels requires a retarded or

slowly developing combustion process The consequent extenshy

sion of heat release j nto 1ate porttt)ns of the engtne cycle

168

tends to raise exhaust gas temperatures thus promoting

complete oxidation of hydrocarbons and carbon monoxide

32 Historical Background and Current Status

321 Early Developm9nt Objectives and Engine Def igns

The prechamber stratified charge engine has existed in various

forms for many years Early work by Ricardo 1 indicated that

the engine could perform very efficiently within a limited

range of carefully controlled operating conditions Both

fuel-injected and carbureted prechambcr engines have been

built A fuel-injected design Lnittally conceived by

Brodersen 11 was the subject of extensive study at the

University of Rochester for nearly a decade 12 13 Unforshy

tunately the University of Rochester work was undertaken prior

to widespread recognition of the automobile emissions problem

and as a consequence emission characteristics of the

Brodersen engine were not determined Another prechamber

engine receiving attention in the early 1960s is that conshy

ceived by R M Heintz 14 bull The objectives of this design

were reduced HC emissions incr0ased fuel economy and more

flexible fuel requirements

Experiments with a prechamber engine design called the torch

ignition enginen were reported n the USSR by Nilov 15

and later by Kerimov and Mekhtier 16 This designation

refers to the torchlike jet of hot comhust1on gases issuing

169

from the precombustion chamber upon j_gnj_ tion In a recent

publication 17 Varshaoski et al have presented emissions

data obtained with a torch ignition engine These data show

significant pollutant reductions relative to conventional

engines however their interpretation in terms of requireshy

ments based on the Federal emissions test procedure is not

clear

l

3 2 2 Current DeveloJ)ments

A carbureted middotthree-valve prechamber engine the Honda CVCC

system has received considerable recent attention as a

potential low emissions power plant 18 This system is

illustrated in Figure 3-2 Hondas current design employs a

conventional engine block and piston assembly Only_ the

cylinder head and fuel inlet system differ from current

automotive practice Each cylinder is equipped with a small

precombustion chamber communicating by means of an orifice

with the main combustion chambe situated above the piston lj

ij_ A small inlet valve is located in each precharnber Larger

inlet and exhaust valves typical of conventlonal automotive

practice are located in the main combustion chamber Proper

proportioning of fuel-air mixture between prechamber and

main chamber is achieved by a combination of throttle conshy

trol and appropriate inlet valve timing A relatively slow

and uniform burning process gjvjng rise to elevated combusshy

tion temperatures late in the expansion stroke and during

the exhaust procezs is achieved H1 gh tewperaturr--s in thin

part of the engine cycle ar-e necessary to promote complete

170

oxidation of HC and CO It si1ould be no~ed that these

elevated exhaust temperatures are necessarily obtained at

the expense of a fuel economy penalty

To reduce HC and CO emissions to required levels it has been

necessary for Honda to employ specially designed inlet and

exhaust systems Supply of extremely rich fuel-air mixtures

to the precombustion chambers requires extensive inlet manifold

heating to provide adequate fuel vaporization This is accomshy

plished with a heat exchange system between inlet and exhaust

streams

To promote maximum oxidation of HC and CO in the lean mixture

CVCC engine exhaust gases it has been necessary to conserve

as much exhaust heat as possible and also to increase exhaust

manifold residence time This has been done by using a relashy

tively large exhaust manifold fitted with an internal heat

shield or liner to minimize heat losses In additj_on the

exhaust ports are equipped with thin metallic liners to

minimize loss of heat from exhaust gases to the cylinder

head casting

Engines similar in concept to the Honda CVCC system are under

development by other companies including Ttyota and Nissan

in Japan and General Motors and Fo~d in the United States

Honda presently markets a CVCC-powered vehicle tn tTapan and

plans US introduction in 1975 Othe~ manufactur~rs

includlnr General Motors and Forgtd 1n thr U S havf~ stated

171

that CVCC-type engines could be manufactured for use in limited

numbers of vehicles by as early as 1977 or 1978

33 Emissions and Fuel Economywith CVCC-Type Engines

331 Recent Emissions Test Results

Results of emissions tests with the Honda engine have been very

promising The emissions levels shown in Table 3-I are typical

and demonstate that the Honda engine can meet statutory 1975-1976

HC and CO stindards and can approach the statutory 1976 NOx

standard 19 Of particular importance durability of this

system appears excellent as evidenced by the high mileage

emissions levels reported in Table 3-I Any deterioration of

l emissions after 50000 miles of engine operation was slight

and apparently insignificant

I Table 3-I

Honda Compound Vortex-Controlled Combustion-Powered Vehicle 1 Emissions

Fuel Economy

Emissions 2 mpg gMile 1972

HC 1975 FTP FTPco NOv

210 50000-Mile Car+ No 2034 Low Mileage Car 3 No 3652 018 212 221089

024 065 198 1976 Standards

213175 20o41 34 - -04o411977 Standards 34 - -

1Honda Civic vehicles 2 1975 CVS C-H procedure with 2000-lb inertia weight3Average of five tests aAverage of four tests

172

Recently the EPA has tested a larger vehicle conve~ted to the

Honda system 20 This vehicle a 1973 Chevrolet Impala with

a 350-CID V-8 engine was equipped with cylinder heads and

induction system built by Honda The vehicle met the present

1976 interim Federal emissions standards though NOx levels

were substantially higher than for the much lighter weight

Honda Civic vehicles

Results of development tests conducted by General Motors are

shown in Table 3-II 21 These tests involved a 5000-pound

Chevrolet Impala with stratified charge engine conversion

HC and CO emissions were below 1977 statutory limits while

NOx emissions ranged from 15 to 2 gmile Average CVS-CH

fuel ec9nomy was 112 miles per gallon

Table 3-II

Emissions and Fuel Economy for Chevrolet Impala Strmiddotatified

Charge Engine Conversion (Ref 21)

Test

Exhaust Emlssions

gMile 1 Fuel

Economy mpgHC co NOx

1 2 3 4 5

Average

020 026 020 029 0 18

023

25 29 31 32 28

29

17 15 19 1 6 19

17

108 117 114 109 111

112

1cvs-CH 5000-lb inertia weight

173

I

332 HC Control Has a Significant Impact on Fuel Economy

In Figure 3-3 fuel economy data for several levels of hydroshy

carbon emissions from QVCC-type stratified charge engines

are plotted 22 23 ~ 24 At the 1 gmile HC level stratified

charge engine fuel economy appears better than the average

fuel economy for 1973-74 production vehicles of equivalent

weight Reduction of HC emissions below the 1-gram level

necessitates lowered compression ratios andor retarded

ignition timing with a consequent loss of efficiencymiddot For

the light-weight (2000-pound) vehicles the O~ gmile IIC

emissions standard can be met with a fuel economy of 25 mpg

a level approximately equal to the average of 1973 producshy

tion vehicles in this weight class 8 For heavier cars the

HC emissions versus fuel economy trade-off appears less

favorable A fuel economy penalty of 10 relative to 1974

production vehicles in the 2750-pound weight class is

required to meet the statutory 04 gmile HC level

333 Effect of NOx Emissions Control on Fuel Economy

Data showing the effect of NOx emissions control appear in

Figure 3-~ 22 These data are based on modifications of a Honda

CVCC-powered Civic vehicle (2000-pound test weight) to meet

increasingly stringent NOx standards ranging from 12 gmile

to as low as 03 gmile For all tests HC and CO emissions

are within the statutory 1977 standards

NOx control as shown in Figure 3-4 has been effected by use

of exhaust gas recirculation 1n comb1nation w1th retarded

174

ignj_tion timing It is clear that control of rmx emissions

to levels below l to 1 5 gmile results in stgnificant fuel

economy penalties The penalty increases uniformly as NOx

emissions are reduced ~nd appears to be 25 or more as the

04 gmile NOx level is approached

It should be emphasized that the data of Fisure 3-4 apply

specifically to a 2000-pound vehicle With increased vehicle

weight NOx emissions control becomes more difficult and the

fuel economy penalty more severe The effect of vehicle

weight on NOx emissions is apparent when comparing the data

of Table 3-I for 2000-pound vehicles with that of Table 3-II

for a 5000-pound vehicle While HC and CO emissio~s for the

two vehicles are roughly comparable there is over a factor

of two difference in average NOx emissions

34 Fuel Requirements

To meet present and future US emissions control standards

compression ratio and maximum ignltion advance are limited

by HC emissions control rather than by the octane quality of

existing gasolines CVCC engines tuned to meet 1975 California

emissions standards appear to be easily satisfied with

presently available 91 RON commercial unleaded gasolines

CVCC engines are lead tolerant and have completed emissions

certification test programs using leaded gasolines However

with the low octane requirement of the CVCC engine as noted

above the economic benefits of lead antlknock compoundt ar-euromiddot

not realized

175

It is possible that fuel volatLLity characteristlcs may be of

importance in relation to vaporization within the high

temperature fuel-rich regions of the prechamber cup inlet

port and prechamber iQlet manifold However experimental

data on this question aomiddot not appear to be available at

present

~O Divided-Chamber Staged Combustion Engines (Large-Volume Prechamber Engines Fuel-Injected Blind Prechamber Engines)

41 General

Dual-chamber engines of a type often called divided-chamber

or large-volume prechamber engines employ a two-stage comshy

bustion process Here initial r~ich mixture combustion and

heat release (first stage of combustion) are followed by rapid

dilution of combustion products with relatively low temperature

air (second stage of combustion) The object of this engine

design is to effect the transitjon from overall rich combustion

products to overall lean products with sufficient speed that

time is not available for formation of significant quantities

of NO During the second low temperature lean stage of

combustion oxidation of HC and CO goes to completion

An experimental divided-chamber engine design that has been

built and tested is represented schematically in Figure ~-1 25 26

A dividing orifice (3) separates the primary combustion

chamber (1) from the secondary combustion chamber (2) which

includes the cylinder volume above the piston top A fuel

injector (4) supplies fuel to the primary chamber only

176

Injection timing is arranged such that fuel continuously

mixes with air entering the primary chamber during the

compression stroke At the end of compression as the

piston nears its top center position the primary chamber

contains an ignitable fuel-air mixture while the secondary

chamber adjacent to the piston top contains only air

Following ignition of the primary chamber mixture by a spark

plug (6) located near the dividing orifice high temperature

rich mixture combustion products expand rapidly into and mix

with the relatively cool air contained in the secondary

chamber The resulting dilution of combustion products with

attendant temperature reduction rapidly suppresses formation

of NO At the same time the presence of excess air in the

secondary chamber tends to promote complete oxidation of HC

and CO

42 Exhaust Emissions and Fuel Economy

Results of limited research conducted both by university and

industrial laboratories indicat~ that NOx reductions of as

much as 80-95 relative to conventional engines are possible

with the divided-chamber staged combustion process Typical

experimentally determined NOx emissions levels are presented

in Figure 4-2 27 Here NOx emissions for two different

divided-chamber configurations 8re compared with typical

emissions levels for conventional uncontrolled automobile

engines The volume ratio 8 appearing as a parameter in

Figure 4-2 represents the fraction of total combustion volume

contained in the primary chamber For a values approaching

I

i J_

177

1

05 or lower NOx emissions reach extremely low levels Howshy

ever maximum power output capability for a given engine size

decreases with decreasing 6 values Optimum primary chamber

volume must ultimately_represent a compromise between low

emissions levels and desired maximum power output

HC and particularly CO emissions from the divided-chamber

engine are substantially lower than eonventional engine

levels However further detailed work with combustion

chamber geometries and fuel injection systems will be necesshy

sary to fully evaluate the potential for reduction of these

emissions

i Recent tests by Ford Motor Company show that the large volume

prechamber engine may be capable of better HC emissions conshy

trol and fuel economy than their PROCO engine This is shown

by the laboratory engine test comparison of Table 4-I 19

Table 4-I

Single-Cylinder Low Emissions middot11 ~ _____En____g__~ne __middot _e_s_-_s_____

Engine

NO--X Reduction

Method

Em1ssions g1 hp-Hr

Fuel Economy

Lb1 hp-HrNOv HC- co

PROCO

Divided Chamber

PROCO

Divided Chamber

EGR

None

EGR

None

10 30

10 04

05 ~o

o J_o 75

130

25

l 1i bull 0

33

0377

0378

0383

0377

178

Fuel injection spray characteristics are critical to control

of HC emissions from this type of engine and Fords success

in this regard is probably due in part to use of the already

highly developed PROCO-gasoline injection system Figure 4-3

is a cutaway view of Fords adaptation of a 400-CID V-8 engine

to the divided-chamber system 2 e

Volkswagen (VW) has recently published results of a program

aimed at development of a large volume precharnber engine 29

In the Volkswagen adaptation the primary chamber which comshy

prises about 30 of the total clearance volume is fueled by a

direct timed injection system and auxiliary fuel for high

power output conditions is supplied to the cylinder region by

a carburetor

Table 4-II presents emissions data for both air-cooled and

water-cooled versions of VW s dtvided-middotchamber engine 3 0

Emissions levels while quite low do not meet the ultimate

1978 statutory US standards

179

Table 4-II

Volkswagen Jarge Volume _Jrechamber Er[ Lne Emissions

Exhaust Emissions

_ _gMile 1

___E_n_gi_n_e__t--H_C___c_o__N_O_x____E_ng__i_n_e_S_p_e_c_i_f_i_c_a_tmiddot_1_middoto_n_s__

20 50 09 841 compression ratio Air-Cooled 16-Liter

prechamber volume 28 of total clearance volume conventional exhaust manishyfold direct prechamber fuel injection

20-Liter 10 40 10 91 compression ratio Water-Cooled prechamber volume 28 of

total clearance volume simple exhaust manifold reactor direct prechamber fuel injection

1cvs c-H

Toyota also has experimented wlth ___a large volume prechamber

engine using direct prechamber fuel injection and has

reported emissions levels comparable to those of Table 4-II 31

43 Problem Areas

A number of major problems inherent in the large volume

prechamber engine remain to be 3olved I~ These problems include the following II

Fuel injection spray characteristics are critically

important to achieving acceptable HC emissions

The feasibility of producing asatisfactory injecshy

tion system hasnot been estab1ished

180

Combustion noise due to high turbulence levels and

hence high rates of heat release and pres[-ure rise

in the prechamber can be excessive It has been

shown that the-noise level can be modified through

careful chamber design and combustion event timing

If the engine is operated with prechamber fuel

injection as the sole fuel source maximum engine

power output is limited This might be overcome

by a~xiliary carburetion of the air inlet for maximum

power demand or possibly by turbocharging Either

approach adds to system complexity

The engine is charmiddotaeter1zed by low exhaust temperatures

typical of most lean mixture engines

References

1 Ricardo H R Recent Research Work on the Internal Combustion Engine 11 SAE Journal Vol 10 p 305-336 (1922)

2 Bishop I N and Simko A Society of Automotive Engineers Paper 680041 (1968)

3 Simko A Choma M A and Repco L L Society of Automotive Engineers Paper 720052 (1972)

4 Mitchell E Cobb JM and Frost R A Society of Automotive Engineers Paper 680042 (1968)

5 Mitchell E Alperstein M and Cobb JM Society of Automotive Engineers Paper 720051 (1972)

6 1975-77 Emission Control Program Status Report submitted to EPA by Ford Motor Company November 26 1973

181

if

7 consultant Report on Emissions Control of Engine Systems National Academy of Sciences Committee on Motor Vehicle Emissions Washington DC September 1974

8 Austin T C and Hellman K H Society of Automotive Engineers Paper 730790 (1973)

9 See Ref 7

10 Alperstein M Schafer G H and Villforth F J Iiil SAE Paper 740563 (1974)

11 US Patent No 2615437 and No 2690741 Method of Operating Internal Combustion Engines Neil O Broderson Rochester New York

12 Conta L~ D and Pandeli American Society of Mechanical Engineers Paper 59-SA-25 (1959)

13 Canta L D and Pandeli American Society of Mechanical Engineers Paper 60-WA-314 (1960)

14 US Patent No 2884913 0 Internal Combustion Engine R Mi Heintz i

15 Nilov N A Automobilnaya Promyshlennost No 8 (1958)

l 16 Kerimov N A and Metehtiev R I Automobilnoya Promyshlennost No 1 p8-11 (1967)

17 Varshaoski I L Konev B F and Klatskin V B Automobilnaya Promyshlennost No 4 (1970)

18 An Evaluation of Three Honda Compound Vortex Controlled Combustion (CVCC) Powered Vehicles Report B-11 issued by Test and Evaluation Branch Environmental Protection Agency December 1972

19 Automotive Spark Ignition Engine Emission Control Systems to Meet Requirements of the 1970 Clean Air Amendments report of the Emissions Control Systems Panel to the Committee on Motor Vehicle Emissions National Academy of Sciences May 1973

20 An Evaluation of a 300-CID Compound Vortex Controlled Combustion (CVCC) Powered Chevrolet Impala Report 74-13 DWP issued by Test and Evaluation Branch Environmental Protection Agency October 1973

21 See Ref 7

22 See Ref 7

23 See Ref 7

24 See Ref 7

182

25 Newhall H K and El-Messiri I A Combustion and Flame 14 p 155-158 (1970)

26 Newhall H K and El-Messiri I A Society of Automotive Engineers Transaction Ford 78 Paper 700491 (1970)

27 El-Messiri I A and Newhall H K Proc Intersociety Energy Conversion Engineering Conference p 63 (1971)

28 See Ref 7

29 Decker G and Brandstetter W MTZ Motortechnische Zeitschrift Vol 34 No 10 p 317-322 (1973)

30 See Ref 7

31 See Ref 7

183

Fig 2-1 FORD PROCO ENGINE

l

Ford Proco Engine Fuel Economy and Emissions _ 15 _ f--1

00 +

I ~ x X gt( X _ x A 7- ~ X x~ ~c - l4catalyst Feed u NOx vs ruel Econ with 1 C0-71 CJ) 14 x x Ynn H( RP c tr ir-t irm vltgtZ G I HC - C0-127 _ A txcessve c

13 Approx W EG R

~ C~~r 351 CID 5000 Lb Inertia Weight

Q 21 A L 0 u w II _j

LJ =gt LL

10

35i CD 4500 Lb Inertia Weight

~ 1974 Production Average Fuel Economy

4 soo _b r-r-r-----z~lt_~~---7--_~--r--1r-7-r1--~-rz7-w~~

150 0 0 Lb PU221ufrac122-1 I

LO 20 30

NOx EMISSIONS-GMSMILE (CVS-CH) Revised216174

0

HKN 71074

Fig 2-2

l

~___-~ ~--=---~ ~=---__---~1 f-=-----1__middot-_~J ~-----------1 ~bull-=-=- (-~-~ LJii-ZJj ~ ~~-~ ~~ -__c~~ 1--~~ ~----~--1 ---------s___-c--1 ~~~-~~~bull r~~-~--middot1 ____c__ J~ p- ~

Texaco TCCS Engine

Shrouded Intake Valve

~ Intakemiddot r~ )p__-- Fuel Nozzle Fuel Nozzte Port ~ -- -yen -_~

X f -J J ( ~1 I --- ~ f middotmiddotj_Ja 1(~-~_ frff 1-Cylinderv~ v_ r--L~ I (~~)J ~- Intake 1 - ------L- middotmiddot - middotmiddot -1 H0 ad middot --- - -- 1 Po rt I 1 I ~~ ) ~ ~ ~~~ -A- I ------

- I _ ---_ ~ P1ston-mgt-lt_ffrac12 T_77~~~--1 i- r_-~J N

- ~- i~-L - _ _ - IExhaust - - I ~ - 1-_ r- bullsect ~ ----lt_ ~ I PortJ~bJ lt 7A--7~ ~1 ~j --~ ~ yl ind er

-__~lli- klmiddot ~ro v_t_gt11J1bull Bti Or K__ - middot ~

I t--tL pgt-- Ultmiddot middot- - Spark Plugr- -1 --U2middot- ~-~

LHorizont al Projections of Nozzle and Spark Plug Centerlines

Fig 2-3 i--1 00 U1

---~---~-~ -------c- --~--- 7middot-r---c-- ~- -~~~==---~~~~~- srsr RZIIEF7 11t111-~-----==-----=-~--~-~~---c=rmiddot=

OPEN CHAMBER TYPE STRATI Fl ED CHARGE ENGINE i-shyCj

DIRECTIONAl~Fsw7 Q

NOZZLE P

I

~J~treg lt-_(__(lt-(11

c_-- _7- -

SPARK PLUG_ l 1__- -_ - l --_ ~ ----__ lt_ lt_ -- --

ltlt_I_--- _

~ gt - _____- -- --~ ~-l_- 1_~ -~- ~ ------

~~~ r_I FUEL SPRAY 2 FUEL-AIR MIXING ZONE ~- _ -------

FLAME FRONT AREA 4 COMBUSTION PRODUCTS

TCCS COMBUSTION SYSTEM

Fig 2-4

3

----==-----~ l~~----bulli r-~ ~-----=-- 1 ~~ ~ -~ ~~ ___-_=gt---l p--- --=-=-_-__71-~-~~ 1-0-- --=---=-- 4 L--_-_-~ P--- ~

25

-c u

f

Cl) 24 gt u _

tgt 23a ~

I

gt-~ 220 2 0 u w 21 _J

lJJ gt LL

2

Texaco TCCS Powered Cricket Vehicle

Max Econ Setting gt A L07 HC

141 CID JQf CR 084 CO 2500 Lb Inertia Wgt

50-so Retard_ 0_73 HC

12 co 051 HC ~ 061 HC

085COA 064CO Retard+ ESPRetard+

EGR

036 HC ~ 115 co Retard +ESP+ EGR

04 06 08 10 12 14 16 18 20 NOx EMISSIONS-GMSMILE (CVS-CH) HtltN1110114

I- 00 -JFig 2-5

-~ ~=- ~ - -i______c_J ~-====c= wr=- ~-~ p--w~~~ rr w -

25

-c u

I

(f)

gt u-lt a_

2

gt-I 20

~ 0 z 0 u LLI

_J

w tJ_

15

I- CJ) CJ)

Turbocharged Texaco TCCS Ml51 Vehicle

Max Econ Adjustment_ HC-3J catalyst Feed C0-70

141 CID 10~1 CR 2750 Inertia Weight 8deg Retard ~

~bull HC-3middot2 catalyst Feed ~~ _ C0-64

_ 5deg Retard HC-0 30 8degRetard LowEGV bullco-11 ~bull HC-3middot6 catalyst Feed WIW21

Med EGR C0-67 1974 Production 33 Average Fuel Economy ~

COmiddoti05 (2750Lb)

I

bull HC-035 co- 141 13deg Retard High EGR

04 10 20 NOx EMISSIONS -GMSMILE (CVS-CH) ~~ts~b~~~74

Fig 2-6

189

Fig 3-1

PRECHAMBER TYPE STRATIFIED CHARGE ENGINE

r Inlet

(Fuel-lean Mixture )

I 0 I

Spark -Prechamber (Fuel-rich mixture)

-Main Chamber

1] HON DA CVCC ENGINE CONCEPT

190

Fig 3-2 Honda CVCC Engine

28 -l u

1

UJ 26 -gt u-(9 CL 24 2-

f

gtshy0gt

22 z ~ _)

u w

20 _J

w ~ LL

18

J= ---- 4 --~~-_----a ~~ _-_bull --~~ 1~~1 ltiil~I ~ ~-r~ ~ -~ ~-~ ~J~-iii-1 ~~1 s _-_ __-

Fuel Economy vs HC Emissions for 3-Valve Prechamber Engines

e NOx-14 15 Liter

bull Honda CVCC 2000 LbsNOx - 12 A Datsun NVCCbull15 Liter

bull ~JOx -09 A 2500 Lbs J LL 1ter NOv -15

2750 Lbs -NOx -17

- I AiJOx -12

0 02 04 06 08 LO 0HYDROCARBON EMiSSlmiddotONS - Glv1 I MILE (CVS-CH) I-

Fig 3-3

J--1

1--Fuel Economy vs NOx Emissions IO N

-- for Honda CVCC Powered Vehiclesr 26 u

l VHc-023 U1 gt umiddot 24_-__

(_IJ o_

~ 22 l

gt-5~-0 z 20 C0-200 u A HC-033w I co -3o_j

_A HC-029w 18 J I C0-27 LL

_ HC-025

HC-017 co -2-3

C0-22

0 -- 02 04 06middot 08 10 12 NOx Ef11SSIONS -GlviS MILE (CVS-CH)

Fig 3-4 middot

I

I

i93

J J

Fig 4-1 Divided Chamber Engine

middot(4) Fuel Injector

1

f J

f ff

f

~ Ii

I f

i

I f ] [

~~

0 0 0 0

i ~ I

1jl

194

E Cl 0

C QJ

CJl 0 _

-1-

z

0

Vl (lJ

-0

X 0

-t-J

V1 ro c X

LLI

Fig ~-2

COMPARISON OF CONVENTIONAL AND DIVIDED COMBUSTION CHAMBER NOx EMISSIONS

5000 MBT Ignition Timing Wide Open Ttl rattle

4000 Conventional Charnber

3000

J = fraction of Total Combustion 2000 Volume in Primary Ct1arnber

Divided Chamber 13 = 0 85

1000

Divided Chamber fo = 0 52

05 06 0 7 08 09 10 11

O~erall Fuel-Air Equivalence Ratio

195

196

AIRBORNE SURVEYS IN URBAN AIR BASINS IMPLICATIONS FOR MODEL DEVELOPMENT

by

Donald L Blumenthal Manager of Program Development

Meteorology Research Inc Altadena California 91001

middotI would like to make several points today First ozonemiddotis basically

a regional long-range problem There is a lot of long range ozone transshy

port and this transport is a normal occurrence The second point is that

ozone is stable in the absence of scavengers Junge mentions in his book

that the residence time of ozone in the troposphere is on the order of a

month Third vertical variations in concentration and ventilation rate are i very important in modeling atmospheres such as Los Angeles Layers aloft

are ventilated down to the surface on occasion and surface pollutants are

ventilated up mountain slopes as Jim Edinger has pointed out before and

often ventilated out of the basin in upper winds Fourth the day to day

carry over of pollutants from one day to the next is a very important considshy

eration in the Los Angeles Basin Finally there is a definite background

level of ozone The geophysical literature says its about O 02 to O 03 ppm (

in various parts of the world Weve seen data varying from 003 to 005 ppm

The difference may be due to calibration differences In any case numbers

like 005 are pretty substantial background levels for ozone

I am going to illustrate the points listed above with some data from

Los Angeles Basin The data were collected during a two-year study funded

by the Air Resources Board some of the analyses were funded by EPA The

study examined the three dimensional distribution of pollutants in the Los

Angeles Basin using airborne sampling systems Coinvestigators on the

project were Dr Ted Smith and Warren White of Meteorology Research Inc (MRI)

197

The first slide shows one of the aircraft we used Its a Cessna 205

which had sampling inlets on the side of the aircraft Figure 2 shows the

instrument system on the inside of the aircraft We were measuring nitrogen

oxides ozone scattering coefficient with a nephelometer condensation nuclei

carbon monoxide and meteorological parameters such as temperature humidity

turbulance Altitude and position were also measured

Figure 4 shows that the typical sampling pattern was a series of spirals

from the top of the mixing layer over an airport virtually to ground level

then we would climb up to the next point on the route and spiral down again

We had three routes (A B C Figure 3) that we would fly We had two airshy

craft and we would fly two of these three routes three times a day any

given day that we could The day I will be talking about September 25~ 1973

we flew what was called the Riverside route (C) and the Los Angeles route

(A) The 25th of July 1973 you might remember was the day before the

federal office buildings were closed in the area here because of smog

Figure 5 shows the surface streamlines at 0300 Pacific Standard Time

about 4 oclock in the morning daylight time on July 25 This streamline

analysis points out the morning stagnation conditions which are a very normal

occurrence in the Los Angeles Basin You start out with very light winds

quite variable maybe a slight off shore flow early in the morning On this

particular day this kind of situation extended well into midday The sea

breeze did not really pick up until up around noon When you have this kind

of a situation and a low radiation inversion at night you have a

long period of accumulation of pollutants all over the Basin espt~cialJy

in the prime source area the southwest portion of the Basin

198

I

Figure 6 shows the streamline pattern at 1600--400 cclock in the

afternoon same day sea breezes develop and with them a transport pattern

that carries pollutants up to the northeast and out toward the eastern por-

tion of the Basin This is a very regular pattern which we see day after l middot

day On July 25 1973 it was a little bit exaggerated The sea breeze was

held off for awhile started a bit late and so there was a very long period

of accumulation in the southwest area and then transport across the Basin

Figure 7 is an average streamline pattern at 1600 PacHic Daylight Time

on low inversion days for August 1970 It is included to show that the pattern

shown before is very typical Flow starts in the western portion of the

Basin and goes right across to the eastern portion This is using surface

data There is a very high average wind velocity in Ontario about 13 m iles

per hour and 23 mph in Riverside This is the average for the whole month

of August at 1600 PDT on low inversion days There is a considerable amount

of transport across the Basin starting relatively slowly in the morning and

accelerating in the afternoon

Figure 8 shows a verticle cross section of the scattering coefficient

The darker areas indicate higher levels of particulates Scattering coefficshy

ient is inversely proportional to visibility In the crosshatched area

visibility is less than about 3 miles In plotting altitude versus distance

inland from the coast you have Santa Monica (SMO) on the coast El Monte (EMT)

Pomona (BRA) Rialto (RIA) Redlands (RED) The lower broken line is surface

ground level The heavy dashed line is the base of the subsidence inversion

that occurred on the two days during this episode The middle line is the

base of the marine inversion There is a large area over in the western

portion of the Basin where emissions accumulate for much of the day At

199

midday the sea breeze has just started ventilating the Santa Monica area

The layer between the inversions is a layer aloft which is fairly well separshy

ated from the surface layer Ozone concentrations for instance in the

layer aloft were on the order of 04 05 ppm using the ARB calibration

method Down in the surface layer they were quite a bit lower in the mornshy

ing due to scavenging

Figure 9 shows that by afternoon the sea breeze starts and you get

kind of a clean air front Sea breeze starts ventilating the whole Basin

the stuff that was over in the west is transported eastward and at approxishy

mately Brackett (BRA) at 1700 PDT there is a clean air front The high conshy

centrations that were over Los Angeles earlier are now centered near Upland

(CAB) The numbers shown over CAB are data taken from a vertical profile

spiral over Upland at about 1600 That turns out to be the time when there

was the worst ozone concentration of the day in the Basin and it did occur

at Upland It could well be a result of the very polluted mass from the

western Basin being transported over the Upland area The layer aloft has

been a bit undercut by the sea breeze and some of the polluted mass has been

around possibly as long as the night before There has been very little

transport in the area aloft ozone concentrations are still very high

Figure 10 shows a trajectory analysis of the air arriving at Upland at

1600 since that was the worst time of the day at Upland We developed a

trajectory envelope using surface wind data and winds aloft so the air

arriving at Upland at 1600 started out somewhere back within this envelope

for example at 1130 PDT We did not go earlier than 1130 because the winds

were pretty much light and variable before that The air that arrives at

Upland at 1600 has been over the western portion of the Basin for much of

200

the morning and q~ite a bit of the evening before Thus there is

a very long period of accumulation and then a transport a pulsing effect

where you have pollutants moved across the Basin

Figure 11 is an isopleth map of surface ozone concentrations Again all

data are corrected to agree with the ARB calibration method Again you can

see that for the hours between 1600 and 1700 using surface data the Upland

area has the highest surface ozone concentrations about 063 ppm The western

area has been well ventilated by the sea breezes and it is cleaned out

The transport is actually pretty much perpendicular to the isopleth line

just about like that

Figure 12 is a vertical profile taken over Upland Cable Airportat

roughly the time of maximum ozone concentration 1636 PDT We are plotting

pollutant concentration on the x-axis versus altitude in meters (since it was

done for an EPA report) Surface leveJ at Upland is a little over 400 meters

the Z line is ozone Ozone concentration within the surface mixing layer

is pegged on the instrument at somewhat above 05 ppm Above the surface

mixing layer it drops off considerably and eventually get down to background

The T line is temperature and you ean see the subsidence inversion

on this day is very nicely documented here and provides a very strong trap

in that area The B line is the scattering coefficient inversely proporshy

tional to visibility Within the surface mixing layer visibility is on the

order of 3 miles or less while up above the surface mixing layer just a few

hundred feet difference visibilities get up to 60 or 80 miles The X is

condensation nuclei the measure of the very fine particles below about 010

micron It is a measure of quite fresh emissions If you have a high condenshy

sation nuclei count there are very fresh combustion emissions If you have

I

201

an aged air mass the condensation nuclei coagulate and the count decreases

considerably You can see that there are still some fresh emissions within

this surface layer as well But up above the surface mixing layer all the

pollutant indicators decrease considerably

Figure 13 is the same type of vertical profile taken over El Monte

which is on the western side of the sea breeze front The sea breeze front

has passed El Monte at this time almost 1700 PDT and again there are

distinct differences between the mass below the mixing layer within the sea

breeze front (below 400 meters) the marine inversion (400 to 800 meters) and

the subsidence inversion The subsidence inversion occurs at about 800 meters

and there is an old layer of very polluted stuff aloft The surface concenshy

trations are lower because of the ventilation by the sea breeze Condensashy

tion nuclei count (X line) within the surface layer is quite high There

are still fresh emissions in the El Monte area The 11 Z line is ozone

about 02 ppm within the surface layer (200 m) but it is 05 ppm up above

the surface mixing layer The scattering coefficient (B line) is very

similar it is lower at the surface and increases to a visibility equivalent

of less than 3 miles above the surface mixing layer The condensation nuclei

count is high in the lower portion of this (eg at 600 m) hut decreases conshy

siderably above This portion of the upper layer (600 m) has been around

at least all morning and condensation nuclei have been scattered from the

area The portion of the upper layer below 600 m has probably just recently

been undercut by the sea breeze and there are still some condensation nuclei

left in it

Figure 14 illustrates a different method of looking at the flushing

problems in the Basin We have tried to develop an objective criteria based

on ground level ozone to show the cleansing of the basin using the time of

202

arrival of clean air We determine the time when the ozone concentrations

drop by a factor of two at any given point The 1600 line means that between

1500 and 1700 the ozone concentration at that point dropped a factor of two

This sort of isopleth chart of when the clean air arrives agrees quite well

with the trajectory analyses although the numbers are a little bit behind

the trajectory analyses for the polluted air Figure 14 again shows the

transport process that takes place across the Basin which is ventilated from

west to east At 1900 some of the fresh ocean air finally gets out to

Redlands

In Figure 15 in order to put this whole flux problem into some perspecshy

tive we looked at the numbers the actual amount of ozone flux across the

basin We calculated the mean trajectory from Torrance towards Redlands

using the surface and upper air data We looked at the flux from the western

basin to the eastern basin basically from Los Angeles and Orange Counties to

Riverside and San Bernardino Counties This is a calculation made at 1700 PDT

We used the winds aloft from Chino as well as the vertical profiles taken at

Pomona and Corona Averaging the ozone concentration throughout the mixing

layer and multiplying by an average wind speed we arrive at a number of 185

metric tons per hour being transported directly from one side of the Basin

to the other If you look at this in terms of actual concentration in the

eastern Basin and assume that the flow was constant for about an hour it

is eno_ugh to fill up the box shown in Figure 15 to 025 ppm ozone which

exceeds the air quality standard by a factor of three (using the ARB calibrashy

tion method) Thus there is a very significant transport of ozone or ozone

precursors from one portion of the Basin to the other side of the Basin One

thing to mention though is that the concentration would not be kept up on a

203

steady state basis because the transport is a result of the pulsing effect

I Illentioned earlier There is a lot of accumulati6n in the western Basin

and these accumulated pollutants are then transported across the Basin This

kind of transport did take place in a couple hours because we also have

measurements from 1500 PDT which give us similar flux numbers

Figure 16 is a trajectory envelope similar to Figure 10 calculated for

Upland at 1600 for the air arriving at Redlands about 600 oclock in the

afternoon I wanted to include this trajectory envelope to show that the

problem is not really simple You cannot say that the air at Redlands came

from Long Beach per se The air at Redlands if you look at the whole

envelope of possible trajectories using upper air data as well as surface

data could have come from anywhere between Downtown Los Angeles and over

the Pacific Ocean south of Long Beach

Another thing to recognize is that the wind actually changes direction

slightly as you go up and down through the mixing layer and the mixing layer

is exactly what it implies There is mixing within the mixing layer so if

you begin with a parcel of air near the surface this parcel may move to the

top of the mixing layer and go one direction for awhile it then may go back

down to the bottom of the mixing layer and move in another direction for

awhile The ratio of the length scales indicata3mixing layer depths of 1500

or 2000 ft and distances on the order of 70 miles This makes it very

difficult for tetroons to follow an air trajectory because they do not go

up and down They stay at one altitude and in one wind regime and yet the

wind regimes are different at different altitudes and the air is continually

mixed up and down through this layer You can often see this on time lapse

photographs

204

The question is where does the pollutant mass go after Redlands Figure

17 is a repeat of Jim Pitts slide from yesterday and it is data for the

same day that we did our analysis It shows the ozone peaks starting at

Pomona and Riverside and on July 25 1973 eventually getting out to Palm

Springs so there is quite a bit of long-range transport The ozone is

stable at 8 00 or 9 00 oclock at night There still are ozone concenshy

trations of 02 ppm it hasnt dissipated even at the surface Ozone does

dilute as the mass moves Other calculations we did were integrations

through the mixing layer of various pollutants such as ozone and CO along

with trajectories that we measured Th~se integrations show just what the

ground data show in Figure 17 The concentrations increase through the western

portion of the Basin and then show a decrease through the eastern portion

of the Basin CO tends to decrease faster than the ozone indicating a

continued production of ozone further east

Figure 18 is a streamline chart on a larger area map for the 16th of

August 1973 It shows the typical streamline patterns that occur for

ventilation from the Basin By mid-afternoon there is flow out through the

major passes to the north and towards Palm Springs (PSP) On this particushy

lar day we had data from Arrowhead showing that the air mass from the Basin

does indeed get up there

Figure 19 shows a vertical profile over Arrowhead early in the morning

16 August 1973 at a time when there was a north wind Ozone level was

about 005 ppm the scattering coefficient was quite low on the order of

probably 60 miles visibility or so Figure 20 is a vertical profile again

over Arrowhead late that afternoon when the winds had switched There is a

flow from the Los Angeles Basin into the Arrowhead area thus one sees a

205

vertical profile that shows a distinct increase near the surface in both the

ozone and the scattering coefficient and in the condensation nuclei Ahove

that you have fairly clean air The top of the polluted level is just about

the top of the mixing level over the Basin

I want to leave the transport now and discuss the complicated vertical

structure that can occur If you want to try to model something try this

one for instance Figure 21 is a vertical profile over Brackett Airport

Pomona about 830 in the morning on 26 July 1973 which is the day after

the episode shown earlier A bit of interpretation shows how complicated

th is can be If one looks at the temperature profile it would be very

difficult to pick out a mixing layer theres a little inversion here another

inversion there several more up here After looking at hundreds of these

profiles though you can start interpreting them What is happening is that

there is a surface mixing layer at about 500 m In this layer there is a

high condensation nuclei (X line) count due to morning traffic The San

Bernardino freeway is quite close to Brackett there is a relatively high

nitrogen oxide count about 02 ppm and the b-scat is fairly high Ozone (Z)

within the surface layer however at this time is quite low The layer beshy

tween 500 m and 700 rn turns out to be the Fontana complex plume Note the

very high b-scat level it is below 3 miles visibility the plume is very

visible especially at this time of the morning when it is fairly stab]e

There is a high nitrogen oxide level (800 m) a high condensation nuclei

level and again a deficit of ozone Above this layer (800 m) you have stuff

that has been left all night very low condensation nuclei indicating a very

aged air mass ozone concentrations about 016 ppm b-scat of about 04 It

has been around all night and not yet had a chance to mix down within the

206

surface layer In fact one good way of determining the surface mixing layer

early in the morning and at night is to look for the ozone deficit Another

thing to mention is that wind reversals occurred for each of these three

layers The winds were fairly light and westerly at the surface slightly

easterly in the 500 m 700 m layer and westerly above 800 m There is a

complicated situation early in the morning but the main problem is that by

the middle of the day there is good surface heating and the pollutants have

all been entrained and mixed down to the ground so in order to modeI what

happens on the second or third day of an episode you must be able to look

at both old pollutants as well as fresh emissions And you need to account

r for ozone that is actually transported down to the surface from layers aloft l

The next slide is a photograph (not included) which is another e xample

of some layers aloft This is due to upslope flow as explained by Jim Edinger

in his publications The mountains are heated during the day in turn heating

the air and making it buoyant there is upslope flow to a point where the

heating cannot overcome the subsidence inversion and the stuff comes right

out from the mountains and spreads out over the Basin The pollutants can

stay up there if the winds aloft are very light and on the subsequent day

will he re-entrained to the surface On the other hand if there are winds

aloft different from those in the surface mixing layer or the wind velocity

aloft is high there can be a very substantial ventilation process for the

Basin Pollutants can be ventilated up the slope and blown away in the upper

winds In the case of the entire July 25th episode winds aloft were quite

light and these upper layers remained

Figure 22 is a vertical profile of one of those upslope flow conditions

in the same location shown in the photograph but on a different day Again

207

there is a relatively high surface concentration of about 03 ppm of ozone

(Z line) a layer of clean air between 900 to 1100 m and then high concenshy

trations of ozone again above 1100 m It has gone up the slopes of the

mountains and then come back out Concentrations in the 1100 to 1300 m area

are just slightly lower than they were at 600 to 800 m area Notice however

that the condensation nuclei count (X line) is quite a bit lower mainly

because the stuff is much more aged above the 1000 m level than it is down

below 900 m

Figure 23 shows the stability of ozone the fact that it can stay around

all night long This is a vertical profile taken over Riverside about 2200

PDT 1000 oclock at night Above the surface mixing layer (600 m) there

are ozone concentrations of about 0 15 ppm (Z line) Within the surface

mixing layer (below 500 m) ozone is completely scavenged decreasing to

zero The nitrogen oxides within this surface layer are being contained and

are around 01 ppm from fresh emissions that occurred during the evening

Condensation nuclei near the surface are very high The temperature profile

is very stable You have a surface based radiation inversion which is a

little strange looking for a radiation inversion~ nevertheless it is quite

stable There is a definite restriction of the mixing--a very difficult

time getting air from below 500 m to above 500 m The ozone that exists in

the 700 m range is in air where the reactions have virtually gone to compleshy

tion and is very stable All the profiles on this night changed very little

the ozone peak stays there High concentrations stay around

Figure 24 is a cross section across theurban plume of the City of St

Louis I wanted to show that this occurrence is not limited to Los Angeles

We have seen ozone formation and transport in other urban plumes These data

l

208

were taken during a project sponsored by EPA in conjunction with R Husar of

Washington University and William Wilson of EPA The dark line on this is

the ozone concentration across the urban plume perpendicular to plume The

dashed line is the scattering coefficient The power plant plume is parallel

to the urban plume The data on the left were taken 35 kilometers down wind

about 1100 oclock in the morning The ozone concentration increases slightly

to 005 ppm in the urban plume there is a deficit of o in the power plant plume3

In the same urban plume same conditions 1500 CDT two hours later further

downwind there has been substantial increase in the ozone in the urban plume

itself The b-scat is very similar to what it was before but the ozone is

now increased quite substantially except in the power plant plume where

there is a strong deficit of ozone due to scavenging by nitrogen oxides So

the formation and transport of ozone and ozone precursors in urban plumes is

a regular occurrence that happens in more places than Los Angeles and as Bob

Neligan showed this morning it can happen over quite a bit longer distances

than we are showing here

To summarize the conclusions as they affect model development first

once ozone is formed in the absence of scavengers ozone is a very stable

compound It remains for long periods of time It can he transported for

very long distances Ozone is a regional problem which cannot be controlled

on a local basis To have effective ozone control middotone must have a regional

control strategy and probably regional type air pollution districts

A second conclusion is that the vertical distribution of pollutants can

be highly complex and models have to include more than just a simple wellshy

mixed surface layer

209

A third conclusion is that layers aloft can persist over night and can

be re-entrained within the surface mixing layer on subsequent days models

should be able to account for old pollution as well as fresh emissions Also

pollutant accumulation and transport can have distinct diurnal patterns that

are strongly dependent on the meteorology Models should be time dependent

and should start at the beginning of the accumulation period In other words

models ought to be able to run for 24 or 48 hours if they have to In this

case in Los Angeles there is often an accumulation of pollutants which starts

in one portion of the Basin at midnight and continues through the next mornshy

ing even before it starts to be transported

As far as recommendations go in many areas a lot of ambient data has

been collected and in some cases the data are actually ahead of some of the

models so I think a research program is needed in developing models that

will account for this vertical structure and the day to day carry over and

the models need to be extended to cover longer distances In addition more

smog chamber work is going to be needed in looking at the effects of carry

over and mixing old pollutants with fresh emissions How people go about

this I leave to the modelers and the smog chamber people They know more

about that than I do

I

210

I

~ INVERTER

AUDIO TAPE

MONIT0R

MONITOR OBSERVER SEAT

MON ITOR

NEPHELOMETFR FLfCTRONICS

j DIGITAL DATA LOGGER

CONDENSATION

VOR DME NEPHELOMETER TUBE

JUNCTION middoteox ASSORTED POWER

AIRBORNE

TEMPERATURE TURBULENCE

middot HUMIDITY

ALTITUDE BOX

__

middotE=-middot RECORDER ----r----------

NUCLEI KJNITOR

CONVERTER

SUPPLIES

INSTRUMENT PACKAGE (

lCO

03

Ndeg

-

-----NEPHELOMETER

BLOWER

Figure 2 Instrumentation Layout for Cessna 205

211

bullubullbullbullbull

Figure 3 Airborne Sampling Routes in the Los Angeles Basin

Figure 4 Vertie al Profile Flight Path

~-~ r~i ~~1 -- ~ ~ ~2-1~ LJ-----~ r~~ ~~ t~~--l

~ ALM l

0 RIA

ec 8v

M

~ Afo

-o

M 0

~IV

ltgt

IN J--1 N

SCALE II fi M I j_ ES 0 3 4 5 =-JSEJ--J~ _middot ~middot- - =- =

I

~

M

N~J

Figure 5 SURFACE STREAMLINE ANALYSIS - 0300 PST 25 July 1973

~~~ ~~-- cp1FJ=D -~~

~ 1

~ ~ 8c

8v

~25

PACIFIC OCEAN

diams Tt

0

9 I 4 5 10 I- m p H - -middotmiddot u 4H__8 middott_

D i6 J4 k W~D SPED llaquotl SNA NJ ~1

SCALE m ICtt84bullmh R v1s1a1L1n (mil 6 ~ CONTOURS REPRESENT

-- 10ml 16km (~() bull ~ ) ~ - 000 ft 3C5

Figure 6 S_cJRFACE WIND STREAMLINES - l 600 PDT JULY 2 S I 8 7 3

l - ~---i ~-=-___-----c---it~~-~~ r----=------1 ~-~~--cpc---_t__A --~ ---llil

~_ - ~-l-cL

34bull vi~-dff

bullbullbullbull bull ~ bull -1 bullbull - -_- L bull-J bull ~bull-bull-ii------~ bullmiddot r_ -~- ~ bullI ~_ bull bull bullbull bull I bull _ - bull -~-~ middotbullbullbull ~ ~ --middot -~- bullbullmiddot ~v ) ~ - -__rl v middotmiddot - 1- ~ -- middot middotmiddot - 1 91 frac12 - ~- lt( middot K i - middot bull - middot - bullmiddot~~-~lJ) obullmiddot~ ~-f- _J_~---Smiddot~middot-~----~~~---gt_middotfY-_middot-~middot --middot-~-~----fJ_middot- middotmiddotbullmiddot u-- bullmiddot ~ ~ -middot L~ bullbull

~bullbullbullbull bullbull l_bull bull bullbullbull EW bullbullbullbull-- ~ __bull f f - middotbull - J middot f bull S bull I ~ -r --

_ bullbull bull- _ bullbull-bull ~ ~ bull bull bull bull I bull bull bull bull bull bull gt - bull middotbulliJ -bull I bull bull _1 bullJ C-- ~-middot _ bull bullbull bullbull bull _____ ~ ~ l _ middot q bull 1 -middot middot ~~middot middot middotbull_ J ~gt - J bull-bullbullbullbull ) _ -middotmiddotbullmiddot J ~middotmiddotmiddot -bullmiddotbull fmiddot 7middot _middotmiddotmiddot bullmiddot(middot Ii~ middotmiddot~_--~middot 1middot__middotmiddotmiddotmiddot middot- gt_ -~ -~-- Imiddotbullmiddotbullbull_ -

- ()_I (w--_ bullbull__(i- bullOmiddotbull bull middotbull -bull-_jlJ middot bull lt 1(middot t gt bull - ~ rbull I bull middot middot- bull41-bull l~r v-middot~- middot middot middot bull_ - middotmiddot ~Jtj (middot~ ~middoti middot middot middot middot middot ~- ~ -tmiddot~ I - middot middot_- ~ - -~ middot_ _- ~bull - _ ~) i bull bullbull bull- middot_ bull middotbull __ ( bull 11bull bull ~ampmiddot ~ l bull bullQ bull - -1 bull JY1 bullbull ~ or bullbullbullbullbull bullbull-bullbull _ ~ - bull bull-bullbullbull middotimiddot middot 91 bull t bull - - tfaw lJ--r- bull bull _ bull middot- - l

f ~~middot--~ middotmiddott ~ltrgtmiddotmiddotJmiddot_bull - ~ - __ middot- LOS ANGELES BASIN - LOW LEVEL -__ jmiddot l-gt bull - bull J iI bullbull bull bull bull _ bullbull _ Jmiddot middotL~_1 middot middot bullbullmiddot ( C middot INVERSION MEAN WIND FLOW _ J

lmiddot - f bullbullbull~ - f 1bullbullbull _ ~)- bull middot- _---_- 7f-~bull~ REGIME _F_~ AUG_UST_~ ~600 P~--- l

-__L-~bull --ncmiddotbull~~-j--bullmiddot~bullmiddot_-bull _fJibullmiddot Imiddotmiddotmiddot-bullmiddot- bullbull ~ bullbullbullbullmiddotmiddotmiddot~middotbull ___ bullJ_ _middot~0))deg bullt t1yensmiddotmiddot ( middot middotmiddot middot middot ~ middot lbullbull1 t_c0 bull -middot---l lt ~middot~- deg bullbull --= bull bull bull I bull bull bull bull bull bull bull bull bullbull _~bull b ---) bullbull-bull ) bulll middotbull middot1middot ) bullT --f bull I bullr ~bullbullbull bullbullbull( - -bull-- ( -o-----_i bull-~-l- i l l J l~-- c middotmiddot _--1 ---I middotmiddot ---- ~bull-bull bulli_ ALT Elmiddot_ bullbullbullbull _- ~~middot bull middot bullbull _ bull middotbull bull~ ~bull middot bull -middot bull--ua_-- bullbull bull

-- 01--- middot_ -middotmiddot hmiddotmiddot __1 ~-- ~ fi~~- ___ - ____ _ -middotmiddotmiddotmiddot~ ) -~-J bull bullbull bull bull 0 uc- -l ~- ~ IT ~~ll ~ bull -middot -middotmiddotmiddotmiddotbullCCAmiddotmiddotmiddot-middot middot bullbullbullbullbull

) i- 5 ~-==-- __ __ - bullbullbull _ bull~ bullbull _ bull bull l T[h4 ------ - 0

i17- o~-lt -(i-_~ 11t~bull-omiddot ~- -- 13 0l~~~bull bull Jbullbull~bull ~ ~bullbullbull bull bull x- middot~---=-~~ -=aJlll8 bull Ibull bull ~~ middotbull rbull~---bull1-~middot-middot _ middotmiddotmiddot-middot 1 0 ~vrbullmiddot ~middot ~ (J~-middot _-_~) ) ~ bull middot

l middot _ POMA_ middot =~~~----ti~ jmiddotmiddotmiddot - middot bull [j

~A ii J0 Vfli middot bullHud __=bt_ bull

CImiddot ~-- ~- middot)middot PACIFIC OCEAN I middot ---- middotmiddot ~

__ middot__ ~ - _ 23~1 middotbull 8 4 1 middot middot ~ middot middot gt ~~- l ~ u middot

bull - bull- I ~------ --1~ i middotmiddotmiddot - n _c-118 1130

~ n r -t ~~gt25) cmiddotbullmiddot

~--lt- ~~- 1-~__( i - t ~ _ middot 0 igt(_J

11bull bull11 ~~ -~[ ~i~gt----gtmiddotmiddotmiddotmiddot--~l_ ~~ ELEVATION

IN FEET bullbull (_- middot bullbullbull -middot middotbull middot ~~ middotmiddot bulltbullbull _ffmiddotmiddot-middot v I )tylt~ -~bullbull1bullbullrbullbull ~-lt -~ ( I~

600~ A0 Cv(A (1829 m AND OVER) deg )_ rJ__~7 middot middot ~--middot L==1 _J bullbullbull - bull -middot~-- rgt ~ middot(Zmiddot- middotbullmiddot middot

Z~C)-tGOO (762 middot 1829 m) 9-N4 __J (r -- lf _ bull bullgt-~~~ ~ _ w _ _ I (1 bullmiddot( middot1 middot -----~~~- middot L-bullmiddotbullW bullbullbull3 STA r I0-4 lODEL

100i -2soo (305~762m) -- Ow - -~1_- i ~~--- bull v~rvt ~~ -middot )) ~--

II gt J (-_bullmiddot middot~ l bull bull tr 1 )~ gt ) bullbull-_bullI-middot -middot bull~0 3 Mor nuq1ENr Wlbull~O JIAtCTIO-bull bull - lbull C---gt bullbull )t bullbull -( I bullf I - 20-00 (61 bull 305 ml J( Jloa xxE- -bullbull00 - -- middot1

0-200 (0middot61m) Wl)7 AVBt~gpound ) bullmiddot-iiNL~ middotntmiddot_ 1 iJJlt( _1J- ~ VAq IA9 IL ITY 0 ~ 10 15 ltS lHPtl

~--_ bull bull I bullbullbullbull 1 ~) J)J ~ bull Is bullmiddot bullbullbullbullbull ~ 3 V IS A VAqlABLE OIR~CTIO- 0 8 16 2-4 km

(SPEEDS SHOWN IN mph 10 mphbull 16 h1llr) -- middot ktr~~~ lt~ ) -middot-SCALE

Figure 7 LOS ANGELES BASIN MEAN WIND FLOW FOR DAYS WITH LOW LEVEL INVERSIONS DURING AUGUST I 970 AT 1600 PDT

-~~~~-=======~middot~-~======~middot--=-==-===gt=---==____________=== ~--=-J~==-- -=-ee----=-------

500

N f-- V

- - - SUBSIDENCE INVERSION

----MARINE INVERSION

bullbull-bull-bullbullGROUND LEVEL

x WINOS ALOFT (kmht)

WESTERN middoteASIN EASTERN BASIN

LAX WINOS EMT IHOS I I

CNO WIHOS

s_ 04 13 1500- 05 02 08

I 06 069 middot

11-1--

04 04 i ~4

06 ~ 4--

I 2

1000 n1 1005 -_E

lll --1 lJ -----------~----

~11

--=i-+- c -- 9 _____ - ~ C

lt I

I 6 4 _r 31

I 6 5 ~~ ~_ bull ---middot- 64 ~li- - middot- bullc - middot-----------

10

SMO (1347 PDT)

EMT (1246 PDT)

BRA CAB (1459 PDT) (1335 PDT

RIA (1349 PDT)

RED (1406PDT)

Figure 8 VERTICAL CROSS-SECTION OF bscat FOR lvflDDAY

T t 10-4 -1)(l n1 s are m

JULY 25 1973

- c - -~

~--~ JC_-_1- ~1pi~ oamp----~JilliiiM~f~-U~ -~--- --~~~ ~~~

-=--~

-E-- O

_ lt

1500 05

06 15

09 __~

1000 --

~- ~---middotmiddot 29

500

oJ11

__a

07

I 07 I

I I

I

09

I

I

I

I 7 ---

11 -----

~ ----- 6

---------------lt- -~middot4 --------

20

29

-

10 10

11 07 08 08

10

08

~8 _____ Y-

N

- - bull SUBSIDENCE INVERSION

----MARINE INVERSION

-bull-bull-bull GROUND LEVEL

WES TERN BASIN EASTERN BASIN x WINOS ALOFT (kmhr)

t t

CNO WINOSILA WllltOS poundMT WINOS

SMO LA EMT BRA CAB RIA RED O (1736 PDT) (1655 PDT) (1707 PDT) (163 PDT) (1823PDT) 1805 PDT)

Figure 9 VERTICAL CROSS-SECTION OF b FOR AFTERlOON OF JULY 25 1973 scat

T bull 1o- 4 - l )(units are m

__~~---iii~~- ~- ~~______ ~~- --~~J---=-~ ~

N ~ -J

PACIFiC OCEAN

0 5 10 15 1111

E 8 4 I 0 8 6 2 ~ bull

SCALE

dh Mes

CONTOURS REPRESENT - 000 ft 305 m

0 SNA

c8s

ec 8v

amp R~b

Figure 10 TRAJECTORY ENVELOPE FOR AIR ARRI1G AT CABLE AIRPORT (CPLAD) 1600 PDT JULY 25 1973

~-~

q_- ~ ------1 H~~~ -~~--~ ___---___--i- __r-=-1--===12---1 ~ ___r~ _==---_ - ~- f~~ ~-- - -5plusmn-at -~middot~

ll~~r1 ri

40

ec 8v

-1 I

amp

0 HQ_

7 0

CAP LAAR) O

VER

PACIFIC OCEAN ~ 0

RLA

4

WHqR d

diams

H ~I

I l

0 COMA

3

L~

LAH

Fa_ f ~~

S ~ LA APCD VALUES ADJUSTED TO AGREE ~

lt

0

5 10 15 mi0 WITH ARB CALIBRATIONE-j I I CONTOURS REPRESENT NZJ ~ 0 a SCALE 6 24 km - 1000 ft 305m COS v~J

______ J 10 ro ( igtf t-i

coFigure 11 SURFACE OZONE CONCENTRATIONS (pphm) I 600- I 700 PDT JULY 25 1973 ~

~~~~~C-~ ------=--~-__-~--~~~=--- ----=--~

N

-E

D1600----------------------------- 1--

14001-------------------------------

1200

I Ground Elevation

1000 middot 445 m ] lampJ

sect ~~ 7 ) SURFACE i6~ 800 MIXED LAYER

~

~ [ J ~ ~ I OZONE CONCENTRATIONS~ 600 E E GREATER THAN

( 50 pohm

400 I C H T Z GROUND LEVEL

200

I PUUloCETER UNIT SnbullBOL

NOc N0 0 ppm01 02 03 04 05 03 z

40 --~45~~ 50 co pm C0 5 10 15 20 25 30 35 I I I I I I I I I I TEIIPERATURE oc T-5 b 5 10 15 20 25 30 35 40 45

I-- 100 RELATIVE HUlillOITY H0 10 20 30 40 50 60 70 60 90 b1eot IOmiddotm- 1 8

CN cmmiddot3 1 IO X0 I 2 3 4 ~ 6 7 8 9 10 URBJLENC-C cm213ue- E

Figure 12 VERTICAL PROFILE OVER CABLE (CAB) J CLY 2 5 l C)7 3 l 63 6 PDT

~ _~ ~--- -

--

1400 I bull bull

1200

1000-5 LampJ 0 ~ I- 800 ~ c(

sooLl

-1-=-1-~--t j --=~c-o-----i-bull 1-~~~ ilt~~ -~-1 lta-abull--~ -c-~---=---r F--- ---- I n_--middot- =~~ ai~IHJ

(~-It

1600 ___________________________________

C r 11 s Ground Elevation t~C E H I~lcc

- ~ 1 90 m

4001 bullc C H

C UNDrnCUTTNG svC ~ Ic- H

SEA BREEZEC II 200

C C

[C -PARAMETER ---UNIT SYMBOL

NOx N0 0 ppm01 02 03 04 05 03 z co ppm C0 5 10 15 20 25 30 35 40 45 50

-5 middot- -~20~----25 TEMPERATURE oc T0 5 10 15 30 35 40 45

100 RELATIVE HUIOITY H0 JO 20 30 40 50 60 70 80 90 bcot 10-4m-1 8

CN crrr3 10 0 I 2 3 4 5 6 7 8 9 10 X TURBULENCE cmZ-13 sec-1 E

N N

_-----=-G--~---

Figure 13 VER TICAL PROFILE AT EL MONTE (EMT) JULY 25 1971 1656 PDT SHOWING UNDERCUTTING BY THE SEA BREEZE

0

middot~_lt ~middotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotbullbull

-~

LACA

0 - )

i r=

-v2v

~

_middot~middot)( I bullbull

bullJ

K~Ji~middot

~~ 61iAS 0

EMT J~J---6~-11 ~orr

PACIFIC OCEAN

WEST 0

SMC

0RLA

14

L~8

R~A

~BL

16 ~ ~

0 5s Pcfrac14A c1i ~ )

wFJfo~J_) ltI~~~

_ff-Clf1ito J )

HILL~

~J U

~ _~~~

~

I o middot

1 1$ ~ 11yen ~middot ~I N

I

N I- I

t

0 --pomiddotmiddot bullmiddot i- 1LO middot Joomiddotmiddotmiddot -- middot middotmiddot -middotmiddot

_middotmiddot 0 middot middotbull MWS r

L4 ( 1 T bull bull __-- -A bullbullbullbull middot

0 i __ bullbull

17 t-J~ N7 a S I ~r ~ 1 rtd ~lt A-~ v- middot ~ - cXa 0

RIA 19

CLO

ltJ~

bull ~ 0

(

--

1

_ _

-2Wl

~s~o -- _)~J0JgtJ~ ___ Q

15 l1JI

0 15 r(A0

CAP

CLARR)~R 1900 1-shyPDT

II (_-L~X L2X I 0~ R[V

0 CCtwA

I

I18=00 POT~ l4 r1

fj

-11J - ----- 11=oomiddotmiddotpor

l~i middotmiddot- o

i

5 10 5 Tl o~1 middot--middotmiddotmiddot middotmiddot

_q it==i--__F-3 9 I I CONTOURS REPRESENT SNA NZJ ~1 o

_- I 0 8 16 24 km I - 1000 ft 305 m middot ~

7 14~CALE --- 2500 ft o2m V lr1 ) middot I i0 _ il o5

16QQ pol(middot v( ____________ _L

I i

Figure 14 APPROXIMATE TIME (PDT) OF ARRIVAL OF SEA BREEZE Jl-LY 25 1973 (Ogt_iective criterion based on ground level ozone concentrations)

~ -___~==~ ~~ - ~ =-~ f7r=~1 _j~-~ --c_~~

u-middot - middot middotmiddotmiddotmiddotmiddot

~- middotmiddot~ ~1 WESTERN BASIN r Joa_middotmiddotmiddotmiddot_ NOxEMISSION RATE ~- 95 METRIC TONShr

-----bull_ ~ ~middot~ I -OUR -----middot )omiddotmiddotmiddot - middot~ l21 (fTI

~ AT middot ~ middotbullmiddot- ~- ~ middot 4bull-middot

I EASTERN BASIN NOx EMISSION RATE 10 METRIC TONS hr

ri r bullbull

t10 Joa

) __ 8v -a_ -- -bull-I O ~AGA -_ ~S ___ _ middotmiddotmiddot -

~ ~v ai- omiddot-middot~-- - ) r -middotmiddotmiddot f middot( ---~ -l A ~ _ (- bull ___

it~ ~~~ middot-middot -- ~-~ ~~~ 0 0 AZU~

AVERAGE CONCEN7RCTi)N iN BOX (IF STEADY STATE)

IS 25 pphm

1 r f--Ji 7 ~Sv PAS ou )V~(~- ~ t i -~ Li_) 03 FLUX THROUGH f~

~ ~JI_~ - amp_ JiM O SHADED BOUNOA~middot~-~ ~~-s-- EMT 185 t 60 METRI~ bull ~ ~ TONShr 0 (m)

c~~~ 1t~CS A~JFP

1000 _29

-i32

_~o tUA

_

1

O~ ~

0 -__rJ( (r- J PACIFIC OCEAN LAX _ C-middotJbull _

l o M R No _

550m

r

A frac14

HAR O HJ LAH

_ o camptA REDLANDS 18QO POT ~ r

I bull ~

RB MEAN TRAJECT~~~y

0

TOA L~S

0 AN

I - ~ 8 OUNOARY ~ ~middotltdeg ~ ~ BETWEEN middot __ WES~ERN ANO- middot middot - ~

I gt I lt bullmiddot bull (EASTERN ~ i middotmiddot middot - - ~

S ~ ~~ ~ - middot-

rt1~1_--t------l

middot1-- BASIN ~-~

1-)~~--middot ~ ~l

~~ ~-bull bull J --

-is-eo -_

0 5 10

j=i r-i C

0 8 ltl

SCALE

5 mi

2~ un

CONTOURS REPRESENT - 1000 ft 3gt5 m

--middotmiddot 2500 ft 1 762 m

~

0SNA

cos 0

_ --~ ----- --- ( bullmiddotmiddotgt

- middotlt- ltgtmiddot t__ Q ~

1 1 rmiddot bullbullbullbullmiddot ~9

NZJ ~ middotmiddot - middot- Alr ---middotmiddot- middot middot( middotmiddotmiddotmiddotv ~ bullbullbullw bullbullbull bullmiddot 1 bullbullr~ ~-- -middot ~--v ~- - I -~

ESTIMATED OZONE FLUX FROM VESTER~ TO EASTER-J BASIN JULY 25 1973 I 700 PDT

C ~IV

N N N

I

l ~

-~~

I

iI

i I

I t

t

~ ---~ --

Figure 15

~Qa llfJD fl(~middot ~ 11f ~I I

l

Lfb ec~s0 CPK v2v 0

ALT 8v Ld~_----1

I

HO-

0 CA

middotLARRv O VE~

1330

ol(Di

A~U

0ENT

~lt

s~e ~ 1530

F8f 1730

~

rbull-~

oc (WljT) -_-~(~~c lt-rw---_

~~ ~-_i~cB~~~

2-~) - ~ ~ l~w-~~ p~- pound)_

0 ojI middot tl-1CfUp I ~ ) 1 ~ J~I i bull middotbull middot~-Li 1)- ) I

DiI ~- 0

i ) 0 l I I

t

A RALc~o JI

C

-~

0 r-iR

~IV 1230 1~

RE PO ~- I - Ftl

) 0 ---~gt- __L8s ~Zi diams ( T~ _middot_ ~~ ~

I AN ~~-~ j t bi 0

~ I

~ I L i

-_gt ji o 5 c 5 Tl middot 0 0 ~-i p__i=r 2=f I_ I 1 NZJSNA 1

1 8 2 4 km )

SCALE I 00 J_(1 CONTOURS REPRESENT cos f

1 0 I --- I - ))) 35

PACIFIC OCEAN

Figure 16 TRAJECTORY E~VELOPE FOR AIR ARRI1gtJG OVER REDL_)DS AT 1800 PDT JULY 23 l =i73

224

JULY 25 1973

LA DOWNTOWN

0sect040 a

~

~ 020 0 X z0 ~ LJ 0 ~ z

~5 040 330POMONA 0 ~ en~ 020 w z _J

w w 0 (9 z O----u-~~-__~_-~~~-------L-~-0--0-0~----- z

ltt~ 040 56 (I)z

0 0o _ RIVERSIDE _J0 20 t6 ~

0~ Qt---0-0--ltrO-ltgt-C~------~~~~ a

LL ~

Rate ~ IO mph___ (I) w

_J~ ~ ~

et~ lt(

3 040 PALM SPRINGS ~

j 020 ~

0------____-----L--___---------L---~--~

105

12 4 8 12 4 8 12 l~-s----am _ pm----1

HOUR OF DAY PST

Figure 17 Diurnal variation July 25 1973 of oxidant concentrations at air monitoring stations at Los Angeles Downtown Pomona Riverside and Palm Springs California Values are corrected data Los Angeles Downtown and Pomona x 11 and Riverside and Palm Springs X 08

CONO S t 1 fRESEIS7

~

~~ 0

ciffmiddotdK ~ ~v~~o

( ~s ~

bull ~r ~ bull 1--~~----Soootl ~ ~ ~ ~ lj i1 d t CJ ~ ampfrsmiddotflt- frac12 ~ middotL~Js _-- ~

_gtgt middot~ ~rroltf~-) ~ 0 s- r

middot-middot- r_~ ~~JtbO ~~bull~Jt ~~~ L r - bull _ ~ I= J 1 ~ ~ ~-~~bullJC ___ -_ middot ~ laquo -poundJ~ ~- middot1~ r-- - V--_1_ ~ I 1 S I

V ~ bullf-uv~ fi -~zumiddot -~middot~ LS gt -tmiddot-F Q~ ~-tv I_~ --- ONT p(_ s ~S ~~~-[ ( 0 c-_ --~ ~~~___d_) lt- ~ I -i-C - -

~----1-1 bull~~POMA ~V BN ) middot-~ f -- s - ~

~VA -middot- ~p AAL a 2~~ ~~middot01 r r ~ middot middot 0-- V

i LAX bull1

~ -~poundJ-i- ltllll _(__1-0~ ~t- degQ-0- ~~ _ _-__~~-qlK ( a_ II ~ ~p-~ ~J

N bull - - 0 r o_ _I ~ -~ ~middot ~ ~amp ~--= ~ ) s ~

- -~- - middotO _a - Tl --0- ov I lHOIO J I bull J -- ~ 6 ~ -__ 2 ~

(__ ~~ _- ~-~ middot8---fl~ -- ~ bull~-abullbull _~ ~-cgt ~ bull bull middot e bull bull l ~ 0

I 1A_ HZJ middoto~J

middot0 (~ ~ S TAA

- ~ - - - --0 () _-j J middotO=c==c-c==cc~~~ l ~~ ~ ~ bull-~---~ ~ bullbull -~ al1 ~ bull __ ~--middotmiddotmiddot

diams Skyforest _ Strawberry Mt Lookout

Figure 18 STRE ~[Ll)ES FOR 1600 PDT on 8 1673

~ ~--

vO 0

N N V1

au

91 V7

-1 ~ -=1 ~~ ~~~~l r=--~d- ---1 _J-_

~E1 ~L1-~f~

3100 ---------------------------------

2900r-----------------------------

T

e w 0

~ 5 Cl Ground Elevation

1560 m

T PARAMETER UNIT SnbullBOL

NOx N 01 02 03 04 05 03

ppm z co ppm C

10 15 20 25 30 35 40 --

45 50

170

I I I z

0 5

-5 - -0~ 5 10 15 20 25 30 35 40 45 TEMPERATURE oc T

0

0

10

I

20

2

30

3

40

4

50

5

60

6

70

7

80

8

90

9

100

o

RELATIVE HUMIDITY

bcot CN

TUR8ULENC~

110-4m-

cm-3 tobull 213 1 cm sec-

H

8 X E N

N OI

Figure 19 VER TI CAL PROFILE OVER ARROWHEAD u-RR_l A CG CST I 6 1973 939 PDT

3100----------------------------------

N2900r----------------------------- -i

N

2700i-------------------------------

2500

e 0 uJ 2300 gt ~ ct

2100

1900i---------------------+--------------

~le 1iation 1360 m) 17001 ~

- -PARA1jETER UNIT SYMBOL

T NOx N1500 o ppm01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50

TEWERATJRE oc T-5 middot --~o--- 5 10 15 20 25 30 35 40 45

IOO RELATIVE HUWIOIT Y H0 10 20 30 40 50 60 70 80 90 bcat 10-~- 1 8

CN cm- 3 104 X0 I 2 3 4 5 6 7 8 9 10 213 1 tURBliiENCE cm sec- E

Figure 20 VERTICAL PROFILE OVER ARROWHEA D -RR 1 --- -AUGlJST 16 I) 16--1S PDT

1-~i w--~i_f l-=--bullC- ---~-4

1600 bull t c- N 8 ff Tbull C[ 8 H 1 bull H z H T ~ C f N 1 H T bull C rn 1 C NE bull-~z Hi400 bull bull tf T bull N ~r --middot _P H -ybull EC N z__e H T i 8 z H Tbull C E HD Z H T POLLUTANTS REMAINING FROM bullt C Hbull L T PREVIOUS DAY1200 Et HO I II -middot-- bull Ct H 9 - H T

___ Hbull( E N 1 a tC N i--_ -1 H

C N Tbull Z HP poundIC C H z_ 1111 1

- bull C H Z l _H_ _J1000 )( cc H -z emiddot ksect bull C N ~ T

)( iz H 8 H TIAI -t XC z 7-- T0 bull pound N t H_8

t-gt

YCpound N 1800 l I-gtltbull - H (Jet

N i -r~Bltt t bull gt- t C X N H T

[ BUOYANT POINT SOURCE PLUMEH 1

N ~z-- -

C H

-bull SUPERIMPOSED ON POLLUTANTSC JZ X H T 600 -~ E c REMAINING FROM PREVIOUS OtY Cl JC t H H f bull cmiddot t HT -fl

C- X t fl _ REMNANT OF NOCTURNAL RADIATION INVERSION(I-----e-C f N K I T H

C Z [ T H x-8 400 _Zc r -H -K SURFACE MIXING LAYERz C II H K 8

C N T pound H M 8 _ I -t ff H E N -9 l

Ground Elevation 305 rn200

PARAMETER UNIT SYMBOL

_ I - I I I NOx N00 ppm01 02 03 04 05 03 z

co ppm C 0 5 IO 15 20 25 30 35 40 45 50

L middot1 TEMPERATURE oc T-5 0 5 IO 15 20 25 30 35 40 45

100 RELATIVE HUPAIDIT y H0 10 20 30 40 50 60 70 80 90 bscot o-4m- 1 B

CN cm-3 x 104 X0 2 3 4 5 6 7 8 9 10 TURBULENC~ cm213sec-1 E N

N co

Figure 21 VERTICAL PROFILE OVER BRACKETT (BRA) JULY 26 1973 0825 PDT SHOWING BUOYANT PLUME AND UNDERCUTTING BY RADIATION INVERSION

N N 01600

___bull C M C

C

1400~~~ t C [ middot H LAYER CAUSED BY

C C H C [ H UPSLOPE FLOWl

1200

1000 ] w

SURFACE MIXING LAYER 0 --= ~ -~~ 6 800~ er

C C

600t-i C C t C

I ~00

Ground Elevation 436 m 2001-------------------------------

PAIUWETU UNIT SYWBOL

NOx N ppm0 0 01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50 I I I I I I I I TEWPERAT1JftE degC T-o b 5 10 15 20 25 30 35 40 45

100 ~EIATIVE HUWIOITY H0 10 20 30 40 50 60 70 80 90 b1tt1 10-m- 8

CN enr3 110 X0 2 3 4 5 6 7 8 9 10 Tu RUL Erct cm23sec- E

Figt1re 22 VERTICAl PROFILE AT RIALTO (RIA) JlJL Y 19 1973 1738 PDT SHOWI=JG LAYER CAUSED BY UPSLOPE FLOW

~~-7 ~ ~- 1 ~iri ~~- ~~-~ ~t ~~ ~ =~middot-1

1200 I t 1 If J-

1000

I C ltTl a_ ~l- t

800

600

L gE __r H

H

400 j (~ c pound N C E I~

t EH -

1-1 M

H H

H M H H

H

H H

11 bull H M H

M H If

H H

H

- C t H ~ C poundmiddot H

I C E I(

200

1600--------------------------- t

T t t T l

l T t

T t_

t 1

l] w ) g f

Tt t

ltt ~ T

t J t T

t J

f 1

t

Klt

H M Cro1nd Elevation 250 m HT X

5Yl80LPAllAlETER ~

NOx N0 0 ppm01 02 03 04 05 03 z

co ppm C0 5 10 io 20 25 30 35 40 45 50

25~--- ---35~~-40 TEMPERATU~E oc T-5 0 5 lO 15 20 30 45

100 RELATIVE HUMIDITY H0 iO 20 30 40 50 60 70 80 90 bact 10--ltllm-1 B

CN cmmiddot3 11 04 X0 I 2 3 4 5 6 7 8 9 10 IURBULENCE cm2hioC-1 E

Figure 23 VERTICAL PROFILE OVER RIVERSIDE (RAL) N

JULY 26 1973 2239 PDT I)

middot==-=-=

0

bull

N w 1--

ii -s~~ l-obull

CJ ~

obull -obull obull

5 02~

bscat

Oa

4l o2J

-I 3 e I 0

--)(

~

Abullu 2

ll

ol

Traverse at 750 m msl 35 km Downwind (SW) of Arch - St Louis Mo 1117 - 1137 CDT

( Power Plant Plume -01 Ibull-[ ~ e

11 bull E I -)(I

I0bull I 1r~ l -

0

I I Io 1 u I

I r- l A bull I i I 1I

H1I I 4 t I II I I

11 I I

I I r I I I

I I qo 01 I I

I I bullJ~viI I middot ~

I

I I

~

Urban Plume

ood 0 10 20 30 40 50

kilometers

o~

02

01

s 1

P

0bull 01

00S~J1 I ti middotmiddot1 middotvmiddotmiddot~ J

Urban Plume

I y

oo 0 10 20 30 40 so

kilometers

Traverse at 750 m msl 46 km Downwind (SVV) of Arch - St Louis Mo 153 0 - J 549 CDT

---- bscat

o-

Power Plant Plume

1l~ 11I 1 t

ill~t fl Ibull I ii

I

lmiddotmiddotrI

I I I I t II

l vrI V

JV-f Jl bull

bull t I bull I

Figure 24

l

232 RELATIVE CONTRIBUTIONS OF STATIONARY ANDMOilILE

SOURCES TO OXIDANT FORMATION IN LOS ANGELES COUN1Y IMPLICATIONS FOR CONTROL STRATEGIES

by Robert G Lunche Air Pollution Control Officer

Los Angeles County Air Pollution Control District Los Angeles California

Introduction

The type of air pollution problem characteristic of the west coast of the

United States and particularly of Southern California has come to be known

as photochemical smog because it is the result of sunlight-energized atmospheric

reations involving oxides of nitrogen and reactive hydrocarbons Its manifesta-

tions- -eye irritation reduced visibility damage to vegetation and accumula-

tion of abnormally high concentrations of ozone or oxidant - -are by now well

known In fact the occurrence of high levels of oxidant which consists almost

entirely of ozone has become the primary indicator for the presence and relative

severity of photochemical smog

During the 25 years since photochemical smog in Los Angeles County was

first identified an extensive program has been underway for control of the responshy

sible contaminant emissions Initially during the 1950 s these programs concenshy

trated on controlling emissions of hydrocarbons from the stationary sources of this

contaminant In the early 60 s programs for the control of hydrocarbon emissions

from motor vehicles in California were begun An exhaust emission control proshy

gram for hydrocarbons and carbon monoxide from new vehicles was begun in 1966

C011trol of oxides of nitrogen emissions from motor vehicles began in 1971

As a result of the overall control program by 1974 emissions of reactive

hydrocarbons from stationary sources have been reduced 70fo from uncontrolled

levels and about the same percentage from mobile sources Oxides of nitrcgen emissions

233

from statjonary sources have been reduced about 53 while emissions from moshy

bile sources are still about 7 above uncontrolled levels due to the increase

in NOx from 1966-1970 models Additional controls already planned for the future

will by 1980 achieve reductions of reactive hydrocarbons from stationary sources

of about 87 from uncontrolled levels and from mobile sources about 93 By

1980 emissions of oxides of nitrogen from stationary sources will have been reshy

duced 53 and from mobile sources 63 from uncontrolled levels The past

present and projected emissions of these contaminants are shown in Figure 1

A I though compliance with the air quality standards has not yet been achieved-shy

and is not likely before 1980- -the results of these programs have been reflected rather

predictably in changes in certain of the manifestations of photochemical smog For

example eye irritation is less frequent and less severe and in some areas js

rarely felt at all any more and damage to vegetation has been markedly reduced

Ozone (or oxidant) concentrations have been decreasing in Southern California

coastal areas since _1964 in areas 10-15 miles from the coast since 1966 and in

inland areas 40-60 miles from the coast since 1970 or 1971 as shown on Figures

2 arrl 3- All of these positive effects have occurred despite the continuing growth

of the area indicating that themiddot control programs are gradually achieving their purpos

a return to clean air

This improvement is al~o refutation of the so-called Big Box -concept which

assumes that the total daily emissions in a given area are somehow uniformly disshy

tributed throughout that area--regardless of its size or of known facts about the

meteorology of the area or the spatial and temporal distribution of its emissions- -

234

and of control strategies based on that concept And since the improvement in

air quality refutes the control strategies based on reductions in total emissions

it thus confirms the value of more recent control strategies which emphasize conshy

trol of motor vehicle emissions and use of a source-effect area concept

Following is a brief listing of the evidence we intend to present as supporting

our views on just what control strategy is appropriate

Examination of relative contributions of HC and NOx from stationarybull and mobile sources demonstrates that motor vehicles are the overwhelming

f source of both contaminants~

I bull Observation of air monitoring data shows that the effects of photochem -

ical smog are not uniformly distributed t_hroughout the county

bull Study of the meteorology of LA County shows consistent paths of trans -

port for various air parcels and consistent relationships between the

areas most seriously affected by photochemical smog and high oxidant

concentrations and certain other areas

bull The upwind areas are found to be source areas--the downwind areas-shy

effect areas

bull Central L A is found to be the predominant source area for the effectI area in which the highest oxidant levels in the SCAB consistently occur

bull The predominant source of emissions in this source area is found to

be motor vehicles

bull Central LA has the highest traffic density I

ij bull Both pr~mary and secondary contaminant concentrations reflect the effects

of the new motor vehicle control program in a predictable fashion 11 I

A strategy based upon these findings is gradually being verified by atmosshybull pheric oxidant data~

235

The Evidence that Motor Vehicle Emissions Are the Principal Source of Oxidant

As seen from Figure 1 at the present time the total daily emissions of I-IC

and_ NOx from all sources in Los Angeles middotcounty are primarily due to the motor

vehicle The problem now is to find the spatial and temporal representation of

emissions which when examined in the light of the known meteorology and geogra -

phy of the Los Angeles region best describes the source of emissions responsible

for the highest observed oxidant readings

In the rollback models used by EPA and others the basin is treated as a

big box with uniformly distributed emissions and peak oxidant is considered to

be proportional to total basinwide hydrocarbon emissions

The fact is that the middotemitted contaminants from which the smog is formed

and the effects which characterize that smog are not evenly distributed throughout

the Los Angeles Basin in other words the basin area under the inversion is not one

large box filled to all corners with homogeneously distributed air contaminants and

photochemical smog

Refutation of Big Box Myth

Examination of atmospheric contaminant concentrations refutes the big box

concept It is found for example that concentrations of djrectly emitted contam -

inants measured at a particular sampling site reflect the emissions within a rather

limited area around that site For this reason contaminant concentration levels

vary from one location to another and each has a characteristic daily pattern which

reflects the daily pattern of emissions in that area

middot 236

The big box concept is further refuted by the fact that peak concentrations

of carbon monoxide and oxides of nitrogen in areas of high traffic density were

fairly static prior to 1966 Thus they did not reflect the 45-50 per cent growth

in motor vehicle registrations and gasoline consumption which occurred in Los

Angeles County between 1955 and 1965 and which caused comparable increases in

total daily emissions of such vehicle-related contaminants This demonstrates

that growth was outward rather than upward so that a larger area of the County

began to be affected by photochemical smog but no area experienced smog ofJ

greater severity than that originally affected by smog formed from the vehicular

emissions which accumulated each weekday in central Los Angeles and were trans-

1 I

ported later that day to the San Gabriel Valley

1 Meteorological Evidence

To verify the geographical dependence of emissions and resulting atmospheric

concentrations let us examine the meteorology of these large areas of Southern

California Both the County and the Basin have many meteorological sub-regions

in which the patterns of wind speed and direction may be similar but within

which the patterns of air transport are parallel with those of adjacent sub-regions

and the respective air parcels do not ever meet or join

The characteristic patterns of inversion height and wind speed and direction

in these sub-regions and their patterns of vehicular emissions together have

created a network of source areas- -those in which the reactant contaminants accu -1T

i ~ mulate in the morning and begin to react--and related receptor areas--those to which

~ the products and associated effects of the photochemical reactions of the contamshy)

inants originally emitted in the source areas are carried by the late morning and

237 middot

afternoon winds ( sea breeze)

Wind-flow patterns show that characteristic patterns of transport for related

source area-effect area combinations are separate and parallel not mixing or

joining Each source area has its own reactor pipeline to its own effect area

or areas

To illustrate this source area-effect area relationship the typical flow of

polluted air from downtown Los Angeles to Pasadena was selected as a worst

case situation for in-depth examination Figure 4 shows that the air in downtown

Los Angeles on the morning of smoggy days moves directly from the central area

to Pasadena

Vehicular traffic is the predominant emission source in both downtown Los

Angeles and Pasadena Thus the air in each locality should contain CO Also

since oxidant would form in the air parcel moving from Los Angeles to Pasadena

oxidant levels would be expected to be higher in Pasadena than in downtown Los

Angeles

Figure 5 shows these relationships for the period 1960-1972 The atmosshy

pheric CO level is similar for the two areas while oxidant levels were higher in

Pasadena than in Los Angeles throughout this time period This demonstrates

that a significant amount of oxidant formed in the air as it moved to Pasadena

containing both the unreactive CO and the photochemical reactants for producing

oxidant Both CO and oxidant show a marked downward trend in each locality since

1965 which emphasizes the effect of vehicle exhaust controls and the correlation

between the localities

238

On a day which is favorable to the formation and accumulation of photoshy

chemical smog a contaminated air parcel normally originates during the

6-9 a m period on a weekday from an area of dense traffic centered just

south and west of Downtown Los Angeles It is oxidant generated within that air

parcel which usually affects Central Los Angeles and the West San Gabriel

middotK IJ l J

Valley area around Pasadena

The traffic area in which this smog had its origin is about the most dense

in Los Angeles County and has been so for the past 25-30 years No area

has a higher effective density thampn-this Using carbon monoxide which

1

is almost entirely attributable to motor vehicles as an indicator of such emis-

sions it is found that the concentrations of emitted vehicular contaminants

middotr i

measured in Central Los Angeles during the past 15 years confirms both this lack

of change in effective density and the absence of any area of any greater effective

density when local differences in inversion are acknowledged

This area the Central Source Area is depicted in Figure 4 The size

and shape of the Central Source Area was ch~sen to be large enough to reduce to

an insignificant level any diffusion or transport into this area from any externally

l generated reactants This conclusion is based in part on the trajectory studies

previously referenced as well as an analysis of the diffusion and transport parashy

meters for the area

239

The Central Source Area has been identified as that geographical region

which contributes essentially all of the primary contaminant emissions giving

rise to the highatmospheric oxidant levels in the West San Gabriel Valley

The proportion of emissions in the CSA due to motor vehicles and that due to

stationary sources is shown in Table 1 For the County as a whole about 80 per

cent of _(6-9) AM reactive hydrocarbons are due to motor vehicle emissions and this

figure rises to 90 per cent for the CSA The same conclusion a pp lies to NOx

emissions The Central Source Area contains the greatest density of vehicle traffic

in the County and thus the greatest density of source emissions Thus it appears

that the source area with the highest density of emissions during the critical (6-9)

AM period is responsible for the highest afternoon oxidant levels observed in Los

A i1geles County and in the South Coast Air Basin These highest oxidant levels

are consistently observed to occur in the San Gabriel Valley This is true whether

the LAAPCD or the ARB oxidant calibration procedure is used

Further the atmospheric concentrations of the primary pollutants can be

identified as originating primarily from the motor vehicle and they reflect the

effects of the motor vehicle emission control program A vehtcular source area

can be identified by its atmospheric levels of CO and NOx Figure 6 compares

measured atmospheric levels with calculated atmospheric levels for CO NOx

and the CONOx ratio in the downtown area

TABLE 1 240

REACTIVE HYDROCARBON EMISSIONS

(6-9) AM

1970

LOS ANGELES COUN1Y middot CENTRAL SOURCE AREA middot SOURCE TONS PER CENT TONS PER CENT

Mobile 1260 81 3 135 91 2

Stationary 290 187 1 3 88

Total 1s~o 1000 148 1000

By 7 -Mode Gallonage

241

The calculated values shown in Figure 6 were derived from a baseline

survey of 1100 vehicles and continued surveillance tests both using the Calishy

fornia 7-Mode test cycle The baseline survey showed that motor vehicles withshy

out exhaust control systems had average exhaust emissions concentrations of 3 4

per cent CO and 1000 parts per million of NOx Baseline emissions data apply

to 1965 and earlier model vehicleg and surveillance data to 1966 and later modelsmiddot

Since it can be concluded from calculations and observations that the dilushy

tion of auto exhaust emissions in the atmosphere on a smoggy day in Los Angeles

is approximately 1000 to 1 the calculated values for CO and NOx prior to 1965 are

34 ppm CO and 1 ppm NOxo After 1965 the changing effect of controlled vehicles

in the total vehicle population is reflected in the calculated values

CO and NOx values measured in the atmosphere are also shown in Figure

6 and confirm the values calculated entirely as diluted vehicular emissions NOx

concentrations measured in the atmosphere tend to be consistently a little lower

than the calculated values probably because photochemical reactions remove some

NOx from the system

The data for CO and NOx calculated and measured show that emissions in

downtown Los Angeles originate almost exclusively from motor vehicles and that

atmospheric concentrations there reflect the average emissions from a representashy

tive vehicle population

The ARB has recently published a report entitled A Trend Study of Two

Indicator Hydrocarbons in the South Coast Air Basin Acetylene was used as a

242

specific indicator of automobile exhaust emissions and it was found to have de-

clined in concentration in the Los Angeles atmosphere at an annual rate of 12 5

per cent since 1970 To quote from this report The California implementation

plan requires an annual average reduction in these emissions (reactive organic

compounds) of 166 tons per day or 11 1 of the 1970 tonnage per year The per cent

reductions in the_ acetylene levels at Los Angeles and Azusa are greater than reshy

quired by the implementation plan Since acetylene is almost entirely associated

J with auto exhaust this demonstrates that the motor vehicle emission control

program is achieving its purpose

To summarize at this point it has been deomonstrated that high oxidant values

are due to motor vehicular emissions of NOx and HC because

NOx and HC are the principal reactants in the oxidant formation process

and they originate primarily from motor vehicle emissions and

The highest oxidant values are recorded in_ effect areas that receive air

from source areas where motor vehicles are clearly identified as the

dominant source of NOx and HC

243

Future Control Strategy

The APCD strategy for achieving and maintaining the oxidant air quality

standard is based upon the fact that high oxidant values are due to motor ve-

hicle emissions of hydrocarlxms arrl nitrogen oxides This strategy is as follows

1 Both Hydrocarbon and Nitrogen Oxides Emissions Must Be Considered To Achieve the Federal Oxidant Standard

There is wide agreement that NOx and HC are the principal reactants in

the oxidant formation process and that vehicular emissions are a major source

of NOx HC and CO

2 Effective Regulation of Atmospheric Concentrations of Both HC and NOx and of the Ratio Between Them is necessary for Attainment of the Federal Air Quality Standard for Oxidant

Basmiddoted on the abundance middotof available experimental evidence it is our firm

position that the most rational approach to solving the photochemical oxidant smog

problem in the South Coast Air Basin (SCAB) is to control the quantities of emissions

from motor vehicles of both smog precursors--Hcmiddot and NOx--their resulting atmosshy

pheric concentrations and the ratios between both contaminants which will result

from these controls

We arc also convinced that the oxidant and nitrogen dioxide air quality stanshy

dards can and will be met not by 1975 or 1977 but by the early 1980 s if the emisshy

sion control program as originally outlined by Ca~ifornia or a slight modification

of it proposed by the District is followed and enforced This should also provide

for continued compliance with these air quality standards at least through 1990

244

It will also allow time for a reappraisal in about 1978 of the whole situation relative

to the ultimate emission standards required and the best approach to their impleshy

mentation

Calculation of the degree of control necessary to attain the air quality

~ standards for oxidant and nitrogen dioxide involves indirect complex methods 1

aimed at determ_ining the degree of control of the primary contaminants directly

emitted by automobiles

The following evidence supports our proposed solution to the problem in

terms of both the atmospheric concentrations of the oxidant precursors NOx

and HC the ratio between them as reflected in their exhaust emission standards

and the resulting atmospheric concentrations of oxidant which comply with the air

quality standards

Chamber Results and Projections to the Atmosphere

The importance of environmental chamberwork cannot be minimized the

j need for and direction of the whole emission control program was based initially

j on the results of chamber experiments In order to understand the importance to

air quality of achieving both the correct low quantities of emissions and the right

ratio we can present several graphic portrayals of analyses of experimental labshy

oratory work together with their relationship to past present and future air quality

in terms of both morning primary reactant concentrations during the morning

traffic peak and the equivalent emissions which would produce them

245

Figure 7 shows maximum ozone levels that were obtained by irradiating

varying amounts of auto exhaust hydrocarbons and oxides of nitrogen in an environshy

mental chamber The corresponding ozone levels then can be found for any comshy

bination of BC and NOx concentrations Thus high ozone is produced with high

emissions of both hydrocarbons and oxides of nitrogen and low oxidant is formed with

low emissions However either low NOx or low HC emissions11 can also produce

low oxidant--graphic and clear evidence of the importance of the NOxHC ratio in

ozone formation Furthermore each and every possible combination of values for

NOx and HC has then a corresponding characteristic maximum chamber ozone

concentration

Using this graph we can estimate what ozone levels would result if certain

atmospheric mixtures of NOx and HC could be injected into the chamber and

irradiated Such estimates were made for 1960 and 1965 using atmospheric data

rlThe points labeles 1960 and 65 show the location of the highest levels of both

HC and NOx found in the air in those years in Downtown Los Angeles (OOLA) area

during the 6-9 AM traffic peak

It has been demonstrated by use of CO and NOx data and CONOx ratios

hnw well the characteristics of vehicle emissions are reflected in the atmosphere

We know what emissions from the average vehicle were then in 1960-1965 both

for HC and NOx so that we can mathematically relate emissions to atmospheric

concentrations for those years and so for future years also knowing or calculating

only what the characteristic emissions will be from the average vehicle

246

The NOx concentrations stayed about the same from 1960 through 1965 because

average vehicle emissions of that contaminant did not change during that time

Mobile source emissions can be shown to have contributed essentially all of this obshy

served result However blow by controls did reduce emissions of HC and the

concentrations dropped accordingly In 1965 the last year before exhaust controls

the point 65 indicates where we were then in terms of maximum ozone formation

to be expected in a chamber with the highest HC and NO concentrations found in the X

air that year Levels of ozone actually measured in the atmosphere however

are higher than those shown on the graph for high NOx and I-IC concentrations for

those years up to the present

The strategy to meet the oxidant standard is obvious--get atmospheric NOx

and HC concentrations out of the area on the chart that produces high ozone levels

and put them in tie areas with the lowest levels This can only be done by implementshy

ing appropriate emission standards

As can be seen that did not happen between 1965 and 1970 because manufacshy

turers used controls on new cars in California which while causing a decrease in

BC (and CO) allowed a large increase in NOx emissions Thus the path line of

the atmosphere on the chart goes up from 65 and diagonally to the left passing

through an area of higher ozone levels The atmospheric concentrations of oxidant

predictably increased during the years 1967 and 1968 By 1970 they dropped to lower

levels - -back to about the same as in 1965- -exactly as predicted by the model The

app14oximate location of the point for 1970 (70) was both predicted on the basis of

247

the mathematical model and confirmed by atm-ospheric measurements of

[)owntown Los Angeles morning summertime NOx and calculated HC values

Again it should be pointed out that those points show the highest possible

concentrations of NOx and HC Years with less restrictive weather conditions

(for accumulating high primary contaminant levels) would cause lower measured

maximum NOx and HC levels but the calculations would still yield the points

shown Thus we are taking the most pessimistic view

Future Projections

In 1973 we were at about the point labeled 73 and ozone levels were beginshy

ning to drop as expected middot It should be emphasized that ozone values plotted on

thi$ graph are for the chamber only- -not the atmosphere The future path the

points 7 4 and on to 90 represents our estimate of future atmospheric levels of

NO and BC expected if the exhaust emission standards are just met While that X -

is optimistic it is all we really can do since performance of future vehicle models

is unknown We will achieve maximum ozone levels at or below the standard by

about 1980-1985 This will only be true however if cars in compliance with the

California interim standards for HC and NOx continue to be added to the vehicle

population at the normal rate These standards provide the optimum ratio of NO X

to HC necessary to provide the nitric oxide (NO) needed for the reaction that re-

moves from the air both oxidant formed photochemically and oxidant which occurs

as natural background which alone may cause the standard to be exceeded This

ratio is about 112 or 2 parts NOx to 1 part HC

248

The optimum NOxHC ratio is a key element in the APCD strategy but will

require a finite time for its attainment Replacement of older cars by newer ones

equipped to meet the most stringent standards is the only reasonable mechanism

which can change it VMT reduction proposed as a prime strategy by EPA cannot

change this crl(ical ratio which is a basic characteristic of the population at any

given time

Validation of the Districts Control Strategy

Figure 8 compares (1) future chamber oxidant levels based upon the

future maximum concentrations of HC and NOx we expect each year with the

California control program (2) calculated atmospheric concentrations using ~ I

our chamber-to-atmasphere empirical translation and (3) actual measured atmos-f 1l pheric oxidant maxima This clearly sets forth the relationship among these three

factors

The chamber concentrations (lower curve) middotare the lowest values shown

The actual atmospheric data (points connected by heavy dotted and solid lines)

vary considerably from year to year partly because of the vagaries of the weather

In all cases the atmospheric oxidant values are higher than the chamber values

because of the addition of vehicle emissions as the air parcel travels from source

to receptor areas The calculated atmospheric data (thin dashed and solid curves)

are shown to be the highest generally exceeding or equalling the actual measured

data and of course always exceeding the chamber data Thus the model paints

the most pessimistic picture possible It can be seen that by about 19801 1985 atmos -

pheric levels should be at or below the Federal air quality standard of 0 08 ppm oxidant

249

3 Motor Vehicle Exhaust Control is the Only Requirement for Achieving the Oxidant Standard by 1980

We can show that the existing motor vehicle control program has resulted

in a significant reduction of oxidant concentrations in the air

The foregoing material explained the relationship between vehicula~ emis -

sions in source areas and the high oxidant levels measured in effect areas This

relationship is exemplified by the downward trend of oxidant levels in the atmosshy

phere and by the similar year-by-year trends of NO and HC emissions from the X

average motor vehicle A projection of these vehicle emissions factors shows that

the associated maximum oxidant level in the atmosphere will meet the oxidant standard

by about 1980-1985

Figure 9 compares by year the number of days that the oxidant air quality

standard was exceeded in three separate areas with the average NO and HC emissions X

per vehicle mile To comply with the air quality regulations the number of days that

this standard is exceeded must be reduced to one per year

The lines plotted on Figure 9 show that a definite relationship exists between

the emissions from the average motor vehicle and the number of days each year that

the oxidant concentration in the air exceeds the clean air standard

The oxidant trendlines for downtown Los Angeles Pasadena arrl Azusa are

all downward and the slopes are about the same This similarity is logical because

the process that results in the suppression of oxidant accumulation simply has been

displaced from one area to another This was a unique one time situation because

of the increase in NOx between 1966 and 1971 After 1971 all areas are down Thus

l

250

the same conclusion is reached that the oxidantstandard will be met in the 1980s

I whether air quality data or vehicle emissions trends are projected middot~ Ul-

This outlook is based on the APCD s belief that future growth in both the

Los Angeles area and SCAB will not create any locality with a traffic density greater

than any traffic density in the area to date For the past 25 years the area around

downtown Los Angeles has been the area of maximum traffic density and therefore

the emissions source area responsible for the maximum effect area measurements

It is assumed that the traffic density in any future source area will be no

greater than the traffic density in downtown Los Angeles Thus since the

vehicular emissions control program will achieve and maintain the air quality

standards in areas affected by vehicular emissions from downtown Los Angeles it

will also achieve and maintain them for any area of SCAB

Summary Conclusions and Recommendations

In conclusion we have shown that a source and effect area analysis of emisshy

sions and resulting oxidant is a more reasonable and accurate representation of

the Los Angeles area for air quality analysis than gross integration metho9s such

as the big box technique It has been shown that motor vehicles are the major and

almost sole contributor to the primary HC and NOx emissions in the downtown source

area which results in the high oxidant levels in the San Gabriel Valley in fact the

highest in SCAB An air quality model and vehicle emissions control strategy has

been suggested to meet the oxidant standard by mid-1980 s

251

We have shown that

bull Only by adjusting the ratio of NOxHC in the motor vehicle emissions to

permit accumulation of sufficient atmospheric NO to sea venge the normal

atmospheric background oxidant can the standard be attained

bull The APCD strategy which provides for implementation of the present

California interim emissions standards for NOx HC and CO for new

motor vehicles in California beginning with the 1975 model vehicles will

result in compliance with the CO N02 and oxidant air quality standards

by the mid 1980 s and will maintain this compliance until 1990 and

possibly longer

bull The effectiveness of the present California motor vehicle control program

is easily demonstrable using air quality data from several areas in Los

Angeles County 1960-1973

bull To assure achievement and maintenance of the air quality goals as now preshy

dicted there must be periodic assessments of the effectiveness of the

motor vehicle control program followed by corrective actions if necessary

What has been accomplished thus far is significant but much more remains

to be done so that the best possible representation of emissions and resulting air

quality may be available for use in this air basin A much better emission inventory

defining the spatial and temporal distribution of both mobile and stationary sources

is needed Better statbnary source information is needed to evaluate the local

effects of these emissions Further detailed studies are needed to establish the

252

true relationship between emissions data from vehicle test cycles and the actual

operation of vehicles neither the 7-mode nor the CVS procedure provides a true

representation of actual vehicle operation Further tracer studies to assess the

transport and dilution of mobile and stationary source emissions from selected

source areas are also needed

253

1111

IUD

a CC I w gt-

1111

1UO

IUD

I 990

IDJO

1180

1111

IUO

FIGURE I

HYDROCARBONS

STATIONARY SOURCES MOTOR VEHICLES

- --

8 12 II 20 742 2l IS 12 I 4

HUNDREDS

HYDROCARBON EMISSIONS STATIONARY SOURCES IN

OXIDES OF

0

OF TONSDAY

FROM MOTOO VEHICLES AND LOS ANGELES COUNTY

NITROGEN

STATIONARY SOURCES

MOTOR VEHICLES

011111111111111111110111bull1111111

IIIIIIHIIIIIIIIIHIUII

llillL Its rd

l1uu~111111u1111111

2 I O 1 J 3

HUND REDS OF TONSDAY

OXIDES OF NITROGEN EMISSIONS FROM MOTOR VEHICLES ANO STATIONARY SOURCES IN LOS ANGELES COUNTY

illl~ -~--~ i~-=i _J~l ~--~ bull_~L- I ~~~-~~--Z ~

6

6S-66 ox

ICS ~A~1 M

i ssmuwmmgt

bullI

e COROyent_

64 ~ IDB RIVERS~

ORAJfD

-

t t 10 miles

bullmiddotsame Avg Cone Both Years

Pigare 2

YEAR OP HIGHEST OXlDANI CONCENTRATIONS

Highest Average of Daily -Maiimum One-Hour Concentrations

During July August amp September 1963-1972

bullLj

I

64

70 s11 3RlU)U0

70

--__ 69bull

N V +=

middot Source Air Resources Board

-200o

t t 10 adlea

tDS ampIJtsect

-1~

-1611ASampXllmiddot bull - bull -z----~------

I ldmmprwJ

IIVERSIDI

~ - 70

OampY -1 U 70 bull L

I

N V1 V

middot-i___

-----------------------------------------------------------i----------------------------

Figure 3

CHANGE OP OXIDANT CONCENTRATIONS

Percent Change from the Highest Three-Year Average to the 1970-72 Average

Of Daily Maximum One-Hour Con~entrationa for JulY August amp September

Source Air Resources Board

256

FIGURE 4 TYPICAL FLOW OF POLLUTED Am PARCEIS CIUGINATING AT DIFFERENT LOCATIONS IN THE LOS ARE~S BASIN - STARTIOO 0900 PST

l I

OAT

TRAJECTORY SUWMATIOl4

----- SMOG ~AVS

I

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullNONbullSlfOG DAYS

ISTARTING Tl~ cgxpsy

~ HAW

(CA

257

FiGURE 5 ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AND OXIDANT IN DOWlflC1N LOS AIDELES (SOURCE AREA) AND PASADENA (EFFECT AREA) 1

1960-1972

LO CARBON MONOXIDE

30

Pasadena

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullbullbullbullbull Downtown Los Angeles

20

10

o_______________________________

OXIDANT

)

2 Down~ Los Angeles

1

o________________________ 1960 1962 196L 1966 1968 1970 1972

YEAR

bullbullbullbullbull

bullbullbullbullbullbullbull

258

FIGURE 6 COMPARISON 01 CALCULATED AND MEASURED ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AN1) OXIDES OF NITROOEN IN DCMNTOWN IDS AIJELES

196o-1972

CARBON MONOXIDE

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ~ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot _-- ---_ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ----middotmiddot-bullw-_~ ---bullbullbull

10

o_______________1111111_____

OXIDES OF NITROGEN25

20

15 bullbullbullbullbullmiddotmiddotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~

1-i 10 middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ---

oS o_______________________

RATIO CONOx

40

50

0 +raquo Cd

p 30

~ 20

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot bullbullbullbullbull middotmiddotmiddotmiddotmiddot-shybullbullbullbullbull 0 u

bullbullbullbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot 10

0 j

ilI 196o 1964 1968 1970 1972 I

YEAR

Measured~D-owntown Los Angeles (90th percentile ofmiddot daily] instantaneous maxima)

Calculated - Aver~ge vehicle emissions - Present control program

259

FIGURE 7

25

t i5

flJ

~ on ~ ~ Q) bO 100 Jo

+gt on z

o5

EFFECT OF CALIFORNIA 1 s AUTO EXHAUST CONTROL ffiOORA M ON MAXIMUM CHAMBER OZONE CONCENTRATION

- PPM

357bullbull

r 76 bull

11 l

30

20

CHAMBER OZONE MAXIMUM

50

10

o___________111111111111______111111111111_____________

0 05 10 15 20 25

Hydrocarbons m-2 (LB-15) - PPM (as Hexane)middot

--

bull bull bull

r--=--~1 ~a==-~ - _~l ~ y--===-- ~~--~-- ~ r---~~

o

o8

~ I

~ 0 H 8 o6 I

c~ ~ 0 z 0 0

8

~ o+ A H gtlto-

02

middoto

Figure 8 Calculated t1ax1mum Levels Instantaneous and Hourly Average

of Atmospheric Oxidant Compared to Measured Los Angeles County Maxima-with Projections to 1990

(California Standards)

~ -Calculated Inst ax ~

f Calculate Max Hr Avg 03

_ bullbull _ _ - i bull

0 bullbull -l bullbull a0Ieasured Inst Lax o3 bull middotmiddotmiddot~bull 0bull _ ____ V ~ ea~ured ~ Hr Avr o3

~~ r---

~ ~ NB r~ima for 197 4 amiddots of 121074--- -_ Chamber Ozone F ~_ _~

- 1L_

~ Federal Primarfo Air ~uality Standard ~6- -UaximumT- our Avera~elr~ppm-------------- --~ ------- -~- -~-- ~

I I I I I I I I I I I I I I I I I N1 O

1960 6i 64 66 ~i middot-o 72 74 76 79 middotso middot92 84 bullg s9 9o

TBAR (end)

0

261 FIGURE -OMPARISON OF ATMOSPHERIC OXIDANT TRENDS WITH AVERAGE NCJx AND

HC EMISSIONS (Grams per Mile from Average Vehicle)

JOO Number of days state oxidant standara wds equalled or exceeded

--- Azusa __ Pasadena ________ Downtown Los Angeles

20

15 u

___ Hydroc_arbons Oxides of Nitrogenbullmiddotmiddotmiddotmiddotmiddotbullbullmiddot 1975 and later-assume middotcalifornia ARB standards

o_ ___________________________11111____

1965 1970 1975middot 198omiddot 198S 1990

135

Some of you may have received copies already those who contributed to the

study should have received copies by this time

One thing that has become apparent during the first day of this

meeting and was even reflected by the previous speaker is that there

remain a lot of unknowns a lot of questions that seem to me should have

been answered in the last ten years In spite of the uncertainties about

the causeeffect relationships between emission sources and photochemical

smog the decision fortunately has been made to go ahead and control the

smog anyway The general conclusion has been that air pollution is

reduced by reducing the emission of air pollutants and an aggressive

automobile emission control program has been initiated although it has

been delayed several times and the results have not come as rapidly as

one would have hoped With the 1975 automobiles there is indeed a subshy

stantial reduction in hydrocarbon and CO emissions this impact should now

begin to be felt over the next 10 years as these vehicles replace those

already on the road

The costs of these emissions controls are large somewhere between

one and five billion dollars per year The costs are large especially in

comparison with the investment that has been made in fundamental research

to understand the nature of the air pollution problem I would like to

discuss several points First I would like to say a few words on the

background of the automotive engine emissions controls then I would like

to give my assessment of the 1975 California vehicle and its emission

control system--just what its strong points and problems are and finally

I will try to identify what the critical problem areas are now in automotive

emissions controls

I believe it is important to remind you that the automobile engine was

developed over the last 50 years with goals in mind which had nothing to do

136

with air pollution As a consequence we have an automobile engine which

is a low-cost production item has a high power-to-weight ratio has

turned out to be a reliable relatively low maintenance very durable

device and in some cases even the fuel economy is not so bad Then after

the fact it was decided that this engine rhould be made to be low

emitting Therefore it is not too surprising that the approach of the

automobile industry has been to modify thi engine in which they have a

great deal of confidence and know how to build inexpensively as little as

possible The control approaches therefore have been minor modifications

to the engine and have now focused upon processing the exhaust This to

my thinking as an engineer is not a good approach But objectively if

one judges simply on the basis of whether emissions are controlled or not

has worked out quite well I do not think we can be too critical of the

add-on catalyst technology if it works The evidence now suggests that it

is going to work that it is probably cost effective and that the autoshy

mobile industry probably deserves more credit than they are receiving for

the job theyve done in developing the oxidation catalyst for the autoshy

mobile engine What Im saying is the add-on approach is not necessarily

all that bad

Again to give some general perspective on how one might approach

automotive emission controls and how we arrived where we are Id like to

discuss Figure 1 which points out several approaches to controlling

emissions from the automobile engine These are

1) preparation of the air fuel mixture which has received only minor

attention by the auto industry

2) modification of the engine itself the combustion process which

is not very evident in the 1975 automobiles but will be the subject of

Dr Newhalls presentation and

I I

I

137

3) the general field of exhaust treatment where most of the effort

has been placed by the U S auto industry

I would like to emphasize that the first area the whole matter of

mixture control that is either improving the present carburetor or

replacing it with a better mixture control system is perhaps the single

technological area which has been most overlooked by the automobile

industry The engine requires a well meteTed fuel-to-air mixture over a

wide variety of operating conditions that is good cycle-to-cycle and

cylinder-to-cylinder control The present systems simply do not do that

It is also evident that the mixture control system must operate with varying

ambient conditions of pressure and temperature The present systems do not

do that adequately There are promising developments in improvement of

mixture control systems both carbureted and fuel injection which do not

appear to be under really aggressive develJpment by the automobile industry

One should question why this is not occurring

I will skip the area of combustion modification because that really

comes under the new generation of engines The combustion modification is

an important approach and will be discussed by the next speaker

The area of exhaust system treatment the third area is the one about

which youve seen the most We early saw the use of air injection and then

improved air injection with thermal reactors Now were seeing oxidation

catalysts on essentially 100 of the U S cars sold in California There

are yet other possibilities for exhaust treatment for the control of

oxides of nitrogen based upon reduction catalysts or what is known as

threeway catalysts another variation of the reduction catalyst and

possibly also the use of particulate traps as a way of keeping lead in

gasoline if that proves a desirable thing to do (which does not appear to

be the case)

138

What about the 1975 California car Most of you probably have enough

interest in this vehicle that youve tried to figure out just what it does

But in case some of you have not been able to straighten its operation out

let me tell you as best I understand what the 1975 California car is

The cars from Detroit are 100 cataly~t eq11ipped There may be an excepshy[

l

1 tion sneaking through here and there but it looks like it is 100 These

are equipped with oxidation catalysts in a variety of configurations and

sizes the major difference being the pellet system which is used by

General Motors versus the monolith system which has been used by Ford and

Chrysler The pellet system appears to be better than the monolithic ~ l l system but it is not so obvious that there are huge differences between the

aocgtnow The catalysts come in a variety of sizes they are connected to

the engine in different ways sometimes there are two catalysts sometimes

a single catalyst (the single catalyst being on the 4 and 6-cylinder

engines) Some of the 8-cylinder engines have two catalysts some of them

have one catalyst All California cars have all of the exhaust going

through catalysts This is not true of some of the Federal cars in which

some of the exhaust goes through catalysts and some does not

Ninety percent of the California cars probably will have air pumps

Practically all the cars from Detroit have electronic ignition systems

which produce more energetic sparks and more reliable ignition The

exhaust gas recirculation (EGR) systems appear to have been improved

somewhat over 1974 but not as much as one would have hoped There were

some early designs of EGR systems which were fully proportional sophistishy

cated systems These do not appear to have come into final certification

so that there still is room for further improvement of the EGR system

The emissions levels in certification of these vehicles are extremely low

139

(Table I) Just how the automc1bile industry selects the emission levels

at which they tune their vehicles has been of great interest The

hydrocarbon and CO levels in certification (with deterioration factors

applied--so this is the effective emissions of the certification vehicles

at the end of 50000 miles) are approximately one-half the California

standards The oxides of nitrogen emissions are approximately two-thirds

of the California standards This safety factor is put in by the automoshy

bile industry to allow for differences between the certification vehicles

and the production vehicles to ensure that they did not get into a situation

of recall of production vehicles which would be very expensive

There appears to have been a great deal of sophistication developed by

the automobile industry in being able to tune their vehicles to specific

emission levels General Motors appears to have done better tuning than

the other manufacturers This leads to the rather interesting result

that a significant number of the 1975 California vehicles meet the 1977

emission standards (Table II) that is approximately 10 of the U S cars

certified for California already meet the 1977 emission standards This

does not mean to say that the industry could immediately put all of their

production into such vehicles and meet the 1977 emission standards because

of a concern about the safety factor for the certification versus producshy

tion vehicles Thirty-four percent of the foreign vehicles certified for

1975 in California meet the 1977 emission standards The 1977 emission

standards are 041 grn hydrocarbon~ 34 gm carbon monoxid~ and 20 gm

oxides of nitrogen This does confirm that the oxidation catalysts are a

more than adequate technology for meeting the 1977 emission standards and

only minor refinements and adjustments to those systems are required to go

ahead with the 1977 emission standards There are some other arguments

against this optimistic viewpoint and Ill deal with those later

140

There is a great uniformity in the deBigns which the U S manufacturshy

ers have selected for the 1975 California vehicles For those of you who

do not live in California about 80 of thl~ vehicles in the rest of the

country will be catalyst equipped General Motors is going with 100

catalysts apparently to realize the fuel economy benefit of their system

which more than pays for the cost of the catalyst system We have the very

interesting situation that the more stringent 1975 emission standards have

not only reduced the emissions of the 1975 vheicles with respect to the

1973-1974 vehicles but have also reduced the cost of operating the car

and have improved fuel economy The idea that emissions control and fuel

economy and economical operation are always one at odds with the other is

simply not true Compared to the previous years vehicles the more

stringent emissions standards of 1975 have brought improvements to fuel

economy because they forced the introduction of more advanced technology

The fuel savings which have been realized produce a net decrease in operashy

tional costs over the lifetime of the car This is not to say that pollution

control doesnt cost something If you were to compare the 1975 vehicle

with a completely uncontrolled vehicle tht~re would indeed be an incremental

cost associated with the 1975 vehicle

The foreign manufacturers have demonstrated a greater variety of

approaches in meeting the 1975 California standards but again they are

producing mostly catalyst equipped vehicles There is a widespread use of

fuel injection by the foreign manufacturers especially the Europeans

apparently because this is the easiest appmiddotroach for them and they realize

that only a fraction of their production comes to the United States

Volkswagen for example apparently has gone to 100 fuel injection on its

air cooled engines to be sold in California Mazda will continue to sell

141

rotary engine vehicles and thereby be the only rotary engine vehicle

manufacturer and marketer in the United States General Motorsgt elimination

of therotary engine stated for reasons of emissions is probably more

influenced by problems with fml economy although the two are a bit

difficult to separate Mazda is meeting the 1975 emissions standards and

in fact can meet the 1977 emission standards It has not solved its fuel

economy difficulties on the 1975 cars they will do better in 1976 All

evidence points to a fuel economy penalty for the rotary engine Nonetheshy

less we do have this option available because of the Japanese Also the

foreign manufacturers are providing us with a small number of diesel

engine cars These are of great interest because of definite fuel economy

advantages The diesel engine vehicles also meet the 1977 emissions

standards right now Also in J975 well 3ee the CVCC engine marketed by

Honda

The costs of the 1975 vehicles over tae lifetime of the vehicle are

definitely lower than the costs of the 197~ vehicles The National Academy

of Sciences estimate averaged over all vehicles is that in comparison to

the 1970 vehicles the lifetime cost of emission control system including

maintenance and fuel economy costs is aboJt $250 per vehicle greater in

1975 than 1970 Since the 1974 vehicles w2re about $500 more expensive

there has been a net saving in going from 1974 to 1975 I think the

conclusion we should draw for 1975 is that the auto industry has done a

pretty good job in meeting these standards This is something which they

said they couldnt do a few years ago something which they said that if

they could do it would be much more expewdve than it has turned out to

be

The same technology can be applied to 1977 models with no technological

difficulty and only slight refinements of the systems The fuel economy

142

penalties as estimated by the National Academy of Sciences are small 3

or less in going to the 1977 standards This estimate does assume further

advancements by the auto industry to improve fuel economy--primarily

improved exhaust gas recirculation systems It is unfortunate that this

issue of fuel economy has become so mixed up with the air pollution question

because the two are only slightly related If one is really concerned about

fuel economy and there isnt too much evidence that the auto industry or

the American public really is too concerned right now there is only one

way to have a drastic effect on fuel economy and that is to decrease the

vehicle weight Until that is done with gains on the order of 50 or

more to worry about 3 or 5 differences in fuel economy related to emission

control systems is simply to focus upon the wrong issue

Now what are the problem areas What remains to be done The

problems certainly arent over with the introduction of the 1975 vehicles

Problem Area Number One Field performance What is going to happen

to these vehicles when they get into actual service Past experience with

the 1971 through 1973 vehicles has been rather poor in that EPA and

California surveillance data show that these vehicles are not meeting the

standards Many of them did not meet the standards when they were new

The situation in general is getting worse at least for CO and hydrocarbons

that is with time the emission levels of CO and hydrocarbons for the 1971 I through 1973 vehicles is degrading There is no in-service experience of

this sort with the 1975 vehicles yet The certification data look quite I promising but the test procedures especially for durability are not ithe same as what occurs in actual use It is generally stated that the

1actual use situation for the catalysts will be more severe than the EPA

test procedure A larger number of cold starts are involved in actual use

than in the EPA test procedure and thermal cycling will probably have an

143

adverse effect on the lifetime of the cata]_yst This is not so obvious

It is also likely that the higher temperature duty cycle in actual use will

improve the performance of the catalyst in that it will help to regenerate

the catalyst through the removal of contaminants as long as one does not

get into an overheat situation The National Academy of Sciences estimate

was that the number of catalyst failures tn the first 50000 miles would

be on the order of about 7 Thats a very difficult number to estimate in

the absence of any real data A 7 failure still leaves a net gain in

emissions control even if nothing is done about this failure This points

to the problem of what happens after 50000 miles The EPA certification

procedure and control program only addresses the first 50000 miles The

second 50000 miles or slightly less for the average car is the responsishy

bility of the states Unfortunately then~ seems to be very little progress

in the area of mandatory inspection and ma-Lntenance--very little thought

being given to whether the replacement ofthe catalyst at 50000 miles

if it has failed is going to be required and how that is going to be

brought about The area of field performance remains a major problem

area one which obviously needs to be monitored as the California Air

Resources Board has been doing in the past but probably even more carefully

because the unknowns are higher with the catalyst systems

Problem Area Number Two Evaporative hydrocarbons from automobiles

It was identified at least 18 months ago that the evaporative emission

control systems are not working that the evaporative emissions are on the

order of 10 times greater than generally thought In the Los Angeles

area cars which are supposed to be under good evaporative emissions

controls are emitting approximately 19 grams per mile of hydrocarbons

through evaporation This apparently has to do with the test procedure used

144

The EPA is pursuing this The California Air Resources Board does have some

consideration going on for this but it appears that the level of activity

in resolving this problem is simply not adequate If we are to go ahead

to 04 of a gram per mile exhaust emissions standards for hydrocarbons

then it just doesnt make sense to let 19 grams per mile equivalent escape

through evaporative sources

Problem Area Number Three What about the secondary effects of the

catalyst control systems Specifically this is the sulfate emissions

problem and I really do not know the answer to that Our appraisal is

that it is not going to be an immediate problem so we can find out what

the problem is in time to solve it The way to solve it now since the

automobile industry is committed to catalysts and it is unreasonable

to expect that they will reverse that technology in any short period of

time is take the sulfur out of the gasoline The cost of removing sulfur

from gasoline is apparently less than one cent per gallon Therefore if

it becomes necessary to be concerned with sulfate emissions the way to

meet the problem is to take the sulfur out of gasoline Obviously sulfate

emissions need to be monitored very carefully to see what happens The

final appraisal is certainly not now available Another secondary effect

of the catalysts is the introduction of significant quantities of platinum

into an environment where it hasnt existed before Not only through

exhaust emissions which appear to be small but also through the disposal

problem of the catalytic reactors Since the quantity of platinum involved

is quite small the argument is sometimes used that platinum does not

represent much of a problem The fact that the amount of platinum in the

catalyst is so small may also mean that its not economical to recover it

This is probably unfortunate because then the disposal of these catalysts

l Jj

145

I becomes important I will not speak to the medical issues because

am not qualified The evidence is that theuro~ platinum will be emitted in a

form which does not enter into biological cycles--but this is no assurance

that it couldnt later be transformed in such a form What is obviously

needed is a very careful monitoring program which hopefully was started

before the catalysts were put into service If it wasnt then it should

be started today

Problem Area Number Four NO control The big problem with NO X X

control is that nobody seems to know or to be willing to establish what

the emission control level should be It is essential that this be tied

down rapidly and that it be fixed for a reiatively long period of time

because the NO level is going to have a VE~ry important ef feet upon the X

development of advanced engine technology The 20 gm level has been

attained in California with some loss of fuel economy through the use of

EGR and it is not unreasonable in our estimation to go to 15 grams per

mile with very little loss in fuel economy To go to 04 gram per mile

with present technology requires the use of one of two catalytic systems

either the reduction catalyst in tandem with the oxidation catalyst or what

is known as the three-way catalyst Both of these systems require technoshy

logical gains The state of development appears to be roughly that of the

oxidation catalyst two years ago The auto industry will probably say

that it is not quite that advanced but that if it were required to go to

04 gram per mile in 1978 that it could be done With the catalyst systems

the fuel economy penalties would not be great in fact the improvement to

the engine which would be required to make the system work would again

probably even allow a slight improvement in fuel economy What the 04

gram per mile NO catalyst system would appear to do however is to X

146

eliminate the possibility of the introduction of stratified charge engines

both the CVCC and the direction injection system and also diesel engines

It is in the context of the advantages of these advanced engines to meet

emission standards with improved fuel economy that one should be very

cautious about the 04 grammile oxides of nitrogen standards for automoshy

biles My own personal opinion is that the number should not be that

stringent that a number of 1 or 15 gm is appropriate Such a level

would require advancements but would not incur great penalties

Other items which I view as problem areas are less technically

involved and therefore require fewer comments

bull Nonregulated pollutants--again thls is a matter of keeping track

of particulates aldehydes hydrocarbon composition to make

certain that important pollutants ire not being overlooked or

that emission control systems are not increasing the output of

some of these pollutants

bull Fuel economy The pressures of fuel economy are going to be used

as arguments against going ahead wlth emissions control Mostly

these two can be resolved simultaneously We should simply ask

the automobile industry to work harder at this

bull Final problem area New fuels Again it does not appear that

the introduction of new fuels will come about as an emissions

control approach but that they may be introduced because of the

changing fuel availability patterns and the energy crisis These

fuels should be watched carefully for their impact upon emissions

This does middotappear to be an area in which a great deal of study is

going on at the present time It is one problem area perhaps in

which the amount of wprk being done is adequate to the problem

which is involved

147

In sunnnary then the appraisal of the 1975 systems is that they are

a big advancement they will be a lot better than most of us thought and

that we should give the automobile industry credit for the job theyve

done in coming up with their emissions control systems

With that boost for the auto industry which Im very unaccustomed

to Ill entertain your questions

-------=-~ ~~~ U- ~a1

~_~a--~-~ -J~ ~ -~r- _ --=~-- -___ja--~ __1~~ ~-~----=

AIR

1-4 FUEL----1

I I ENGINE

I II

_________ EXHAUST SYSTEM I bull EXHAUST

I I I

+ MIXTURE CONTROL COMBUSTION MODIFICATION EXHAUST TREATMENT

FuelAir Metering Ignition Air Jnjection FuelAir Mixing Chamber Geometry Thermal Reactor Fuel Vaporization Spark Timing Oxidation Catalyst Mixture Distribution Staged Combustion Reduction Catalyst Fuel Characteristics Ex tern almiddot Combustion Three Way Catalyst Exhaust Gas Redrculation Particulate Trap

FIGURE 1 Approaches to the Control of Engine Emissions

~ i 00

149

TABLE I

Average Emissions of 1975 Certification Vehicles (As Corrected Using the 50000-Mile Deterioration Factor)

Emissions in gmi Fraction of Standard HC CO NO HC CO NO

Federal 1975 X X

AMC 065 67 25 043 045 080

Chrysler 074 77 25 049 051 082

Ford 081 92 24 054 061 078

GM 083 80 23 055 053 074

Weighted Average 080 82 24 053 055 076

California 1975

AMC 042 49 17 047 054 087

Chrysler 048 61 16 053 067 082

Ford 052 56 13 058 062 067

GM 065 55 16 0 72 061 082

Weighted Average 058 56 16 064 062 078

kWeighted average assumes the following market shares AMC 3 Chrysler 16 Ford 27 and GM 54

150

TABLE II

Total Number of Vehicles Certified for California 1975 Standard and the Number (and percentage) of These Able to Meet

Certain More Stringent Standards

Calif 1975 Federal 1977 Hypothesized Hypothes ized 099020 04J420 049020 093420

i ~

Manufacturer no () no () no () no ()

AMC 16 (100) 1 ( 6) ti ( 38) 3 (19)

Chrysler 21 (100) 2 ( 9) ( 33) 0 ( O)

Ford 26 (100) 4 (15) -middot ( 15) 5 (19)

l GM 46 (100) 1 ( 2) -1 ( 9) 5 (11)

Foreign 62 (100) 21 (34) 3H (61) 28 (45)

1J

f

-l

151

CURRENT STATUS OF ALTERNATIVE AUTOM)BIIE ENGINE TECHNOLCXY

by

Henry K Newhall Project Leader Fuels Division

Chevron Research CanpanyRicbmmd California

I

iH1middot

10 1ntroduction and General Background

I

11 General

The term stratified ct1arge englne has been used for many

years in connection with a variety of unconventional engine

combustion systems Common to nearly all such systems is

the combustion of fuel-air mixtures havlng a significant

gradation or stratification in fuel- concentration within the

engine combustion chamber Henee the term nstratifled charge

Historically the objective of stratified charge engine designs

has been to permit spark ignition engine operation with average

or overall fuel-air ratios lean beyond the ignition limits of

conventional combustion systems The advantages of this type

of operation will be enumerated shortly Attempts at achieving

this objective date back to the first or second decade of this

century 1

More recently the stratified charge engine has been recognized

as a potential means for control of vehicle pollutant emissions

with minimum loss of fuel economy As a consequence the

various stratified charge concepts have been the focus of

renewed interest

152

12 Advantages and Disadvantages of Lean Mixture Operation

Fuel-lean combustion as achieved in a number of the stratified

charge engine designs receiving current attention has both

advantages and disadvantages wnen considered from the comshy

bined standpoints of emissionsmiddot control vehicle performance

and fuel economy

Advantages of lean mixture operation include the following

Excess oxygen contained in lean mixture combustion

gases helps to promote complete oxidation of hydroshy

carbons (HG) and carbon monoxide (CO) both in the

engine cylinder and in the exhaust system

Lean mixture combustion results in reduced peak

engine cycle temperatures and can therefore yield

lowered nitrogen oxide (NOx) emissions

Thermodynamic properties of lean mixture combustion

products are favorable from the standpoint of engine

cycle thermal efficiency (reduced extent cf dissociashy

tion and higher effective specific heats ratio)

Lean mixture operation caG reduce or eliminate the

need for air throttling as a means of engine load

control The consequent reduction in pumping losses

can result in significantly improved part load fuel

economy

153

Disadvantages of lean mixture operation include the following

Relatively low combustion gas temperatures during

the engine cycle expansion and exhaust processes

are inherent i~ lean mixture operation As a conseshy

quence hydrocarbon oxidation reactions are retarded

and unburned hydrocarbon exhaust emissions can be

excessive

Engine modifications aimed at raising exhaust temperashy

i tures for improved HC emissions control (retarded middot~

ignition timing lowered compression ratlo protrtacted combustion) necessarily impair engine fuel economy1 I

1j bull If lean mixture operation is to be maintained over ~

the entire engine load range maximum power output t l and hence vehicle performance are significantly

impaired

Lean mixture exhaust gases are not amenable to treatshy

ment by existing reducing catalysts for NOx emissions

control

Lean mixture combustion if not carefully controlled

can result in formation of undesirable odorant

materials that appear ln significant concentrations

in the engine exhaust Diesel exhaust odor is typical

of this problem and is thought to derive from lean mixshy

ture regions of the combustion chamber

154

Measures required for control of NOx emissions

to low levels (as example EGR) can accentuate

the above HC and odorant emissions problems

Successful developmentmiddotor the several stratified charge

engine designs now receiving serious attention will depend

very much on the balance that can be achieved among the

foregoing favorable and unfavorable features of lean comshy

bustion This balance will of course depend ultimately on

the standards or goals that are set for emissions control

fuel economy vehicle performance and cost Of particular

importance are the relationships between three factors -

UBHC emissions NOx emissions and fuel economy

13 Stratified Charge Engine Concepts

Charge stratification permitting lean mixture operation has

been achieved in a number of ways using differing concepts

and design configurations

Irrespective of the means used for achieving charge stratifishy

cation two distinct types of combustion process can be idenshy

tified One approach involves ignition of a small and

localized quantity of flammable mixture which in turn serves

to ignite a much larger quantity of adjoining or sur~rounding

fuel-lean mixture - too lean for ignition under normal cirshy

cumstances Requisite m1xture stratification has been achieved

155

in several different ways rangiDg from use of fuel injection

djrectly into open combustion chambers to use of dual

combustion chambers divided physically into rich and lean

mixture regions Under most operating conditions the

overall or average fuel-air ratio is fuel-lean and the

advantages enumerated above for lean operation can be realized

A second approach involves timed staging of the combustion

process An initial rich mj_xture stage in which major comshy

bustion reactions are completed is followed by rapid mixing

of rich mixture combustion products with an excess of air

Mixing and the resultant temperature reduction can in

principle occur so rapidly that minimum opportunity for NO

formation exists and as a consequence NOx emissions are

low Sufficient excess air is made available to encourage

complete oxidation of hydrocarbons and CO in the engine

cylinder and exhaust system The staged combustion concept

has been specifically exploited 1n so-called divided-chamber

or large volume prechamber engine designs But lt will be

seen that staging is also inherent to some degree in other

types of stratified charge engines

The foregoing would indicate that stratified charge engines

can be categorized either as lean burn engines or staged

combustion engines In reality the division between conshy

cepts is not so clear cut Many engines encompass features

of both concepts

156

14 Scope of This Report

During the past several years a large number of engine designs

falling into the broad category of stratified charge engines

have been proposed Many of these have been evaluated by comshy

petent organizations and have been found lacking in one or a

number of important areas A much smaller number of stratified

charge engine designs have shown promise for improved emissions

control and fuel economy with acceptable performance durashy

bility and production feasibility These are currently

receiving intensive research andor development efforts by

major organizations - both domestic and foreign

The purpose of this report is not to enumerate and describe the

many variations of stratified charge engine design that have

been proposed in recent years Rather it is intended to focus

on those engines that are receiving serious development efforts

and for which a reasonably Jarge and sound body of experimental

data has evolved It is hoped that this approach will lead to

a reliable appraisal of the potential for stratified charge

engine systems

20 Open-Chamber Stratified Charge Engines

21 General

From the standpoint of mechanical design stratified charge

engines can be conveniently divided into two types open-chamber

and dual-chamber The open-chamber stratjfied charge engine

has a long history of research lnterest Those crigines

157

reaching the most advanced stages of development are probably

the Ford-programmed c~mbustion process (PROC0) 2 3 and Texacos

controlled combustion process (TCCS) 4 5 Both engines employ a

combination of inlet aar swirl and direct timed combustion

chamber fuel injection to achieve a local fuel-rich ignitable

mixture near the point of ignition _For both engines the overshy

all mixture ratio under most operating conditions is fuel lean

Aside from these general design features that are common to

the two engiries details of their respective engine_cycle proshy

cesses are quite different and these differences reflect

strongly in comparisons of engine performance and emissions

characteristics

22 The Ford PROCO Engin~

221 Description

The Ford PROCO engine is an outgrowth of a stratified charge

development program initiated by Ford in the late 1950s The

development objective at that time was an engine having dieselshy

like fuel economy but with performance noise levels and

driveability comparable to those of conventional engines In

the 1960s objectives were broadened to include exhaust

emissions control

A recent developmental version of the PROCO engine is shown in

Figure 2-1 Fuel is injected directly into the combustion chamber

during the compression stroke resulting in vaporjzation and

formation of a rich mixture cloud or kernel in the immediate

158

vicinity of the spark plug(s) A flame initiated in this rich

mixture region propagates outwardly to the increasingly fuelshy

lean regions of the chamber At the same time high air swirl

velocities resulting from special orientation of the air inlet

system help to promote rapid mixing of fuel-rich combustion

products with excess air contained in the lean region Air

swirl is augmented by the squ1sh action of the piston as it

approaches the combustion chamber roof at the end of the comshy

pression stroke The effect of rapid mixing can be viewed as

promoting a second stage of cori1bustion in which rlch mixture

zone products mix with air contained in lean regions Charge

stratification permits operation with very lean fuel-air mixshy

tures with attendent fuel economy and emissj_ons advantages In

addition charge stratification and direct fuel injection pershy

mit use of high compression ratios with gasolines of moderate

octane quality - again giving a substantial fuel economy

advantage

Present engine operation includes enrichment under maximum

power demand conditions to mixture ratios richer than

stoichiometric Performance therefore closely matches

that of conventionally powered vehicles

Nearly all PROCO development plans at the present time include

use of oxidizing catalysts for HC emissions control For a

given HC emissions standard oxidizing catalyts permit use

of leaner air-fuel ratios (lower exhaust temperatures)

1

l

159

together with fuel injection and ignition timing charactershy

istics optimized for improved fuel economy

222 Emissions and Fuel Economy

Figure 2-2 is a plot of PROCO vehicle fuel economy versus NOx

emissions based or1 the Federal CVS-CH test procedure Also

included are corresponding HC and CO emissions levels Only

the most recent test data have been plotted since these are

most representative of current program directions and also

reflect most accurately current emphasis on improved vehicle

fuel economy 6 7 For comparison purposes average fuel

economies for 1974 production vehicles weighing 4500 pounds

and 5000 pounds have been plotted~ (The CVS-C values

reported in Reference 8 have been adjusted by 5 to obtain

estimated CVS-CH values)

Data points to the left on Figure 2-2 at the o4 gmile

NOx level represent efforts to achieve statutory 1977

emissions levels 6 While the NOx target of o4 gmile was

met the requisite use of exhaust gas recirculation (EGR)

resulted in HC emissions above the statutory level

A redefined NOx target of 2 gn1ile has resulted in the recent

data points appearing in the upper right hand region of

Figure 2-2 7 The HC and CO emissions values listed are

without exhaust oxidation catalysts Assuming catalyst middotl

conversion efficiencies of 50-60 at the end of 50000 miles

of operation HC and CO levels will approach but not meet

160

statutory levels It is clear that excellent fuel economies

have been obtained at the indlcated levels of emissions

control - some 40 to 45 improved re1at1ve to 1974 produc-

tj_on vehicle averages for the same weight class

The cross-hatched horizontal band appearing across the upper

part of Figure 2-2 represents the reductions in NOx emissions

achieveble with use of EGR if HC emissions are unrestricted

The statutory 04 gmile level can apparently be achieved

with this engine with little or no loss of fuel economy but

with significant increases in HC emissions The HC increase

is ascribed to the quenching effect of EGR in lean-middotmixture

regions of the combustion chamber

223 Fuel Requirements

Current PROCO engines operated v1ith 11 1 compression ratio

yield a significant fuel economy advantage over conventional

production engines at current compression ratios According

to Ford engineers the PROCO engine at this compression

ratio j_s satisfied by typical fu1J-boi1ing commercial gasoshy

lines of 91 RON rating Conventional engines are limited to

compression ratios of about 81 and possibly less for

operation on similar fuels

Results of preliminary experiments indicate that the PROCO

engine may be less sensitive to fuel volatility than convenshy

tional engines - m1 important ff1ctor in flextb1 llty from the

standpoint of the fuel supplier

161

224 Present Status

Present development objectives are two-fold

Develop calibrations for alternate emissions target

levels carefully defining the fueleconofuy pbtenshy

tial associated with each level of emissions control

Convert engine and auxiliary systems to designs

feasible for high volume production

23 The Texaco TCCS Stratified Charge Engine

231 General Description

Like the Ford PROCO engine Texacos TCCS system involves_

coordinated air swirl and direct combustion chamber fuel

injection to achieve charge stratification Inlet portshy

induced cylinder air swirl rates typically approach ten times

the rotational engine speed A sectional view of the TCCS

combustion chamber is shown in Figure 2-3

Unlike the PROCO engine fuel injection in the TCCS engine

begins very late in the compression stroke - just before th~

desired time of ignition As shown in Figure 2-4 the first

portion of fuel injected is immediately swept by the swirling

air into the spark plug region where ignition occurs and a

flame front is established The continuing stream of injected

fuel mixes with swirling air and is swept into the flame

region In many respects the Texaco process resembles the

162

spray burning typical of dj_esel combustion ~r1th the difshy

ference that ignition is achieved by energy from an elec-

tric spark rather than by high compression temperatures

The Texaco engine like the diesel engine does not have a

significant fuel octane requirement Further use of positive

spark ignition obviates fuel I

cetane requirements character-

istic of diesel engines The resultant flexibility of the

TCCS engine regarding fuel requirements is a si~1ificant

attribute

In contrast to the TCCS system Fords PROCO system employs

relatively early injection vaporization and mixing of fuel

with air The combustion process more closely resembles the

premixed flame propagation typical of conventional gasoline

engines The PROCO engine therefore has a definite fuel

octane requirement and cannot be considered a multifuel

system

The TCCS engine operates with hi__gh compression ratios and

with little or no inlet air throttling except at idle conshy

ditions As a consequence fuel economy is excellent--both

at full load and under part load operating conditions

232 Exhaust Emissions and Fuel Economv

Low exhaust temperatures characteristlc of the TCCS system

have necessitated use of exhaust oxidation catalysts for

control of HC emissions to low lf~Vels A11 recent development

163

programs have therefore included use of exhaust oxidation

catalysts and most of the data reported here r~present tests

with catalysts installed or with engines tuned for use with

catalysts

Figures 2-5 and 2-6 present fuel economy data at several

exhaust emissions levels for two vehicles--a US Army M-151

vehicle with naturally aspirated 4-cylinder TCCS conversion

and a Plymouth Cricket with turbocharged 4-cylinder TCCS

engine 9 10 1urbocharging has been used to advantage to

increase maximum power output Also plotted in these figures

I are average fuel economies for 1974 production vehicles of

similar weight 8

I When optimized for maximum fuel economy the rrccs vehicles

can meet NOx levels of about 2 gmile It should be noted

that these are relatively lightueight vehicles and that

increasing vehicle weight to the 4000-5000 pound level could

result in significantly increased NOx emissions Figur~s 2-5

and 2-6 both show that engine modifications for reduced NOx

levels including retarded combustion timing EGR and increased

exhaust back pressure result in substantial fuel economy

penalties

For the naturally aspirated engine reducing NOx emissions

from the 2 gmile level to O l~ gmile incurred a fuel

economy penalty of 20 Reducing NOx from the tllrbocharged

164

engine from 15 gmile to 04 gmile gave a 25 fuel economy

penalty Fuel economies for both engines appear to decrease

uniformly as NOx emissions are lowered

For the current TCCS systems most of the fuel economy penalty

associated with emissions control can be ascribed to control

of NOx emissions although several of the measures used for

NOx control (retarded cornbusticn timing and increased exhaust

back pressure) also help to reduce HG emissions HC and CO

emissions ari effectively controlled with oxidation catalysts

resulting in relatively minor reductions in engine efficiency

233 TCCS Fuel Reauirements

The TCCS engine is unique among current stratified charge

systems in its multifuel capability Successful operation

with a nuraber of fuels ranging from gasoline to No 2 diesel

Table 2-I

Emissions and Fuel Economy of Turbocharged TCCS Engine-Powered Vehicle 1

Fuel

Emissions gMile 2 Fuel Economy

mng 2HC co NOx

Gasoline

JP-4

100-600

No 2 Diesel

033

026

014

027

104

109

072

J bull l ~

-

061

050

059

060

197

202

213

230

1M-151 vehicle 8 degrees coffibustion retard 16 light load EGR tw0 catalysts (Ref 10)

2 CVS-CH 2750 pounds tnert1a welght

165

l

has been demonstrated Table ~-I lists emissions levels and

fuel economies obtained with a turbocharged TCCS-powered

M-151 vehicle when operated on each of four different fuels 10

These fuels encompass wide ranges in gravity volatjlity

octane number and cetane leve 1 as middotshown in Table 2-II

Table 2-II

Fuel Specifications for TCCS Emissions Tests (Reference 10)

Gravity 0 API Sulfur

OFDistillation~

Gasolj_ne 100-600 JP-4 No 2

Diesel

88 -

86 124 233 342 388

0024 912

-

486 012

110 170 358 544 615

0002 57 356

541 0020

136 230 314 459 505

-middot --

369 0065

390 435 508 562 594

--

lta 9

IBP 10 50 90 EP

TEL gGal Research Octane Cetane No

Generally the emissions levels were little affected by the

wide variations in fuel properties Vehicle fuel economy

varied in proportion to fuel energy content

As stated above the TCCS engine is unique in its multifuel

capability The results of Tables 2-I and 2-II demonshy

strate that the engine has neither 8ign1ficant fuel octane

nor cetane requirements and further that it can tolerate

166

wide variations j_n fuel volati1tty rhe flexibility offered

by this type of system could be of major importance in

future years

234 Durability Performance Production Readiness

Emissions control system durability has been demonstrated by

mileage accumulation tests Ignltion system service is more

severe than for conventional engines due to heterogeneity of

the fuel-air mixture and also to the high compression ratios

involved The ignition system has been the subject of

intensive development and significant progress in system

reliability has been made

A preproduction prototype engine employing the TCCS process is

now being developed by the Hercules Division of White Motors

Corporation under contract to the US Army Tank Automotive

Command Southwest Research Inr)titute will conduct reliability

tests on the White-developed enGines when installed in Military

vehlcles

30 Small Volume Prechambcr Eng1nes (3-Valve Prechamber Engines Jet Ignition Engines Torch Ignition Engines)

31 General

A number of designs achieve charge stratification through

division of the combustion region into two adjacent chambers

The emissions reduction potentiampl for two types of dualshy

chamber engines has been demonstrated F1 rst ~ j n B desJgn

trad1t1on~JJy caJJld the nrreebrnber engine a 2m211 auxil1ary

167

or ignition chamber equipped w1th a spark plug communicates

with the much larger main combustion chamber located in the

space above the piston (Figure 3-1) The prechamber which

typically contains 5-15 of the total combustion volume

is supplied with a small quantity of fuel-rich ignitable

fuel-air mixture while a large quantity of very lean and

normally unignitable mixture is applied to the main chamber

above the piston Expansion of high temperature flame

products from the prechamber leads to ignition and burning

of the lean maj_n chamber fuel-a_r charge Ignitionmiddot and

combustion in the lean main chamber region are promoted both

by the high temperatures of prechamber gases and bythe

mixing that accompanies the jet-like motion of prechamber

products into the main chamber

I jl

I i j

I

Operation with lean overall mixtures tends to limit peak comshy

bustion temperatures thus minimizing the formation of nitric

oxide Further lean mixture combustion products contain

sufficient oxygen for complete oxidation of HC and CO in the

engine cylinder and exhaust system

It should be reemphasized here that a iraditional problem

with lean mixture engines has been low exhaust temperatures

which tend to quench HC oxidation reactions leading to

excessive emissions

Control of HC emissions to low levels requires a retarded or

slowly developing combustion process The consequent extenshy

sion of heat release j nto 1ate porttt)ns of the engtne cycle

168

tends to raise exhaust gas temperatures thus promoting

complete oxidation of hydrocarbons and carbon monoxide

32 Historical Background and Current Status

321 Early Developm9nt Objectives and Engine Def igns

The prechamber stratified charge engine has existed in various

forms for many years Early work by Ricardo 1 indicated that

the engine could perform very efficiently within a limited

range of carefully controlled operating conditions Both

fuel-injected and carbureted prechambcr engines have been

built A fuel-injected design Lnittally conceived by

Brodersen 11 was the subject of extensive study at the

University of Rochester for nearly a decade 12 13 Unforshy

tunately the University of Rochester work was undertaken prior

to widespread recognition of the automobile emissions problem

and as a consequence emission characteristics of the

Brodersen engine were not determined Another prechamber

engine receiving attention in the early 1960s is that conshy

ceived by R M Heintz 14 bull The objectives of this design

were reduced HC emissions incr0ased fuel economy and more

flexible fuel requirements

Experiments with a prechamber engine design called the torch

ignition enginen were reported n the USSR by Nilov 15

and later by Kerimov and Mekhtier 16 This designation

refers to the torchlike jet of hot comhust1on gases issuing

169

from the precombustion chamber upon j_gnj_ tion In a recent

publication 17 Varshaoski et al have presented emissions

data obtained with a torch ignition engine These data show

significant pollutant reductions relative to conventional

engines however their interpretation in terms of requireshy

ments based on the Federal emissions test procedure is not

clear

l

3 2 2 Current DeveloJ)ments

A carbureted middotthree-valve prechamber engine the Honda CVCC

system has received considerable recent attention as a

potential low emissions power plant 18 This system is

illustrated in Figure 3-2 Hondas current design employs a

conventional engine block and piston assembly Only_ the

cylinder head and fuel inlet system differ from current

automotive practice Each cylinder is equipped with a small

precombustion chamber communicating by means of an orifice

with the main combustion chambe situated above the piston lj

ij_ A small inlet valve is located in each precharnber Larger

inlet and exhaust valves typical of conventlonal automotive

practice are located in the main combustion chamber Proper

proportioning of fuel-air mixture between prechamber and

main chamber is achieved by a combination of throttle conshy

trol and appropriate inlet valve timing A relatively slow

and uniform burning process gjvjng rise to elevated combusshy

tion temperatures late in the expansion stroke and during

the exhaust procezs is achieved H1 gh tewperaturr--s in thin

part of the engine cycle ar-e necessary to promote complete

170

oxidation of HC and CO It si1ould be no~ed that these

elevated exhaust temperatures are necessarily obtained at

the expense of a fuel economy penalty

To reduce HC and CO emissions to required levels it has been

necessary for Honda to employ specially designed inlet and

exhaust systems Supply of extremely rich fuel-air mixtures

to the precombustion chambers requires extensive inlet manifold

heating to provide adequate fuel vaporization This is accomshy

plished with a heat exchange system between inlet and exhaust

streams

To promote maximum oxidation of HC and CO in the lean mixture

CVCC engine exhaust gases it has been necessary to conserve

as much exhaust heat as possible and also to increase exhaust

manifold residence time This has been done by using a relashy

tively large exhaust manifold fitted with an internal heat

shield or liner to minimize heat losses In additj_on the

exhaust ports are equipped with thin metallic liners to

minimize loss of heat from exhaust gases to the cylinder

head casting

Engines similar in concept to the Honda CVCC system are under

development by other companies including Ttyota and Nissan

in Japan and General Motors and Fo~d in the United States

Honda presently markets a CVCC-powered vehicle tn tTapan and

plans US introduction in 1975 Othe~ manufactur~rs

includlnr General Motors and Forgtd 1n thr U S havf~ stated

171

that CVCC-type engines could be manufactured for use in limited

numbers of vehicles by as early as 1977 or 1978

33 Emissions and Fuel Economywith CVCC-Type Engines

331 Recent Emissions Test Results

Results of emissions tests with the Honda engine have been very

promising The emissions levels shown in Table 3-I are typical

and demonstate that the Honda engine can meet statutory 1975-1976

HC and CO stindards and can approach the statutory 1976 NOx

standard 19 Of particular importance durability of this

system appears excellent as evidenced by the high mileage

emissions levels reported in Table 3-I Any deterioration of

l emissions after 50000 miles of engine operation was slight

and apparently insignificant

I Table 3-I

Honda Compound Vortex-Controlled Combustion-Powered Vehicle 1 Emissions

Fuel Economy

Emissions 2 mpg gMile 1972

HC 1975 FTP FTPco NOv

210 50000-Mile Car+ No 2034 Low Mileage Car 3 No 3652 018 212 221089

024 065 198 1976 Standards

213175 20o41 34 - -04o411977 Standards 34 - -

1Honda Civic vehicles 2 1975 CVS C-H procedure with 2000-lb inertia weight3Average of five tests aAverage of four tests

172

Recently the EPA has tested a larger vehicle conve~ted to the

Honda system 20 This vehicle a 1973 Chevrolet Impala with

a 350-CID V-8 engine was equipped with cylinder heads and

induction system built by Honda The vehicle met the present

1976 interim Federal emissions standards though NOx levels

were substantially higher than for the much lighter weight

Honda Civic vehicles

Results of development tests conducted by General Motors are

shown in Table 3-II 21 These tests involved a 5000-pound

Chevrolet Impala with stratified charge engine conversion

HC and CO emissions were below 1977 statutory limits while

NOx emissions ranged from 15 to 2 gmile Average CVS-CH

fuel ec9nomy was 112 miles per gallon

Table 3-II

Emissions and Fuel Economy for Chevrolet Impala Strmiddotatified

Charge Engine Conversion (Ref 21)

Test

Exhaust Emlssions

gMile 1 Fuel

Economy mpgHC co NOx

1 2 3 4 5

Average

020 026 020 029 0 18

023

25 29 31 32 28

29

17 15 19 1 6 19

17

108 117 114 109 111

112

1cvs-CH 5000-lb inertia weight

173

I

332 HC Control Has a Significant Impact on Fuel Economy

In Figure 3-3 fuel economy data for several levels of hydroshy

carbon emissions from QVCC-type stratified charge engines

are plotted 22 23 ~ 24 At the 1 gmile HC level stratified

charge engine fuel economy appears better than the average

fuel economy for 1973-74 production vehicles of equivalent

weight Reduction of HC emissions below the 1-gram level

necessitates lowered compression ratios andor retarded

ignition timing with a consequent loss of efficiencymiddot For

the light-weight (2000-pound) vehicles the O~ gmile IIC

emissions standard can be met with a fuel economy of 25 mpg

a level approximately equal to the average of 1973 producshy

tion vehicles in this weight class 8 For heavier cars the

HC emissions versus fuel economy trade-off appears less

favorable A fuel economy penalty of 10 relative to 1974

production vehicles in the 2750-pound weight class is

required to meet the statutory 04 gmile HC level

333 Effect of NOx Emissions Control on Fuel Economy

Data showing the effect of NOx emissions control appear in

Figure 3-~ 22 These data are based on modifications of a Honda

CVCC-powered Civic vehicle (2000-pound test weight) to meet

increasingly stringent NOx standards ranging from 12 gmile

to as low as 03 gmile For all tests HC and CO emissions

are within the statutory 1977 standards

NOx control as shown in Figure 3-4 has been effected by use

of exhaust gas recirculation 1n comb1nation w1th retarded

174

ignj_tion timing It is clear that control of rmx emissions

to levels below l to 1 5 gmile results in stgnificant fuel

economy penalties The penalty increases uniformly as NOx

emissions are reduced ~nd appears to be 25 or more as the

04 gmile NOx level is approached

It should be emphasized that the data of Fisure 3-4 apply

specifically to a 2000-pound vehicle With increased vehicle

weight NOx emissions control becomes more difficult and the

fuel economy penalty more severe The effect of vehicle

weight on NOx emissions is apparent when comparing the data

of Table 3-I for 2000-pound vehicles with that of Table 3-II

for a 5000-pound vehicle While HC and CO emissio~s for the

two vehicles are roughly comparable there is over a factor

of two difference in average NOx emissions

34 Fuel Requirements

To meet present and future US emissions control standards

compression ratio and maximum ignltion advance are limited

by HC emissions control rather than by the octane quality of

existing gasolines CVCC engines tuned to meet 1975 California

emissions standards appear to be easily satisfied with

presently available 91 RON commercial unleaded gasolines

CVCC engines are lead tolerant and have completed emissions

certification test programs using leaded gasolines However

with the low octane requirement of the CVCC engine as noted

above the economic benefits of lead antlknock compoundt ar-euromiddot

not realized

175

It is possible that fuel volatLLity characteristlcs may be of

importance in relation to vaporization within the high

temperature fuel-rich regions of the prechamber cup inlet

port and prechamber iQlet manifold However experimental

data on this question aomiddot not appear to be available at

present

~O Divided-Chamber Staged Combustion Engines (Large-Volume Prechamber Engines Fuel-Injected Blind Prechamber Engines)

41 General

Dual-chamber engines of a type often called divided-chamber

or large-volume prechamber engines employ a two-stage comshy

bustion process Here initial r~ich mixture combustion and

heat release (first stage of combustion) are followed by rapid

dilution of combustion products with relatively low temperature

air (second stage of combustion) The object of this engine

design is to effect the transitjon from overall rich combustion

products to overall lean products with sufficient speed that

time is not available for formation of significant quantities

of NO During the second low temperature lean stage of

combustion oxidation of HC and CO goes to completion

An experimental divided-chamber engine design that has been

built and tested is represented schematically in Figure ~-1 25 26

A dividing orifice (3) separates the primary combustion

chamber (1) from the secondary combustion chamber (2) which

includes the cylinder volume above the piston top A fuel

injector (4) supplies fuel to the primary chamber only

176

Injection timing is arranged such that fuel continuously

mixes with air entering the primary chamber during the

compression stroke At the end of compression as the

piston nears its top center position the primary chamber

contains an ignitable fuel-air mixture while the secondary

chamber adjacent to the piston top contains only air

Following ignition of the primary chamber mixture by a spark

plug (6) located near the dividing orifice high temperature

rich mixture combustion products expand rapidly into and mix

with the relatively cool air contained in the secondary

chamber The resulting dilution of combustion products with

attendant temperature reduction rapidly suppresses formation

of NO At the same time the presence of excess air in the

secondary chamber tends to promote complete oxidation of HC

and CO

42 Exhaust Emissions and Fuel Economy

Results of limited research conducted both by university and

industrial laboratories indicat~ that NOx reductions of as

much as 80-95 relative to conventional engines are possible

with the divided-chamber staged combustion process Typical

experimentally determined NOx emissions levels are presented

in Figure 4-2 27 Here NOx emissions for two different

divided-chamber configurations 8re compared with typical

emissions levels for conventional uncontrolled automobile

engines The volume ratio 8 appearing as a parameter in

Figure 4-2 represents the fraction of total combustion volume

contained in the primary chamber For a values approaching

I

i J_

177

1

05 or lower NOx emissions reach extremely low levels Howshy

ever maximum power output capability for a given engine size

decreases with decreasing 6 values Optimum primary chamber

volume must ultimately_represent a compromise between low

emissions levels and desired maximum power output

HC and particularly CO emissions from the divided-chamber

engine are substantially lower than eonventional engine

levels However further detailed work with combustion

chamber geometries and fuel injection systems will be necesshy

sary to fully evaluate the potential for reduction of these

emissions

i Recent tests by Ford Motor Company show that the large volume

prechamber engine may be capable of better HC emissions conshy

trol and fuel economy than their PROCO engine This is shown

by the laboratory engine test comparison of Table 4-I 19

Table 4-I

Single-Cylinder Low Emissions middot11 ~ _____En____g__~ne __middot _e_s_-_s_____

Engine

NO--X Reduction

Method

Em1ssions g1 hp-Hr

Fuel Economy

Lb1 hp-HrNOv HC- co

PROCO

Divided Chamber

PROCO

Divided Chamber

EGR

None

EGR

None

10 30

10 04

05 ~o

o J_o 75

130

25

l 1i bull 0

33

0377

0378

0383

0377

178

Fuel injection spray characteristics are critical to control

of HC emissions from this type of engine and Fords success

in this regard is probably due in part to use of the already

highly developed PROCO-gasoline injection system Figure 4-3

is a cutaway view of Fords adaptation of a 400-CID V-8 engine

to the divided-chamber system 2 e

Volkswagen (VW) has recently published results of a program

aimed at development of a large volume precharnber engine 29

In the Volkswagen adaptation the primary chamber which comshy

prises about 30 of the total clearance volume is fueled by a

direct timed injection system and auxiliary fuel for high

power output conditions is supplied to the cylinder region by

a carburetor

Table 4-II presents emissions data for both air-cooled and

water-cooled versions of VW s dtvided-middotchamber engine 3 0

Emissions levels while quite low do not meet the ultimate

1978 statutory US standards

179

Table 4-II

Volkswagen Jarge Volume _Jrechamber Er[ Lne Emissions

Exhaust Emissions

_ _gMile 1

___E_n_gi_n_e__t--H_C___c_o__N_O_x____E_ng__i_n_e_S_p_e_c_i_f_i_c_a_tmiddot_1_middoto_n_s__

20 50 09 841 compression ratio Air-Cooled 16-Liter

prechamber volume 28 of total clearance volume conventional exhaust manishyfold direct prechamber fuel injection

20-Liter 10 40 10 91 compression ratio Water-Cooled prechamber volume 28 of

total clearance volume simple exhaust manifold reactor direct prechamber fuel injection

1cvs c-H

Toyota also has experimented wlth ___a large volume prechamber

engine using direct prechamber fuel injection and has

reported emissions levels comparable to those of Table 4-II 31

43 Problem Areas

A number of major problems inherent in the large volume

prechamber engine remain to be 3olved I~ These problems include the following II

Fuel injection spray characteristics are critically

important to achieving acceptable HC emissions

The feasibility of producing asatisfactory injecshy

tion system hasnot been estab1ished

180

Combustion noise due to high turbulence levels and

hence high rates of heat release and pres[-ure rise

in the prechamber can be excessive It has been

shown that the-noise level can be modified through

careful chamber design and combustion event timing

If the engine is operated with prechamber fuel

injection as the sole fuel source maximum engine

power output is limited This might be overcome

by a~xiliary carburetion of the air inlet for maximum

power demand or possibly by turbocharging Either

approach adds to system complexity

The engine is charmiddotaeter1zed by low exhaust temperatures

typical of most lean mixture engines

References

1 Ricardo H R Recent Research Work on the Internal Combustion Engine 11 SAE Journal Vol 10 p 305-336 (1922)

2 Bishop I N and Simko A Society of Automotive Engineers Paper 680041 (1968)

3 Simko A Choma M A and Repco L L Society of Automotive Engineers Paper 720052 (1972)

4 Mitchell E Cobb JM and Frost R A Society of Automotive Engineers Paper 680042 (1968)

5 Mitchell E Alperstein M and Cobb JM Society of Automotive Engineers Paper 720051 (1972)

6 1975-77 Emission Control Program Status Report submitted to EPA by Ford Motor Company November 26 1973

181

if

7 consultant Report on Emissions Control of Engine Systems National Academy of Sciences Committee on Motor Vehicle Emissions Washington DC September 1974

8 Austin T C and Hellman K H Society of Automotive Engineers Paper 730790 (1973)

9 See Ref 7

10 Alperstein M Schafer G H and Villforth F J Iiil SAE Paper 740563 (1974)

11 US Patent No 2615437 and No 2690741 Method of Operating Internal Combustion Engines Neil O Broderson Rochester New York

12 Conta L~ D and Pandeli American Society of Mechanical Engineers Paper 59-SA-25 (1959)

13 Canta L D and Pandeli American Society of Mechanical Engineers Paper 60-WA-314 (1960)

14 US Patent No 2884913 0 Internal Combustion Engine R Mi Heintz i

15 Nilov N A Automobilnaya Promyshlennost No 8 (1958)

l 16 Kerimov N A and Metehtiev R I Automobilnoya Promyshlennost No 1 p8-11 (1967)

17 Varshaoski I L Konev B F and Klatskin V B Automobilnaya Promyshlennost No 4 (1970)

18 An Evaluation of Three Honda Compound Vortex Controlled Combustion (CVCC) Powered Vehicles Report B-11 issued by Test and Evaluation Branch Environmental Protection Agency December 1972

19 Automotive Spark Ignition Engine Emission Control Systems to Meet Requirements of the 1970 Clean Air Amendments report of the Emissions Control Systems Panel to the Committee on Motor Vehicle Emissions National Academy of Sciences May 1973

20 An Evaluation of a 300-CID Compound Vortex Controlled Combustion (CVCC) Powered Chevrolet Impala Report 74-13 DWP issued by Test and Evaluation Branch Environmental Protection Agency October 1973

21 See Ref 7

22 See Ref 7

23 See Ref 7

24 See Ref 7

182

25 Newhall H K and El-Messiri I A Combustion and Flame 14 p 155-158 (1970)

26 Newhall H K and El-Messiri I A Society of Automotive Engineers Transaction Ford 78 Paper 700491 (1970)

27 El-Messiri I A and Newhall H K Proc Intersociety Energy Conversion Engineering Conference p 63 (1971)

28 See Ref 7

29 Decker G and Brandstetter W MTZ Motortechnische Zeitschrift Vol 34 No 10 p 317-322 (1973)

30 See Ref 7

31 See Ref 7

183

Fig 2-1 FORD PROCO ENGINE

l

Ford Proco Engine Fuel Economy and Emissions _ 15 _ f--1

00 +

I ~ x X gt( X _ x A 7- ~ X x~ ~c - l4catalyst Feed u NOx vs ruel Econ with 1 C0-71 CJ) 14 x x Ynn H( RP c tr ir-t irm vltgtZ G I HC - C0-127 _ A txcessve c

13 Approx W EG R

~ C~~r 351 CID 5000 Lb Inertia Weight

Q 21 A L 0 u w II _j

LJ =gt LL

10

35i CD 4500 Lb Inertia Weight

~ 1974 Production Average Fuel Economy

4 soo _b r-r-r-----z~lt_~~---7--_~--r--1r-7-r1--~-rz7-w~~

150 0 0 Lb PU221ufrac122-1 I

LO 20 30

NOx EMISSIONS-GMSMILE (CVS-CH) Revised216174

0

HKN 71074

Fig 2-2

l

~___-~ ~--=---~ ~=---__---~1 f-=-----1__middot-_~J ~-----------1 ~bull-=-=- (-~-~ LJii-ZJj ~ ~~-~ ~~ -__c~~ 1--~~ ~----~--1 ---------s___-c--1 ~~~-~~~bull r~~-~--middot1 ____c__ J~ p- ~

Texaco TCCS Engine

Shrouded Intake Valve

~ Intakemiddot r~ )p__-- Fuel Nozzle Fuel Nozzte Port ~ -- -yen -_~

X f -J J ( ~1 I --- ~ f middotmiddotj_Ja 1(~-~_ frff 1-Cylinderv~ v_ r--L~ I (~~)J ~- Intake 1 - ------L- middotmiddot - middotmiddot -1 H0 ad middot --- - -- 1 Po rt I 1 I ~~ ) ~ ~ ~~~ -A- I ------

- I _ ---_ ~ P1ston-mgt-lt_ffrac12 T_77~~~--1 i- r_-~J N

- ~- i~-L - _ _ - IExhaust - - I ~ - 1-_ r- bullsect ~ ----lt_ ~ I PortJ~bJ lt 7A--7~ ~1 ~j --~ ~ yl ind er

-__~lli- klmiddot ~ro v_t_gt11J1bull Bti Or K__ - middot ~

I t--tL pgt-- Ultmiddot middot- - Spark Plugr- -1 --U2middot- ~-~

LHorizont al Projections of Nozzle and Spark Plug Centerlines

Fig 2-3 i--1 00 U1

---~---~-~ -------c- --~--- 7middot-r---c-- ~- -~~~==---~~~~~- srsr RZIIEF7 11t111-~-----==-----=-~--~-~~---c=rmiddot=

OPEN CHAMBER TYPE STRATI Fl ED CHARGE ENGINE i-shyCj

DIRECTIONAl~Fsw7 Q

NOZZLE P

I

~J~treg lt-_(__(lt-(11

c_-- _7- -

SPARK PLUG_ l 1__- -_ - l --_ ~ ----__ lt_ lt_ -- --

ltlt_I_--- _

~ gt - _____- -- --~ ~-l_- 1_~ -~- ~ ------

~~~ r_I FUEL SPRAY 2 FUEL-AIR MIXING ZONE ~- _ -------

FLAME FRONT AREA 4 COMBUSTION PRODUCTS

TCCS COMBUSTION SYSTEM

Fig 2-4

3

----==-----~ l~~----bulli r-~ ~-----=-- 1 ~~ ~ -~ ~~ ___-_=gt---l p--- --=-=-_-__71-~-~~ 1-0-- --=---=-- 4 L--_-_-~ P--- ~

25

-c u

f

Cl) 24 gt u _

tgt 23a ~

I

gt-~ 220 2 0 u w 21 _J

lJJ gt LL

2

Texaco TCCS Powered Cricket Vehicle

Max Econ Setting gt A L07 HC

141 CID JQf CR 084 CO 2500 Lb Inertia Wgt

50-so Retard_ 0_73 HC

12 co 051 HC ~ 061 HC

085COA 064CO Retard+ ESPRetard+

EGR

036 HC ~ 115 co Retard +ESP+ EGR

04 06 08 10 12 14 16 18 20 NOx EMISSIONS-GMSMILE (CVS-CH) HtltN1110114

I- 00 -JFig 2-5

-~ ~=- ~ - -i______c_J ~-====c= wr=- ~-~ p--w~~~ rr w -

25

-c u

I

(f)

gt u-lt a_

2

gt-I 20

~ 0 z 0 u LLI

_J

w tJ_

15

I- CJ) CJ)

Turbocharged Texaco TCCS Ml51 Vehicle

Max Econ Adjustment_ HC-3J catalyst Feed C0-70

141 CID 10~1 CR 2750 Inertia Weight 8deg Retard ~

~bull HC-3middot2 catalyst Feed ~~ _ C0-64

_ 5deg Retard HC-0 30 8degRetard LowEGV bullco-11 ~bull HC-3middot6 catalyst Feed WIW21

Med EGR C0-67 1974 Production 33 Average Fuel Economy ~

COmiddoti05 (2750Lb)

I

bull HC-035 co- 141 13deg Retard High EGR

04 10 20 NOx EMISSIONS -GMSMILE (CVS-CH) ~~ts~b~~~74

Fig 2-6

189

Fig 3-1

PRECHAMBER TYPE STRATIFIED CHARGE ENGINE

r Inlet

(Fuel-lean Mixture )

I 0 I

Spark -Prechamber (Fuel-rich mixture)

-Main Chamber

1] HON DA CVCC ENGINE CONCEPT

190

Fig 3-2 Honda CVCC Engine

28 -l u

1

UJ 26 -gt u-(9 CL 24 2-

f

gtshy0gt

22 z ~ _)

u w

20 _J

w ~ LL

18

J= ---- 4 --~~-_----a ~~ _-_bull --~~ 1~~1 ltiil~I ~ ~-r~ ~ -~ ~-~ ~J~-iii-1 ~~1 s _-_ __-

Fuel Economy vs HC Emissions for 3-Valve Prechamber Engines

e NOx-14 15 Liter

bull Honda CVCC 2000 LbsNOx - 12 A Datsun NVCCbull15 Liter

bull ~JOx -09 A 2500 Lbs J LL 1ter NOv -15

2750 Lbs -NOx -17

- I AiJOx -12

0 02 04 06 08 LO 0HYDROCARBON EMiSSlmiddotONS - Glv1 I MILE (CVS-CH) I-

Fig 3-3

J--1

1--Fuel Economy vs NOx Emissions IO N

-- for Honda CVCC Powered Vehiclesr 26 u

l VHc-023 U1 gt umiddot 24_-__

(_IJ o_

~ 22 l

gt-5~-0 z 20 C0-200 u A HC-033w I co -3o_j

_A HC-029w 18 J I C0-27 LL

_ HC-025

HC-017 co -2-3

C0-22

0 -- 02 04 06middot 08 10 12 NOx Ef11SSIONS -GlviS MILE (CVS-CH)

Fig 3-4 middot

I

I

i93

J J

Fig 4-1 Divided Chamber Engine

middot(4) Fuel Injector

1

f J

f ff

f

~ Ii

I f

i

I f ] [

~~

0 0 0 0

i ~ I

1jl

194

E Cl 0

C QJ

CJl 0 _

-1-

z

0

Vl (lJ

-0

X 0

-t-J

V1 ro c X

LLI

Fig ~-2

COMPARISON OF CONVENTIONAL AND DIVIDED COMBUSTION CHAMBER NOx EMISSIONS

5000 MBT Ignition Timing Wide Open Ttl rattle

4000 Conventional Charnber

3000

J = fraction of Total Combustion 2000 Volume in Primary Ct1arnber

Divided Chamber 13 = 0 85

1000

Divided Chamber fo = 0 52

05 06 0 7 08 09 10 11

O~erall Fuel-Air Equivalence Ratio

195

196

AIRBORNE SURVEYS IN URBAN AIR BASINS IMPLICATIONS FOR MODEL DEVELOPMENT

by

Donald L Blumenthal Manager of Program Development

Meteorology Research Inc Altadena California 91001

middotI would like to make several points today First ozonemiddotis basically

a regional long-range problem There is a lot of long range ozone transshy

port and this transport is a normal occurrence The second point is that

ozone is stable in the absence of scavengers Junge mentions in his book

that the residence time of ozone in the troposphere is on the order of a

month Third vertical variations in concentration and ventilation rate are i very important in modeling atmospheres such as Los Angeles Layers aloft

are ventilated down to the surface on occasion and surface pollutants are

ventilated up mountain slopes as Jim Edinger has pointed out before and

often ventilated out of the basin in upper winds Fourth the day to day

carry over of pollutants from one day to the next is a very important considshy

eration in the Los Angeles Basin Finally there is a definite background

level of ozone The geophysical literature says its about O 02 to O 03 ppm (

in various parts of the world Weve seen data varying from 003 to 005 ppm

The difference may be due to calibration differences In any case numbers

like 005 are pretty substantial background levels for ozone

I am going to illustrate the points listed above with some data from

Los Angeles Basin The data were collected during a two-year study funded

by the Air Resources Board some of the analyses were funded by EPA The

study examined the three dimensional distribution of pollutants in the Los

Angeles Basin using airborne sampling systems Coinvestigators on the

project were Dr Ted Smith and Warren White of Meteorology Research Inc (MRI)

197

The first slide shows one of the aircraft we used Its a Cessna 205

which had sampling inlets on the side of the aircraft Figure 2 shows the

instrument system on the inside of the aircraft We were measuring nitrogen

oxides ozone scattering coefficient with a nephelometer condensation nuclei

carbon monoxide and meteorological parameters such as temperature humidity

turbulance Altitude and position were also measured

Figure 4 shows that the typical sampling pattern was a series of spirals

from the top of the mixing layer over an airport virtually to ground level

then we would climb up to the next point on the route and spiral down again

We had three routes (A B C Figure 3) that we would fly We had two airshy

craft and we would fly two of these three routes three times a day any

given day that we could The day I will be talking about September 25~ 1973

we flew what was called the Riverside route (C) and the Los Angeles route

(A) The 25th of July 1973 you might remember was the day before the

federal office buildings were closed in the area here because of smog

Figure 5 shows the surface streamlines at 0300 Pacific Standard Time

about 4 oclock in the morning daylight time on July 25 This streamline

analysis points out the morning stagnation conditions which are a very normal

occurrence in the Los Angeles Basin You start out with very light winds

quite variable maybe a slight off shore flow early in the morning On this

particular day this kind of situation extended well into midday The sea

breeze did not really pick up until up around noon When you have this kind

of a situation and a low radiation inversion at night you have a

long period of accumulation of pollutants all over the Basin espt~cialJy

in the prime source area the southwest portion of the Basin

198

I

Figure 6 shows the streamline pattern at 1600--400 cclock in the

afternoon same day sea breezes develop and with them a transport pattern

that carries pollutants up to the northeast and out toward the eastern por-

tion of the Basin This is a very regular pattern which we see day after l middot

day On July 25 1973 it was a little bit exaggerated The sea breeze was

held off for awhile started a bit late and so there was a very long period

of accumulation in the southwest area and then transport across the Basin

Figure 7 is an average streamline pattern at 1600 PacHic Daylight Time

on low inversion days for August 1970 It is included to show that the pattern

shown before is very typical Flow starts in the western portion of the

Basin and goes right across to the eastern portion This is using surface

data There is a very high average wind velocity in Ontario about 13 m iles

per hour and 23 mph in Riverside This is the average for the whole month

of August at 1600 PDT on low inversion days There is a considerable amount

of transport across the Basin starting relatively slowly in the morning and

accelerating in the afternoon

Figure 8 shows a verticle cross section of the scattering coefficient

The darker areas indicate higher levels of particulates Scattering coefficshy

ient is inversely proportional to visibility In the crosshatched area

visibility is less than about 3 miles In plotting altitude versus distance

inland from the coast you have Santa Monica (SMO) on the coast El Monte (EMT)

Pomona (BRA) Rialto (RIA) Redlands (RED) The lower broken line is surface

ground level The heavy dashed line is the base of the subsidence inversion

that occurred on the two days during this episode The middle line is the

base of the marine inversion There is a large area over in the western

portion of the Basin where emissions accumulate for much of the day At

199

midday the sea breeze has just started ventilating the Santa Monica area

The layer between the inversions is a layer aloft which is fairly well separshy

ated from the surface layer Ozone concentrations for instance in the

layer aloft were on the order of 04 05 ppm using the ARB calibration

method Down in the surface layer they were quite a bit lower in the mornshy

ing due to scavenging

Figure 9 shows that by afternoon the sea breeze starts and you get

kind of a clean air front Sea breeze starts ventilating the whole Basin

the stuff that was over in the west is transported eastward and at approxishy

mately Brackett (BRA) at 1700 PDT there is a clean air front The high conshy

centrations that were over Los Angeles earlier are now centered near Upland

(CAB) The numbers shown over CAB are data taken from a vertical profile

spiral over Upland at about 1600 That turns out to be the time when there

was the worst ozone concentration of the day in the Basin and it did occur

at Upland It could well be a result of the very polluted mass from the

western Basin being transported over the Upland area The layer aloft has

been a bit undercut by the sea breeze and some of the polluted mass has been

around possibly as long as the night before There has been very little

transport in the area aloft ozone concentrations are still very high

Figure 10 shows a trajectory analysis of the air arriving at Upland at

1600 since that was the worst time of the day at Upland We developed a

trajectory envelope using surface wind data and winds aloft so the air

arriving at Upland at 1600 started out somewhere back within this envelope

for example at 1130 PDT We did not go earlier than 1130 because the winds

were pretty much light and variable before that The air that arrives at

Upland at 1600 has been over the western portion of the Basin for much of

200

the morning and q~ite a bit of the evening before Thus there is

a very long period of accumulation and then a transport a pulsing effect

where you have pollutants moved across the Basin

Figure 11 is an isopleth map of surface ozone concentrations Again all

data are corrected to agree with the ARB calibration method Again you can

see that for the hours between 1600 and 1700 using surface data the Upland

area has the highest surface ozone concentrations about 063 ppm The western

area has been well ventilated by the sea breezes and it is cleaned out

The transport is actually pretty much perpendicular to the isopleth line

just about like that

Figure 12 is a vertical profile taken over Upland Cable Airportat

roughly the time of maximum ozone concentration 1636 PDT We are plotting

pollutant concentration on the x-axis versus altitude in meters (since it was

done for an EPA report) Surface leveJ at Upland is a little over 400 meters

the Z line is ozone Ozone concentration within the surface mixing layer

is pegged on the instrument at somewhat above 05 ppm Above the surface

mixing layer it drops off considerably and eventually get down to background

The T line is temperature and you ean see the subsidence inversion

on this day is very nicely documented here and provides a very strong trap

in that area The B line is the scattering coefficient inversely proporshy

tional to visibility Within the surface mixing layer visibility is on the

order of 3 miles or less while up above the surface mixing layer just a few

hundred feet difference visibilities get up to 60 or 80 miles The X is

condensation nuclei the measure of the very fine particles below about 010

micron It is a measure of quite fresh emissions If you have a high condenshy

sation nuclei count there are very fresh combustion emissions If you have

I

201

an aged air mass the condensation nuclei coagulate and the count decreases

considerably You can see that there are still some fresh emissions within

this surface layer as well But up above the surface mixing layer all the

pollutant indicators decrease considerably

Figure 13 is the same type of vertical profile taken over El Monte

which is on the western side of the sea breeze front The sea breeze front

has passed El Monte at this time almost 1700 PDT and again there are

distinct differences between the mass below the mixing layer within the sea

breeze front (below 400 meters) the marine inversion (400 to 800 meters) and

the subsidence inversion The subsidence inversion occurs at about 800 meters

and there is an old layer of very polluted stuff aloft The surface concenshy

trations are lower because of the ventilation by the sea breeze Condensashy

tion nuclei count (X line) within the surface layer is quite high There

are still fresh emissions in the El Monte area The 11 Z line is ozone

about 02 ppm within the surface layer (200 m) but it is 05 ppm up above

the surface mixing layer The scattering coefficient (B line) is very

similar it is lower at the surface and increases to a visibility equivalent

of less than 3 miles above the surface mixing layer The condensation nuclei

count is high in the lower portion of this (eg at 600 m) hut decreases conshy

siderably above This portion of the upper layer (600 m) has been around

at least all morning and condensation nuclei have been scattered from the

area The portion of the upper layer below 600 m has probably just recently

been undercut by the sea breeze and there are still some condensation nuclei

left in it

Figure 14 illustrates a different method of looking at the flushing

problems in the Basin We have tried to develop an objective criteria based

on ground level ozone to show the cleansing of the basin using the time of

202

arrival of clean air We determine the time when the ozone concentrations

drop by a factor of two at any given point The 1600 line means that between

1500 and 1700 the ozone concentration at that point dropped a factor of two

This sort of isopleth chart of when the clean air arrives agrees quite well

with the trajectory analyses although the numbers are a little bit behind

the trajectory analyses for the polluted air Figure 14 again shows the

transport process that takes place across the Basin which is ventilated from

west to east At 1900 some of the fresh ocean air finally gets out to

Redlands

In Figure 15 in order to put this whole flux problem into some perspecshy

tive we looked at the numbers the actual amount of ozone flux across the

basin We calculated the mean trajectory from Torrance towards Redlands

using the surface and upper air data We looked at the flux from the western

basin to the eastern basin basically from Los Angeles and Orange Counties to

Riverside and San Bernardino Counties This is a calculation made at 1700 PDT

We used the winds aloft from Chino as well as the vertical profiles taken at

Pomona and Corona Averaging the ozone concentration throughout the mixing

layer and multiplying by an average wind speed we arrive at a number of 185

metric tons per hour being transported directly from one side of the Basin

to the other If you look at this in terms of actual concentration in the

eastern Basin and assume that the flow was constant for about an hour it

is eno_ugh to fill up the box shown in Figure 15 to 025 ppm ozone which

exceeds the air quality standard by a factor of three (using the ARB calibrashy

tion method) Thus there is a very significant transport of ozone or ozone

precursors from one portion of the Basin to the other side of the Basin One

thing to mention though is that the concentration would not be kept up on a

203

steady state basis because the transport is a result of the pulsing effect

I Illentioned earlier There is a lot of accumulati6n in the western Basin

and these accumulated pollutants are then transported across the Basin This

kind of transport did take place in a couple hours because we also have

measurements from 1500 PDT which give us similar flux numbers

Figure 16 is a trajectory envelope similar to Figure 10 calculated for

Upland at 1600 for the air arriving at Redlands about 600 oclock in the

afternoon I wanted to include this trajectory envelope to show that the

problem is not really simple You cannot say that the air at Redlands came

from Long Beach per se The air at Redlands if you look at the whole

envelope of possible trajectories using upper air data as well as surface

data could have come from anywhere between Downtown Los Angeles and over

the Pacific Ocean south of Long Beach

Another thing to recognize is that the wind actually changes direction

slightly as you go up and down through the mixing layer and the mixing layer

is exactly what it implies There is mixing within the mixing layer so if

you begin with a parcel of air near the surface this parcel may move to the

top of the mixing layer and go one direction for awhile it then may go back

down to the bottom of the mixing layer and move in another direction for

awhile The ratio of the length scales indicata3mixing layer depths of 1500

or 2000 ft and distances on the order of 70 miles This makes it very

difficult for tetroons to follow an air trajectory because they do not go

up and down They stay at one altitude and in one wind regime and yet the

wind regimes are different at different altitudes and the air is continually

mixed up and down through this layer You can often see this on time lapse

photographs

204

The question is where does the pollutant mass go after Redlands Figure

17 is a repeat of Jim Pitts slide from yesterday and it is data for the

same day that we did our analysis It shows the ozone peaks starting at

Pomona and Riverside and on July 25 1973 eventually getting out to Palm

Springs so there is quite a bit of long-range transport The ozone is

stable at 8 00 or 9 00 oclock at night There still are ozone concenshy

trations of 02 ppm it hasnt dissipated even at the surface Ozone does

dilute as the mass moves Other calculations we did were integrations

through the mixing layer of various pollutants such as ozone and CO along

with trajectories that we measured Th~se integrations show just what the

ground data show in Figure 17 The concentrations increase through the western

portion of the Basin and then show a decrease through the eastern portion

of the Basin CO tends to decrease faster than the ozone indicating a

continued production of ozone further east

Figure 18 is a streamline chart on a larger area map for the 16th of

August 1973 It shows the typical streamline patterns that occur for

ventilation from the Basin By mid-afternoon there is flow out through the

major passes to the north and towards Palm Springs (PSP) On this particushy

lar day we had data from Arrowhead showing that the air mass from the Basin

does indeed get up there

Figure 19 shows a vertical profile over Arrowhead early in the morning

16 August 1973 at a time when there was a north wind Ozone level was

about 005 ppm the scattering coefficient was quite low on the order of

probably 60 miles visibility or so Figure 20 is a vertical profile again

over Arrowhead late that afternoon when the winds had switched There is a

flow from the Los Angeles Basin into the Arrowhead area thus one sees a

205

vertical profile that shows a distinct increase near the surface in both the

ozone and the scattering coefficient and in the condensation nuclei Ahove

that you have fairly clean air The top of the polluted level is just about

the top of the mixing level over the Basin

I want to leave the transport now and discuss the complicated vertical

structure that can occur If you want to try to model something try this

one for instance Figure 21 is a vertical profile over Brackett Airport

Pomona about 830 in the morning on 26 July 1973 which is the day after

the episode shown earlier A bit of interpretation shows how complicated

th is can be If one looks at the temperature profile it would be very

difficult to pick out a mixing layer theres a little inversion here another

inversion there several more up here After looking at hundreds of these

profiles though you can start interpreting them What is happening is that

there is a surface mixing layer at about 500 m In this layer there is a

high condensation nuclei (X line) count due to morning traffic The San

Bernardino freeway is quite close to Brackett there is a relatively high

nitrogen oxide count about 02 ppm and the b-scat is fairly high Ozone (Z)

within the surface layer however at this time is quite low The layer beshy

tween 500 m and 700 rn turns out to be the Fontana complex plume Note the

very high b-scat level it is below 3 miles visibility the plume is very

visible especially at this time of the morning when it is fairly stab]e

There is a high nitrogen oxide level (800 m) a high condensation nuclei

level and again a deficit of ozone Above this layer (800 m) you have stuff

that has been left all night very low condensation nuclei indicating a very

aged air mass ozone concentrations about 016 ppm b-scat of about 04 It

has been around all night and not yet had a chance to mix down within the

206

surface layer In fact one good way of determining the surface mixing layer

early in the morning and at night is to look for the ozone deficit Another

thing to mention is that wind reversals occurred for each of these three

layers The winds were fairly light and westerly at the surface slightly

easterly in the 500 m 700 m layer and westerly above 800 m There is a

complicated situation early in the morning but the main problem is that by

the middle of the day there is good surface heating and the pollutants have

all been entrained and mixed down to the ground so in order to modeI what

happens on the second or third day of an episode you must be able to look

at both old pollutants as well as fresh emissions And you need to account

r for ozone that is actually transported down to the surface from layers aloft l

The next slide is a photograph (not included) which is another e xample

of some layers aloft This is due to upslope flow as explained by Jim Edinger

in his publications The mountains are heated during the day in turn heating

the air and making it buoyant there is upslope flow to a point where the

heating cannot overcome the subsidence inversion and the stuff comes right

out from the mountains and spreads out over the Basin The pollutants can

stay up there if the winds aloft are very light and on the subsequent day

will he re-entrained to the surface On the other hand if there are winds

aloft different from those in the surface mixing layer or the wind velocity

aloft is high there can be a very substantial ventilation process for the

Basin Pollutants can be ventilated up the slope and blown away in the upper

winds In the case of the entire July 25th episode winds aloft were quite

light and these upper layers remained

Figure 22 is a vertical profile of one of those upslope flow conditions

in the same location shown in the photograph but on a different day Again

207

there is a relatively high surface concentration of about 03 ppm of ozone

(Z line) a layer of clean air between 900 to 1100 m and then high concenshy

trations of ozone again above 1100 m It has gone up the slopes of the

mountains and then come back out Concentrations in the 1100 to 1300 m area

are just slightly lower than they were at 600 to 800 m area Notice however

that the condensation nuclei count (X line) is quite a bit lower mainly

because the stuff is much more aged above the 1000 m level than it is down

below 900 m

Figure 23 shows the stability of ozone the fact that it can stay around

all night long This is a vertical profile taken over Riverside about 2200

PDT 1000 oclock at night Above the surface mixing layer (600 m) there

are ozone concentrations of about 0 15 ppm (Z line) Within the surface

mixing layer (below 500 m) ozone is completely scavenged decreasing to

zero The nitrogen oxides within this surface layer are being contained and

are around 01 ppm from fresh emissions that occurred during the evening

Condensation nuclei near the surface are very high The temperature profile

is very stable You have a surface based radiation inversion which is a

little strange looking for a radiation inversion~ nevertheless it is quite

stable There is a definite restriction of the mixing--a very difficult

time getting air from below 500 m to above 500 m The ozone that exists in

the 700 m range is in air where the reactions have virtually gone to compleshy

tion and is very stable All the profiles on this night changed very little

the ozone peak stays there High concentrations stay around

Figure 24 is a cross section across theurban plume of the City of St

Louis I wanted to show that this occurrence is not limited to Los Angeles

We have seen ozone formation and transport in other urban plumes These data

l

208

were taken during a project sponsored by EPA in conjunction with R Husar of

Washington University and William Wilson of EPA The dark line on this is

the ozone concentration across the urban plume perpendicular to plume The

dashed line is the scattering coefficient The power plant plume is parallel

to the urban plume The data on the left were taken 35 kilometers down wind

about 1100 oclock in the morning The ozone concentration increases slightly

to 005 ppm in the urban plume there is a deficit of o in the power plant plume3

In the same urban plume same conditions 1500 CDT two hours later further

downwind there has been substantial increase in the ozone in the urban plume

itself The b-scat is very similar to what it was before but the ozone is

now increased quite substantially except in the power plant plume where

there is a strong deficit of ozone due to scavenging by nitrogen oxides So

the formation and transport of ozone and ozone precursors in urban plumes is

a regular occurrence that happens in more places than Los Angeles and as Bob

Neligan showed this morning it can happen over quite a bit longer distances

than we are showing here

To summarize the conclusions as they affect model development first

once ozone is formed in the absence of scavengers ozone is a very stable

compound It remains for long periods of time It can he transported for

very long distances Ozone is a regional problem which cannot be controlled

on a local basis To have effective ozone control middotone must have a regional

control strategy and probably regional type air pollution districts

A second conclusion is that the vertical distribution of pollutants can

be highly complex and models have to include more than just a simple wellshy

mixed surface layer

209

A third conclusion is that layers aloft can persist over night and can

be re-entrained within the surface mixing layer on subsequent days models

should be able to account for old pollution as well as fresh emissions Also

pollutant accumulation and transport can have distinct diurnal patterns that

are strongly dependent on the meteorology Models should be time dependent

and should start at the beginning of the accumulation period In other words

models ought to be able to run for 24 or 48 hours if they have to In this

case in Los Angeles there is often an accumulation of pollutants which starts

in one portion of the Basin at midnight and continues through the next mornshy

ing even before it starts to be transported

As far as recommendations go in many areas a lot of ambient data has

been collected and in some cases the data are actually ahead of some of the

models so I think a research program is needed in developing models that

will account for this vertical structure and the day to day carry over and

the models need to be extended to cover longer distances In addition more

smog chamber work is going to be needed in looking at the effects of carry

over and mixing old pollutants with fresh emissions How people go about

this I leave to the modelers and the smog chamber people They know more

about that than I do

I

210

I

~ INVERTER

AUDIO TAPE

MONIT0R

MONITOR OBSERVER SEAT

MON ITOR

NEPHELOMETFR FLfCTRONICS

j DIGITAL DATA LOGGER

CONDENSATION

VOR DME NEPHELOMETER TUBE

JUNCTION middoteox ASSORTED POWER

AIRBORNE

TEMPERATURE TURBULENCE

middot HUMIDITY

ALTITUDE BOX

__

middotE=-middot RECORDER ----r----------

NUCLEI KJNITOR

CONVERTER

SUPPLIES

INSTRUMENT PACKAGE (

lCO

03

Ndeg

-

-----NEPHELOMETER

BLOWER

Figure 2 Instrumentation Layout for Cessna 205

211

bullubullbullbullbull

Figure 3 Airborne Sampling Routes in the Los Angeles Basin

Figure 4 Vertie al Profile Flight Path

~-~ r~i ~~1 -- ~ ~ ~2-1~ LJ-----~ r~~ ~~ t~~--l

~ ALM l

0 RIA

ec 8v

M

~ Afo

-o

M 0

~IV

ltgt

IN J--1 N

SCALE II fi M I j_ ES 0 3 4 5 =-JSEJ--J~ _middot ~middot- - =- =

I

~

M

N~J

Figure 5 SURFACE STREAMLINE ANALYSIS - 0300 PST 25 July 1973

~~~ ~~-- cp1FJ=D -~~

~ 1

~ ~ 8c

8v

~25

PACIFIC OCEAN

diams Tt

0

9 I 4 5 10 I- m p H - -middotmiddot u 4H__8 middott_

D i6 J4 k W~D SPED llaquotl SNA NJ ~1

SCALE m ICtt84bullmh R v1s1a1L1n (mil 6 ~ CONTOURS REPRESENT

-- 10ml 16km (~() bull ~ ) ~ - 000 ft 3C5

Figure 6 S_cJRFACE WIND STREAMLINES - l 600 PDT JULY 2 S I 8 7 3

l - ~---i ~-=-___-----c---it~~-~~ r----=------1 ~-~~--cpc---_t__A --~ ---llil

~_ - ~-l-cL

34bull vi~-dff

bullbullbullbull bull ~ bull -1 bullbull - -_- L bull-J bull ~bull-bull-ii------~ bullmiddot r_ -~- ~ bullI ~_ bull bull bullbull bull I bull _ - bull -~-~ middotbullbullbull ~ ~ --middot -~- bullbullmiddot ~v ) ~ - -__rl v middotmiddot - 1- ~ -- middot middotmiddot - 1 91 frac12 - ~- lt( middot K i - middot bull - middot - bullmiddot~~-~lJ) obullmiddot~ ~-f- _J_~---Smiddot~middot-~----~~~---gt_middotfY-_middot-~middot --middot-~-~----fJ_middot- middotmiddotbullmiddot u-- bullmiddot ~ ~ -middot L~ bullbull

~bullbullbullbull bullbull l_bull bull bullbullbull EW bullbullbullbull-- ~ __bull f f - middotbull - J middot f bull S bull I ~ -r --

_ bullbull bull- _ bullbull-bull ~ ~ bull bull bull bull I bull bull bull bull bull bull gt - bull middotbulliJ -bull I bull bull _1 bullJ C-- ~-middot _ bull bullbull bullbull bull _____ ~ ~ l _ middot q bull 1 -middot middot ~~middot middot middotbull_ J ~gt - J bull-bullbullbullbull ) _ -middotmiddotbullmiddot J ~middotmiddotmiddot -bullmiddotbull fmiddot 7middot _middotmiddotmiddot bullmiddot(middot Ii~ middotmiddot~_--~middot 1middot__middotmiddotmiddotmiddot middot- gt_ -~ -~-- Imiddotbullmiddotbullbull_ -

- ()_I (w--_ bullbull__(i- bullOmiddotbull bull middotbull -bull-_jlJ middot bull lt 1(middot t gt bull - ~ rbull I bull middot middot- bull41-bull l~r v-middot~- middot middot middot bull_ - middotmiddot ~Jtj (middot~ ~middoti middot middot middot middot middot ~- ~ -tmiddot~ I - middot middot_- ~ - -~ middot_ _- ~bull - _ ~) i bull bullbull bull- middot_ bull middotbull __ ( bull 11bull bull ~ampmiddot ~ l bull bullQ bull - -1 bull JY1 bullbull ~ or bullbullbullbullbull bullbull-bullbull _ ~ - bull bull-bullbullbull middotimiddot middot 91 bull t bull - - tfaw lJ--r- bull bull _ bull middot- - l

f ~~middot--~ middotmiddott ~ltrgtmiddotmiddotJmiddot_bull - ~ - __ middot- LOS ANGELES BASIN - LOW LEVEL -__ jmiddot l-gt bull - bull J iI bullbull bull bull bull _ bullbull _ Jmiddot middotL~_1 middot middot bullbullmiddot ( C middot INVERSION MEAN WIND FLOW _ J

lmiddot - f bullbullbull~ - f 1bullbullbull _ ~)- bull middot- _---_- 7f-~bull~ REGIME _F_~ AUG_UST_~ ~600 P~--- l

-__L-~bull --ncmiddotbull~~-j--bullmiddot~bullmiddot_-bull _fJibullmiddot Imiddotmiddotmiddot-bullmiddot- bullbull ~ bullbullbullbullmiddotmiddotmiddot~middotbull ___ bullJ_ _middot~0))deg bullt t1yensmiddotmiddot ( middot middotmiddot middot middot ~ middot lbullbull1 t_c0 bull -middot---l lt ~middot~- deg bullbull --= bull bull bull I bull bull bull bull bull bull bull bull bullbull _~bull b ---) bullbull-bull ) bulll middotbull middot1middot ) bullT --f bull I bullr ~bullbullbull bullbullbull( - -bull-- ( -o-----_i bull-~-l- i l l J l~-- c middotmiddot _--1 ---I middotmiddot ---- ~bull-bull bulli_ ALT Elmiddot_ bullbullbullbull _- ~~middot bull middot bullbull _ bull middotbull bull~ ~bull middot bull -middot bull--ua_-- bullbull bull

-- 01--- middot_ -middotmiddot hmiddotmiddot __1 ~-- ~ fi~~- ___ - ____ _ -middotmiddotmiddotmiddot~ ) -~-J bull bullbull bull bull 0 uc- -l ~- ~ IT ~~ll ~ bull -middot -middotmiddotmiddotmiddotbullCCAmiddotmiddotmiddot-middot middot bullbullbullbullbull

) i- 5 ~-==-- __ __ - bullbullbull _ bull~ bullbull _ bull bull l T[h4 ------ - 0

i17- o~-lt -(i-_~ 11t~bull-omiddot ~- -- 13 0l~~~bull bull Jbullbull~bull ~ ~bullbullbull bull bull x- middot~---=-~~ -=aJlll8 bull Ibull bull ~~ middotbull rbull~---bull1-~middot-middot _ middotmiddotmiddot-middot 1 0 ~vrbullmiddot ~middot ~ (J~-middot _-_~) ) ~ bull middot

l middot _ POMA_ middot =~~~----ti~ jmiddotmiddotmiddot - middot bull [j

~A ii J0 Vfli middot bullHud __=bt_ bull

CImiddot ~-- ~- middot)middot PACIFIC OCEAN I middot ---- middotmiddot ~

__ middot__ ~ - _ 23~1 middotbull 8 4 1 middot middot ~ middot middot gt ~~- l ~ u middot

bull - bull- I ~------ --1~ i middotmiddotmiddot - n _c-118 1130

~ n r -t ~~gt25) cmiddotbullmiddot

~--lt- ~~- 1-~__( i - t ~ _ middot 0 igt(_J

11bull bull11 ~~ -~[ ~i~gt----gtmiddotmiddotmiddotmiddot--~l_ ~~ ELEVATION

IN FEET bullbull (_- middot bullbullbull -middot middotbull middot ~~ middotmiddot bulltbullbull _ffmiddotmiddot-middot v I )tylt~ -~bullbull1bullbullrbullbull ~-lt -~ ( I~

600~ A0 Cv(A (1829 m AND OVER) deg )_ rJ__~7 middot middot ~--middot L==1 _J bullbullbull - bull -middot~-- rgt ~ middot(Zmiddot- middotbullmiddot middot

Z~C)-tGOO (762 middot 1829 m) 9-N4 __J (r -- lf _ bull bullgt-~~~ ~ _ w _ _ I (1 bullmiddot( middot1 middot -----~~~- middot L-bullmiddotbullW bullbullbull3 STA r I0-4 lODEL

100i -2soo (305~762m) -- Ow - -~1_- i ~~--- bull v~rvt ~~ -middot )) ~--

II gt J (-_bullmiddot middot~ l bull bull tr 1 )~ gt ) bullbull-_bullI-middot -middot bull~0 3 Mor nuq1ENr Wlbull~O JIAtCTIO-bull bull - lbull C---gt bullbull )t bullbull -( I bullf I - 20-00 (61 bull 305 ml J( Jloa xxE- -bullbull00 - -- middot1

0-200 (0middot61m) Wl)7 AVBt~gpound ) bullmiddot-iiNL~ middotntmiddot_ 1 iJJlt( _1J- ~ VAq IA9 IL ITY 0 ~ 10 15 ltS lHPtl

~--_ bull bull I bullbullbullbull 1 ~) J)J ~ bull Is bullmiddot bullbullbullbullbull ~ 3 V IS A VAqlABLE OIR~CTIO- 0 8 16 2-4 km

(SPEEDS SHOWN IN mph 10 mphbull 16 h1llr) -- middot ktr~~~ lt~ ) -middot-SCALE

Figure 7 LOS ANGELES BASIN MEAN WIND FLOW FOR DAYS WITH LOW LEVEL INVERSIONS DURING AUGUST I 970 AT 1600 PDT

-~~~~-=======~middot~-~======~middot--=-==-===gt=---==____________=== ~--=-J~==-- -=-ee----=-------

500

N f-- V

- - - SUBSIDENCE INVERSION

----MARINE INVERSION

bullbull-bull-bullbullGROUND LEVEL

x WINOS ALOFT (kmht)

WESTERN middoteASIN EASTERN BASIN

LAX WINOS EMT IHOS I I

CNO WIHOS

s_ 04 13 1500- 05 02 08

I 06 069 middot

11-1--

04 04 i ~4

06 ~ 4--

I 2

1000 n1 1005 -_E

lll --1 lJ -----------~----

~11

--=i-+- c -- 9 _____ - ~ C

lt I

I 6 4 _r 31

I 6 5 ~~ ~_ bull ---middot- 64 ~li- - middot- bullc - middot-----------

10

SMO (1347 PDT)

EMT (1246 PDT)

BRA CAB (1459 PDT) (1335 PDT

RIA (1349 PDT)

RED (1406PDT)

Figure 8 VERTICAL CROSS-SECTION OF bscat FOR lvflDDAY

T t 10-4 -1)(l n1 s are m

JULY 25 1973

- c - -~

~--~ JC_-_1- ~1pi~ oamp----~JilliiiM~f~-U~ -~--- --~~~ ~~~

-=--~

-E-- O

_ lt

1500 05

06 15

09 __~

1000 --

~- ~---middotmiddot 29

500

oJ11

__a

07

I 07 I

I I

I

09

I

I

I

I 7 ---

11 -----

~ ----- 6

---------------lt- -~middot4 --------

20

29

-

10 10

11 07 08 08

10

08

~8 _____ Y-

N

- - bull SUBSIDENCE INVERSION

----MARINE INVERSION

-bull-bull-bull GROUND LEVEL

WES TERN BASIN EASTERN BASIN x WINOS ALOFT (kmhr)

t t

CNO WINOSILA WllltOS poundMT WINOS

SMO LA EMT BRA CAB RIA RED O (1736 PDT) (1655 PDT) (1707 PDT) (163 PDT) (1823PDT) 1805 PDT)

Figure 9 VERTICAL CROSS-SECTION OF b FOR AFTERlOON OF JULY 25 1973 scat

T bull 1o- 4 - l )(units are m

__~~---iii~~- ~- ~~______ ~~- --~~J---=-~ ~

N ~ -J

PACIFiC OCEAN

0 5 10 15 1111

E 8 4 I 0 8 6 2 ~ bull

SCALE

dh Mes

CONTOURS REPRESENT - 000 ft 305 m

0 SNA

c8s

ec 8v

amp R~b

Figure 10 TRAJECTORY ENVELOPE FOR AIR ARRI1G AT CABLE AIRPORT (CPLAD) 1600 PDT JULY 25 1973

~-~

q_- ~ ------1 H~~~ -~~--~ ___---___--i- __r-=-1--===12---1 ~ ___r~ _==---_ - ~- f~~ ~-- - -5plusmn-at -~middot~

ll~~r1 ri

40

ec 8v

-1 I

amp

0 HQ_

7 0

CAP LAAR) O

VER

PACIFIC OCEAN ~ 0

RLA

4

WHqR d

diams

H ~I

I l

0 COMA

3

L~

LAH

Fa_ f ~~

S ~ LA APCD VALUES ADJUSTED TO AGREE ~

lt

0

5 10 15 mi0 WITH ARB CALIBRATIONE-j I I CONTOURS REPRESENT NZJ ~ 0 a SCALE 6 24 km - 1000 ft 305m COS v~J

______ J 10 ro ( igtf t-i

coFigure 11 SURFACE OZONE CONCENTRATIONS (pphm) I 600- I 700 PDT JULY 25 1973 ~

~~~~~C-~ ------=--~-__-~--~~~=--- ----=--~

N

-E

D1600----------------------------- 1--

14001-------------------------------

1200

I Ground Elevation

1000 middot 445 m ] lampJ

sect ~~ 7 ) SURFACE i6~ 800 MIXED LAYER

~

~ [ J ~ ~ I OZONE CONCENTRATIONS~ 600 E E GREATER THAN

( 50 pohm

400 I C H T Z GROUND LEVEL

200

I PUUloCETER UNIT SnbullBOL

NOc N0 0 ppm01 02 03 04 05 03 z

40 --~45~~ 50 co pm C0 5 10 15 20 25 30 35 I I I I I I I I I I TEIIPERATURE oc T-5 b 5 10 15 20 25 30 35 40 45

I-- 100 RELATIVE HUlillOITY H0 10 20 30 40 50 60 70 60 90 b1eot IOmiddotm- 1 8

CN cmmiddot3 1 IO X0 I 2 3 4 ~ 6 7 8 9 10 URBJLENC-C cm213ue- E

Figure 12 VERTICAL PROFILE OVER CABLE (CAB) J CLY 2 5 l C)7 3 l 63 6 PDT

~ _~ ~--- -

--

1400 I bull bull

1200

1000-5 LampJ 0 ~ I- 800 ~ c(

sooLl

-1-=-1-~--t j --=~c-o-----i-bull 1-~~~ ilt~~ -~-1 lta-abull--~ -c-~---=---r F--- ---- I n_--middot- =~~ ai~IHJ

(~-It

1600 ___________________________________

C r 11 s Ground Elevation t~C E H I~lcc

- ~ 1 90 m

4001 bullc C H

C UNDrnCUTTNG svC ~ Ic- H

SEA BREEZEC II 200

C C

[C -PARAMETER ---UNIT SYMBOL

NOx N0 0 ppm01 02 03 04 05 03 z co ppm C0 5 10 15 20 25 30 35 40 45 50

-5 middot- -~20~----25 TEMPERATURE oc T0 5 10 15 30 35 40 45

100 RELATIVE HUIOITY H0 JO 20 30 40 50 60 70 80 90 bcot 10-4m-1 8

CN crrr3 10 0 I 2 3 4 5 6 7 8 9 10 X TURBULENCE cmZ-13 sec-1 E

N N

_-----=-G--~---

Figure 13 VER TICAL PROFILE AT EL MONTE (EMT) JULY 25 1971 1656 PDT SHOWING UNDERCUTTING BY THE SEA BREEZE

0

middot~_lt ~middotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotbullbull

-~

LACA

0 - )

i r=

-v2v

~

_middot~middot)( I bullbull

bullJ

K~Ji~middot

~~ 61iAS 0

EMT J~J---6~-11 ~orr

PACIFIC OCEAN

WEST 0

SMC

0RLA

14

L~8

R~A

~BL

16 ~ ~

0 5s Pcfrac14A c1i ~ )

wFJfo~J_) ltI~~~

_ff-Clf1ito J )

HILL~

~J U

~ _~~~

~

I o middot

1 1$ ~ 11yen ~middot ~I N

I

N I- I

t

0 --pomiddotmiddot bullmiddot i- 1LO middot Joomiddotmiddotmiddot -- middot middotmiddot -middotmiddot

_middotmiddot 0 middot middotbull MWS r

L4 ( 1 T bull bull __-- -A bullbullbullbull middot

0 i __ bullbull

17 t-J~ N7 a S I ~r ~ 1 rtd ~lt A-~ v- middot ~ - cXa 0

RIA 19

CLO

ltJ~

bull ~ 0

(

--

1

_ _

-2Wl

~s~o -- _)~J0JgtJ~ ___ Q

15 l1JI

0 15 r(A0

CAP

CLARR)~R 1900 1-shyPDT

II (_-L~X L2X I 0~ R[V

0 CCtwA

I

I18=00 POT~ l4 r1

fj

-11J - ----- 11=oomiddotmiddotpor

l~i middotmiddot- o

i

5 10 5 Tl o~1 middot--middotmiddotmiddot middotmiddot

_q it==i--__F-3 9 I I CONTOURS REPRESENT SNA NZJ ~1 o

_- I 0 8 16 24 km I - 1000 ft 305 m middot ~

7 14~CALE --- 2500 ft o2m V lr1 ) middot I i0 _ il o5

16QQ pol(middot v( ____________ _L

I i

Figure 14 APPROXIMATE TIME (PDT) OF ARRIVAL OF SEA BREEZE Jl-LY 25 1973 (Ogt_iective criterion based on ground level ozone concentrations)

~ -___~==~ ~~ - ~ =-~ f7r=~1 _j~-~ --c_~~

u-middot - middot middotmiddotmiddotmiddotmiddot

~- middotmiddot~ ~1 WESTERN BASIN r Joa_middotmiddotmiddotmiddot_ NOxEMISSION RATE ~- 95 METRIC TONShr

-----bull_ ~ ~middot~ I -OUR -----middot )omiddotmiddotmiddot - middot~ l21 (fTI

~ AT middot ~ middotbullmiddot- ~- ~ middot 4bull-middot

I EASTERN BASIN NOx EMISSION RATE 10 METRIC TONS hr

ri r bullbull

t10 Joa

) __ 8v -a_ -- -bull-I O ~AGA -_ ~S ___ _ middotmiddotmiddot -

~ ~v ai- omiddot-middot~-- - ) r -middotmiddotmiddot f middot( ---~ -l A ~ _ (- bull ___

it~ ~~~ middot-middot -- ~-~ ~~~ 0 0 AZU~

AVERAGE CONCEN7RCTi)N iN BOX (IF STEADY STATE)

IS 25 pphm

1 r f--Ji 7 ~Sv PAS ou )V~(~- ~ t i -~ Li_) 03 FLUX THROUGH f~

~ ~JI_~ - amp_ JiM O SHADED BOUNOA~middot~-~ ~~-s-- EMT 185 t 60 METRI~ bull ~ ~ TONShr 0 (m)

c~~~ 1t~CS A~JFP

1000 _29

-i32

_~o tUA

_

1

O~ ~

0 -__rJ( (r- J PACIFIC OCEAN LAX _ C-middotJbull _

l o M R No _

550m

r

A frac14

HAR O HJ LAH

_ o camptA REDLANDS 18QO POT ~ r

I bull ~

RB MEAN TRAJECT~~~y

0

TOA L~S

0 AN

I - ~ 8 OUNOARY ~ ~middotltdeg ~ ~ BETWEEN middot __ WES~ERN ANO- middot middot - ~

I gt I lt bullmiddot bull (EASTERN ~ i middotmiddot middot - - ~

S ~ ~~ ~ - middot-

rt1~1_--t------l

middot1-- BASIN ~-~

1-)~~--middot ~ ~l

~~ ~-bull bull J --

-is-eo -_

0 5 10

j=i r-i C

0 8 ltl

SCALE

5 mi

2~ un

CONTOURS REPRESENT - 1000 ft 3gt5 m

--middotmiddot 2500 ft 1 762 m

~

0SNA

cos 0

_ --~ ----- --- ( bullmiddotmiddotgt

- middotlt- ltgtmiddot t__ Q ~

1 1 rmiddot bullbullbullbullmiddot ~9

NZJ ~ middotmiddot - middot- Alr ---middotmiddot- middot middot( middotmiddotmiddotmiddotv ~ bullbullbullw bullbullbull bullmiddot 1 bullbullr~ ~-- -middot ~--v ~- - I -~

ESTIMATED OZONE FLUX FROM VESTER~ TO EASTER-J BASIN JULY 25 1973 I 700 PDT

C ~IV

N N N

I

l ~

-~~

I

iI

i I

I t

t

~ ---~ --

Figure 15

~Qa llfJD fl(~middot ~ 11f ~I I

l

Lfb ec~s0 CPK v2v 0

ALT 8v Ld~_----1

I

HO-

0 CA

middotLARRv O VE~

1330

ol(Di

A~U

0ENT

~lt

s~e ~ 1530

F8f 1730

~

rbull-~

oc (WljT) -_-~(~~c lt-rw---_

~~ ~-_i~cB~~~

2-~) - ~ ~ l~w-~~ p~- pound)_

0 ojI middot tl-1CfUp I ~ ) 1 ~ J~I i bull middotbull middot~-Li 1)- ) I

DiI ~- 0

i ) 0 l I I

t

A RALc~o JI

C

-~

0 r-iR

~IV 1230 1~

RE PO ~- I - Ftl

) 0 ---~gt- __L8s ~Zi diams ( T~ _middot_ ~~ ~

I AN ~~-~ j t bi 0

~ I

~ I L i

-_gt ji o 5 c 5 Tl middot 0 0 ~-i p__i=r 2=f I_ I 1 NZJSNA 1

1 8 2 4 km )

SCALE I 00 J_(1 CONTOURS REPRESENT cos f

1 0 I --- I - ))) 35

PACIFIC OCEAN

Figure 16 TRAJECTORY E~VELOPE FOR AIR ARRI1gtJG OVER REDL_)DS AT 1800 PDT JULY 23 l =i73

224

JULY 25 1973

LA DOWNTOWN

0sect040 a

~

~ 020 0 X z0 ~ LJ 0 ~ z

~5 040 330POMONA 0 ~ en~ 020 w z _J

w w 0 (9 z O----u-~~-__~_-~~~-------L-~-0--0-0~----- z

ltt~ 040 56 (I)z

0 0o _ RIVERSIDE _J0 20 t6 ~

0~ Qt---0-0--ltrO-ltgt-C~------~~~~ a

LL ~

Rate ~ IO mph___ (I) w

_J~ ~ ~

et~ lt(

3 040 PALM SPRINGS ~

j 020 ~

0------____-----L--___---------L---~--~

105

12 4 8 12 4 8 12 l~-s----am _ pm----1

HOUR OF DAY PST

Figure 17 Diurnal variation July 25 1973 of oxidant concentrations at air monitoring stations at Los Angeles Downtown Pomona Riverside and Palm Springs California Values are corrected data Los Angeles Downtown and Pomona x 11 and Riverside and Palm Springs X 08

CONO S t 1 fRESEIS7

~

~~ 0

ciffmiddotdK ~ ~v~~o

( ~s ~

bull ~r ~ bull 1--~~----Soootl ~ ~ ~ ~ lj i1 d t CJ ~ ampfrsmiddotflt- frac12 ~ middotL~Js _-- ~

_gtgt middot~ ~rroltf~-) ~ 0 s- r

middot-middot- r_~ ~~JtbO ~~bull~Jt ~~~ L r - bull _ ~ I= J 1 ~ ~ ~-~~bullJC ___ -_ middot ~ laquo -poundJ~ ~- middot1~ r-- - V--_1_ ~ I 1 S I

V ~ bullf-uv~ fi -~zumiddot -~middot~ LS gt -tmiddot-F Q~ ~-tv I_~ --- ONT p(_ s ~S ~~~-[ ( 0 c-_ --~ ~~~___d_) lt- ~ I -i-C - -

~----1-1 bull~~POMA ~V BN ) middot-~ f -- s - ~

~VA -middot- ~p AAL a 2~~ ~~middot01 r r ~ middot middot 0-- V

i LAX bull1

~ -~poundJ-i- ltllll _(__1-0~ ~t- degQ-0- ~~ _ _-__~~-qlK ( a_ II ~ ~p-~ ~J

N bull - - 0 r o_ _I ~ -~ ~middot ~ ~amp ~--= ~ ) s ~

- -~- - middotO _a - Tl --0- ov I lHOIO J I bull J -- ~ 6 ~ -__ 2 ~

(__ ~~ _- ~-~ middot8---fl~ -- ~ bull~-abullbull _~ ~-cgt ~ bull bull middot e bull bull l ~ 0

I 1A_ HZJ middoto~J

middot0 (~ ~ S TAA

- ~ - - - --0 () _-j J middotO=c==c-c==cc~~~ l ~~ ~ ~ bull-~---~ ~ bullbull -~ al1 ~ bull __ ~--middotmiddotmiddot

diams Skyforest _ Strawberry Mt Lookout

Figure 18 STRE ~[Ll)ES FOR 1600 PDT on 8 1673

~ ~--

vO 0

N N V1

au

91 V7

-1 ~ -=1 ~~ ~~~~l r=--~d- ---1 _J-_

~E1 ~L1-~f~

3100 ---------------------------------

2900r-----------------------------

T

e w 0

~ 5 Cl Ground Elevation

1560 m

T PARAMETER UNIT SnbullBOL

NOx N 01 02 03 04 05 03

ppm z co ppm C

10 15 20 25 30 35 40 --

45 50

170

I I I z

0 5

-5 - -0~ 5 10 15 20 25 30 35 40 45 TEMPERATURE oc T

0

0

10

I

20

2

30

3

40

4

50

5

60

6

70

7

80

8

90

9

100

o

RELATIVE HUMIDITY

bcot CN

TUR8ULENC~

110-4m-

cm-3 tobull 213 1 cm sec-

H

8 X E N

N OI

Figure 19 VER TI CAL PROFILE OVER ARROWHEAD u-RR_l A CG CST I 6 1973 939 PDT

3100----------------------------------

N2900r----------------------------- -i

N

2700i-------------------------------

2500

e 0 uJ 2300 gt ~ ct

2100

1900i---------------------+--------------

~le 1iation 1360 m) 17001 ~

- -PARA1jETER UNIT SYMBOL

T NOx N1500 o ppm01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50

TEWERATJRE oc T-5 middot --~o--- 5 10 15 20 25 30 35 40 45

IOO RELATIVE HUWIOIT Y H0 10 20 30 40 50 60 70 80 90 bcat 10-~- 1 8

CN cm- 3 104 X0 I 2 3 4 5 6 7 8 9 10 213 1 tURBliiENCE cm sec- E

Figure 20 VERTICAL PROFILE OVER ARROWHEA D -RR 1 --- -AUGlJST 16 I) 16--1S PDT

1-~i w--~i_f l-=--bullC- ---~-4

1600 bull t c- N 8 ff Tbull C[ 8 H 1 bull H z H T ~ C f N 1 H T bull C rn 1 C NE bull-~z Hi400 bull bull tf T bull N ~r --middot _P H -ybull EC N z__e H T i 8 z H Tbull C E HD Z H T POLLUTANTS REMAINING FROM bullt C Hbull L T PREVIOUS DAY1200 Et HO I II -middot-- bull Ct H 9 - H T

___ Hbull( E N 1 a tC N i--_ -1 H

C N Tbull Z HP poundIC C H z_ 1111 1

- bull C H Z l _H_ _J1000 )( cc H -z emiddot ksect bull C N ~ T

)( iz H 8 H TIAI -t XC z 7-- T0 bull pound N t H_8

t-gt

YCpound N 1800 l I-gtltbull - H (Jet

N i -r~Bltt t bull gt- t C X N H T

[ BUOYANT POINT SOURCE PLUMEH 1

N ~z-- -

C H

-bull SUPERIMPOSED ON POLLUTANTSC JZ X H T 600 -~ E c REMAINING FROM PREVIOUS OtY Cl JC t H H f bull cmiddot t HT -fl

C- X t fl _ REMNANT OF NOCTURNAL RADIATION INVERSION(I-----e-C f N K I T H

C Z [ T H x-8 400 _Zc r -H -K SURFACE MIXING LAYERz C II H K 8

C N T pound H M 8 _ I -t ff H E N -9 l

Ground Elevation 305 rn200

PARAMETER UNIT SYMBOL

_ I - I I I NOx N00 ppm01 02 03 04 05 03 z

co ppm C 0 5 IO 15 20 25 30 35 40 45 50

L middot1 TEMPERATURE oc T-5 0 5 IO 15 20 25 30 35 40 45

100 RELATIVE HUPAIDIT y H0 10 20 30 40 50 60 70 80 90 bscot o-4m- 1 B

CN cm-3 x 104 X0 2 3 4 5 6 7 8 9 10 TURBULENC~ cm213sec-1 E N

N co

Figure 21 VERTICAL PROFILE OVER BRACKETT (BRA) JULY 26 1973 0825 PDT SHOWING BUOYANT PLUME AND UNDERCUTTING BY RADIATION INVERSION

N N 01600

___bull C M C

C

1400~~~ t C [ middot H LAYER CAUSED BY

C C H C [ H UPSLOPE FLOWl

1200

1000 ] w

SURFACE MIXING LAYER 0 --= ~ -~~ 6 800~ er

C C

600t-i C C t C

I ~00

Ground Elevation 436 m 2001-------------------------------

PAIUWETU UNIT SYWBOL

NOx N ppm0 0 01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50 I I I I I I I I TEWPERAT1JftE degC T-o b 5 10 15 20 25 30 35 40 45

100 ~EIATIVE HUWIOITY H0 10 20 30 40 50 60 70 80 90 b1tt1 10-m- 8

CN enr3 110 X0 2 3 4 5 6 7 8 9 10 Tu RUL Erct cm23sec- E

Figt1re 22 VERTICAl PROFILE AT RIALTO (RIA) JlJL Y 19 1973 1738 PDT SHOWI=JG LAYER CAUSED BY UPSLOPE FLOW

~~-7 ~ ~- 1 ~iri ~~- ~~-~ ~t ~~ ~ =~middot-1

1200 I t 1 If J-

1000

I C ltTl a_ ~l- t

800

600

L gE __r H

H

400 j (~ c pound N C E I~

t EH -

1-1 M

H H

H M H H

H

H H

11 bull H M H

M H If

H H

H

- C t H ~ C poundmiddot H

I C E I(

200

1600--------------------------- t

T t t T l

l T t

T t_

t 1

l] w ) g f

Tt t

ltt ~ T

t J t T

t J

f 1

t

Klt

H M Cro1nd Elevation 250 m HT X

5Yl80LPAllAlETER ~

NOx N0 0 ppm01 02 03 04 05 03 z

co ppm C0 5 10 io 20 25 30 35 40 45 50

25~--- ---35~~-40 TEMPERATU~E oc T-5 0 5 lO 15 20 30 45

100 RELATIVE HUMIDITY H0 iO 20 30 40 50 60 70 80 90 bact 10--ltllm-1 B

CN cmmiddot3 11 04 X0 I 2 3 4 5 6 7 8 9 10 IURBULENCE cm2hioC-1 E

Figure 23 VERTICAL PROFILE OVER RIVERSIDE (RAL) N

JULY 26 1973 2239 PDT I)

middot==-=-=

0

bull

N w 1--

ii -s~~ l-obull

CJ ~

obull -obull obull

5 02~

bscat

Oa

4l o2J

-I 3 e I 0

--)(

~

Abullu 2

ll

ol

Traverse at 750 m msl 35 km Downwind (SW) of Arch - St Louis Mo 1117 - 1137 CDT

( Power Plant Plume -01 Ibull-[ ~ e

11 bull E I -)(I

I0bull I 1r~ l -

0

I I Io 1 u I

I r- l A bull I i I 1I

H1I I 4 t I II I I

11 I I

I I r I I I

I I qo 01 I I

I I bullJ~viI I middot ~

I

I I

~

Urban Plume

ood 0 10 20 30 40 50

kilometers

o~

02

01

s 1

P

0bull 01

00S~J1 I ti middotmiddot1 middotvmiddotmiddot~ J

Urban Plume

I y

oo 0 10 20 30 40 so

kilometers

Traverse at 750 m msl 46 km Downwind (SVV) of Arch - St Louis Mo 153 0 - J 549 CDT

---- bscat

o-

Power Plant Plume

1l~ 11I 1 t

ill~t fl Ibull I ii

I

lmiddotmiddotrI

I I I I t II

l vrI V

JV-f Jl bull

bull t I bull I

Figure 24

l

232 RELATIVE CONTRIBUTIONS OF STATIONARY ANDMOilILE

SOURCES TO OXIDANT FORMATION IN LOS ANGELES COUN1Y IMPLICATIONS FOR CONTROL STRATEGIES

by Robert G Lunche Air Pollution Control Officer

Los Angeles County Air Pollution Control District Los Angeles California

Introduction

The type of air pollution problem characteristic of the west coast of the

United States and particularly of Southern California has come to be known

as photochemical smog because it is the result of sunlight-energized atmospheric

reations involving oxides of nitrogen and reactive hydrocarbons Its manifesta-

tions- -eye irritation reduced visibility damage to vegetation and accumula-

tion of abnormally high concentrations of ozone or oxidant - -are by now well

known In fact the occurrence of high levels of oxidant which consists almost

entirely of ozone has become the primary indicator for the presence and relative

severity of photochemical smog

During the 25 years since photochemical smog in Los Angeles County was

first identified an extensive program has been underway for control of the responshy

sible contaminant emissions Initially during the 1950 s these programs concenshy

trated on controlling emissions of hydrocarbons from the stationary sources of this

contaminant In the early 60 s programs for the control of hydrocarbon emissions

from motor vehicles in California were begun An exhaust emission control proshy

gram for hydrocarbons and carbon monoxide from new vehicles was begun in 1966

C011trol of oxides of nitrogen emissions from motor vehicles began in 1971

As a result of the overall control program by 1974 emissions of reactive

hydrocarbons from stationary sources have been reduced 70fo from uncontrolled

levels and about the same percentage from mobile sources Oxides of nitrcgen emissions

233

from statjonary sources have been reduced about 53 while emissions from moshy

bile sources are still about 7 above uncontrolled levels due to the increase

in NOx from 1966-1970 models Additional controls already planned for the future

will by 1980 achieve reductions of reactive hydrocarbons from stationary sources

of about 87 from uncontrolled levels and from mobile sources about 93 By

1980 emissions of oxides of nitrogen from stationary sources will have been reshy

duced 53 and from mobile sources 63 from uncontrolled levels The past

present and projected emissions of these contaminants are shown in Figure 1

A I though compliance with the air quality standards has not yet been achieved-shy

and is not likely before 1980- -the results of these programs have been reflected rather

predictably in changes in certain of the manifestations of photochemical smog For

example eye irritation is less frequent and less severe and in some areas js

rarely felt at all any more and damage to vegetation has been markedly reduced

Ozone (or oxidant) concentrations have been decreasing in Southern California

coastal areas since _1964 in areas 10-15 miles from the coast since 1966 and in

inland areas 40-60 miles from the coast since 1970 or 1971 as shown on Figures

2 arrl 3- All of these positive effects have occurred despite the continuing growth

of the area indicating that themiddot control programs are gradually achieving their purpos

a return to clean air

This improvement is al~o refutation of the so-called Big Box -concept which

assumes that the total daily emissions in a given area are somehow uniformly disshy

tributed throughout that area--regardless of its size or of known facts about the

meteorology of the area or the spatial and temporal distribution of its emissions- -

234

and of control strategies based on that concept And since the improvement in

air quality refutes the control strategies based on reductions in total emissions

it thus confirms the value of more recent control strategies which emphasize conshy

trol of motor vehicle emissions and use of a source-effect area concept

Following is a brief listing of the evidence we intend to present as supporting

our views on just what control strategy is appropriate

Examination of relative contributions of HC and NOx from stationarybull and mobile sources demonstrates that motor vehicles are the overwhelming

f source of both contaminants~

I bull Observation of air monitoring data shows that the effects of photochem -

ical smog are not uniformly distributed t_hroughout the county

bull Study of the meteorology of LA County shows consistent paths of trans -

port for various air parcels and consistent relationships between the

areas most seriously affected by photochemical smog and high oxidant

concentrations and certain other areas

bull The upwind areas are found to be source areas--the downwind areas-shy

effect areas

bull Central L A is found to be the predominant source area for the effectI area in which the highest oxidant levels in the SCAB consistently occur

bull The predominant source of emissions in this source area is found to

be motor vehicles

bull Central LA has the highest traffic density I

ij bull Both pr~mary and secondary contaminant concentrations reflect the effects

of the new motor vehicle control program in a predictable fashion 11 I

A strategy based upon these findings is gradually being verified by atmosshybull pheric oxidant data~

235

The Evidence that Motor Vehicle Emissions Are the Principal Source of Oxidant

As seen from Figure 1 at the present time the total daily emissions of I-IC

and_ NOx from all sources in Los Angeles middotcounty are primarily due to the motor

vehicle The problem now is to find the spatial and temporal representation of

emissions which when examined in the light of the known meteorology and geogra -

phy of the Los Angeles region best describes the source of emissions responsible

for the highest observed oxidant readings

In the rollback models used by EPA and others the basin is treated as a

big box with uniformly distributed emissions and peak oxidant is considered to

be proportional to total basinwide hydrocarbon emissions

The fact is that the middotemitted contaminants from which the smog is formed

and the effects which characterize that smog are not evenly distributed throughout

the Los Angeles Basin in other words the basin area under the inversion is not one

large box filled to all corners with homogeneously distributed air contaminants and

photochemical smog

Refutation of Big Box Myth

Examination of atmospheric contaminant concentrations refutes the big box

concept It is found for example that concentrations of djrectly emitted contam -

inants measured at a particular sampling site reflect the emissions within a rather

limited area around that site For this reason contaminant concentration levels

vary from one location to another and each has a characteristic daily pattern which

reflects the daily pattern of emissions in that area

middot 236

The big box concept is further refuted by the fact that peak concentrations

of carbon monoxide and oxides of nitrogen in areas of high traffic density were

fairly static prior to 1966 Thus they did not reflect the 45-50 per cent growth

in motor vehicle registrations and gasoline consumption which occurred in Los

Angeles County between 1955 and 1965 and which caused comparable increases in

total daily emissions of such vehicle-related contaminants This demonstrates

that growth was outward rather than upward so that a larger area of the County

began to be affected by photochemical smog but no area experienced smog ofJ

greater severity than that originally affected by smog formed from the vehicular

emissions which accumulated each weekday in central Los Angeles and were trans-

1 I

ported later that day to the San Gabriel Valley

1 Meteorological Evidence

To verify the geographical dependence of emissions and resulting atmospheric

concentrations let us examine the meteorology of these large areas of Southern

California Both the County and the Basin have many meteorological sub-regions

in which the patterns of wind speed and direction may be similar but within

which the patterns of air transport are parallel with those of adjacent sub-regions

and the respective air parcels do not ever meet or join

The characteristic patterns of inversion height and wind speed and direction

in these sub-regions and their patterns of vehicular emissions together have

created a network of source areas- -those in which the reactant contaminants accu -1T

i ~ mulate in the morning and begin to react--and related receptor areas--those to which

~ the products and associated effects of the photochemical reactions of the contamshy)

inants originally emitted in the source areas are carried by the late morning and

237 middot

afternoon winds ( sea breeze)

Wind-flow patterns show that characteristic patterns of transport for related

source area-effect area combinations are separate and parallel not mixing or

joining Each source area has its own reactor pipeline to its own effect area

or areas

To illustrate this source area-effect area relationship the typical flow of

polluted air from downtown Los Angeles to Pasadena was selected as a worst

case situation for in-depth examination Figure 4 shows that the air in downtown

Los Angeles on the morning of smoggy days moves directly from the central area

to Pasadena

Vehicular traffic is the predominant emission source in both downtown Los

Angeles and Pasadena Thus the air in each locality should contain CO Also

since oxidant would form in the air parcel moving from Los Angeles to Pasadena

oxidant levels would be expected to be higher in Pasadena than in downtown Los

Angeles

Figure 5 shows these relationships for the period 1960-1972 The atmosshy

pheric CO level is similar for the two areas while oxidant levels were higher in

Pasadena than in Los Angeles throughout this time period This demonstrates

that a significant amount of oxidant formed in the air as it moved to Pasadena

containing both the unreactive CO and the photochemical reactants for producing

oxidant Both CO and oxidant show a marked downward trend in each locality since

1965 which emphasizes the effect of vehicle exhaust controls and the correlation

between the localities

238

On a day which is favorable to the formation and accumulation of photoshy

chemical smog a contaminated air parcel normally originates during the

6-9 a m period on a weekday from an area of dense traffic centered just

south and west of Downtown Los Angeles It is oxidant generated within that air

parcel which usually affects Central Los Angeles and the West San Gabriel

middotK IJ l J

Valley area around Pasadena

The traffic area in which this smog had its origin is about the most dense

in Los Angeles County and has been so for the past 25-30 years No area

has a higher effective density thampn-this Using carbon monoxide which

1

is almost entirely attributable to motor vehicles as an indicator of such emis-

sions it is found that the concentrations of emitted vehicular contaminants

middotr i

measured in Central Los Angeles during the past 15 years confirms both this lack

of change in effective density and the absence of any area of any greater effective

density when local differences in inversion are acknowledged

This area the Central Source Area is depicted in Figure 4 The size

and shape of the Central Source Area was ch~sen to be large enough to reduce to

an insignificant level any diffusion or transport into this area from any externally

l generated reactants This conclusion is based in part on the trajectory studies

previously referenced as well as an analysis of the diffusion and transport parashy

meters for the area

239

The Central Source Area has been identified as that geographical region

which contributes essentially all of the primary contaminant emissions giving

rise to the highatmospheric oxidant levels in the West San Gabriel Valley

The proportion of emissions in the CSA due to motor vehicles and that due to

stationary sources is shown in Table 1 For the County as a whole about 80 per

cent of _(6-9) AM reactive hydrocarbons are due to motor vehicle emissions and this

figure rises to 90 per cent for the CSA The same conclusion a pp lies to NOx

emissions The Central Source Area contains the greatest density of vehicle traffic

in the County and thus the greatest density of source emissions Thus it appears

that the source area with the highest density of emissions during the critical (6-9)

AM period is responsible for the highest afternoon oxidant levels observed in Los

A i1geles County and in the South Coast Air Basin These highest oxidant levels

are consistently observed to occur in the San Gabriel Valley This is true whether

the LAAPCD or the ARB oxidant calibration procedure is used

Further the atmospheric concentrations of the primary pollutants can be

identified as originating primarily from the motor vehicle and they reflect the

effects of the motor vehicle emission control program A vehtcular source area

can be identified by its atmospheric levels of CO and NOx Figure 6 compares

measured atmospheric levels with calculated atmospheric levels for CO NOx

and the CONOx ratio in the downtown area

TABLE 1 240

REACTIVE HYDROCARBON EMISSIONS

(6-9) AM

1970

LOS ANGELES COUN1Y middot CENTRAL SOURCE AREA middot SOURCE TONS PER CENT TONS PER CENT

Mobile 1260 81 3 135 91 2

Stationary 290 187 1 3 88

Total 1s~o 1000 148 1000

By 7 -Mode Gallonage

241

The calculated values shown in Figure 6 were derived from a baseline

survey of 1100 vehicles and continued surveillance tests both using the Calishy

fornia 7-Mode test cycle The baseline survey showed that motor vehicles withshy

out exhaust control systems had average exhaust emissions concentrations of 3 4

per cent CO and 1000 parts per million of NOx Baseline emissions data apply

to 1965 and earlier model vehicleg and surveillance data to 1966 and later modelsmiddot

Since it can be concluded from calculations and observations that the dilushy

tion of auto exhaust emissions in the atmosphere on a smoggy day in Los Angeles

is approximately 1000 to 1 the calculated values for CO and NOx prior to 1965 are

34 ppm CO and 1 ppm NOxo After 1965 the changing effect of controlled vehicles

in the total vehicle population is reflected in the calculated values

CO and NOx values measured in the atmosphere are also shown in Figure

6 and confirm the values calculated entirely as diluted vehicular emissions NOx

concentrations measured in the atmosphere tend to be consistently a little lower

than the calculated values probably because photochemical reactions remove some

NOx from the system

The data for CO and NOx calculated and measured show that emissions in

downtown Los Angeles originate almost exclusively from motor vehicles and that

atmospheric concentrations there reflect the average emissions from a representashy

tive vehicle population

The ARB has recently published a report entitled A Trend Study of Two

Indicator Hydrocarbons in the South Coast Air Basin Acetylene was used as a

242

specific indicator of automobile exhaust emissions and it was found to have de-

clined in concentration in the Los Angeles atmosphere at an annual rate of 12 5

per cent since 1970 To quote from this report The California implementation

plan requires an annual average reduction in these emissions (reactive organic

compounds) of 166 tons per day or 11 1 of the 1970 tonnage per year The per cent

reductions in the_ acetylene levels at Los Angeles and Azusa are greater than reshy

quired by the implementation plan Since acetylene is almost entirely associated

J with auto exhaust this demonstrates that the motor vehicle emission control

program is achieving its purpose

To summarize at this point it has been deomonstrated that high oxidant values

are due to motor vehicular emissions of NOx and HC because

NOx and HC are the principal reactants in the oxidant formation process

and they originate primarily from motor vehicle emissions and

The highest oxidant values are recorded in_ effect areas that receive air

from source areas where motor vehicles are clearly identified as the

dominant source of NOx and HC

243

Future Control Strategy

The APCD strategy for achieving and maintaining the oxidant air quality

standard is based upon the fact that high oxidant values are due to motor ve-

hicle emissions of hydrocarlxms arrl nitrogen oxides This strategy is as follows

1 Both Hydrocarbon and Nitrogen Oxides Emissions Must Be Considered To Achieve the Federal Oxidant Standard

There is wide agreement that NOx and HC are the principal reactants in

the oxidant formation process and that vehicular emissions are a major source

of NOx HC and CO

2 Effective Regulation of Atmospheric Concentrations of Both HC and NOx and of the Ratio Between Them is necessary for Attainment of the Federal Air Quality Standard for Oxidant

Basmiddoted on the abundance middotof available experimental evidence it is our firm

position that the most rational approach to solving the photochemical oxidant smog

problem in the South Coast Air Basin (SCAB) is to control the quantities of emissions

from motor vehicles of both smog precursors--Hcmiddot and NOx--their resulting atmosshy

pheric concentrations and the ratios between both contaminants which will result

from these controls

We arc also convinced that the oxidant and nitrogen dioxide air quality stanshy

dards can and will be met not by 1975 or 1977 but by the early 1980 s if the emisshy

sion control program as originally outlined by Ca~ifornia or a slight modification

of it proposed by the District is followed and enforced This should also provide

for continued compliance with these air quality standards at least through 1990

244

It will also allow time for a reappraisal in about 1978 of the whole situation relative

to the ultimate emission standards required and the best approach to their impleshy

mentation

Calculation of the degree of control necessary to attain the air quality

~ standards for oxidant and nitrogen dioxide involves indirect complex methods 1

aimed at determ_ining the degree of control of the primary contaminants directly

emitted by automobiles

The following evidence supports our proposed solution to the problem in

terms of both the atmospheric concentrations of the oxidant precursors NOx

and HC the ratio between them as reflected in their exhaust emission standards

and the resulting atmospheric concentrations of oxidant which comply with the air

quality standards

Chamber Results and Projections to the Atmosphere

The importance of environmental chamberwork cannot be minimized the

j need for and direction of the whole emission control program was based initially

j on the results of chamber experiments In order to understand the importance to

air quality of achieving both the correct low quantities of emissions and the right

ratio we can present several graphic portrayals of analyses of experimental labshy

oratory work together with their relationship to past present and future air quality

in terms of both morning primary reactant concentrations during the morning

traffic peak and the equivalent emissions which would produce them

245

Figure 7 shows maximum ozone levels that were obtained by irradiating

varying amounts of auto exhaust hydrocarbons and oxides of nitrogen in an environshy

mental chamber The corresponding ozone levels then can be found for any comshy

bination of BC and NOx concentrations Thus high ozone is produced with high

emissions of both hydrocarbons and oxides of nitrogen and low oxidant is formed with

low emissions However either low NOx or low HC emissions11 can also produce

low oxidant--graphic and clear evidence of the importance of the NOxHC ratio in

ozone formation Furthermore each and every possible combination of values for

NOx and HC has then a corresponding characteristic maximum chamber ozone

concentration

Using this graph we can estimate what ozone levels would result if certain

atmospheric mixtures of NOx and HC could be injected into the chamber and

irradiated Such estimates were made for 1960 and 1965 using atmospheric data

rlThe points labeles 1960 and 65 show the location of the highest levels of both

HC and NOx found in the air in those years in Downtown Los Angeles (OOLA) area

during the 6-9 AM traffic peak

It has been demonstrated by use of CO and NOx data and CONOx ratios

hnw well the characteristics of vehicle emissions are reflected in the atmosphere

We know what emissions from the average vehicle were then in 1960-1965 both

for HC and NOx so that we can mathematically relate emissions to atmospheric

concentrations for those years and so for future years also knowing or calculating

only what the characteristic emissions will be from the average vehicle

246

The NOx concentrations stayed about the same from 1960 through 1965 because

average vehicle emissions of that contaminant did not change during that time

Mobile source emissions can be shown to have contributed essentially all of this obshy

served result However blow by controls did reduce emissions of HC and the

concentrations dropped accordingly In 1965 the last year before exhaust controls

the point 65 indicates where we were then in terms of maximum ozone formation

to be expected in a chamber with the highest HC and NO concentrations found in the X

air that year Levels of ozone actually measured in the atmosphere however

are higher than those shown on the graph for high NOx and I-IC concentrations for

those years up to the present

The strategy to meet the oxidant standard is obvious--get atmospheric NOx

and HC concentrations out of the area on the chart that produces high ozone levels

and put them in tie areas with the lowest levels This can only be done by implementshy

ing appropriate emission standards

As can be seen that did not happen between 1965 and 1970 because manufacshy

turers used controls on new cars in California which while causing a decrease in

BC (and CO) allowed a large increase in NOx emissions Thus the path line of

the atmosphere on the chart goes up from 65 and diagonally to the left passing

through an area of higher ozone levels The atmospheric concentrations of oxidant

predictably increased during the years 1967 and 1968 By 1970 they dropped to lower

levels - -back to about the same as in 1965- -exactly as predicted by the model The

app14oximate location of the point for 1970 (70) was both predicted on the basis of

247

the mathematical model and confirmed by atm-ospheric measurements of

[)owntown Los Angeles morning summertime NOx and calculated HC values

Again it should be pointed out that those points show the highest possible

concentrations of NOx and HC Years with less restrictive weather conditions

(for accumulating high primary contaminant levels) would cause lower measured

maximum NOx and HC levels but the calculations would still yield the points

shown Thus we are taking the most pessimistic view

Future Projections

In 1973 we were at about the point labeled 73 and ozone levels were beginshy

ning to drop as expected middot It should be emphasized that ozone values plotted on

thi$ graph are for the chamber only- -not the atmosphere The future path the

points 7 4 and on to 90 represents our estimate of future atmospheric levels of

NO and BC expected if the exhaust emission standards are just met While that X -

is optimistic it is all we really can do since performance of future vehicle models

is unknown We will achieve maximum ozone levels at or below the standard by

about 1980-1985 This will only be true however if cars in compliance with the

California interim standards for HC and NOx continue to be added to the vehicle

population at the normal rate These standards provide the optimum ratio of NO X

to HC necessary to provide the nitric oxide (NO) needed for the reaction that re-

moves from the air both oxidant formed photochemically and oxidant which occurs

as natural background which alone may cause the standard to be exceeded This

ratio is about 112 or 2 parts NOx to 1 part HC

248

The optimum NOxHC ratio is a key element in the APCD strategy but will

require a finite time for its attainment Replacement of older cars by newer ones

equipped to meet the most stringent standards is the only reasonable mechanism

which can change it VMT reduction proposed as a prime strategy by EPA cannot

change this crl(ical ratio which is a basic characteristic of the population at any

given time

Validation of the Districts Control Strategy

Figure 8 compares (1) future chamber oxidant levels based upon the

future maximum concentrations of HC and NOx we expect each year with the

California control program (2) calculated atmospheric concentrations using ~ I

our chamber-to-atmasphere empirical translation and (3) actual measured atmos-f 1l pheric oxidant maxima This clearly sets forth the relationship among these three

factors

The chamber concentrations (lower curve) middotare the lowest values shown

The actual atmospheric data (points connected by heavy dotted and solid lines)

vary considerably from year to year partly because of the vagaries of the weather

In all cases the atmospheric oxidant values are higher than the chamber values

because of the addition of vehicle emissions as the air parcel travels from source

to receptor areas The calculated atmospheric data (thin dashed and solid curves)

are shown to be the highest generally exceeding or equalling the actual measured

data and of course always exceeding the chamber data Thus the model paints

the most pessimistic picture possible It can be seen that by about 19801 1985 atmos -

pheric levels should be at or below the Federal air quality standard of 0 08 ppm oxidant

249

3 Motor Vehicle Exhaust Control is the Only Requirement for Achieving the Oxidant Standard by 1980

We can show that the existing motor vehicle control program has resulted

in a significant reduction of oxidant concentrations in the air

The foregoing material explained the relationship between vehicula~ emis -

sions in source areas and the high oxidant levels measured in effect areas This

relationship is exemplified by the downward trend of oxidant levels in the atmosshy

phere and by the similar year-by-year trends of NO and HC emissions from the X

average motor vehicle A projection of these vehicle emissions factors shows that

the associated maximum oxidant level in the atmosphere will meet the oxidant standard

by about 1980-1985

Figure 9 compares by year the number of days that the oxidant air quality

standard was exceeded in three separate areas with the average NO and HC emissions X

per vehicle mile To comply with the air quality regulations the number of days that

this standard is exceeded must be reduced to one per year

The lines plotted on Figure 9 show that a definite relationship exists between

the emissions from the average motor vehicle and the number of days each year that

the oxidant concentration in the air exceeds the clean air standard

The oxidant trendlines for downtown Los Angeles Pasadena arrl Azusa are

all downward and the slopes are about the same This similarity is logical because

the process that results in the suppression of oxidant accumulation simply has been

displaced from one area to another This was a unique one time situation because

of the increase in NOx between 1966 and 1971 After 1971 all areas are down Thus

l

250

the same conclusion is reached that the oxidantstandard will be met in the 1980s

I whether air quality data or vehicle emissions trends are projected middot~ Ul-

This outlook is based on the APCD s belief that future growth in both the

Los Angeles area and SCAB will not create any locality with a traffic density greater

than any traffic density in the area to date For the past 25 years the area around

downtown Los Angeles has been the area of maximum traffic density and therefore

the emissions source area responsible for the maximum effect area measurements

It is assumed that the traffic density in any future source area will be no

greater than the traffic density in downtown Los Angeles Thus since the

vehicular emissions control program will achieve and maintain the air quality

standards in areas affected by vehicular emissions from downtown Los Angeles it

will also achieve and maintain them for any area of SCAB

Summary Conclusions and Recommendations

In conclusion we have shown that a source and effect area analysis of emisshy

sions and resulting oxidant is a more reasonable and accurate representation of

the Los Angeles area for air quality analysis than gross integration metho9s such

as the big box technique It has been shown that motor vehicles are the major and

almost sole contributor to the primary HC and NOx emissions in the downtown source

area which results in the high oxidant levels in the San Gabriel Valley in fact the

highest in SCAB An air quality model and vehicle emissions control strategy has

been suggested to meet the oxidant standard by mid-1980 s

251

We have shown that

bull Only by adjusting the ratio of NOxHC in the motor vehicle emissions to

permit accumulation of sufficient atmospheric NO to sea venge the normal

atmospheric background oxidant can the standard be attained

bull The APCD strategy which provides for implementation of the present

California interim emissions standards for NOx HC and CO for new

motor vehicles in California beginning with the 1975 model vehicles will

result in compliance with the CO N02 and oxidant air quality standards

by the mid 1980 s and will maintain this compliance until 1990 and

possibly longer

bull The effectiveness of the present California motor vehicle control program

is easily demonstrable using air quality data from several areas in Los

Angeles County 1960-1973

bull To assure achievement and maintenance of the air quality goals as now preshy

dicted there must be periodic assessments of the effectiveness of the

motor vehicle control program followed by corrective actions if necessary

What has been accomplished thus far is significant but much more remains

to be done so that the best possible representation of emissions and resulting air

quality may be available for use in this air basin A much better emission inventory

defining the spatial and temporal distribution of both mobile and stationary sources

is needed Better statbnary source information is needed to evaluate the local

effects of these emissions Further detailed studies are needed to establish the

252

true relationship between emissions data from vehicle test cycles and the actual

operation of vehicles neither the 7-mode nor the CVS procedure provides a true

representation of actual vehicle operation Further tracer studies to assess the

transport and dilution of mobile and stationary source emissions from selected

source areas are also needed

253

1111

IUD

a CC I w gt-

1111

1UO

IUD

I 990

IDJO

1180

1111

IUO

FIGURE I

HYDROCARBONS

STATIONARY SOURCES MOTOR VEHICLES

- --

8 12 II 20 742 2l IS 12 I 4

HUNDREDS

HYDROCARBON EMISSIONS STATIONARY SOURCES IN

OXIDES OF

0

OF TONSDAY

FROM MOTOO VEHICLES AND LOS ANGELES COUNTY

NITROGEN

STATIONARY SOURCES

MOTOR VEHICLES

011111111111111111110111bull1111111

IIIIIIHIIIIIIIIIHIUII

llillL Its rd

l1uu~111111u1111111

2 I O 1 J 3

HUND REDS OF TONSDAY

OXIDES OF NITROGEN EMISSIONS FROM MOTOR VEHICLES ANO STATIONARY SOURCES IN LOS ANGELES COUNTY

illl~ -~--~ i~-=i _J~l ~--~ bull_~L- I ~~~-~~--Z ~

6

6S-66 ox

ICS ~A~1 M

i ssmuwmmgt

bullI

e COROyent_

64 ~ IDB RIVERS~

ORAJfD

-

t t 10 miles

bullmiddotsame Avg Cone Both Years

Pigare 2

YEAR OP HIGHEST OXlDANI CONCENTRATIONS

Highest Average of Daily -Maiimum One-Hour Concentrations

During July August amp September 1963-1972

bullLj

I

64

70 s11 3RlU)U0

70

--__ 69bull

N V +=

middot Source Air Resources Board

-200o

t t 10 adlea

tDS ampIJtsect

-1~

-1611ASampXllmiddot bull - bull -z----~------

I ldmmprwJ

IIVERSIDI

~ - 70

OampY -1 U 70 bull L

I

N V1 V

middot-i___

-----------------------------------------------------------i----------------------------

Figure 3

CHANGE OP OXIDANT CONCENTRATIONS

Percent Change from the Highest Three-Year Average to the 1970-72 Average

Of Daily Maximum One-Hour Con~entrationa for JulY August amp September

Source Air Resources Board

256

FIGURE 4 TYPICAL FLOW OF POLLUTED Am PARCEIS CIUGINATING AT DIFFERENT LOCATIONS IN THE LOS ARE~S BASIN - STARTIOO 0900 PST

l I

OAT

TRAJECTORY SUWMATIOl4

----- SMOG ~AVS

I

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullNONbullSlfOG DAYS

ISTARTING Tl~ cgxpsy

~ HAW

(CA

257

FiGURE 5 ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AND OXIDANT IN DOWlflC1N LOS AIDELES (SOURCE AREA) AND PASADENA (EFFECT AREA) 1

1960-1972

LO CARBON MONOXIDE

30

Pasadena

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullbullbullbullbull Downtown Los Angeles

20

10

o_______________________________

OXIDANT

)

2 Down~ Los Angeles

1

o________________________ 1960 1962 196L 1966 1968 1970 1972

YEAR

bullbullbullbullbull

bullbullbullbullbullbullbull

258

FIGURE 6 COMPARISON 01 CALCULATED AND MEASURED ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AN1) OXIDES OF NITROOEN IN DCMNTOWN IDS AIJELES

196o-1972

CARBON MONOXIDE

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ~ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot _-- ---_ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ----middotmiddot-bullw-_~ ---bullbullbull

10

o_______________1111111_____

OXIDES OF NITROGEN25

20

15 bullbullbullbullbullmiddotmiddotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~

1-i 10 middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ---

oS o_______________________

RATIO CONOx

40

50

0 +raquo Cd

p 30

~ 20

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot bullbullbullbullbull middotmiddotmiddotmiddotmiddot-shybullbullbullbullbull 0 u

bullbullbullbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot 10

0 j

ilI 196o 1964 1968 1970 1972 I

YEAR

Measured~D-owntown Los Angeles (90th percentile ofmiddot daily] instantaneous maxima)

Calculated - Aver~ge vehicle emissions - Present control program

259

FIGURE 7

25

t i5

flJ

~ on ~ ~ Q) bO 100 Jo

+gt on z

o5

EFFECT OF CALIFORNIA 1 s AUTO EXHAUST CONTROL ffiOORA M ON MAXIMUM CHAMBER OZONE CONCENTRATION

- PPM

357bullbull

r 76 bull

11 l

30

20

CHAMBER OZONE MAXIMUM

50

10

o___________111111111111______111111111111_____________

0 05 10 15 20 25

Hydrocarbons m-2 (LB-15) - PPM (as Hexane)middot

--

bull bull bull

r--=--~1 ~a==-~ - _~l ~ y--===-- ~~--~-- ~ r---~~

o

o8

~ I

~ 0 H 8 o6 I

c~ ~ 0 z 0 0

8

~ o+ A H gtlto-

02

middoto

Figure 8 Calculated t1ax1mum Levels Instantaneous and Hourly Average

of Atmospheric Oxidant Compared to Measured Los Angeles County Maxima-with Projections to 1990

(California Standards)

~ -Calculated Inst ax ~

f Calculate Max Hr Avg 03

_ bullbull _ _ - i bull

0 bullbull -l bullbull a0Ieasured Inst Lax o3 bull middotmiddotmiddot~bull 0bull _ ____ V ~ ea~ured ~ Hr Avr o3

~~ r---

~ ~ NB r~ima for 197 4 amiddots of 121074--- -_ Chamber Ozone F ~_ _~

- 1L_

~ Federal Primarfo Air ~uality Standard ~6- -UaximumT- our Avera~elr~ppm-------------- --~ ------- -~- -~-- ~

I I I I I I I I I I I I I I I I I N1 O

1960 6i 64 66 ~i middot-o 72 74 76 79 middotso middot92 84 bullg s9 9o

TBAR (end)

0

261 FIGURE -OMPARISON OF ATMOSPHERIC OXIDANT TRENDS WITH AVERAGE NCJx AND

HC EMISSIONS (Grams per Mile from Average Vehicle)

JOO Number of days state oxidant standara wds equalled or exceeded

--- Azusa __ Pasadena ________ Downtown Los Angeles

20

15 u

___ Hydroc_arbons Oxides of Nitrogenbullmiddotmiddotmiddotmiddotmiddotbullbullmiddot 1975 and later-assume middotcalifornia ARB standards

o_ ___________________________11111____

1965 1970 1975middot 198omiddot 198S 1990

136

with air pollution As a consequence we have an automobile engine which

is a low-cost production item has a high power-to-weight ratio has

turned out to be a reliable relatively low maintenance very durable

device and in some cases even the fuel economy is not so bad Then after

the fact it was decided that this engine rhould be made to be low

emitting Therefore it is not too surprising that the approach of the

automobile industry has been to modify thi engine in which they have a

great deal of confidence and know how to build inexpensively as little as

possible The control approaches therefore have been minor modifications

to the engine and have now focused upon processing the exhaust This to

my thinking as an engineer is not a good approach But objectively if

one judges simply on the basis of whether emissions are controlled or not

has worked out quite well I do not think we can be too critical of the

add-on catalyst technology if it works The evidence now suggests that it

is going to work that it is probably cost effective and that the autoshy

mobile industry probably deserves more credit than they are receiving for

the job theyve done in developing the oxidation catalyst for the autoshy

mobile engine What Im saying is the add-on approach is not necessarily

all that bad

Again to give some general perspective on how one might approach

automotive emission controls and how we arrived where we are Id like to

discuss Figure 1 which points out several approaches to controlling

emissions from the automobile engine These are

1) preparation of the air fuel mixture which has received only minor

attention by the auto industry

2) modification of the engine itself the combustion process which

is not very evident in the 1975 automobiles but will be the subject of

Dr Newhalls presentation and

I I

I

137

3) the general field of exhaust treatment where most of the effort

has been placed by the U S auto industry

I would like to emphasize that the first area the whole matter of

mixture control that is either improving the present carburetor or

replacing it with a better mixture control system is perhaps the single

technological area which has been most overlooked by the automobile

industry The engine requires a well meteTed fuel-to-air mixture over a

wide variety of operating conditions that is good cycle-to-cycle and

cylinder-to-cylinder control The present systems simply do not do that

It is also evident that the mixture control system must operate with varying

ambient conditions of pressure and temperature The present systems do not

do that adequately There are promising developments in improvement of

mixture control systems both carbureted and fuel injection which do not

appear to be under really aggressive develJpment by the automobile industry

One should question why this is not occurring

I will skip the area of combustion modification because that really

comes under the new generation of engines The combustion modification is

an important approach and will be discussed by the next speaker

The area of exhaust system treatment the third area is the one about

which youve seen the most We early saw the use of air injection and then

improved air injection with thermal reactors Now were seeing oxidation

catalysts on essentially 100 of the U S cars sold in California There

are yet other possibilities for exhaust treatment for the control of

oxides of nitrogen based upon reduction catalysts or what is known as

threeway catalysts another variation of the reduction catalyst and

possibly also the use of particulate traps as a way of keeping lead in

gasoline if that proves a desirable thing to do (which does not appear to

be the case)

138

What about the 1975 California car Most of you probably have enough

interest in this vehicle that youve tried to figure out just what it does

But in case some of you have not been able to straighten its operation out

let me tell you as best I understand what the 1975 California car is

The cars from Detroit are 100 cataly~t eq11ipped There may be an excepshy[

l

1 tion sneaking through here and there but it looks like it is 100 These

are equipped with oxidation catalysts in a variety of configurations and

sizes the major difference being the pellet system which is used by

General Motors versus the monolith system which has been used by Ford and

Chrysler The pellet system appears to be better than the monolithic ~ l l system but it is not so obvious that there are huge differences between the

aocgtnow The catalysts come in a variety of sizes they are connected to

the engine in different ways sometimes there are two catalysts sometimes

a single catalyst (the single catalyst being on the 4 and 6-cylinder

engines) Some of the 8-cylinder engines have two catalysts some of them

have one catalyst All California cars have all of the exhaust going

through catalysts This is not true of some of the Federal cars in which

some of the exhaust goes through catalysts and some does not

Ninety percent of the California cars probably will have air pumps

Practically all the cars from Detroit have electronic ignition systems

which produce more energetic sparks and more reliable ignition The

exhaust gas recirculation (EGR) systems appear to have been improved

somewhat over 1974 but not as much as one would have hoped There were

some early designs of EGR systems which were fully proportional sophistishy

cated systems These do not appear to have come into final certification

so that there still is room for further improvement of the EGR system

The emissions levels in certification of these vehicles are extremely low

139

(Table I) Just how the automc1bile industry selects the emission levels

at which they tune their vehicles has been of great interest The

hydrocarbon and CO levels in certification (with deterioration factors

applied--so this is the effective emissions of the certification vehicles

at the end of 50000 miles) are approximately one-half the California

standards The oxides of nitrogen emissions are approximately two-thirds

of the California standards This safety factor is put in by the automoshy

bile industry to allow for differences between the certification vehicles

and the production vehicles to ensure that they did not get into a situation

of recall of production vehicles which would be very expensive

There appears to have been a great deal of sophistication developed by

the automobile industry in being able to tune their vehicles to specific

emission levels General Motors appears to have done better tuning than

the other manufacturers This leads to the rather interesting result

that a significant number of the 1975 California vehicles meet the 1977

emission standards (Table II) that is approximately 10 of the U S cars

certified for California already meet the 1977 emission standards This

does not mean to say that the industry could immediately put all of their

production into such vehicles and meet the 1977 emission standards because

of a concern about the safety factor for the certification versus producshy

tion vehicles Thirty-four percent of the foreign vehicles certified for

1975 in California meet the 1977 emission standards The 1977 emission

standards are 041 grn hydrocarbon~ 34 gm carbon monoxid~ and 20 gm

oxides of nitrogen This does confirm that the oxidation catalysts are a

more than adequate technology for meeting the 1977 emission standards and

only minor refinements and adjustments to those systems are required to go

ahead with the 1977 emission standards There are some other arguments

against this optimistic viewpoint and Ill deal with those later

140

There is a great uniformity in the deBigns which the U S manufacturshy

ers have selected for the 1975 California vehicles For those of you who

do not live in California about 80 of thl~ vehicles in the rest of the

country will be catalyst equipped General Motors is going with 100

catalysts apparently to realize the fuel economy benefit of their system

which more than pays for the cost of the catalyst system We have the very

interesting situation that the more stringent 1975 emission standards have

not only reduced the emissions of the 1975 vheicles with respect to the

1973-1974 vehicles but have also reduced the cost of operating the car

and have improved fuel economy The idea that emissions control and fuel

economy and economical operation are always one at odds with the other is

simply not true Compared to the previous years vehicles the more

stringent emissions standards of 1975 have brought improvements to fuel

economy because they forced the introduction of more advanced technology

The fuel savings which have been realized produce a net decrease in operashy

tional costs over the lifetime of the car This is not to say that pollution

control doesnt cost something If you were to compare the 1975 vehicle

with a completely uncontrolled vehicle tht~re would indeed be an incremental

cost associated with the 1975 vehicle

The foreign manufacturers have demonstrated a greater variety of

approaches in meeting the 1975 California standards but again they are

producing mostly catalyst equipped vehicles There is a widespread use of

fuel injection by the foreign manufacturers especially the Europeans

apparently because this is the easiest appmiddotroach for them and they realize

that only a fraction of their production comes to the United States

Volkswagen for example apparently has gone to 100 fuel injection on its

air cooled engines to be sold in California Mazda will continue to sell

141

rotary engine vehicles and thereby be the only rotary engine vehicle

manufacturer and marketer in the United States General Motorsgt elimination

of therotary engine stated for reasons of emissions is probably more

influenced by problems with fml economy although the two are a bit

difficult to separate Mazda is meeting the 1975 emissions standards and

in fact can meet the 1977 emission standards It has not solved its fuel

economy difficulties on the 1975 cars they will do better in 1976 All

evidence points to a fuel economy penalty for the rotary engine Nonetheshy

less we do have this option available because of the Japanese Also the

foreign manufacturers are providing us with a small number of diesel

engine cars These are of great interest because of definite fuel economy

advantages The diesel engine vehicles also meet the 1977 emissions

standards right now Also in J975 well 3ee the CVCC engine marketed by

Honda

The costs of the 1975 vehicles over tae lifetime of the vehicle are

definitely lower than the costs of the 197~ vehicles The National Academy

of Sciences estimate averaged over all vehicles is that in comparison to

the 1970 vehicles the lifetime cost of emission control system including

maintenance and fuel economy costs is aboJt $250 per vehicle greater in

1975 than 1970 Since the 1974 vehicles w2re about $500 more expensive

there has been a net saving in going from 1974 to 1975 I think the

conclusion we should draw for 1975 is that the auto industry has done a

pretty good job in meeting these standards This is something which they

said they couldnt do a few years ago something which they said that if

they could do it would be much more expewdve than it has turned out to

be

The same technology can be applied to 1977 models with no technological

difficulty and only slight refinements of the systems The fuel economy

142

penalties as estimated by the National Academy of Sciences are small 3

or less in going to the 1977 standards This estimate does assume further

advancements by the auto industry to improve fuel economy--primarily

improved exhaust gas recirculation systems It is unfortunate that this

issue of fuel economy has become so mixed up with the air pollution question

because the two are only slightly related If one is really concerned about

fuel economy and there isnt too much evidence that the auto industry or

the American public really is too concerned right now there is only one

way to have a drastic effect on fuel economy and that is to decrease the

vehicle weight Until that is done with gains on the order of 50 or

more to worry about 3 or 5 differences in fuel economy related to emission

control systems is simply to focus upon the wrong issue

Now what are the problem areas What remains to be done The

problems certainly arent over with the introduction of the 1975 vehicles

Problem Area Number One Field performance What is going to happen

to these vehicles when they get into actual service Past experience with

the 1971 through 1973 vehicles has been rather poor in that EPA and

California surveillance data show that these vehicles are not meeting the

standards Many of them did not meet the standards when they were new

The situation in general is getting worse at least for CO and hydrocarbons

that is with time the emission levels of CO and hydrocarbons for the 1971 I through 1973 vehicles is degrading There is no in-service experience of

this sort with the 1975 vehicles yet The certification data look quite I promising but the test procedures especially for durability are not ithe same as what occurs in actual use It is generally stated that the

1actual use situation for the catalysts will be more severe than the EPA

test procedure A larger number of cold starts are involved in actual use

than in the EPA test procedure and thermal cycling will probably have an

143

adverse effect on the lifetime of the cata]_yst This is not so obvious

It is also likely that the higher temperature duty cycle in actual use will

improve the performance of the catalyst in that it will help to regenerate

the catalyst through the removal of contaminants as long as one does not

get into an overheat situation The National Academy of Sciences estimate

was that the number of catalyst failures tn the first 50000 miles would

be on the order of about 7 Thats a very difficult number to estimate in

the absence of any real data A 7 failure still leaves a net gain in

emissions control even if nothing is done about this failure This points

to the problem of what happens after 50000 miles The EPA certification

procedure and control program only addresses the first 50000 miles The

second 50000 miles or slightly less for the average car is the responsishy

bility of the states Unfortunately then~ seems to be very little progress

in the area of mandatory inspection and ma-Lntenance--very little thought

being given to whether the replacement ofthe catalyst at 50000 miles

if it has failed is going to be required and how that is going to be

brought about The area of field performance remains a major problem

area one which obviously needs to be monitored as the California Air

Resources Board has been doing in the past but probably even more carefully

because the unknowns are higher with the catalyst systems

Problem Area Number Two Evaporative hydrocarbons from automobiles

It was identified at least 18 months ago that the evaporative emission

control systems are not working that the evaporative emissions are on the

order of 10 times greater than generally thought In the Los Angeles

area cars which are supposed to be under good evaporative emissions

controls are emitting approximately 19 grams per mile of hydrocarbons

through evaporation This apparently has to do with the test procedure used

144

The EPA is pursuing this The California Air Resources Board does have some

consideration going on for this but it appears that the level of activity

in resolving this problem is simply not adequate If we are to go ahead

to 04 of a gram per mile exhaust emissions standards for hydrocarbons

then it just doesnt make sense to let 19 grams per mile equivalent escape

through evaporative sources

Problem Area Number Three What about the secondary effects of the

catalyst control systems Specifically this is the sulfate emissions

problem and I really do not know the answer to that Our appraisal is

that it is not going to be an immediate problem so we can find out what

the problem is in time to solve it The way to solve it now since the

automobile industry is committed to catalysts and it is unreasonable

to expect that they will reverse that technology in any short period of

time is take the sulfur out of the gasoline The cost of removing sulfur

from gasoline is apparently less than one cent per gallon Therefore if

it becomes necessary to be concerned with sulfate emissions the way to

meet the problem is to take the sulfur out of gasoline Obviously sulfate

emissions need to be monitored very carefully to see what happens The

final appraisal is certainly not now available Another secondary effect

of the catalysts is the introduction of significant quantities of platinum

into an environment where it hasnt existed before Not only through

exhaust emissions which appear to be small but also through the disposal

problem of the catalytic reactors Since the quantity of platinum involved

is quite small the argument is sometimes used that platinum does not

represent much of a problem The fact that the amount of platinum in the

catalyst is so small may also mean that its not economical to recover it

This is probably unfortunate because then the disposal of these catalysts

l Jj

145

I becomes important I will not speak to the medical issues because

am not qualified The evidence is that theuro~ platinum will be emitted in a

form which does not enter into biological cycles--but this is no assurance

that it couldnt later be transformed in such a form What is obviously

needed is a very careful monitoring program which hopefully was started

before the catalysts were put into service If it wasnt then it should

be started today

Problem Area Number Four NO control The big problem with NO X X

control is that nobody seems to know or to be willing to establish what

the emission control level should be It is essential that this be tied

down rapidly and that it be fixed for a reiatively long period of time

because the NO level is going to have a VE~ry important ef feet upon the X

development of advanced engine technology The 20 gm level has been

attained in California with some loss of fuel economy through the use of

EGR and it is not unreasonable in our estimation to go to 15 grams per

mile with very little loss in fuel economy To go to 04 gram per mile

with present technology requires the use of one of two catalytic systems

either the reduction catalyst in tandem with the oxidation catalyst or what

is known as the three-way catalyst Both of these systems require technoshy

logical gains The state of development appears to be roughly that of the

oxidation catalyst two years ago The auto industry will probably say

that it is not quite that advanced but that if it were required to go to

04 gram per mile in 1978 that it could be done With the catalyst systems

the fuel economy penalties would not be great in fact the improvement to

the engine which would be required to make the system work would again

probably even allow a slight improvement in fuel economy What the 04

gram per mile NO catalyst system would appear to do however is to X

146

eliminate the possibility of the introduction of stratified charge engines

both the CVCC and the direction injection system and also diesel engines

It is in the context of the advantages of these advanced engines to meet

emission standards with improved fuel economy that one should be very

cautious about the 04 grammile oxides of nitrogen standards for automoshy

biles My own personal opinion is that the number should not be that

stringent that a number of 1 or 15 gm is appropriate Such a level

would require advancements but would not incur great penalties

Other items which I view as problem areas are less technically

involved and therefore require fewer comments

bull Nonregulated pollutants--again thls is a matter of keeping track

of particulates aldehydes hydrocarbon composition to make

certain that important pollutants ire not being overlooked or

that emission control systems are not increasing the output of

some of these pollutants

bull Fuel economy The pressures of fuel economy are going to be used

as arguments against going ahead wlth emissions control Mostly

these two can be resolved simultaneously We should simply ask

the automobile industry to work harder at this

bull Final problem area New fuels Again it does not appear that

the introduction of new fuels will come about as an emissions

control approach but that they may be introduced because of the

changing fuel availability patterns and the energy crisis These

fuels should be watched carefully for their impact upon emissions

This does middotappear to be an area in which a great deal of study is

going on at the present time It is one problem area perhaps in

which the amount of wprk being done is adequate to the problem

which is involved

147

In sunnnary then the appraisal of the 1975 systems is that they are

a big advancement they will be a lot better than most of us thought and

that we should give the automobile industry credit for the job theyve

done in coming up with their emissions control systems

With that boost for the auto industry which Im very unaccustomed

to Ill entertain your questions

-------=-~ ~~~ U- ~a1

~_~a--~-~ -J~ ~ -~r- _ --=~-- -___ja--~ __1~~ ~-~----=

AIR

1-4 FUEL----1

I I ENGINE

I II

_________ EXHAUST SYSTEM I bull EXHAUST

I I I

+ MIXTURE CONTROL COMBUSTION MODIFICATION EXHAUST TREATMENT

FuelAir Metering Ignition Air Jnjection FuelAir Mixing Chamber Geometry Thermal Reactor Fuel Vaporization Spark Timing Oxidation Catalyst Mixture Distribution Staged Combustion Reduction Catalyst Fuel Characteristics Ex tern almiddot Combustion Three Way Catalyst Exhaust Gas Redrculation Particulate Trap

FIGURE 1 Approaches to the Control of Engine Emissions

~ i 00

149

TABLE I

Average Emissions of 1975 Certification Vehicles (As Corrected Using the 50000-Mile Deterioration Factor)

Emissions in gmi Fraction of Standard HC CO NO HC CO NO

Federal 1975 X X

AMC 065 67 25 043 045 080

Chrysler 074 77 25 049 051 082

Ford 081 92 24 054 061 078

GM 083 80 23 055 053 074

Weighted Average 080 82 24 053 055 076

California 1975

AMC 042 49 17 047 054 087

Chrysler 048 61 16 053 067 082

Ford 052 56 13 058 062 067

GM 065 55 16 0 72 061 082

Weighted Average 058 56 16 064 062 078

kWeighted average assumes the following market shares AMC 3 Chrysler 16 Ford 27 and GM 54

150

TABLE II

Total Number of Vehicles Certified for California 1975 Standard and the Number (and percentage) of These Able to Meet

Certain More Stringent Standards

Calif 1975 Federal 1977 Hypothesized Hypothes ized 099020 04J420 049020 093420

i ~

Manufacturer no () no () no () no ()

AMC 16 (100) 1 ( 6) ti ( 38) 3 (19)

Chrysler 21 (100) 2 ( 9) ( 33) 0 ( O)

Ford 26 (100) 4 (15) -middot ( 15) 5 (19)

l GM 46 (100) 1 ( 2) -1 ( 9) 5 (11)

Foreign 62 (100) 21 (34) 3H (61) 28 (45)

1J

f

-l

151

CURRENT STATUS OF ALTERNATIVE AUTOM)BIIE ENGINE TECHNOLCXY

by

Henry K Newhall Project Leader Fuels Division

Chevron Research CanpanyRicbmmd California

I

iH1middot

10 1ntroduction and General Background

I

11 General

The term stratified ct1arge englne has been used for many

years in connection with a variety of unconventional engine

combustion systems Common to nearly all such systems is

the combustion of fuel-air mixtures havlng a significant

gradation or stratification in fuel- concentration within the

engine combustion chamber Henee the term nstratifled charge

Historically the objective of stratified charge engine designs

has been to permit spark ignition engine operation with average

or overall fuel-air ratios lean beyond the ignition limits of

conventional combustion systems The advantages of this type

of operation will be enumerated shortly Attempts at achieving

this objective date back to the first or second decade of this

century 1

More recently the stratified charge engine has been recognized

as a potential means for control of vehicle pollutant emissions

with minimum loss of fuel economy As a consequence the

various stratified charge concepts have been the focus of

renewed interest

152

12 Advantages and Disadvantages of Lean Mixture Operation

Fuel-lean combustion as achieved in a number of the stratified

charge engine designs receiving current attention has both

advantages and disadvantages wnen considered from the comshy

bined standpoints of emissionsmiddot control vehicle performance

and fuel economy

Advantages of lean mixture operation include the following

Excess oxygen contained in lean mixture combustion

gases helps to promote complete oxidation of hydroshy

carbons (HG) and carbon monoxide (CO) both in the

engine cylinder and in the exhaust system

Lean mixture combustion results in reduced peak

engine cycle temperatures and can therefore yield

lowered nitrogen oxide (NOx) emissions

Thermodynamic properties of lean mixture combustion

products are favorable from the standpoint of engine

cycle thermal efficiency (reduced extent cf dissociashy

tion and higher effective specific heats ratio)

Lean mixture operation caG reduce or eliminate the

need for air throttling as a means of engine load

control The consequent reduction in pumping losses

can result in significantly improved part load fuel

economy

153

Disadvantages of lean mixture operation include the following

Relatively low combustion gas temperatures during

the engine cycle expansion and exhaust processes

are inherent i~ lean mixture operation As a conseshy

quence hydrocarbon oxidation reactions are retarded

and unburned hydrocarbon exhaust emissions can be

excessive

Engine modifications aimed at raising exhaust temperashy

i tures for improved HC emissions control (retarded middot~

ignition timing lowered compression ratlo protrtacted combustion) necessarily impair engine fuel economy1 I

1j bull If lean mixture operation is to be maintained over ~

the entire engine load range maximum power output t l and hence vehicle performance are significantly

impaired

Lean mixture exhaust gases are not amenable to treatshy

ment by existing reducing catalysts for NOx emissions

control

Lean mixture combustion if not carefully controlled

can result in formation of undesirable odorant

materials that appear ln significant concentrations

in the engine exhaust Diesel exhaust odor is typical

of this problem and is thought to derive from lean mixshy

ture regions of the combustion chamber

154

Measures required for control of NOx emissions

to low levels (as example EGR) can accentuate

the above HC and odorant emissions problems

Successful developmentmiddotor the several stratified charge

engine designs now receiving serious attention will depend

very much on the balance that can be achieved among the

foregoing favorable and unfavorable features of lean comshy

bustion This balance will of course depend ultimately on

the standards or goals that are set for emissions control

fuel economy vehicle performance and cost Of particular

importance are the relationships between three factors -

UBHC emissions NOx emissions and fuel economy

13 Stratified Charge Engine Concepts

Charge stratification permitting lean mixture operation has

been achieved in a number of ways using differing concepts

and design configurations

Irrespective of the means used for achieving charge stratifishy

cation two distinct types of combustion process can be idenshy

tified One approach involves ignition of a small and

localized quantity of flammable mixture which in turn serves

to ignite a much larger quantity of adjoining or sur~rounding

fuel-lean mixture - too lean for ignition under normal cirshy

cumstances Requisite m1xture stratification has been achieved

155

in several different ways rangiDg from use of fuel injection

djrectly into open combustion chambers to use of dual

combustion chambers divided physically into rich and lean

mixture regions Under most operating conditions the

overall or average fuel-air ratio is fuel-lean and the

advantages enumerated above for lean operation can be realized

A second approach involves timed staging of the combustion

process An initial rich mj_xture stage in which major comshy

bustion reactions are completed is followed by rapid mixing

of rich mixture combustion products with an excess of air

Mixing and the resultant temperature reduction can in

principle occur so rapidly that minimum opportunity for NO

formation exists and as a consequence NOx emissions are

low Sufficient excess air is made available to encourage

complete oxidation of hydrocarbons and CO in the engine

cylinder and exhaust system The staged combustion concept

has been specifically exploited 1n so-called divided-chamber

or large volume prechamber engine designs But lt will be

seen that staging is also inherent to some degree in other

types of stratified charge engines

The foregoing would indicate that stratified charge engines

can be categorized either as lean burn engines or staged

combustion engines In reality the division between conshy

cepts is not so clear cut Many engines encompass features

of both concepts

156

14 Scope of This Report

During the past several years a large number of engine designs

falling into the broad category of stratified charge engines

have been proposed Many of these have been evaluated by comshy

petent organizations and have been found lacking in one or a

number of important areas A much smaller number of stratified

charge engine designs have shown promise for improved emissions

control and fuel economy with acceptable performance durashy

bility and production feasibility These are currently

receiving intensive research andor development efforts by

major organizations - both domestic and foreign

The purpose of this report is not to enumerate and describe the

many variations of stratified charge engine design that have

been proposed in recent years Rather it is intended to focus

on those engines that are receiving serious development efforts

and for which a reasonably Jarge and sound body of experimental

data has evolved It is hoped that this approach will lead to

a reliable appraisal of the potential for stratified charge

engine systems

20 Open-Chamber Stratified Charge Engines

21 General

From the standpoint of mechanical design stratified charge

engines can be conveniently divided into two types open-chamber

and dual-chamber The open-chamber stratjfied charge engine

has a long history of research lnterest Those crigines

157

reaching the most advanced stages of development are probably

the Ford-programmed c~mbustion process (PROC0) 2 3 and Texacos

controlled combustion process (TCCS) 4 5 Both engines employ a

combination of inlet aar swirl and direct timed combustion

chamber fuel injection to achieve a local fuel-rich ignitable

mixture near the point of ignition _For both engines the overshy

all mixture ratio under most operating conditions is fuel lean

Aside from these general design features that are common to

the two engiries details of their respective engine_cycle proshy

cesses are quite different and these differences reflect

strongly in comparisons of engine performance and emissions

characteristics

22 The Ford PROCO Engin~

221 Description

The Ford PROCO engine is an outgrowth of a stratified charge

development program initiated by Ford in the late 1950s The

development objective at that time was an engine having dieselshy

like fuel economy but with performance noise levels and

driveability comparable to those of conventional engines In

the 1960s objectives were broadened to include exhaust

emissions control

A recent developmental version of the PROCO engine is shown in

Figure 2-1 Fuel is injected directly into the combustion chamber

during the compression stroke resulting in vaporjzation and

formation of a rich mixture cloud or kernel in the immediate

158

vicinity of the spark plug(s) A flame initiated in this rich

mixture region propagates outwardly to the increasingly fuelshy

lean regions of the chamber At the same time high air swirl

velocities resulting from special orientation of the air inlet

system help to promote rapid mixing of fuel-rich combustion

products with excess air contained in the lean region Air

swirl is augmented by the squ1sh action of the piston as it

approaches the combustion chamber roof at the end of the comshy

pression stroke The effect of rapid mixing can be viewed as

promoting a second stage of cori1bustion in which rlch mixture

zone products mix with air contained in lean regions Charge

stratification permits operation with very lean fuel-air mixshy

tures with attendent fuel economy and emissj_ons advantages In

addition charge stratification and direct fuel injection pershy

mit use of high compression ratios with gasolines of moderate

octane quality - again giving a substantial fuel economy

advantage

Present engine operation includes enrichment under maximum

power demand conditions to mixture ratios richer than

stoichiometric Performance therefore closely matches

that of conventionally powered vehicles

Nearly all PROCO development plans at the present time include

use of oxidizing catalysts for HC emissions control For a

given HC emissions standard oxidizing catalyts permit use

of leaner air-fuel ratios (lower exhaust temperatures)

1

l

159

together with fuel injection and ignition timing charactershy

istics optimized for improved fuel economy

222 Emissions and Fuel Economy

Figure 2-2 is a plot of PROCO vehicle fuel economy versus NOx

emissions based or1 the Federal CVS-CH test procedure Also

included are corresponding HC and CO emissions levels Only

the most recent test data have been plotted since these are

most representative of current program directions and also

reflect most accurately current emphasis on improved vehicle

fuel economy 6 7 For comparison purposes average fuel

economies for 1974 production vehicles weighing 4500 pounds

and 5000 pounds have been plotted~ (The CVS-C values

reported in Reference 8 have been adjusted by 5 to obtain

estimated CVS-CH values)

Data points to the left on Figure 2-2 at the o4 gmile

NOx level represent efforts to achieve statutory 1977

emissions levels 6 While the NOx target of o4 gmile was

met the requisite use of exhaust gas recirculation (EGR)

resulted in HC emissions above the statutory level

A redefined NOx target of 2 gn1ile has resulted in the recent

data points appearing in the upper right hand region of

Figure 2-2 7 The HC and CO emissions values listed are

without exhaust oxidation catalysts Assuming catalyst middotl

conversion efficiencies of 50-60 at the end of 50000 miles

of operation HC and CO levels will approach but not meet

160

statutory levels It is clear that excellent fuel economies

have been obtained at the indlcated levels of emissions

control - some 40 to 45 improved re1at1ve to 1974 produc-

tj_on vehicle averages for the same weight class

The cross-hatched horizontal band appearing across the upper

part of Figure 2-2 represents the reductions in NOx emissions

achieveble with use of EGR if HC emissions are unrestricted

The statutory 04 gmile level can apparently be achieved

with this engine with little or no loss of fuel economy but

with significant increases in HC emissions The HC increase

is ascribed to the quenching effect of EGR in lean-middotmixture

regions of the combustion chamber

223 Fuel Requirements

Current PROCO engines operated v1ith 11 1 compression ratio

yield a significant fuel economy advantage over conventional

production engines at current compression ratios According

to Ford engineers the PROCO engine at this compression

ratio j_s satisfied by typical fu1J-boi1ing commercial gasoshy

lines of 91 RON rating Conventional engines are limited to

compression ratios of about 81 and possibly less for

operation on similar fuels

Results of preliminary experiments indicate that the PROCO

engine may be less sensitive to fuel volatility than convenshy

tional engines - m1 important ff1ctor in flextb1 llty from the

standpoint of the fuel supplier

161

224 Present Status

Present development objectives are two-fold

Develop calibrations for alternate emissions target

levels carefully defining the fueleconofuy pbtenshy

tial associated with each level of emissions control

Convert engine and auxiliary systems to designs

feasible for high volume production

23 The Texaco TCCS Stratified Charge Engine

231 General Description

Like the Ford PROCO engine Texacos TCCS system involves_

coordinated air swirl and direct combustion chamber fuel

injection to achieve charge stratification Inlet portshy

induced cylinder air swirl rates typically approach ten times

the rotational engine speed A sectional view of the TCCS

combustion chamber is shown in Figure 2-3

Unlike the PROCO engine fuel injection in the TCCS engine

begins very late in the compression stroke - just before th~

desired time of ignition As shown in Figure 2-4 the first

portion of fuel injected is immediately swept by the swirling

air into the spark plug region where ignition occurs and a

flame front is established The continuing stream of injected

fuel mixes with swirling air and is swept into the flame

region In many respects the Texaco process resembles the

162

spray burning typical of dj_esel combustion ~r1th the difshy

ference that ignition is achieved by energy from an elec-

tric spark rather than by high compression temperatures

The Texaco engine like the diesel engine does not have a

significant fuel octane requirement Further use of positive

spark ignition obviates fuel I

cetane requirements character-

istic of diesel engines The resultant flexibility of the

TCCS engine regarding fuel requirements is a si~1ificant

attribute

In contrast to the TCCS system Fords PROCO system employs

relatively early injection vaporization and mixing of fuel

with air The combustion process more closely resembles the

premixed flame propagation typical of conventional gasoline

engines The PROCO engine therefore has a definite fuel

octane requirement and cannot be considered a multifuel

system

The TCCS engine operates with hi__gh compression ratios and

with little or no inlet air throttling except at idle conshy

ditions As a consequence fuel economy is excellent--both

at full load and under part load operating conditions

232 Exhaust Emissions and Fuel Economv

Low exhaust temperatures characteristlc of the TCCS system

have necessitated use of exhaust oxidation catalysts for

control of HC emissions to low lf~Vels A11 recent development

163

programs have therefore included use of exhaust oxidation

catalysts and most of the data reported here r~present tests

with catalysts installed or with engines tuned for use with

catalysts

Figures 2-5 and 2-6 present fuel economy data at several

exhaust emissions levels for two vehicles--a US Army M-151

vehicle with naturally aspirated 4-cylinder TCCS conversion

and a Plymouth Cricket with turbocharged 4-cylinder TCCS

engine 9 10 1urbocharging has been used to advantage to

increase maximum power output Also plotted in these figures

I are average fuel economies for 1974 production vehicles of

similar weight 8

I When optimized for maximum fuel economy the rrccs vehicles

can meet NOx levels of about 2 gmile It should be noted

that these are relatively lightueight vehicles and that

increasing vehicle weight to the 4000-5000 pound level could

result in significantly increased NOx emissions Figur~s 2-5

and 2-6 both show that engine modifications for reduced NOx

levels including retarded combustion timing EGR and increased

exhaust back pressure result in substantial fuel economy

penalties

For the naturally aspirated engine reducing NOx emissions

from the 2 gmile level to O l~ gmile incurred a fuel

economy penalty of 20 Reducing NOx from the tllrbocharged

164

engine from 15 gmile to 04 gmile gave a 25 fuel economy

penalty Fuel economies for both engines appear to decrease

uniformly as NOx emissions are lowered

For the current TCCS systems most of the fuel economy penalty

associated with emissions control can be ascribed to control

of NOx emissions although several of the measures used for

NOx control (retarded cornbusticn timing and increased exhaust

back pressure) also help to reduce HG emissions HC and CO

emissions ari effectively controlled with oxidation catalysts

resulting in relatively minor reductions in engine efficiency

233 TCCS Fuel Reauirements

The TCCS engine is unique among current stratified charge

systems in its multifuel capability Successful operation

with a nuraber of fuels ranging from gasoline to No 2 diesel

Table 2-I

Emissions and Fuel Economy of Turbocharged TCCS Engine-Powered Vehicle 1

Fuel

Emissions gMile 2 Fuel Economy

mng 2HC co NOx

Gasoline

JP-4

100-600

No 2 Diesel

033

026

014

027

104

109

072

J bull l ~

-

061

050

059

060

197

202

213

230

1M-151 vehicle 8 degrees coffibustion retard 16 light load EGR tw0 catalysts (Ref 10)

2 CVS-CH 2750 pounds tnert1a welght

165

l

has been demonstrated Table ~-I lists emissions levels and

fuel economies obtained with a turbocharged TCCS-powered

M-151 vehicle when operated on each of four different fuels 10

These fuels encompass wide ranges in gravity volatjlity

octane number and cetane leve 1 as middotshown in Table 2-II

Table 2-II

Fuel Specifications for TCCS Emissions Tests (Reference 10)

Gravity 0 API Sulfur

OFDistillation~

Gasolj_ne 100-600 JP-4 No 2

Diesel

88 -

86 124 233 342 388

0024 912

-

486 012

110 170 358 544 615

0002 57 356

541 0020

136 230 314 459 505

-middot --

369 0065

390 435 508 562 594

--

lta 9

IBP 10 50 90 EP

TEL gGal Research Octane Cetane No

Generally the emissions levels were little affected by the

wide variations in fuel properties Vehicle fuel economy

varied in proportion to fuel energy content

As stated above the TCCS engine is unique in its multifuel

capability The results of Tables 2-I and 2-II demonshy

strate that the engine has neither 8ign1ficant fuel octane

nor cetane requirements and further that it can tolerate

166

wide variations j_n fuel volati1tty rhe flexibility offered

by this type of system could be of major importance in

future years

234 Durability Performance Production Readiness

Emissions control system durability has been demonstrated by

mileage accumulation tests Ignltion system service is more

severe than for conventional engines due to heterogeneity of

the fuel-air mixture and also to the high compression ratios

involved The ignition system has been the subject of

intensive development and significant progress in system

reliability has been made

A preproduction prototype engine employing the TCCS process is

now being developed by the Hercules Division of White Motors

Corporation under contract to the US Army Tank Automotive

Command Southwest Research Inr)titute will conduct reliability

tests on the White-developed enGines when installed in Military

vehlcles

30 Small Volume Prechambcr Eng1nes (3-Valve Prechamber Engines Jet Ignition Engines Torch Ignition Engines)

31 General

A number of designs achieve charge stratification through

division of the combustion region into two adjacent chambers

The emissions reduction potentiampl for two types of dualshy

chamber engines has been demonstrated F1 rst ~ j n B desJgn

trad1t1on~JJy caJJld the nrreebrnber engine a 2m211 auxil1ary

167

or ignition chamber equipped w1th a spark plug communicates

with the much larger main combustion chamber located in the

space above the piston (Figure 3-1) The prechamber which

typically contains 5-15 of the total combustion volume

is supplied with a small quantity of fuel-rich ignitable

fuel-air mixture while a large quantity of very lean and

normally unignitable mixture is applied to the main chamber

above the piston Expansion of high temperature flame

products from the prechamber leads to ignition and burning

of the lean maj_n chamber fuel-a_r charge Ignitionmiddot and

combustion in the lean main chamber region are promoted both

by the high temperatures of prechamber gases and bythe

mixing that accompanies the jet-like motion of prechamber

products into the main chamber

I jl

I i j

I

Operation with lean overall mixtures tends to limit peak comshy

bustion temperatures thus minimizing the formation of nitric

oxide Further lean mixture combustion products contain

sufficient oxygen for complete oxidation of HC and CO in the

engine cylinder and exhaust system

It should be reemphasized here that a iraditional problem

with lean mixture engines has been low exhaust temperatures

which tend to quench HC oxidation reactions leading to

excessive emissions

Control of HC emissions to low levels requires a retarded or

slowly developing combustion process The consequent extenshy

sion of heat release j nto 1ate porttt)ns of the engtne cycle

168

tends to raise exhaust gas temperatures thus promoting

complete oxidation of hydrocarbons and carbon monoxide

32 Historical Background and Current Status

321 Early Developm9nt Objectives and Engine Def igns

The prechamber stratified charge engine has existed in various

forms for many years Early work by Ricardo 1 indicated that

the engine could perform very efficiently within a limited

range of carefully controlled operating conditions Both

fuel-injected and carbureted prechambcr engines have been

built A fuel-injected design Lnittally conceived by

Brodersen 11 was the subject of extensive study at the

University of Rochester for nearly a decade 12 13 Unforshy

tunately the University of Rochester work was undertaken prior

to widespread recognition of the automobile emissions problem

and as a consequence emission characteristics of the

Brodersen engine were not determined Another prechamber

engine receiving attention in the early 1960s is that conshy

ceived by R M Heintz 14 bull The objectives of this design

were reduced HC emissions incr0ased fuel economy and more

flexible fuel requirements

Experiments with a prechamber engine design called the torch

ignition enginen were reported n the USSR by Nilov 15

and later by Kerimov and Mekhtier 16 This designation

refers to the torchlike jet of hot comhust1on gases issuing

169

from the precombustion chamber upon j_gnj_ tion In a recent

publication 17 Varshaoski et al have presented emissions

data obtained with a torch ignition engine These data show

significant pollutant reductions relative to conventional

engines however their interpretation in terms of requireshy

ments based on the Federal emissions test procedure is not

clear

l

3 2 2 Current DeveloJ)ments

A carbureted middotthree-valve prechamber engine the Honda CVCC

system has received considerable recent attention as a

potential low emissions power plant 18 This system is

illustrated in Figure 3-2 Hondas current design employs a

conventional engine block and piston assembly Only_ the

cylinder head and fuel inlet system differ from current

automotive practice Each cylinder is equipped with a small

precombustion chamber communicating by means of an orifice

with the main combustion chambe situated above the piston lj

ij_ A small inlet valve is located in each precharnber Larger

inlet and exhaust valves typical of conventlonal automotive

practice are located in the main combustion chamber Proper

proportioning of fuel-air mixture between prechamber and

main chamber is achieved by a combination of throttle conshy

trol and appropriate inlet valve timing A relatively slow

and uniform burning process gjvjng rise to elevated combusshy

tion temperatures late in the expansion stroke and during

the exhaust procezs is achieved H1 gh tewperaturr--s in thin

part of the engine cycle ar-e necessary to promote complete

170

oxidation of HC and CO It si1ould be no~ed that these

elevated exhaust temperatures are necessarily obtained at

the expense of a fuel economy penalty

To reduce HC and CO emissions to required levels it has been

necessary for Honda to employ specially designed inlet and

exhaust systems Supply of extremely rich fuel-air mixtures

to the precombustion chambers requires extensive inlet manifold

heating to provide adequate fuel vaporization This is accomshy

plished with a heat exchange system between inlet and exhaust

streams

To promote maximum oxidation of HC and CO in the lean mixture

CVCC engine exhaust gases it has been necessary to conserve

as much exhaust heat as possible and also to increase exhaust

manifold residence time This has been done by using a relashy

tively large exhaust manifold fitted with an internal heat

shield or liner to minimize heat losses In additj_on the

exhaust ports are equipped with thin metallic liners to

minimize loss of heat from exhaust gases to the cylinder

head casting

Engines similar in concept to the Honda CVCC system are under

development by other companies including Ttyota and Nissan

in Japan and General Motors and Fo~d in the United States

Honda presently markets a CVCC-powered vehicle tn tTapan and

plans US introduction in 1975 Othe~ manufactur~rs

includlnr General Motors and Forgtd 1n thr U S havf~ stated

171

that CVCC-type engines could be manufactured for use in limited

numbers of vehicles by as early as 1977 or 1978

33 Emissions and Fuel Economywith CVCC-Type Engines

331 Recent Emissions Test Results

Results of emissions tests with the Honda engine have been very

promising The emissions levels shown in Table 3-I are typical

and demonstate that the Honda engine can meet statutory 1975-1976

HC and CO stindards and can approach the statutory 1976 NOx

standard 19 Of particular importance durability of this

system appears excellent as evidenced by the high mileage

emissions levels reported in Table 3-I Any deterioration of

l emissions after 50000 miles of engine operation was slight

and apparently insignificant

I Table 3-I

Honda Compound Vortex-Controlled Combustion-Powered Vehicle 1 Emissions

Fuel Economy

Emissions 2 mpg gMile 1972

HC 1975 FTP FTPco NOv

210 50000-Mile Car+ No 2034 Low Mileage Car 3 No 3652 018 212 221089

024 065 198 1976 Standards

213175 20o41 34 - -04o411977 Standards 34 - -

1Honda Civic vehicles 2 1975 CVS C-H procedure with 2000-lb inertia weight3Average of five tests aAverage of four tests

172

Recently the EPA has tested a larger vehicle conve~ted to the

Honda system 20 This vehicle a 1973 Chevrolet Impala with

a 350-CID V-8 engine was equipped with cylinder heads and

induction system built by Honda The vehicle met the present

1976 interim Federal emissions standards though NOx levels

were substantially higher than for the much lighter weight

Honda Civic vehicles

Results of development tests conducted by General Motors are

shown in Table 3-II 21 These tests involved a 5000-pound

Chevrolet Impala with stratified charge engine conversion

HC and CO emissions were below 1977 statutory limits while

NOx emissions ranged from 15 to 2 gmile Average CVS-CH

fuel ec9nomy was 112 miles per gallon

Table 3-II

Emissions and Fuel Economy for Chevrolet Impala Strmiddotatified

Charge Engine Conversion (Ref 21)

Test

Exhaust Emlssions

gMile 1 Fuel

Economy mpgHC co NOx

1 2 3 4 5

Average

020 026 020 029 0 18

023

25 29 31 32 28

29

17 15 19 1 6 19

17

108 117 114 109 111

112

1cvs-CH 5000-lb inertia weight

173

I

332 HC Control Has a Significant Impact on Fuel Economy

In Figure 3-3 fuel economy data for several levels of hydroshy

carbon emissions from QVCC-type stratified charge engines

are plotted 22 23 ~ 24 At the 1 gmile HC level stratified

charge engine fuel economy appears better than the average

fuel economy for 1973-74 production vehicles of equivalent

weight Reduction of HC emissions below the 1-gram level

necessitates lowered compression ratios andor retarded

ignition timing with a consequent loss of efficiencymiddot For

the light-weight (2000-pound) vehicles the O~ gmile IIC

emissions standard can be met with a fuel economy of 25 mpg

a level approximately equal to the average of 1973 producshy

tion vehicles in this weight class 8 For heavier cars the

HC emissions versus fuel economy trade-off appears less

favorable A fuel economy penalty of 10 relative to 1974

production vehicles in the 2750-pound weight class is

required to meet the statutory 04 gmile HC level

333 Effect of NOx Emissions Control on Fuel Economy

Data showing the effect of NOx emissions control appear in

Figure 3-~ 22 These data are based on modifications of a Honda

CVCC-powered Civic vehicle (2000-pound test weight) to meet

increasingly stringent NOx standards ranging from 12 gmile

to as low as 03 gmile For all tests HC and CO emissions

are within the statutory 1977 standards

NOx control as shown in Figure 3-4 has been effected by use

of exhaust gas recirculation 1n comb1nation w1th retarded

174

ignj_tion timing It is clear that control of rmx emissions

to levels below l to 1 5 gmile results in stgnificant fuel

economy penalties The penalty increases uniformly as NOx

emissions are reduced ~nd appears to be 25 or more as the

04 gmile NOx level is approached

It should be emphasized that the data of Fisure 3-4 apply

specifically to a 2000-pound vehicle With increased vehicle

weight NOx emissions control becomes more difficult and the

fuel economy penalty more severe The effect of vehicle

weight on NOx emissions is apparent when comparing the data

of Table 3-I for 2000-pound vehicles with that of Table 3-II

for a 5000-pound vehicle While HC and CO emissio~s for the

two vehicles are roughly comparable there is over a factor

of two difference in average NOx emissions

34 Fuel Requirements

To meet present and future US emissions control standards

compression ratio and maximum ignltion advance are limited

by HC emissions control rather than by the octane quality of

existing gasolines CVCC engines tuned to meet 1975 California

emissions standards appear to be easily satisfied with

presently available 91 RON commercial unleaded gasolines

CVCC engines are lead tolerant and have completed emissions

certification test programs using leaded gasolines However

with the low octane requirement of the CVCC engine as noted

above the economic benefits of lead antlknock compoundt ar-euromiddot

not realized

175

It is possible that fuel volatLLity characteristlcs may be of

importance in relation to vaporization within the high

temperature fuel-rich regions of the prechamber cup inlet

port and prechamber iQlet manifold However experimental

data on this question aomiddot not appear to be available at

present

~O Divided-Chamber Staged Combustion Engines (Large-Volume Prechamber Engines Fuel-Injected Blind Prechamber Engines)

41 General

Dual-chamber engines of a type often called divided-chamber

or large-volume prechamber engines employ a two-stage comshy

bustion process Here initial r~ich mixture combustion and

heat release (first stage of combustion) are followed by rapid

dilution of combustion products with relatively low temperature

air (second stage of combustion) The object of this engine

design is to effect the transitjon from overall rich combustion

products to overall lean products with sufficient speed that

time is not available for formation of significant quantities

of NO During the second low temperature lean stage of

combustion oxidation of HC and CO goes to completion

An experimental divided-chamber engine design that has been

built and tested is represented schematically in Figure ~-1 25 26

A dividing orifice (3) separates the primary combustion

chamber (1) from the secondary combustion chamber (2) which

includes the cylinder volume above the piston top A fuel

injector (4) supplies fuel to the primary chamber only

176

Injection timing is arranged such that fuel continuously

mixes with air entering the primary chamber during the

compression stroke At the end of compression as the

piston nears its top center position the primary chamber

contains an ignitable fuel-air mixture while the secondary

chamber adjacent to the piston top contains only air

Following ignition of the primary chamber mixture by a spark

plug (6) located near the dividing orifice high temperature

rich mixture combustion products expand rapidly into and mix

with the relatively cool air contained in the secondary

chamber The resulting dilution of combustion products with

attendant temperature reduction rapidly suppresses formation

of NO At the same time the presence of excess air in the

secondary chamber tends to promote complete oxidation of HC

and CO

42 Exhaust Emissions and Fuel Economy

Results of limited research conducted both by university and

industrial laboratories indicat~ that NOx reductions of as

much as 80-95 relative to conventional engines are possible

with the divided-chamber staged combustion process Typical

experimentally determined NOx emissions levels are presented

in Figure 4-2 27 Here NOx emissions for two different

divided-chamber configurations 8re compared with typical

emissions levels for conventional uncontrolled automobile

engines The volume ratio 8 appearing as a parameter in

Figure 4-2 represents the fraction of total combustion volume

contained in the primary chamber For a values approaching

I

i J_

177

1

05 or lower NOx emissions reach extremely low levels Howshy

ever maximum power output capability for a given engine size

decreases with decreasing 6 values Optimum primary chamber

volume must ultimately_represent a compromise between low

emissions levels and desired maximum power output

HC and particularly CO emissions from the divided-chamber

engine are substantially lower than eonventional engine

levels However further detailed work with combustion

chamber geometries and fuel injection systems will be necesshy

sary to fully evaluate the potential for reduction of these

emissions

i Recent tests by Ford Motor Company show that the large volume

prechamber engine may be capable of better HC emissions conshy

trol and fuel economy than their PROCO engine This is shown

by the laboratory engine test comparison of Table 4-I 19

Table 4-I

Single-Cylinder Low Emissions middot11 ~ _____En____g__~ne __middot _e_s_-_s_____

Engine

NO--X Reduction

Method

Em1ssions g1 hp-Hr

Fuel Economy

Lb1 hp-HrNOv HC- co

PROCO

Divided Chamber

PROCO

Divided Chamber

EGR

None

EGR

None

10 30

10 04

05 ~o

o J_o 75

130

25

l 1i bull 0

33

0377

0378

0383

0377

178

Fuel injection spray characteristics are critical to control

of HC emissions from this type of engine and Fords success

in this regard is probably due in part to use of the already

highly developed PROCO-gasoline injection system Figure 4-3

is a cutaway view of Fords adaptation of a 400-CID V-8 engine

to the divided-chamber system 2 e

Volkswagen (VW) has recently published results of a program

aimed at development of a large volume precharnber engine 29

In the Volkswagen adaptation the primary chamber which comshy

prises about 30 of the total clearance volume is fueled by a

direct timed injection system and auxiliary fuel for high

power output conditions is supplied to the cylinder region by

a carburetor

Table 4-II presents emissions data for both air-cooled and

water-cooled versions of VW s dtvided-middotchamber engine 3 0

Emissions levels while quite low do not meet the ultimate

1978 statutory US standards

179

Table 4-II

Volkswagen Jarge Volume _Jrechamber Er[ Lne Emissions

Exhaust Emissions

_ _gMile 1

___E_n_gi_n_e__t--H_C___c_o__N_O_x____E_ng__i_n_e_S_p_e_c_i_f_i_c_a_tmiddot_1_middoto_n_s__

20 50 09 841 compression ratio Air-Cooled 16-Liter

prechamber volume 28 of total clearance volume conventional exhaust manishyfold direct prechamber fuel injection

20-Liter 10 40 10 91 compression ratio Water-Cooled prechamber volume 28 of

total clearance volume simple exhaust manifold reactor direct prechamber fuel injection

1cvs c-H

Toyota also has experimented wlth ___a large volume prechamber

engine using direct prechamber fuel injection and has

reported emissions levels comparable to those of Table 4-II 31

43 Problem Areas

A number of major problems inherent in the large volume

prechamber engine remain to be 3olved I~ These problems include the following II

Fuel injection spray characteristics are critically

important to achieving acceptable HC emissions

The feasibility of producing asatisfactory injecshy

tion system hasnot been estab1ished

180

Combustion noise due to high turbulence levels and

hence high rates of heat release and pres[-ure rise

in the prechamber can be excessive It has been

shown that the-noise level can be modified through

careful chamber design and combustion event timing

If the engine is operated with prechamber fuel

injection as the sole fuel source maximum engine

power output is limited This might be overcome

by a~xiliary carburetion of the air inlet for maximum

power demand or possibly by turbocharging Either

approach adds to system complexity

The engine is charmiddotaeter1zed by low exhaust temperatures

typical of most lean mixture engines

References

1 Ricardo H R Recent Research Work on the Internal Combustion Engine 11 SAE Journal Vol 10 p 305-336 (1922)

2 Bishop I N and Simko A Society of Automotive Engineers Paper 680041 (1968)

3 Simko A Choma M A and Repco L L Society of Automotive Engineers Paper 720052 (1972)

4 Mitchell E Cobb JM and Frost R A Society of Automotive Engineers Paper 680042 (1968)

5 Mitchell E Alperstein M and Cobb JM Society of Automotive Engineers Paper 720051 (1972)

6 1975-77 Emission Control Program Status Report submitted to EPA by Ford Motor Company November 26 1973

181

if

7 consultant Report on Emissions Control of Engine Systems National Academy of Sciences Committee on Motor Vehicle Emissions Washington DC September 1974

8 Austin T C and Hellman K H Society of Automotive Engineers Paper 730790 (1973)

9 See Ref 7

10 Alperstein M Schafer G H and Villforth F J Iiil SAE Paper 740563 (1974)

11 US Patent No 2615437 and No 2690741 Method of Operating Internal Combustion Engines Neil O Broderson Rochester New York

12 Conta L~ D and Pandeli American Society of Mechanical Engineers Paper 59-SA-25 (1959)

13 Canta L D and Pandeli American Society of Mechanical Engineers Paper 60-WA-314 (1960)

14 US Patent No 2884913 0 Internal Combustion Engine R Mi Heintz i

15 Nilov N A Automobilnaya Promyshlennost No 8 (1958)

l 16 Kerimov N A and Metehtiev R I Automobilnoya Promyshlennost No 1 p8-11 (1967)

17 Varshaoski I L Konev B F and Klatskin V B Automobilnaya Promyshlennost No 4 (1970)

18 An Evaluation of Three Honda Compound Vortex Controlled Combustion (CVCC) Powered Vehicles Report B-11 issued by Test and Evaluation Branch Environmental Protection Agency December 1972

19 Automotive Spark Ignition Engine Emission Control Systems to Meet Requirements of the 1970 Clean Air Amendments report of the Emissions Control Systems Panel to the Committee on Motor Vehicle Emissions National Academy of Sciences May 1973

20 An Evaluation of a 300-CID Compound Vortex Controlled Combustion (CVCC) Powered Chevrolet Impala Report 74-13 DWP issued by Test and Evaluation Branch Environmental Protection Agency October 1973

21 See Ref 7

22 See Ref 7

23 See Ref 7

24 See Ref 7

182

25 Newhall H K and El-Messiri I A Combustion and Flame 14 p 155-158 (1970)

26 Newhall H K and El-Messiri I A Society of Automotive Engineers Transaction Ford 78 Paper 700491 (1970)

27 El-Messiri I A and Newhall H K Proc Intersociety Energy Conversion Engineering Conference p 63 (1971)

28 See Ref 7

29 Decker G and Brandstetter W MTZ Motortechnische Zeitschrift Vol 34 No 10 p 317-322 (1973)

30 See Ref 7

31 See Ref 7

183

Fig 2-1 FORD PROCO ENGINE

l

Ford Proco Engine Fuel Economy and Emissions _ 15 _ f--1

00 +

I ~ x X gt( X _ x A 7- ~ X x~ ~c - l4catalyst Feed u NOx vs ruel Econ with 1 C0-71 CJ) 14 x x Ynn H( RP c tr ir-t irm vltgtZ G I HC - C0-127 _ A txcessve c

13 Approx W EG R

~ C~~r 351 CID 5000 Lb Inertia Weight

Q 21 A L 0 u w II _j

LJ =gt LL

10

35i CD 4500 Lb Inertia Weight

~ 1974 Production Average Fuel Economy

4 soo _b r-r-r-----z~lt_~~---7--_~--r--1r-7-r1--~-rz7-w~~

150 0 0 Lb PU221ufrac122-1 I

LO 20 30

NOx EMISSIONS-GMSMILE (CVS-CH) Revised216174

0

HKN 71074

Fig 2-2

l

~___-~ ~--=---~ ~=---__---~1 f-=-----1__middot-_~J ~-----------1 ~bull-=-=- (-~-~ LJii-ZJj ~ ~~-~ ~~ -__c~~ 1--~~ ~----~--1 ---------s___-c--1 ~~~-~~~bull r~~-~--middot1 ____c__ J~ p- ~

Texaco TCCS Engine

Shrouded Intake Valve

~ Intakemiddot r~ )p__-- Fuel Nozzle Fuel Nozzte Port ~ -- -yen -_~

X f -J J ( ~1 I --- ~ f middotmiddotj_Ja 1(~-~_ frff 1-Cylinderv~ v_ r--L~ I (~~)J ~- Intake 1 - ------L- middotmiddot - middotmiddot -1 H0 ad middot --- - -- 1 Po rt I 1 I ~~ ) ~ ~ ~~~ -A- I ------

- I _ ---_ ~ P1ston-mgt-lt_ffrac12 T_77~~~--1 i- r_-~J N

- ~- i~-L - _ _ - IExhaust - - I ~ - 1-_ r- bullsect ~ ----lt_ ~ I PortJ~bJ lt 7A--7~ ~1 ~j --~ ~ yl ind er

-__~lli- klmiddot ~ro v_t_gt11J1bull Bti Or K__ - middot ~

I t--tL pgt-- Ultmiddot middot- - Spark Plugr- -1 --U2middot- ~-~

LHorizont al Projections of Nozzle and Spark Plug Centerlines

Fig 2-3 i--1 00 U1

---~---~-~ -------c- --~--- 7middot-r---c-- ~- -~~~==---~~~~~- srsr RZIIEF7 11t111-~-----==-----=-~--~-~~---c=rmiddot=

OPEN CHAMBER TYPE STRATI Fl ED CHARGE ENGINE i-shyCj

DIRECTIONAl~Fsw7 Q

NOZZLE P

I

~J~treg lt-_(__(lt-(11

c_-- _7- -

SPARK PLUG_ l 1__- -_ - l --_ ~ ----__ lt_ lt_ -- --

ltlt_I_--- _

~ gt - _____- -- --~ ~-l_- 1_~ -~- ~ ------

~~~ r_I FUEL SPRAY 2 FUEL-AIR MIXING ZONE ~- _ -------

FLAME FRONT AREA 4 COMBUSTION PRODUCTS

TCCS COMBUSTION SYSTEM

Fig 2-4

3

----==-----~ l~~----bulli r-~ ~-----=-- 1 ~~ ~ -~ ~~ ___-_=gt---l p--- --=-=-_-__71-~-~~ 1-0-- --=---=-- 4 L--_-_-~ P--- ~

25

-c u

f

Cl) 24 gt u _

tgt 23a ~

I

gt-~ 220 2 0 u w 21 _J

lJJ gt LL

2

Texaco TCCS Powered Cricket Vehicle

Max Econ Setting gt A L07 HC

141 CID JQf CR 084 CO 2500 Lb Inertia Wgt

50-so Retard_ 0_73 HC

12 co 051 HC ~ 061 HC

085COA 064CO Retard+ ESPRetard+

EGR

036 HC ~ 115 co Retard +ESP+ EGR

04 06 08 10 12 14 16 18 20 NOx EMISSIONS-GMSMILE (CVS-CH) HtltN1110114

I- 00 -JFig 2-5

-~ ~=- ~ - -i______c_J ~-====c= wr=- ~-~ p--w~~~ rr w -

25

-c u

I

(f)

gt u-lt a_

2

gt-I 20

~ 0 z 0 u LLI

_J

w tJ_

15

I- CJ) CJ)

Turbocharged Texaco TCCS Ml51 Vehicle

Max Econ Adjustment_ HC-3J catalyst Feed C0-70

141 CID 10~1 CR 2750 Inertia Weight 8deg Retard ~

~bull HC-3middot2 catalyst Feed ~~ _ C0-64

_ 5deg Retard HC-0 30 8degRetard LowEGV bullco-11 ~bull HC-3middot6 catalyst Feed WIW21

Med EGR C0-67 1974 Production 33 Average Fuel Economy ~

COmiddoti05 (2750Lb)

I

bull HC-035 co- 141 13deg Retard High EGR

04 10 20 NOx EMISSIONS -GMSMILE (CVS-CH) ~~ts~b~~~74

Fig 2-6

189

Fig 3-1

PRECHAMBER TYPE STRATIFIED CHARGE ENGINE

r Inlet

(Fuel-lean Mixture )

I 0 I

Spark -Prechamber (Fuel-rich mixture)

-Main Chamber

1] HON DA CVCC ENGINE CONCEPT

190

Fig 3-2 Honda CVCC Engine

28 -l u

1

UJ 26 -gt u-(9 CL 24 2-

f

gtshy0gt

22 z ~ _)

u w

20 _J

w ~ LL

18

J= ---- 4 --~~-_----a ~~ _-_bull --~~ 1~~1 ltiil~I ~ ~-r~ ~ -~ ~-~ ~J~-iii-1 ~~1 s _-_ __-

Fuel Economy vs HC Emissions for 3-Valve Prechamber Engines

e NOx-14 15 Liter

bull Honda CVCC 2000 LbsNOx - 12 A Datsun NVCCbull15 Liter

bull ~JOx -09 A 2500 Lbs J LL 1ter NOv -15

2750 Lbs -NOx -17

- I AiJOx -12

0 02 04 06 08 LO 0HYDROCARBON EMiSSlmiddotONS - Glv1 I MILE (CVS-CH) I-

Fig 3-3

J--1

1--Fuel Economy vs NOx Emissions IO N

-- for Honda CVCC Powered Vehiclesr 26 u

l VHc-023 U1 gt umiddot 24_-__

(_IJ o_

~ 22 l

gt-5~-0 z 20 C0-200 u A HC-033w I co -3o_j

_A HC-029w 18 J I C0-27 LL

_ HC-025

HC-017 co -2-3

C0-22

0 -- 02 04 06middot 08 10 12 NOx Ef11SSIONS -GlviS MILE (CVS-CH)

Fig 3-4 middot

I

I

i93

J J

Fig 4-1 Divided Chamber Engine

middot(4) Fuel Injector

1

f J

f ff

f

~ Ii

I f

i

I f ] [

~~

0 0 0 0

i ~ I

1jl

194

E Cl 0

C QJ

CJl 0 _

-1-

z

0

Vl (lJ

-0

X 0

-t-J

V1 ro c X

LLI

Fig ~-2

COMPARISON OF CONVENTIONAL AND DIVIDED COMBUSTION CHAMBER NOx EMISSIONS

5000 MBT Ignition Timing Wide Open Ttl rattle

4000 Conventional Charnber

3000

J = fraction of Total Combustion 2000 Volume in Primary Ct1arnber

Divided Chamber 13 = 0 85

1000

Divided Chamber fo = 0 52

05 06 0 7 08 09 10 11

O~erall Fuel-Air Equivalence Ratio

195

196

AIRBORNE SURVEYS IN URBAN AIR BASINS IMPLICATIONS FOR MODEL DEVELOPMENT

by

Donald L Blumenthal Manager of Program Development

Meteorology Research Inc Altadena California 91001

middotI would like to make several points today First ozonemiddotis basically

a regional long-range problem There is a lot of long range ozone transshy

port and this transport is a normal occurrence The second point is that

ozone is stable in the absence of scavengers Junge mentions in his book

that the residence time of ozone in the troposphere is on the order of a

month Third vertical variations in concentration and ventilation rate are i very important in modeling atmospheres such as Los Angeles Layers aloft

are ventilated down to the surface on occasion and surface pollutants are

ventilated up mountain slopes as Jim Edinger has pointed out before and

often ventilated out of the basin in upper winds Fourth the day to day

carry over of pollutants from one day to the next is a very important considshy

eration in the Los Angeles Basin Finally there is a definite background

level of ozone The geophysical literature says its about O 02 to O 03 ppm (

in various parts of the world Weve seen data varying from 003 to 005 ppm

The difference may be due to calibration differences In any case numbers

like 005 are pretty substantial background levels for ozone

I am going to illustrate the points listed above with some data from

Los Angeles Basin The data were collected during a two-year study funded

by the Air Resources Board some of the analyses were funded by EPA The

study examined the three dimensional distribution of pollutants in the Los

Angeles Basin using airborne sampling systems Coinvestigators on the

project were Dr Ted Smith and Warren White of Meteorology Research Inc (MRI)

197

The first slide shows one of the aircraft we used Its a Cessna 205

which had sampling inlets on the side of the aircraft Figure 2 shows the

instrument system on the inside of the aircraft We were measuring nitrogen

oxides ozone scattering coefficient with a nephelometer condensation nuclei

carbon monoxide and meteorological parameters such as temperature humidity

turbulance Altitude and position were also measured

Figure 4 shows that the typical sampling pattern was a series of spirals

from the top of the mixing layer over an airport virtually to ground level

then we would climb up to the next point on the route and spiral down again

We had three routes (A B C Figure 3) that we would fly We had two airshy

craft and we would fly two of these three routes three times a day any

given day that we could The day I will be talking about September 25~ 1973

we flew what was called the Riverside route (C) and the Los Angeles route

(A) The 25th of July 1973 you might remember was the day before the

federal office buildings were closed in the area here because of smog

Figure 5 shows the surface streamlines at 0300 Pacific Standard Time

about 4 oclock in the morning daylight time on July 25 This streamline

analysis points out the morning stagnation conditions which are a very normal

occurrence in the Los Angeles Basin You start out with very light winds

quite variable maybe a slight off shore flow early in the morning On this

particular day this kind of situation extended well into midday The sea

breeze did not really pick up until up around noon When you have this kind

of a situation and a low radiation inversion at night you have a

long period of accumulation of pollutants all over the Basin espt~cialJy

in the prime source area the southwest portion of the Basin

198

I

Figure 6 shows the streamline pattern at 1600--400 cclock in the

afternoon same day sea breezes develop and with them a transport pattern

that carries pollutants up to the northeast and out toward the eastern por-

tion of the Basin This is a very regular pattern which we see day after l middot

day On July 25 1973 it was a little bit exaggerated The sea breeze was

held off for awhile started a bit late and so there was a very long period

of accumulation in the southwest area and then transport across the Basin

Figure 7 is an average streamline pattern at 1600 PacHic Daylight Time

on low inversion days for August 1970 It is included to show that the pattern

shown before is very typical Flow starts in the western portion of the

Basin and goes right across to the eastern portion This is using surface

data There is a very high average wind velocity in Ontario about 13 m iles

per hour and 23 mph in Riverside This is the average for the whole month

of August at 1600 PDT on low inversion days There is a considerable amount

of transport across the Basin starting relatively slowly in the morning and

accelerating in the afternoon

Figure 8 shows a verticle cross section of the scattering coefficient

The darker areas indicate higher levels of particulates Scattering coefficshy

ient is inversely proportional to visibility In the crosshatched area

visibility is less than about 3 miles In plotting altitude versus distance

inland from the coast you have Santa Monica (SMO) on the coast El Monte (EMT)

Pomona (BRA) Rialto (RIA) Redlands (RED) The lower broken line is surface

ground level The heavy dashed line is the base of the subsidence inversion

that occurred on the two days during this episode The middle line is the

base of the marine inversion There is a large area over in the western

portion of the Basin where emissions accumulate for much of the day At

199

midday the sea breeze has just started ventilating the Santa Monica area

The layer between the inversions is a layer aloft which is fairly well separshy

ated from the surface layer Ozone concentrations for instance in the

layer aloft were on the order of 04 05 ppm using the ARB calibration

method Down in the surface layer they were quite a bit lower in the mornshy

ing due to scavenging

Figure 9 shows that by afternoon the sea breeze starts and you get

kind of a clean air front Sea breeze starts ventilating the whole Basin

the stuff that was over in the west is transported eastward and at approxishy

mately Brackett (BRA) at 1700 PDT there is a clean air front The high conshy

centrations that were over Los Angeles earlier are now centered near Upland

(CAB) The numbers shown over CAB are data taken from a vertical profile

spiral over Upland at about 1600 That turns out to be the time when there

was the worst ozone concentration of the day in the Basin and it did occur

at Upland It could well be a result of the very polluted mass from the

western Basin being transported over the Upland area The layer aloft has

been a bit undercut by the sea breeze and some of the polluted mass has been

around possibly as long as the night before There has been very little

transport in the area aloft ozone concentrations are still very high

Figure 10 shows a trajectory analysis of the air arriving at Upland at

1600 since that was the worst time of the day at Upland We developed a

trajectory envelope using surface wind data and winds aloft so the air

arriving at Upland at 1600 started out somewhere back within this envelope

for example at 1130 PDT We did not go earlier than 1130 because the winds

were pretty much light and variable before that The air that arrives at

Upland at 1600 has been over the western portion of the Basin for much of

200

the morning and q~ite a bit of the evening before Thus there is

a very long period of accumulation and then a transport a pulsing effect

where you have pollutants moved across the Basin

Figure 11 is an isopleth map of surface ozone concentrations Again all

data are corrected to agree with the ARB calibration method Again you can

see that for the hours between 1600 and 1700 using surface data the Upland

area has the highest surface ozone concentrations about 063 ppm The western

area has been well ventilated by the sea breezes and it is cleaned out

The transport is actually pretty much perpendicular to the isopleth line

just about like that

Figure 12 is a vertical profile taken over Upland Cable Airportat

roughly the time of maximum ozone concentration 1636 PDT We are plotting

pollutant concentration on the x-axis versus altitude in meters (since it was

done for an EPA report) Surface leveJ at Upland is a little over 400 meters

the Z line is ozone Ozone concentration within the surface mixing layer

is pegged on the instrument at somewhat above 05 ppm Above the surface

mixing layer it drops off considerably and eventually get down to background

The T line is temperature and you ean see the subsidence inversion

on this day is very nicely documented here and provides a very strong trap

in that area The B line is the scattering coefficient inversely proporshy

tional to visibility Within the surface mixing layer visibility is on the

order of 3 miles or less while up above the surface mixing layer just a few

hundred feet difference visibilities get up to 60 or 80 miles The X is

condensation nuclei the measure of the very fine particles below about 010

micron It is a measure of quite fresh emissions If you have a high condenshy

sation nuclei count there are very fresh combustion emissions If you have

I

201

an aged air mass the condensation nuclei coagulate and the count decreases

considerably You can see that there are still some fresh emissions within

this surface layer as well But up above the surface mixing layer all the

pollutant indicators decrease considerably

Figure 13 is the same type of vertical profile taken over El Monte

which is on the western side of the sea breeze front The sea breeze front

has passed El Monte at this time almost 1700 PDT and again there are

distinct differences between the mass below the mixing layer within the sea

breeze front (below 400 meters) the marine inversion (400 to 800 meters) and

the subsidence inversion The subsidence inversion occurs at about 800 meters

and there is an old layer of very polluted stuff aloft The surface concenshy

trations are lower because of the ventilation by the sea breeze Condensashy

tion nuclei count (X line) within the surface layer is quite high There

are still fresh emissions in the El Monte area The 11 Z line is ozone

about 02 ppm within the surface layer (200 m) but it is 05 ppm up above

the surface mixing layer The scattering coefficient (B line) is very

similar it is lower at the surface and increases to a visibility equivalent

of less than 3 miles above the surface mixing layer The condensation nuclei

count is high in the lower portion of this (eg at 600 m) hut decreases conshy

siderably above This portion of the upper layer (600 m) has been around

at least all morning and condensation nuclei have been scattered from the

area The portion of the upper layer below 600 m has probably just recently

been undercut by the sea breeze and there are still some condensation nuclei

left in it

Figure 14 illustrates a different method of looking at the flushing

problems in the Basin We have tried to develop an objective criteria based

on ground level ozone to show the cleansing of the basin using the time of

202

arrival of clean air We determine the time when the ozone concentrations

drop by a factor of two at any given point The 1600 line means that between

1500 and 1700 the ozone concentration at that point dropped a factor of two

This sort of isopleth chart of when the clean air arrives agrees quite well

with the trajectory analyses although the numbers are a little bit behind

the trajectory analyses for the polluted air Figure 14 again shows the

transport process that takes place across the Basin which is ventilated from

west to east At 1900 some of the fresh ocean air finally gets out to

Redlands

In Figure 15 in order to put this whole flux problem into some perspecshy

tive we looked at the numbers the actual amount of ozone flux across the

basin We calculated the mean trajectory from Torrance towards Redlands

using the surface and upper air data We looked at the flux from the western

basin to the eastern basin basically from Los Angeles and Orange Counties to

Riverside and San Bernardino Counties This is a calculation made at 1700 PDT

We used the winds aloft from Chino as well as the vertical profiles taken at

Pomona and Corona Averaging the ozone concentration throughout the mixing

layer and multiplying by an average wind speed we arrive at a number of 185

metric tons per hour being transported directly from one side of the Basin

to the other If you look at this in terms of actual concentration in the

eastern Basin and assume that the flow was constant for about an hour it

is eno_ugh to fill up the box shown in Figure 15 to 025 ppm ozone which

exceeds the air quality standard by a factor of three (using the ARB calibrashy

tion method) Thus there is a very significant transport of ozone or ozone

precursors from one portion of the Basin to the other side of the Basin One

thing to mention though is that the concentration would not be kept up on a

203

steady state basis because the transport is a result of the pulsing effect

I Illentioned earlier There is a lot of accumulati6n in the western Basin

and these accumulated pollutants are then transported across the Basin This

kind of transport did take place in a couple hours because we also have

measurements from 1500 PDT which give us similar flux numbers

Figure 16 is a trajectory envelope similar to Figure 10 calculated for

Upland at 1600 for the air arriving at Redlands about 600 oclock in the

afternoon I wanted to include this trajectory envelope to show that the

problem is not really simple You cannot say that the air at Redlands came

from Long Beach per se The air at Redlands if you look at the whole

envelope of possible trajectories using upper air data as well as surface

data could have come from anywhere between Downtown Los Angeles and over

the Pacific Ocean south of Long Beach

Another thing to recognize is that the wind actually changes direction

slightly as you go up and down through the mixing layer and the mixing layer

is exactly what it implies There is mixing within the mixing layer so if

you begin with a parcel of air near the surface this parcel may move to the

top of the mixing layer and go one direction for awhile it then may go back

down to the bottom of the mixing layer and move in another direction for

awhile The ratio of the length scales indicata3mixing layer depths of 1500

or 2000 ft and distances on the order of 70 miles This makes it very

difficult for tetroons to follow an air trajectory because they do not go

up and down They stay at one altitude and in one wind regime and yet the

wind regimes are different at different altitudes and the air is continually

mixed up and down through this layer You can often see this on time lapse

photographs

204

The question is where does the pollutant mass go after Redlands Figure

17 is a repeat of Jim Pitts slide from yesterday and it is data for the

same day that we did our analysis It shows the ozone peaks starting at

Pomona and Riverside and on July 25 1973 eventually getting out to Palm

Springs so there is quite a bit of long-range transport The ozone is

stable at 8 00 or 9 00 oclock at night There still are ozone concenshy

trations of 02 ppm it hasnt dissipated even at the surface Ozone does

dilute as the mass moves Other calculations we did were integrations

through the mixing layer of various pollutants such as ozone and CO along

with trajectories that we measured Th~se integrations show just what the

ground data show in Figure 17 The concentrations increase through the western

portion of the Basin and then show a decrease through the eastern portion

of the Basin CO tends to decrease faster than the ozone indicating a

continued production of ozone further east

Figure 18 is a streamline chart on a larger area map for the 16th of

August 1973 It shows the typical streamline patterns that occur for

ventilation from the Basin By mid-afternoon there is flow out through the

major passes to the north and towards Palm Springs (PSP) On this particushy

lar day we had data from Arrowhead showing that the air mass from the Basin

does indeed get up there

Figure 19 shows a vertical profile over Arrowhead early in the morning

16 August 1973 at a time when there was a north wind Ozone level was

about 005 ppm the scattering coefficient was quite low on the order of

probably 60 miles visibility or so Figure 20 is a vertical profile again

over Arrowhead late that afternoon when the winds had switched There is a

flow from the Los Angeles Basin into the Arrowhead area thus one sees a

205

vertical profile that shows a distinct increase near the surface in both the

ozone and the scattering coefficient and in the condensation nuclei Ahove

that you have fairly clean air The top of the polluted level is just about

the top of the mixing level over the Basin

I want to leave the transport now and discuss the complicated vertical

structure that can occur If you want to try to model something try this

one for instance Figure 21 is a vertical profile over Brackett Airport

Pomona about 830 in the morning on 26 July 1973 which is the day after

the episode shown earlier A bit of interpretation shows how complicated

th is can be If one looks at the temperature profile it would be very

difficult to pick out a mixing layer theres a little inversion here another

inversion there several more up here After looking at hundreds of these

profiles though you can start interpreting them What is happening is that

there is a surface mixing layer at about 500 m In this layer there is a

high condensation nuclei (X line) count due to morning traffic The San

Bernardino freeway is quite close to Brackett there is a relatively high

nitrogen oxide count about 02 ppm and the b-scat is fairly high Ozone (Z)

within the surface layer however at this time is quite low The layer beshy

tween 500 m and 700 rn turns out to be the Fontana complex plume Note the

very high b-scat level it is below 3 miles visibility the plume is very

visible especially at this time of the morning when it is fairly stab]e

There is a high nitrogen oxide level (800 m) a high condensation nuclei

level and again a deficit of ozone Above this layer (800 m) you have stuff

that has been left all night very low condensation nuclei indicating a very

aged air mass ozone concentrations about 016 ppm b-scat of about 04 It

has been around all night and not yet had a chance to mix down within the

206

surface layer In fact one good way of determining the surface mixing layer

early in the morning and at night is to look for the ozone deficit Another

thing to mention is that wind reversals occurred for each of these three

layers The winds were fairly light and westerly at the surface slightly

easterly in the 500 m 700 m layer and westerly above 800 m There is a

complicated situation early in the morning but the main problem is that by

the middle of the day there is good surface heating and the pollutants have

all been entrained and mixed down to the ground so in order to modeI what

happens on the second or third day of an episode you must be able to look

at both old pollutants as well as fresh emissions And you need to account

r for ozone that is actually transported down to the surface from layers aloft l

The next slide is a photograph (not included) which is another e xample

of some layers aloft This is due to upslope flow as explained by Jim Edinger

in his publications The mountains are heated during the day in turn heating

the air and making it buoyant there is upslope flow to a point where the

heating cannot overcome the subsidence inversion and the stuff comes right

out from the mountains and spreads out over the Basin The pollutants can

stay up there if the winds aloft are very light and on the subsequent day

will he re-entrained to the surface On the other hand if there are winds

aloft different from those in the surface mixing layer or the wind velocity

aloft is high there can be a very substantial ventilation process for the

Basin Pollutants can be ventilated up the slope and blown away in the upper

winds In the case of the entire July 25th episode winds aloft were quite

light and these upper layers remained

Figure 22 is a vertical profile of one of those upslope flow conditions

in the same location shown in the photograph but on a different day Again

207

there is a relatively high surface concentration of about 03 ppm of ozone

(Z line) a layer of clean air between 900 to 1100 m and then high concenshy

trations of ozone again above 1100 m It has gone up the slopes of the

mountains and then come back out Concentrations in the 1100 to 1300 m area

are just slightly lower than they were at 600 to 800 m area Notice however

that the condensation nuclei count (X line) is quite a bit lower mainly

because the stuff is much more aged above the 1000 m level than it is down

below 900 m

Figure 23 shows the stability of ozone the fact that it can stay around

all night long This is a vertical profile taken over Riverside about 2200

PDT 1000 oclock at night Above the surface mixing layer (600 m) there

are ozone concentrations of about 0 15 ppm (Z line) Within the surface

mixing layer (below 500 m) ozone is completely scavenged decreasing to

zero The nitrogen oxides within this surface layer are being contained and

are around 01 ppm from fresh emissions that occurred during the evening

Condensation nuclei near the surface are very high The temperature profile

is very stable You have a surface based radiation inversion which is a

little strange looking for a radiation inversion~ nevertheless it is quite

stable There is a definite restriction of the mixing--a very difficult

time getting air from below 500 m to above 500 m The ozone that exists in

the 700 m range is in air where the reactions have virtually gone to compleshy

tion and is very stable All the profiles on this night changed very little

the ozone peak stays there High concentrations stay around

Figure 24 is a cross section across theurban plume of the City of St

Louis I wanted to show that this occurrence is not limited to Los Angeles

We have seen ozone formation and transport in other urban plumes These data

l

208

were taken during a project sponsored by EPA in conjunction with R Husar of

Washington University and William Wilson of EPA The dark line on this is

the ozone concentration across the urban plume perpendicular to plume The

dashed line is the scattering coefficient The power plant plume is parallel

to the urban plume The data on the left were taken 35 kilometers down wind

about 1100 oclock in the morning The ozone concentration increases slightly

to 005 ppm in the urban plume there is a deficit of o in the power plant plume3

In the same urban plume same conditions 1500 CDT two hours later further

downwind there has been substantial increase in the ozone in the urban plume

itself The b-scat is very similar to what it was before but the ozone is

now increased quite substantially except in the power plant plume where

there is a strong deficit of ozone due to scavenging by nitrogen oxides So

the formation and transport of ozone and ozone precursors in urban plumes is

a regular occurrence that happens in more places than Los Angeles and as Bob

Neligan showed this morning it can happen over quite a bit longer distances

than we are showing here

To summarize the conclusions as they affect model development first

once ozone is formed in the absence of scavengers ozone is a very stable

compound It remains for long periods of time It can he transported for

very long distances Ozone is a regional problem which cannot be controlled

on a local basis To have effective ozone control middotone must have a regional

control strategy and probably regional type air pollution districts

A second conclusion is that the vertical distribution of pollutants can

be highly complex and models have to include more than just a simple wellshy

mixed surface layer

209

A third conclusion is that layers aloft can persist over night and can

be re-entrained within the surface mixing layer on subsequent days models

should be able to account for old pollution as well as fresh emissions Also

pollutant accumulation and transport can have distinct diurnal patterns that

are strongly dependent on the meteorology Models should be time dependent

and should start at the beginning of the accumulation period In other words

models ought to be able to run for 24 or 48 hours if they have to In this

case in Los Angeles there is often an accumulation of pollutants which starts

in one portion of the Basin at midnight and continues through the next mornshy

ing even before it starts to be transported

As far as recommendations go in many areas a lot of ambient data has

been collected and in some cases the data are actually ahead of some of the

models so I think a research program is needed in developing models that

will account for this vertical structure and the day to day carry over and

the models need to be extended to cover longer distances In addition more

smog chamber work is going to be needed in looking at the effects of carry

over and mixing old pollutants with fresh emissions How people go about

this I leave to the modelers and the smog chamber people They know more

about that than I do

I

210

I

~ INVERTER

AUDIO TAPE

MONIT0R

MONITOR OBSERVER SEAT

MON ITOR

NEPHELOMETFR FLfCTRONICS

j DIGITAL DATA LOGGER

CONDENSATION

VOR DME NEPHELOMETER TUBE

JUNCTION middoteox ASSORTED POWER

AIRBORNE

TEMPERATURE TURBULENCE

middot HUMIDITY

ALTITUDE BOX

__

middotE=-middot RECORDER ----r----------

NUCLEI KJNITOR

CONVERTER

SUPPLIES

INSTRUMENT PACKAGE (

lCO

03

Ndeg

-

-----NEPHELOMETER

BLOWER

Figure 2 Instrumentation Layout for Cessna 205

211

bullubullbullbullbull

Figure 3 Airborne Sampling Routes in the Los Angeles Basin

Figure 4 Vertie al Profile Flight Path

~-~ r~i ~~1 -- ~ ~ ~2-1~ LJ-----~ r~~ ~~ t~~--l

~ ALM l

0 RIA

ec 8v

M

~ Afo

-o

M 0

~IV

ltgt

IN J--1 N

SCALE II fi M I j_ ES 0 3 4 5 =-JSEJ--J~ _middot ~middot- - =- =

I

~

M

N~J

Figure 5 SURFACE STREAMLINE ANALYSIS - 0300 PST 25 July 1973

~~~ ~~-- cp1FJ=D -~~

~ 1

~ ~ 8c

8v

~25

PACIFIC OCEAN

diams Tt

0

9 I 4 5 10 I- m p H - -middotmiddot u 4H__8 middott_

D i6 J4 k W~D SPED llaquotl SNA NJ ~1

SCALE m ICtt84bullmh R v1s1a1L1n (mil 6 ~ CONTOURS REPRESENT

-- 10ml 16km (~() bull ~ ) ~ - 000 ft 3C5

Figure 6 S_cJRFACE WIND STREAMLINES - l 600 PDT JULY 2 S I 8 7 3

l - ~---i ~-=-___-----c---it~~-~~ r----=------1 ~-~~--cpc---_t__A --~ ---llil

~_ - ~-l-cL

34bull vi~-dff

bullbullbullbull bull ~ bull -1 bullbull - -_- L bull-J bull ~bull-bull-ii------~ bullmiddot r_ -~- ~ bullI ~_ bull bull bullbull bull I bull _ - bull -~-~ middotbullbullbull ~ ~ --middot -~- bullbullmiddot ~v ) ~ - -__rl v middotmiddot - 1- ~ -- middot middotmiddot - 1 91 frac12 - ~- lt( middot K i - middot bull - middot - bullmiddot~~-~lJ) obullmiddot~ ~-f- _J_~---Smiddot~middot-~----~~~---gt_middotfY-_middot-~middot --middot-~-~----fJ_middot- middotmiddotbullmiddot u-- bullmiddot ~ ~ -middot L~ bullbull

~bullbullbullbull bullbull l_bull bull bullbullbull EW bullbullbullbull-- ~ __bull f f - middotbull - J middot f bull S bull I ~ -r --

_ bullbull bull- _ bullbull-bull ~ ~ bull bull bull bull I bull bull bull bull bull bull gt - bull middotbulliJ -bull I bull bull _1 bullJ C-- ~-middot _ bull bullbull bullbull bull _____ ~ ~ l _ middot q bull 1 -middot middot ~~middot middot middotbull_ J ~gt - J bull-bullbullbullbull ) _ -middotmiddotbullmiddot J ~middotmiddotmiddot -bullmiddotbull fmiddot 7middot _middotmiddotmiddot bullmiddot(middot Ii~ middotmiddot~_--~middot 1middot__middotmiddotmiddotmiddot middot- gt_ -~ -~-- Imiddotbullmiddotbullbull_ -

- ()_I (w--_ bullbull__(i- bullOmiddotbull bull middotbull -bull-_jlJ middot bull lt 1(middot t gt bull - ~ rbull I bull middot middot- bull41-bull l~r v-middot~- middot middot middot bull_ - middotmiddot ~Jtj (middot~ ~middoti middot middot middot middot middot ~- ~ -tmiddot~ I - middot middot_- ~ - -~ middot_ _- ~bull - _ ~) i bull bullbull bull- middot_ bull middotbull __ ( bull 11bull bull ~ampmiddot ~ l bull bullQ bull - -1 bull JY1 bullbull ~ or bullbullbullbullbull bullbull-bullbull _ ~ - bull bull-bullbullbull middotimiddot middot 91 bull t bull - - tfaw lJ--r- bull bull _ bull middot- - l

f ~~middot--~ middotmiddott ~ltrgtmiddotmiddotJmiddot_bull - ~ - __ middot- LOS ANGELES BASIN - LOW LEVEL -__ jmiddot l-gt bull - bull J iI bullbull bull bull bull _ bullbull _ Jmiddot middotL~_1 middot middot bullbullmiddot ( C middot INVERSION MEAN WIND FLOW _ J

lmiddot - f bullbullbull~ - f 1bullbullbull _ ~)- bull middot- _---_- 7f-~bull~ REGIME _F_~ AUG_UST_~ ~600 P~--- l

-__L-~bull --ncmiddotbull~~-j--bullmiddot~bullmiddot_-bull _fJibullmiddot Imiddotmiddotmiddot-bullmiddot- bullbull ~ bullbullbullbullmiddotmiddotmiddot~middotbull ___ bullJ_ _middot~0))deg bullt t1yensmiddotmiddot ( middot middotmiddot middot middot ~ middot lbullbull1 t_c0 bull -middot---l lt ~middot~- deg bullbull --= bull bull bull I bull bull bull bull bull bull bull bull bullbull _~bull b ---) bullbull-bull ) bulll middotbull middot1middot ) bullT --f bull I bullr ~bullbullbull bullbullbull( - -bull-- ( -o-----_i bull-~-l- i l l J l~-- c middotmiddot _--1 ---I middotmiddot ---- ~bull-bull bulli_ ALT Elmiddot_ bullbullbullbull _- ~~middot bull middot bullbull _ bull middotbull bull~ ~bull middot bull -middot bull--ua_-- bullbull bull

-- 01--- middot_ -middotmiddot hmiddotmiddot __1 ~-- ~ fi~~- ___ - ____ _ -middotmiddotmiddotmiddot~ ) -~-J bull bullbull bull bull 0 uc- -l ~- ~ IT ~~ll ~ bull -middot -middotmiddotmiddotmiddotbullCCAmiddotmiddotmiddot-middot middot bullbullbullbullbull

) i- 5 ~-==-- __ __ - bullbullbull _ bull~ bullbull _ bull bull l T[h4 ------ - 0

i17- o~-lt -(i-_~ 11t~bull-omiddot ~- -- 13 0l~~~bull bull Jbullbull~bull ~ ~bullbullbull bull bull x- middot~---=-~~ -=aJlll8 bull Ibull bull ~~ middotbull rbull~---bull1-~middot-middot _ middotmiddotmiddot-middot 1 0 ~vrbullmiddot ~middot ~ (J~-middot _-_~) ) ~ bull middot

l middot _ POMA_ middot =~~~----ti~ jmiddotmiddotmiddot - middot bull [j

~A ii J0 Vfli middot bullHud __=bt_ bull

CImiddot ~-- ~- middot)middot PACIFIC OCEAN I middot ---- middotmiddot ~

__ middot__ ~ - _ 23~1 middotbull 8 4 1 middot middot ~ middot middot gt ~~- l ~ u middot

bull - bull- I ~------ --1~ i middotmiddotmiddot - n _c-118 1130

~ n r -t ~~gt25) cmiddotbullmiddot

~--lt- ~~- 1-~__( i - t ~ _ middot 0 igt(_J

11bull bull11 ~~ -~[ ~i~gt----gtmiddotmiddotmiddotmiddot--~l_ ~~ ELEVATION

IN FEET bullbull (_- middot bullbullbull -middot middotbull middot ~~ middotmiddot bulltbullbull _ffmiddotmiddot-middot v I )tylt~ -~bullbull1bullbullrbullbull ~-lt -~ ( I~

600~ A0 Cv(A (1829 m AND OVER) deg )_ rJ__~7 middot middot ~--middot L==1 _J bullbullbull - bull -middot~-- rgt ~ middot(Zmiddot- middotbullmiddot middot

Z~C)-tGOO (762 middot 1829 m) 9-N4 __J (r -- lf _ bull bullgt-~~~ ~ _ w _ _ I (1 bullmiddot( middot1 middot -----~~~- middot L-bullmiddotbullW bullbullbull3 STA r I0-4 lODEL

100i -2soo (305~762m) -- Ow - -~1_- i ~~--- bull v~rvt ~~ -middot )) ~--

II gt J (-_bullmiddot middot~ l bull bull tr 1 )~ gt ) bullbull-_bullI-middot -middot bull~0 3 Mor nuq1ENr Wlbull~O JIAtCTIO-bull bull - lbull C---gt bullbull )t bullbull -( I bullf I - 20-00 (61 bull 305 ml J( Jloa xxE- -bullbull00 - -- middot1

0-200 (0middot61m) Wl)7 AVBt~gpound ) bullmiddot-iiNL~ middotntmiddot_ 1 iJJlt( _1J- ~ VAq IA9 IL ITY 0 ~ 10 15 ltS lHPtl

~--_ bull bull I bullbullbullbull 1 ~) J)J ~ bull Is bullmiddot bullbullbullbullbull ~ 3 V IS A VAqlABLE OIR~CTIO- 0 8 16 2-4 km

(SPEEDS SHOWN IN mph 10 mphbull 16 h1llr) -- middot ktr~~~ lt~ ) -middot-SCALE

Figure 7 LOS ANGELES BASIN MEAN WIND FLOW FOR DAYS WITH LOW LEVEL INVERSIONS DURING AUGUST I 970 AT 1600 PDT

-~~~~-=======~middot~-~======~middot--=-==-===gt=---==____________=== ~--=-J~==-- -=-ee----=-------

500

N f-- V

- - - SUBSIDENCE INVERSION

----MARINE INVERSION

bullbull-bull-bullbullGROUND LEVEL

x WINOS ALOFT (kmht)

WESTERN middoteASIN EASTERN BASIN

LAX WINOS EMT IHOS I I

CNO WIHOS

s_ 04 13 1500- 05 02 08

I 06 069 middot

11-1--

04 04 i ~4

06 ~ 4--

I 2

1000 n1 1005 -_E

lll --1 lJ -----------~----

~11

--=i-+- c -- 9 _____ - ~ C

lt I

I 6 4 _r 31

I 6 5 ~~ ~_ bull ---middot- 64 ~li- - middot- bullc - middot-----------

10

SMO (1347 PDT)

EMT (1246 PDT)

BRA CAB (1459 PDT) (1335 PDT

RIA (1349 PDT)

RED (1406PDT)

Figure 8 VERTICAL CROSS-SECTION OF bscat FOR lvflDDAY

T t 10-4 -1)(l n1 s are m

JULY 25 1973

- c - -~

~--~ JC_-_1- ~1pi~ oamp----~JilliiiM~f~-U~ -~--- --~~~ ~~~

-=--~

-E-- O

_ lt

1500 05

06 15

09 __~

1000 --

~- ~---middotmiddot 29

500

oJ11

__a

07

I 07 I

I I

I

09

I

I

I

I 7 ---

11 -----

~ ----- 6

---------------lt- -~middot4 --------

20

29

-

10 10

11 07 08 08

10

08

~8 _____ Y-

N

- - bull SUBSIDENCE INVERSION

----MARINE INVERSION

-bull-bull-bull GROUND LEVEL

WES TERN BASIN EASTERN BASIN x WINOS ALOFT (kmhr)

t t

CNO WINOSILA WllltOS poundMT WINOS

SMO LA EMT BRA CAB RIA RED O (1736 PDT) (1655 PDT) (1707 PDT) (163 PDT) (1823PDT) 1805 PDT)

Figure 9 VERTICAL CROSS-SECTION OF b FOR AFTERlOON OF JULY 25 1973 scat

T bull 1o- 4 - l )(units are m

__~~---iii~~- ~- ~~______ ~~- --~~J---=-~ ~

N ~ -J

PACIFiC OCEAN

0 5 10 15 1111

E 8 4 I 0 8 6 2 ~ bull

SCALE

dh Mes

CONTOURS REPRESENT - 000 ft 305 m

0 SNA

c8s

ec 8v

amp R~b

Figure 10 TRAJECTORY ENVELOPE FOR AIR ARRI1G AT CABLE AIRPORT (CPLAD) 1600 PDT JULY 25 1973

~-~

q_- ~ ------1 H~~~ -~~--~ ___---___--i- __r-=-1--===12---1 ~ ___r~ _==---_ - ~- f~~ ~-- - -5plusmn-at -~middot~

ll~~r1 ri

40

ec 8v

-1 I

amp

0 HQ_

7 0

CAP LAAR) O

VER

PACIFIC OCEAN ~ 0

RLA

4

WHqR d

diams

H ~I

I l

0 COMA

3

L~

LAH

Fa_ f ~~

S ~ LA APCD VALUES ADJUSTED TO AGREE ~

lt

0

5 10 15 mi0 WITH ARB CALIBRATIONE-j I I CONTOURS REPRESENT NZJ ~ 0 a SCALE 6 24 km - 1000 ft 305m COS v~J

______ J 10 ro ( igtf t-i

coFigure 11 SURFACE OZONE CONCENTRATIONS (pphm) I 600- I 700 PDT JULY 25 1973 ~

~~~~~C-~ ------=--~-__-~--~~~=--- ----=--~

N

-E

D1600----------------------------- 1--

14001-------------------------------

1200

I Ground Elevation

1000 middot 445 m ] lampJ

sect ~~ 7 ) SURFACE i6~ 800 MIXED LAYER

~

~ [ J ~ ~ I OZONE CONCENTRATIONS~ 600 E E GREATER THAN

( 50 pohm

400 I C H T Z GROUND LEVEL

200

I PUUloCETER UNIT SnbullBOL

NOc N0 0 ppm01 02 03 04 05 03 z

40 --~45~~ 50 co pm C0 5 10 15 20 25 30 35 I I I I I I I I I I TEIIPERATURE oc T-5 b 5 10 15 20 25 30 35 40 45

I-- 100 RELATIVE HUlillOITY H0 10 20 30 40 50 60 70 60 90 b1eot IOmiddotm- 1 8

CN cmmiddot3 1 IO X0 I 2 3 4 ~ 6 7 8 9 10 URBJLENC-C cm213ue- E

Figure 12 VERTICAL PROFILE OVER CABLE (CAB) J CLY 2 5 l C)7 3 l 63 6 PDT

~ _~ ~--- -

--

1400 I bull bull

1200

1000-5 LampJ 0 ~ I- 800 ~ c(

sooLl

-1-=-1-~--t j --=~c-o-----i-bull 1-~~~ ilt~~ -~-1 lta-abull--~ -c-~---=---r F--- ---- I n_--middot- =~~ ai~IHJ

(~-It

1600 ___________________________________

C r 11 s Ground Elevation t~C E H I~lcc

- ~ 1 90 m

4001 bullc C H

C UNDrnCUTTNG svC ~ Ic- H

SEA BREEZEC II 200

C C

[C -PARAMETER ---UNIT SYMBOL

NOx N0 0 ppm01 02 03 04 05 03 z co ppm C0 5 10 15 20 25 30 35 40 45 50

-5 middot- -~20~----25 TEMPERATURE oc T0 5 10 15 30 35 40 45

100 RELATIVE HUIOITY H0 JO 20 30 40 50 60 70 80 90 bcot 10-4m-1 8

CN crrr3 10 0 I 2 3 4 5 6 7 8 9 10 X TURBULENCE cmZ-13 sec-1 E

N N

_-----=-G--~---

Figure 13 VER TICAL PROFILE AT EL MONTE (EMT) JULY 25 1971 1656 PDT SHOWING UNDERCUTTING BY THE SEA BREEZE

0

middot~_lt ~middotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotbullbull

-~

LACA

0 - )

i r=

-v2v

~

_middot~middot)( I bullbull

bullJ

K~Ji~middot

~~ 61iAS 0

EMT J~J---6~-11 ~orr

PACIFIC OCEAN

WEST 0

SMC

0RLA

14

L~8

R~A

~BL

16 ~ ~

0 5s Pcfrac14A c1i ~ )

wFJfo~J_) ltI~~~

_ff-Clf1ito J )

HILL~

~J U

~ _~~~

~

I o middot

1 1$ ~ 11yen ~middot ~I N

I

N I- I

t

0 --pomiddotmiddot bullmiddot i- 1LO middot Joomiddotmiddotmiddot -- middot middotmiddot -middotmiddot

_middotmiddot 0 middot middotbull MWS r

L4 ( 1 T bull bull __-- -A bullbullbullbull middot

0 i __ bullbull

17 t-J~ N7 a S I ~r ~ 1 rtd ~lt A-~ v- middot ~ - cXa 0

RIA 19

CLO

ltJ~

bull ~ 0

(

--

1

_ _

-2Wl

~s~o -- _)~J0JgtJ~ ___ Q

15 l1JI

0 15 r(A0

CAP

CLARR)~R 1900 1-shyPDT

II (_-L~X L2X I 0~ R[V

0 CCtwA

I

I18=00 POT~ l4 r1

fj

-11J - ----- 11=oomiddotmiddotpor

l~i middotmiddot- o

i

5 10 5 Tl o~1 middot--middotmiddotmiddot middotmiddot

_q it==i--__F-3 9 I I CONTOURS REPRESENT SNA NZJ ~1 o

_- I 0 8 16 24 km I - 1000 ft 305 m middot ~

7 14~CALE --- 2500 ft o2m V lr1 ) middot I i0 _ il o5

16QQ pol(middot v( ____________ _L

I i

Figure 14 APPROXIMATE TIME (PDT) OF ARRIVAL OF SEA BREEZE Jl-LY 25 1973 (Ogt_iective criterion based on ground level ozone concentrations)

~ -___~==~ ~~ - ~ =-~ f7r=~1 _j~-~ --c_~~

u-middot - middot middotmiddotmiddotmiddotmiddot

~- middotmiddot~ ~1 WESTERN BASIN r Joa_middotmiddotmiddotmiddot_ NOxEMISSION RATE ~- 95 METRIC TONShr

-----bull_ ~ ~middot~ I -OUR -----middot )omiddotmiddotmiddot - middot~ l21 (fTI

~ AT middot ~ middotbullmiddot- ~- ~ middot 4bull-middot

I EASTERN BASIN NOx EMISSION RATE 10 METRIC TONS hr

ri r bullbull

t10 Joa

) __ 8v -a_ -- -bull-I O ~AGA -_ ~S ___ _ middotmiddotmiddot -

~ ~v ai- omiddot-middot~-- - ) r -middotmiddotmiddot f middot( ---~ -l A ~ _ (- bull ___

it~ ~~~ middot-middot -- ~-~ ~~~ 0 0 AZU~

AVERAGE CONCEN7RCTi)N iN BOX (IF STEADY STATE)

IS 25 pphm

1 r f--Ji 7 ~Sv PAS ou )V~(~- ~ t i -~ Li_) 03 FLUX THROUGH f~

~ ~JI_~ - amp_ JiM O SHADED BOUNOA~middot~-~ ~~-s-- EMT 185 t 60 METRI~ bull ~ ~ TONShr 0 (m)

c~~~ 1t~CS A~JFP

1000 _29

-i32

_~o tUA

_

1

O~ ~

0 -__rJ( (r- J PACIFIC OCEAN LAX _ C-middotJbull _

l o M R No _

550m

r

A frac14

HAR O HJ LAH

_ o camptA REDLANDS 18QO POT ~ r

I bull ~

RB MEAN TRAJECT~~~y

0

TOA L~S

0 AN

I - ~ 8 OUNOARY ~ ~middotltdeg ~ ~ BETWEEN middot __ WES~ERN ANO- middot middot - ~

I gt I lt bullmiddot bull (EASTERN ~ i middotmiddot middot - - ~

S ~ ~~ ~ - middot-

rt1~1_--t------l

middot1-- BASIN ~-~

1-)~~--middot ~ ~l

~~ ~-bull bull J --

-is-eo -_

0 5 10

j=i r-i C

0 8 ltl

SCALE

5 mi

2~ un

CONTOURS REPRESENT - 1000 ft 3gt5 m

--middotmiddot 2500 ft 1 762 m

~

0SNA

cos 0

_ --~ ----- --- ( bullmiddotmiddotgt

- middotlt- ltgtmiddot t__ Q ~

1 1 rmiddot bullbullbullbullmiddot ~9

NZJ ~ middotmiddot - middot- Alr ---middotmiddot- middot middot( middotmiddotmiddotmiddotv ~ bullbullbullw bullbullbull bullmiddot 1 bullbullr~ ~-- -middot ~--v ~- - I -~

ESTIMATED OZONE FLUX FROM VESTER~ TO EASTER-J BASIN JULY 25 1973 I 700 PDT

C ~IV

N N N

I

l ~

-~~

I

iI

i I

I t

t

~ ---~ --

Figure 15

~Qa llfJD fl(~middot ~ 11f ~I I

l

Lfb ec~s0 CPK v2v 0

ALT 8v Ld~_----1

I

HO-

0 CA

middotLARRv O VE~

1330

ol(Di

A~U

0ENT

~lt

s~e ~ 1530

F8f 1730

~

rbull-~

oc (WljT) -_-~(~~c lt-rw---_

~~ ~-_i~cB~~~

2-~) - ~ ~ l~w-~~ p~- pound)_

0 ojI middot tl-1CfUp I ~ ) 1 ~ J~I i bull middotbull middot~-Li 1)- ) I

DiI ~- 0

i ) 0 l I I

t

A RALc~o JI

C

-~

0 r-iR

~IV 1230 1~

RE PO ~- I - Ftl

) 0 ---~gt- __L8s ~Zi diams ( T~ _middot_ ~~ ~

I AN ~~-~ j t bi 0

~ I

~ I L i

-_gt ji o 5 c 5 Tl middot 0 0 ~-i p__i=r 2=f I_ I 1 NZJSNA 1

1 8 2 4 km )

SCALE I 00 J_(1 CONTOURS REPRESENT cos f

1 0 I --- I - ))) 35

PACIFIC OCEAN

Figure 16 TRAJECTORY E~VELOPE FOR AIR ARRI1gtJG OVER REDL_)DS AT 1800 PDT JULY 23 l =i73

224

JULY 25 1973

LA DOWNTOWN

0sect040 a

~

~ 020 0 X z0 ~ LJ 0 ~ z

~5 040 330POMONA 0 ~ en~ 020 w z _J

w w 0 (9 z O----u-~~-__~_-~~~-------L-~-0--0-0~----- z

ltt~ 040 56 (I)z

0 0o _ RIVERSIDE _J0 20 t6 ~

0~ Qt---0-0--ltrO-ltgt-C~------~~~~ a

LL ~

Rate ~ IO mph___ (I) w

_J~ ~ ~

et~ lt(

3 040 PALM SPRINGS ~

j 020 ~

0------____-----L--___---------L---~--~

105

12 4 8 12 4 8 12 l~-s----am _ pm----1

HOUR OF DAY PST

Figure 17 Diurnal variation July 25 1973 of oxidant concentrations at air monitoring stations at Los Angeles Downtown Pomona Riverside and Palm Springs California Values are corrected data Los Angeles Downtown and Pomona x 11 and Riverside and Palm Springs X 08

CONO S t 1 fRESEIS7

~

~~ 0

ciffmiddotdK ~ ~v~~o

( ~s ~

bull ~r ~ bull 1--~~----Soootl ~ ~ ~ ~ lj i1 d t CJ ~ ampfrsmiddotflt- frac12 ~ middotL~Js _-- ~

_gtgt middot~ ~rroltf~-) ~ 0 s- r

middot-middot- r_~ ~~JtbO ~~bull~Jt ~~~ L r - bull _ ~ I= J 1 ~ ~ ~-~~bullJC ___ -_ middot ~ laquo -poundJ~ ~- middot1~ r-- - V--_1_ ~ I 1 S I

V ~ bullf-uv~ fi -~zumiddot -~middot~ LS gt -tmiddot-F Q~ ~-tv I_~ --- ONT p(_ s ~S ~~~-[ ( 0 c-_ --~ ~~~___d_) lt- ~ I -i-C - -

~----1-1 bull~~POMA ~V BN ) middot-~ f -- s - ~

~VA -middot- ~p AAL a 2~~ ~~middot01 r r ~ middot middot 0-- V

i LAX bull1

~ -~poundJ-i- ltllll _(__1-0~ ~t- degQ-0- ~~ _ _-__~~-qlK ( a_ II ~ ~p-~ ~J

N bull - - 0 r o_ _I ~ -~ ~middot ~ ~amp ~--= ~ ) s ~

- -~- - middotO _a - Tl --0- ov I lHOIO J I bull J -- ~ 6 ~ -__ 2 ~

(__ ~~ _- ~-~ middot8---fl~ -- ~ bull~-abullbull _~ ~-cgt ~ bull bull middot e bull bull l ~ 0

I 1A_ HZJ middoto~J

middot0 (~ ~ S TAA

- ~ - - - --0 () _-j J middotO=c==c-c==cc~~~ l ~~ ~ ~ bull-~---~ ~ bullbull -~ al1 ~ bull __ ~--middotmiddotmiddot

diams Skyforest _ Strawberry Mt Lookout

Figure 18 STRE ~[Ll)ES FOR 1600 PDT on 8 1673

~ ~--

vO 0

N N V1

au

91 V7

-1 ~ -=1 ~~ ~~~~l r=--~d- ---1 _J-_

~E1 ~L1-~f~

3100 ---------------------------------

2900r-----------------------------

T

e w 0

~ 5 Cl Ground Elevation

1560 m

T PARAMETER UNIT SnbullBOL

NOx N 01 02 03 04 05 03

ppm z co ppm C

10 15 20 25 30 35 40 --

45 50

170

I I I z

0 5

-5 - -0~ 5 10 15 20 25 30 35 40 45 TEMPERATURE oc T

0

0

10

I

20

2

30

3

40

4

50

5

60

6

70

7

80

8

90

9

100

o

RELATIVE HUMIDITY

bcot CN

TUR8ULENC~

110-4m-

cm-3 tobull 213 1 cm sec-

H

8 X E N

N OI

Figure 19 VER TI CAL PROFILE OVER ARROWHEAD u-RR_l A CG CST I 6 1973 939 PDT

3100----------------------------------

N2900r----------------------------- -i

N

2700i-------------------------------

2500

e 0 uJ 2300 gt ~ ct

2100

1900i---------------------+--------------

~le 1iation 1360 m) 17001 ~

- -PARA1jETER UNIT SYMBOL

T NOx N1500 o ppm01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50

TEWERATJRE oc T-5 middot --~o--- 5 10 15 20 25 30 35 40 45

IOO RELATIVE HUWIOIT Y H0 10 20 30 40 50 60 70 80 90 bcat 10-~- 1 8

CN cm- 3 104 X0 I 2 3 4 5 6 7 8 9 10 213 1 tURBliiENCE cm sec- E

Figure 20 VERTICAL PROFILE OVER ARROWHEA D -RR 1 --- -AUGlJST 16 I) 16--1S PDT

1-~i w--~i_f l-=--bullC- ---~-4

1600 bull t c- N 8 ff Tbull C[ 8 H 1 bull H z H T ~ C f N 1 H T bull C rn 1 C NE bull-~z Hi400 bull bull tf T bull N ~r --middot _P H -ybull EC N z__e H T i 8 z H Tbull C E HD Z H T POLLUTANTS REMAINING FROM bullt C Hbull L T PREVIOUS DAY1200 Et HO I II -middot-- bull Ct H 9 - H T

___ Hbull( E N 1 a tC N i--_ -1 H

C N Tbull Z HP poundIC C H z_ 1111 1

- bull C H Z l _H_ _J1000 )( cc H -z emiddot ksect bull C N ~ T

)( iz H 8 H TIAI -t XC z 7-- T0 bull pound N t H_8

t-gt

YCpound N 1800 l I-gtltbull - H (Jet

N i -r~Bltt t bull gt- t C X N H T

[ BUOYANT POINT SOURCE PLUMEH 1

N ~z-- -

C H

-bull SUPERIMPOSED ON POLLUTANTSC JZ X H T 600 -~ E c REMAINING FROM PREVIOUS OtY Cl JC t H H f bull cmiddot t HT -fl

C- X t fl _ REMNANT OF NOCTURNAL RADIATION INVERSION(I-----e-C f N K I T H

C Z [ T H x-8 400 _Zc r -H -K SURFACE MIXING LAYERz C II H K 8

C N T pound H M 8 _ I -t ff H E N -9 l

Ground Elevation 305 rn200

PARAMETER UNIT SYMBOL

_ I - I I I NOx N00 ppm01 02 03 04 05 03 z

co ppm C 0 5 IO 15 20 25 30 35 40 45 50

L middot1 TEMPERATURE oc T-5 0 5 IO 15 20 25 30 35 40 45

100 RELATIVE HUPAIDIT y H0 10 20 30 40 50 60 70 80 90 bscot o-4m- 1 B

CN cm-3 x 104 X0 2 3 4 5 6 7 8 9 10 TURBULENC~ cm213sec-1 E N

N co

Figure 21 VERTICAL PROFILE OVER BRACKETT (BRA) JULY 26 1973 0825 PDT SHOWING BUOYANT PLUME AND UNDERCUTTING BY RADIATION INVERSION

N N 01600

___bull C M C

C

1400~~~ t C [ middot H LAYER CAUSED BY

C C H C [ H UPSLOPE FLOWl

1200

1000 ] w

SURFACE MIXING LAYER 0 --= ~ -~~ 6 800~ er

C C

600t-i C C t C

I ~00

Ground Elevation 436 m 2001-------------------------------

PAIUWETU UNIT SYWBOL

NOx N ppm0 0 01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50 I I I I I I I I TEWPERAT1JftE degC T-o b 5 10 15 20 25 30 35 40 45

100 ~EIATIVE HUWIOITY H0 10 20 30 40 50 60 70 80 90 b1tt1 10-m- 8

CN enr3 110 X0 2 3 4 5 6 7 8 9 10 Tu RUL Erct cm23sec- E

Figt1re 22 VERTICAl PROFILE AT RIALTO (RIA) JlJL Y 19 1973 1738 PDT SHOWI=JG LAYER CAUSED BY UPSLOPE FLOW

~~-7 ~ ~- 1 ~iri ~~- ~~-~ ~t ~~ ~ =~middot-1

1200 I t 1 If J-

1000

I C ltTl a_ ~l- t

800

600

L gE __r H

H

400 j (~ c pound N C E I~

t EH -

1-1 M

H H

H M H H

H

H H

11 bull H M H

M H If

H H

H

- C t H ~ C poundmiddot H

I C E I(

200

1600--------------------------- t

T t t T l

l T t

T t_

t 1

l] w ) g f

Tt t

ltt ~ T

t J t T

t J

f 1

t

Klt

H M Cro1nd Elevation 250 m HT X

5Yl80LPAllAlETER ~

NOx N0 0 ppm01 02 03 04 05 03 z

co ppm C0 5 10 io 20 25 30 35 40 45 50

25~--- ---35~~-40 TEMPERATU~E oc T-5 0 5 lO 15 20 30 45

100 RELATIVE HUMIDITY H0 iO 20 30 40 50 60 70 80 90 bact 10--ltllm-1 B

CN cmmiddot3 11 04 X0 I 2 3 4 5 6 7 8 9 10 IURBULENCE cm2hioC-1 E

Figure 23 VERTICAL PROFILE OVER RIVERSIDE (RAL) N

JULY 26 1973 2239 PDT I)

middot==-=-=

0

bull

N w 1--

ii -s~~ l-obull

CJ ~

obull -obull obull

5 02~

bscat

Oa

4l o2J

-I 3 e I 0

--)(

~

Abullu 2

ll

ol

Traverse at 750 m msl 35 km Downwind (SW) of Arch - St Louis Mo 1117 - 1137 CDT

( Power Plant Plume -01 Ibull-[ ~ e

11 bull E I -)(I

I0bull I 1r~ l -

0

I I Io 1 u I

I r- l A bull I i I 1I

H1I I 4 t I II I I

11 I I

I I r I I I

I I qo 01 I I

I I bullJ~viI I middot ~

I

I I

~

Urban Plume

ood 0 10 20 30 40 50

kilometers

o~

02

01

s 1

P

0bull 01

00S~J1 I ti middotmiddot1 middotvmiddotmiddot~ J

Urban Plume

I y

oo 0 10 20 30 40 so

kilometers

Traverse at 750 m msl 46 km Downwind (SVV) of Arch - St Louis Mo 153 0 - J 549 CDT

---- bscat

o-

Power Plant Plume

1l~ 11I 1 t

ill~t fl Ibull I ii

I

lmiddotmiddotrI

I I I I t II

l vrI V

JV-f Jl bull

bull t I bull I

Figure 24

l

232 RELATIVE CONTRIBUTIONS OF STATIONARY ANDMOilILE

SOURCES TO OXIDANT FORMATION IN LOS ANGELES COUN1Y IMPLICATIONS FOR CONTROL STRATEGIES

by Robert G Lunche Air Pollution Control Officer

Los Angeles County Air Pollution Control District Los Angeles California

Introduction

The type of air pollution problem characteristic of the west coast of the

United States and particularly of Southern California has come to be known

as photochemical smog because it is the result of sunlight-energized atmospheric

reations involving oxides of nitrogen and reactive hydrocarbons Its manifesta-

tions- -eye irritation reduced visibility damage to vegetation and accumula-

tion of abnormally high concentrations of ozone or oxidant - -are by now well

known In fact the occurrence of high levels of oxidant which consists almost

entirely of ozone has become the primary indicator for the presence and relative

severity of photochemical smog

During the 25 years since photochemical smog in Los Angeles County was

first identified an extensive program has been underway for control of the responshy

sible contaminant emissions Initially during the 1950 s these programs concenshy

trated on controlling emissions of hydrocarbons from the stationary sources of this

contaminant In the early 60 s programs for the control of hydrocarbon emissions

from motor vehicles in California were begun An exhaust emission control proshy

gram for hydrocarbons and carbon monoxide from new vehicles was begun in 1966

C011trol of oxides of nitrogen emissions from motor vehicles began in 1971

As a result of the overall control program by 1974 emissions of reactive

hydrocarbons from stationary sources have been reduced 70fo from uncontrolled

levels and about the same percentage from mobile sources Oxides of nitrcgen emissions

233

from statjonary sources have been reduced about 53 while emissions from moshy

bile sources are still about 7 above uncontrolled levels due to the increase

in NOx from 1966-1970 models Additional controls already planned for the future

will by 1980 achieve reductions of reactive hydrocarbons from stationary sources

of about 87 from uncontrolled levels and from mobile sources about 93 By

1980 emissions of oxides of nitrogen from stationary sources will have been reshy

duced 53 and from mobile sources 63 from uncontrolled levels The past

present and projected emissions of these contaminants are shown in Figure 1

A I though compliance with the air quality standards has not yet been achieved-shy

and is not likely before 1980- -the results of these programs have been reflected rather

predictably in changes in certain of the manifestations of photochemical smog For

example eye irritation is less frequent and less severe and in some areas js

rarely felt at all any more and damage to vegetation has been markedly reduced

Ozone (or oxidant) concentrations have been decreasing in Southern California

coastal areas since _1964 in areas 10-15 miles from the coast since 1966 and in

inland areas 40-60 miles from the coast since 1970 or 1971 as shown on Figures

2 arrl 3- All of these positive effects have occurred despite the continuing growth

of the area indicating that themiddot control programs are gradually achieving their purpos

a return to clean air

This improvement is al~o refutation of the so-called Big Box -concept which

assumes that the total daily emissions in a given area are somehow uniformly disshy

tributed throughout that area--regardless of its size or of known facts about the

meteorology of the area or the spatial and temporal distribution of its emissions- -

234

and of control strategies based on that concept And since the improvement in

air quality refutes the control strategies based on reductions in total emissions

it thus confirms the value of more recent control strategies which emphasize conshy

trol of motor vehicle emissions and use of a source-effect area concept

Following is a brief listing of the evidence we intend to present as supporting

our views on just what control strategy is appropriate

Examination of relative contributions of HC and NOx from stationarybull and mobile sources demonstrates that motor vehicles are the overwhelming

f source of both contaminants~

I bull Observation of air monitoring data shows that the effects of photochem -

ical smog are not uniformly distributed t_hroughout the county

bull Study of the meteorology of LA County shows consistent paths of trans -

port for various air parcels and consistent relationships between the

areas most seriously affected by photochemical smog and high oxidant

concentrations and certain other areas

bull The upwind areas are found to be source areas--the downwind areas-shy

effect areas

bull Central L A is found to be the predominant source area for the effectI area in which the highest oxidant levels in the SCAB consistently occur

bull The predominant source of emissions in this source area is found to

be motor vehicles

bull Central LA has the highest traffic density I

ij bull Both pr~mary and secondary contaminant concentrations reflect the effects

of the new motor vehicle control program in a predictable fashion 11 I

A strategy based upon these findings is gradually being verified by atmosshybull pheric oxidant data~

235

The Evidence that Motor Vehicle Emissions Are the Principal Source of Oxidant

As seen from Figure 1 at the present time the total daily emissions of I-IC

and_ NOx from all sources in Los Angeles middotcounty are primarily due to the motor

vehicle The problem now is to find the spatial and temporal representation of

emissions which when examined in the light of the known meteorology and geogra -

phy of the Los Angeles region best describes the source of emissions responsible

for the highest observed oxidant readings

In the rollback models used by EPA and others the basin is treated as a

big box with uniformly distributed emissions and peak oxidant is considered to

be proportional to total basinwide hydrocarbon emissions

The fact is that the middotemitted contaminants from which the smog is formed

and the effects which characterize that smog are not evenly distributed throughout

the Los Angeles Basin in other words the basin area under the inversion is not one

large box filled to all corners with homogeneously distributed air contaminants and

photochemical smog

Refutation of Big Box Myth

Examination of atmospheric contaminant concentrations refutes the big box

concept It is found for example that concentrations of djrectly emitted contam -

inants measured at a particular sampling site reflect the emissions within a rather

limited area around that site For this reason contaminant concentration levels

vary from one location to another and each has a characteristic daily pattern which

reflects the daily pattern of emissions in that area

middot 236

The big box concept is further refuted by the fact that peak concentrations

of carbon monoxide and oxides of nitrogen in areas of high traffic density were

fairly static prior to 1966 Thus they did not reflect the 45-50 per cent growth

in motor vehicle registrations and gasoline consumption which occurred in Los

Angeles County between 1955 and 1965 and which caused comparable increases in

total daily emissions of such vehicle-related contaminants This demonstrates

that growth was outward rather than upward so that a larger area of the County

began to be affected by photochemical smog but no area experienced smog ofJ

greater severity than that originally affected by smog formed from the vehicular

emissions which accumulated each weekday in central Los Angeles and were trans-

1 I

ported later that day to the San Gabriel Valley

1 Meteorological Evidence

To verify the geographical dependence of emissions and resulting atmospheric

concentrations let us examine the meteorology of these large areas of Southern

California Both the County and the Basin have many meteorological sub-regions

in which the patterns of wind speed and direction may be similar but within

which the patterns of air transport are parallel with those of adjacent sub-regions

and the respective air parcels do not ever meet or join

The characteristic patterns of inversion height and wind speed and direction

in these sub-regions and their patterns of vehicular emissions together have

created a network of source areas- -those in which the reactant contaminants accu -1T

i ~ mulate in the morning and begin to react--and related receptor areas--those to which

~ the products and associated effects of the photochemical reactions of the contamshy)

inants originally emitted in the source areas are carried by the late morning and

237 middot

afternoon winds ( sea breeze)

Wind-flow patterns show that characteristic patterns of transport for related

source area-effect area combinations are separate and parallel not mixing or

joining Each source area has its own reactor pipeline to its own effect area

or areas

To illustrate this source area-effect area relationship the typical flow of

polluted air from downtown Los Angeles to Pasadena was selected as a worst

case situation for in-depth examination Figure 4 shows that the air in downtown

Los Angeles on the morning of smoggy days moves directly from the central area

to Pasadena

Vehicular traffic is the predominant emission source in both downtown Los

Angeles and Pasadena Thus the air in each locality should contain CO Also

since oxidant would form in the air parcel moving from Los Angeles to Pasadena

oxidant levels would be expected to be higher in Pasadena than in downtown Los

Angeles

Figure 5 shows these relationships for the period 1960-1972 The atmosshy

pheric CO level is similar for the two areas while oxidant levels were higher in

Pasadena than in Los Angeles throughout this time period This demonstrates

that a significant amount of oxidant formed in the air as it moved to Pasadena

containing both the unreactive CO and the photochemical reactants for producing

oxidant Both CO and oxidant show a marked downward trend in each locality since

1965 which emphasizes the effect of vehicle exhaust controls and the correlation

between the localities

238

On a day which is favorable to the formation and accumulation of photoshy

chemical smog a contaminated air parcel normally originates during the

6-9 a m period on a weekday from an area of dense traffic centered just

south and west of Downtown Los Angeles It is oxidant generated within that air

parcel which usually affects Central Los Angeles and the West San Gabriel

middotK IJ l J

Valley area around Pasadena

The traffic area in which this smog had its origin is about the most dense

in Los Angeles County and has been so for the past 25-30 years No area

has a higher effective density thampn-this Using carbon monoxide which

1

is almost entirely attributable to motor vehicles as an indicator of such emis-

sions it is found that the concentrations of emitted vehicular contaminants

middotr i

measured in Central Los Angeles during the past 15 years confirms both this lack

of change in effective density and the absence of any area of any greater effective

density when local differences in inversion are acknowledged

This area the Central Source Area is depicted in Figure 4 The size

and shape of the Central Source Area was ch~sen to be large enough to reduce to

an insignificant level any diffusion or transport into this area from any externally

l generated reactants This conclusion is based in part on the trajectory studies

previously referenced as well as an analysis of the diffusion and transport parashy

meters for the area

239

The Central Source Area has been identified as that geographical region

which contributes essentially all of the primary contaminant emissions giving

rise to the highatmospheric oxidant levels in the West San Gabriel Valley

The proportion of emissions in the CSA due to motor vehicles and that due to

stationary sources is shown in Table 1 For the County as a whole about 80 per

cent of _(6-9) AM reactive hydrocarbons are due to motor vehicle emissions and this

figure rises to 90 per cent for the CSA The same conclusion a pp lies to NOx

emissions The Central Source Area contains the greatest density of vehicle traffic

in the County and thus the greatest density of source emissions Thus it appears

that the source area with the highest density of emissions during the critical (6-9)

AM period is responsible for the highest afternoon oxidant levels observed in Los

A i1geles County and in the South Coast Air Basin These highest oxidant levels

are consistently observed to occur in the San Gabriel Valley This is true whether

the LAAPCD or the ARB oxidant calibration procedure is used

Further the atmospheric concentrations of the primary pollutants can be

identified as originating primarily from the motor vehicle and they reflect the

effects of the motor vehicle emission control program A vehtcular source area

can be identified by its atmospheric levels of CO and NOx Figure 6 compares

measured atmospheric levels with calculated atmospheric levels for CO NOx

and the CONOx ratio in the downtown area

TABLE 1 240

REACTIVE HYDROCARBON EMISSIONS

(6-9) AM

1970

LOS ANGELES COUN1Y middot CENTRAL SOURCE AREA middot SOURCE TONS PER CENT TONS PER CENT

Mobile 1260 81 3 135 91 2

Stationary 290 187 1 3 88

Total 1s~o 1000 148 1000

By 7 -Mode Gallonage

241

The calculated values shown in Figure 6 were derived from a baseline

survey of 1100 vehicles and continued surveillance tests both using the Calishy

fornia 7-Mode test cycle The baseline survey showed that motor vehicles withshy

out exhaust control systems had average exhaust emissions concentrations of 3 4

per cent CO and 1000 parts per million of NOx Baseline emissions data apply

to 1965 and earlier model vehicleg and surveillance data to 1966 and later modelsmiddot

Since it can be concluded from calculations and observations that the dilushy

tion of auto exhaust emissions in the atmosphere on a smoggy day in Los Angeles

is approximately 1000 to 1 the calculated values for CO and NOx prior to 1965 are

34 ppm CO and 1 ppm NOxo After 1965 the changing effect of controlled vehicles

in the total vehicle population is reflected in the calculated values

CO and NOx values measured in the atmosphere are also shown in Figure

6 and confirm the values calculated entirely as diluted vehicular emissions NOx

concentrations measured in the atmosphere tend to be consistently a little lower

than the calculated values probably because photochemical reactions remove some

NOx from the system

The data for CO and NOx calculated and measured show that emissions in

downtown Los Angeles originate almost exclusively from motor vehicles and that

atmospheric concentrations there reflect the average emissions from a representashy

tive vehicle population

The ARB has recently published a report entitled A Trend Study of Two

Indicator Hydrocarbons in the South Coast Air Basin Acetylene was used as a

242

specific indicator of automobile exhaust emissions and it was found to have de-

clined in concentration in the Los Angeles atmosphere at an annual rate of 12 5

per cent since 1970 To quote from this report The California implementation

plan requires an annual average reduction in these emissions (reactive organic

compounds) of 166 tons per day or 11 1 of the 1970 tonnage per year The per cent

reductions in the_ acetylene levels at Los Angeles and Azusa are greater than reshy

quired by the implementation plan Since acetylene is almost entirely associated

J with auto exhaust this demonstrates that the motor vehicle emission control

program is achieving its purpose

To summarize at this point it has been deomonstrated that high oxidant values

are due to motor vehicular emissions of NOx and HC because

NOx and HC are the principal reactants in the oxidant formation process

and they originate primarily from motor vehicle emissions and

The highest oxidant values are recorded in_ effect areas that receive air

from source areas where motor vehicles are clearly identified as the

dominant source of NOx and HC

243

Future Control Strategy

The APCD strategy for achieving and maintaining the oxidant air quality

standard is based upon the fact that high oxidant values are due to motor ve-

hicle emissions of hydrocarlxms arrl nitrogen oxides This strategy is as follows

1 Both Hydrocarbon and Nitrogen Oxides Emissions Must Be Considered To Achieve the Federal Oxidant Standard

There is wide agreement that NOx and HC are the principal reactants in

the oxidant formation process and that vehicular emissions are a major source

of NOx HC and CO

2 Effective Regulation of Atmospheric Concentrations of Both HC and NOx and of the Ratio Between Them is necessary for Attainment of the Federal Air Quality Standard for Oxidant

Basmiddoted on the abundance middotof available experimental evidence it is our firm

position that the most rational approach to solving the photochemical oxidant smog

problem in the South Coast Air Basin (SCAB) is to control the quantities of emissions

from motor vehicles of both smog precursors--Hcmiddot and NOx--their resulting atmosshy

pheric concentrations and the ratios between both contaminants which will result

from these controls

We arc also convinced that the oxidant and nitrogen dioxide air quality stanshy

dards can and will be met not by 1975 or 1977 but by the early 1980 s if the emisshy

sion control program as originally outlined by Ca~ifornia or a slight modification

of it proposed by the District is followed and enforced This should also provide

for continued compliance with these air quality standards at least through 1990

244

It will also allow time for a reappraisal in about 1978 of the whole situation relative

to the ultimate emission standards required and the best approach to their impleshy

mentation

Calculation of the degree of control necessary to attain the air quality

~ standards for oxidant and nitrogen dioxide involves indirect complex methods 1

aimed at determ_ining the degree of control of the primary contaminants directly

emitted by automobiles

The following evidence supports our proposed solution to the problem in

terms of both the atmospheric concentrations of the oxidant precursors NOx

and HC the ratio between them as reflected in their exhaust emission standards

and the resulting atmospheric concentrations of oxidant which comply with the air

quality standards

Chamber Results and Projections to the Atmosphere

The importance of environmental chamberwork cannot be minimized the

j need for and direction of the whole emission control program was based initially

j on the results of chamber experiments In order to understand the importance to

air quality of achieving both the correct low quantities of emissions and the right

ratio we can present several graphic portrayals of analyses of experimental labshy

oratory work together with their relationship to past present and future air quality

in terms of both morning primary reactant concentrations during the morning

traffic peak and the equivalent emissions which would produce them

245

Figure 7 shows maximum ozone levels that were obtained by irradiating

varying amounts of auto exhaust hydrocarbons and oxides of nitrogen in an environshy

mental chamber The corresponding ozone levels then can be found for any comshy

bination of BC and NOx concentrations Thus high ozone is produced with high

emissions of both hydrocarbons and oxides of nitrogen and low oxidant is formed with

low emissions However either low NOx or low HC emissions11 can also produce

low oxidant--graphic and clear evidence of the importance of the NOxHC ratio in

ozone formation Furthermore each and every possible combination of values for

NOx and HC has then a corresponding characteristic maximum chamber ozone

concentration

Using this graph we can estimate what ozone levels would result if certain

atmospheric mixtures of NOx and HC could be injected into the chamber and

irradiated Such estimates were made for 1960 and 1965 using atmospheric data

rlThe points labeles 1960 and 65 show the location of the highest levels of both

HC and NOx found in the air in those years in Downtown Los Angeles (OOLA) area

during the 6-9 AM traffic peak

It has been demonstrated by use of CO and NOx data and CONOx ratios

hnw well the characteristics of vehicle emissions are reflected in the atmosphere

We know what emissions from the average vehicle were then in 1960-1965 both

for HC and NOx so that we can mathematically relate emissions to atmospheric

concentrations for those years and so for future years also knowing or calculating

only what the characteristic emissions will be from the average vehicle

246

The NOx concentrations stayed about the same from 1960 through 1965 because

average vehicle emissions of that contaminant did not change during that time

Mobile source emissions can be shown to have contributed essentially all of this obshy

served result However blow by controls did reduce emissions of HC and the

concentrations dropped accordingly In 1965 the last year before exhaust controls

the point 65 indicates where we were then in terms of maximum ozone formation

to be expected in a chamber with the highest HC and NO concentrations found in the X

air that year Levels of ozone actually measured in the atmosphere however

are higher than those shown on the graph for high NOx and I-IC concentrations for

those years up to the present

The strategy to meet the oxidant standard is obvious--get atmospheric NOx

and HC concentrations out of the area on the chart that produces high ozone levels

and put them in tie areas with the lowest levels This can only be done by implementshy

ing appropriate emission standards

As can be seen that did not happen between 1965 and 1970 because manufacshy

turers used controls on new cars in California which while causing a decrease in

BC (and CO) allowed a large increase in NOx emissions Thus the path line of

the atmosphere on the chart goes up from 65 and diagonally to the left passing

through an area of higher ozone levels The atmospheric concentrations of oxidant

predictably increased during the years 1967 and 1968 By 1970 they dropped to lower

levels - -back to about the same as in 1965- -exactly as predicted by the model The

app14oximate location of the point for 1970 (70) was both predicted on the basis of

247

the mathematical model and confirmed by atm-ospheric measurements of

[)owntown Los Angeles morning summertime NOx and calculated HC values

Again it should be pointed out that those points show the highest possible

concentrations of NOx and HC Years with less restrictive weather conditions

(for accumulating high primary contaminant levels) would cause lower measured

maximum NOx and HC levels but the calculations would still yield the points

shown Thus we are taking the most pessimistic view

Future Projections

In 1973 we were at about the point labeled 73 and ozone levels were beginshy

ning to drop as expected middot It should be emphasized that ozone values plotted on

thi$ graph are for the chamber only- -not the atmosphere The future path the

points 7 4 and on to 90 represents our estimate of future atmospheric levels of

NO and BC expected if the exhaust emission standards are just met While that X -

is optimistic it is all we really can do since performance of future vehicle models

is unknown We will achieve maximum ozone levels at or below the standard by

about 1980-1985 This will only be true however if cars in compliance with the

California interim standards for HC and NOx continue to be added to the vehicle

population at the normal rate These standards provide the optimum ratio of NO X

to HC necessary to provide the nitric oxide (NO) needed for the reaction that re-

moves from the air both oxidant formed photochemically and oxidant which occurs

as natural background which alone may cause the standard to be exceeded This

ratio is about 112 or 2 parts NOx to 1 part HC

248

The optimum NOxHC ratio is a key element in the APCD strategy but will

require a finite time for its attainment Replacement of older cars by newer ones

equipped to meet the most stringent standards is the only reasonable mechanism

which can change it VMT reduction proposed as a prime strategy by EPA cannot

change this crl(ical ratio which is a basic characteristic of the population at any

given time

Validation of the Districts Control Strategy

Figure 8 compares (1) future chamber oxidant levels based upon the

future maximum concentrations of HC and NOx we expect each year with the

California control program (2) calculated atmospheric concentrations using ~ I

our chamber-to-atmasphere empirical translation and (3) actual measured atmos-f 1l pheric oxidant maxima This clearly sets forth the relationship among these three

factors

The chamber concentrations (lower curve) middotare the lowest values shown

The actual atmospheric data (points connected by heavy dotted and solid lines)

vary considerably from year to year partly because of the vagaries of the weather

In all cases the atmospheric oxidant values are higher than the chamber values

because of the addition of vehicle emissions as the air parcel travels from source

to receptor areas The calculated atmospheric data (thin dashed and solid curves)

are shown to be the highest generally exceeding or equalling the actual measured

data and of course always exceeding the chamber data Thus the model paints

the most pessimistic picture possible It can be seen that by about 19801 1985 atmos -

pheric levels should be at or below the Federal air quality standard of 0 08 ppm oxidant

249

3 Motor Vehicle Exhaust Control is the Only Requirement for Achieving the Oxidant Standard by 1980

We can show that the existing motor vehicle control program has resulted

in a significant reduction of oxidant concentrations in the air

The foregoing material explained the relationship between vehicula~ emis -

sions in source areas and the high oxidant levels measured in effect areas This

relationship is exemplified by the downward trend of oxidant levels in the atmosshy

phere and by the similar year-by-year trends of NO and HC emissions from the X

average motor vehicle A projection of these vehicle emissions factors shows that

the associated maximum oxidant level in the atmosphere will meet the oxidant standard

by about 1980-1985

Figure 9 compares by year the number of days that the oxidant air quality

standard was exceeded in three separate areas with the average NO and HC emissions X

per vehicle mile To comply with the air quality regulations the number of days that

this standard is exceeded must be reduced to one per year

The lines plotted on Figure 9 show that a definite relationship exists between

the emissions from the average motor vehicle and the number of days each year that

the oxidant concentration in the air exceeds the clean air standard

The oxidant trendlines for downtown Los Angeles Pasadena arrl Azusa are

all downward and the slopes are about the same This similarity is logical because

the process that results in the suppression of oxidant accumulation simply has been

displaced from one area to another This was a unique one time situation because

of the increase in NOx between 1966 and 1971 After 1971 all areas are down Thus

l

250

the same conclusion is reached that the oxidantstandard will be met in the 1980s

I whether air quality data or vehicle emissions trends are projected middot~ Ul-

This outlook is based on the APCD s belief that future growth in both the

Los Angeles area and SCAB will not create any locality with a traffic density greater

than any traffic density in the area to date For the past 25 years the area around

downtown Los Angeles has been the area of maximum traffic density and therefore

the emissions source area responsible for the maximum effect area measurements

It is assumed that the traffic density in any future source area will be no

greater than the traffic density in downtown Los Angeles Thus since the

vehicular emissions control program will achieve and maintain the air quality

standards in areas affected by vehicular emissions from downtown Los Angeles it

will also achieve and maintain them for any area of SCAB

Summary Conclusions and Recommendations

In conclusion we have shown that a source and effect area analysis of emisshy

sions and resulting oxidant is a more reasonable and accurate representation of

the Los Angeles area for air quality analysis than gross integration metho9s such

as the big box technique It has been shown that motor vehicles are the major and

almost sole contributor to the primary HC and NOx emissions in the downtown source

area which results in the high oxidant levels in the San Gabriel Valley in fact the

highest in SCAB An air quality model and vehicle emissions control strategy has

been suggested to meet the oxidant standard by mid-1980 s

251

We have shown that

bull Only by adjusting the ratio of NOxHC in the motor vehicle emissions to

permit accumulation of sufficient atmospheric NO to sea venge the normal

atmospheric background oxidant can the standard be attained

bull The APCD strategy which provides for implementation of the present

California interim emissions standards for NOx HC and CO for new

motor vehicles in California beginning with the 1975 model vehicles will

result in compliance with the CO N02 and oxidant air quality standards

by the mid 1980 s and will maintain this compliance until 1990 and

possibly longer

bull The effectiveness of the present California motor vehicle control program

is easily demonstrable using air quality data from several areas in Los

Angeles County 1960-1973

bull To assure achievement and maintenance of the air quality goals as now preshy

dicted there must be periodic assessments of the effectiveness of the

motor vehicle control program followed by corrective actions if necessary

What has been accomplished thus far is significant but much more remains

to be done so that the best possible representation of emissions and resulting air

quality may be available for use in this air basin A much better emission inventory

defining the spatial and temporal distribution of both mobile and stationary sources

is needed Better statbnary source information is needed to evaluate the local

effects of these emissions Further detailed studies are needed to establish the

252

true relationship between emissions data from vehicle test cycles and the actual

operation of vehicles neither the 7-mode nor the CVS procedure provides a true

representation of actual vehicle operation Further tracer studies to assess the

transport and dilution of mobile and stationary source emissions from selected

source areas are also needed

253

1111

IUD

a CC I w gt-

1111

1UO

IUD

I 990

IDJO

1180

1111

IUO

FIGURE I

HYDROCARBONS

STATIONARY SOURCES MOTOR VEHICLES

- --

8 12 II 20 742 2l IS 12 I 4

HUNDREDS

HYDROCARBON EMISSIONS STATIONARY SOURCES IN

OXIDES OF

0

OF TONSDAY

FROM MOTOO VEHICLES AND LOS ANGELES COUNTY

NITROGEN

STATIONARY SOURCES

MOTOR VEHICLES

011111111111111111110111bull1111111

IIIIIIHIIIIIIIIIHIUII

llillL Its rd

l1uu~111111u1111111

2 I O 1 J 3

HUND REDS OF TONSDAY

OXIDES OF NITROGEN EMISSIONS FROM MOTOR VEHICLES ANO STATIONARY SOURCES IN LOS ANGELES COUNTY

illl~ -~--~ i~-=i _J~l ~--~ bull_~L- I ~~~-~~--Z ~

6

6S-66 ox

ICS ~A~1 M

i ssmuwmmgt

bullI

e COROyent_

64 ~ IDB RIVERS~

ORAJfD

-

t t 10 miles

bullmiddotsame Avg Cone Both Years

Pigare 2

YEAR OP HIGHEST OXlDANI CONCENTRATIONS

Highest Average of Daily -Maiimum One-Hour Concentrations

During July August amp September 1963-1972

bullLj

I

64

70 s11 3RlU)U0

70

--__ 69bull

N V +=

middot Source Air Resources Board

-200o

t t 10 adlea

tDS ampIJtsect

-1~

-1611ASampXllmiddot bull - bull -z----~------

I ldmmprwJ

IIVERSIDI

~ - 70

OampY -1 U 70 bull L

I

N V1 V

middot-i___

-----------------------------------------------------------i----------------------------

Figure 3

CHANGE OP OXIDANT CONCENTRATIONS

Percent Change from the Highest Three-Year Average to the 1970-72 Average

Of Daily Maximum One-Hour Con~entrationa for JulY August amp September

Source Air Resources Board

256

FIGURE 4 TYPICAL FLOW OF POLLUTED Am PARCEIS CIUGINATING AT DIFFERENT LOCATIONS IN THE LOS ARE~S BASIN - STARTIOO 0900 PST

l I

OAT

TRAJECTORY SUWMATIOl4

----- SMOG ~AVS

I

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullNONbullSlfOG DAYS

ISTARTING Tl~ cgxpsy

~ HAW

(CA

257

FiGURE 5 ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AND OXIDANT IN DOWlflC1N LOS AIDELES (SOURCE AREA) AND PASADENA (EFFECT AREA) 1

1960-1972

LO CARBON MONOXIDE

30

Pasadena

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullbullbullbullbull Downtown Los Angeles

20

10

o_______________________________

OXIDANT

)

2 Down~ Los Angeles

1

o________________________ 1960 1962 196L 1966 1968 1970 1972

YEAR

bullbullbullbullbull

bullbullbullbullbullbullbull

258

FIGURE 6 COMPARISON 01 CALCULATED AND MEASURED ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AN1) OXIDES OF NITROOEN IN DCMNTOWN IDS AIJELES

196o-1972

CARBON MONOXIDE

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ~ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot _-- ---_ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ----middotmiddot-bullw-_~ ---bullbullbull

10

o_______________1111111_____

OXIDES OF NITROGEN25

20

15 bullbullbullbullbullmiddotmiddotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~

1-i 10 middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ---

oS o_______________________

RATIO CONOx

40

50

0 +raquo Cd

p 30

~ 20

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot bullbullbullbullbull middotmiddotmiddotmiddotmiddot-shybullbullbullbullbull 0 u

bullbullbullbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot 10

0 j

ilI 196o 1964 1968 1970 1972 I

YEAR

Measured~D-owntown Los Angeles (90th percentile ofmiddot daily] instantaneous maxima)

Calculated - Aver~ge vehicle emissions - Present control program

259

FIGURE 7

25

t i5

flJ

~ on ~ ~ Q) bO 100 Jo

+gt on z

o5

EFFECT OF CALIFORNIA 1 s AUTO EXHAUST CONTROL ffiOORA M ON MAXIMUM CHAMBER OZONE CONCENTRATION

- PPM

357bullbull

r 76 bull

11 l

30

20

CHAMBER OZONE MAXIMUM

50

10

o___________111111111111______111111111111_____________

0 05 10 15 20 25

Hydrocarbons m-2 (LB-15) - PPM (as Hexane)middot

--

bull bull bull

r--=--~1 ~a==-~ - _~l ~ y--===-- ~~--~-- ~ r---~~

o

o8

~ I

~ 0 H 8 o6 I

c~ ~ 0 z 0 0

8

~ o+ A H gtlto-

02

middoto

Figure 8 Calculated t1ax1mum Levels Instantaneous and Hourly Average

of Atmospheric Oxidant Compared to Measured Los Angeles County Maxima-with Projections to 1990

(California Standards)

~ -Calculated Inst ax ~

f Calculate Max Hr Avg 03

_ bullbull _ _ - i bull

0 bullbull -l bullbull a0Ieasured Inst Lax o3 bull middotmiddotmiddot~bull 0bull _ ____ V ~ ea~ured ~ Hr Avr o3

~~ r---

~ ~ NB r~ima for 197 4 amiddots of 121074--- -_ Chamber Ozone F ~_ _~

- 1L_

~ Federal Primarfo Air ~uality Standard ~6- -UaximumT- our Avera~elr~ppm-------------- --~ ------- -~- -~-- ~

I I I I I I I I I I I I I I I I I N1 O

1960 6i 64 66 ~i middot-o 72 74 76 79 middotso middot92 84 bullg s9 9o

TBAR (end)

0

261 FIGURE -OMPARISON OF ATMOSPHERIC OXIDANT TRENDS WITH AVERAGE NCJx AND

HC EMISSIONS (Grams per Mile from Average Vehicle)

JOO Number of days state oxidant standara wds equalled or exceeded

--- Azusa __ Pasadena ________ Downtown Los Angeles

20

15 u

___ Hydroc_arbons Oxides of Nitrogenbullmiddotmiddotmiddotmiddotmiddotbullbullmiddot 1975 and later-assume middotcalifornia ARB standards

o_ ___________________________11111____

1965 1970 1975middot 198omiddot 198S 1990

137

3) the general field of exhaust treatment where most of the effort

has been placed by the U S auto industry

I would like to emphasize that the first area the whole matter of

mixture control that is either improving the present carburetor or

replacing it with a better mixture control system is perhaps the single

technological area which has been most overlooked by the automobile

industry The engine requires a well meteTed fuel-to-air mixture over a

wide variety of operating conditions that is good cycle-to-cycle and

cylinder-to-cylinder control The present systems simply do not do that

It is also evident that the mixture control system must operate with varying

ambient conditions of pressure and temperature The present systems do not

do that adequately There are promising developments in improvement of

mixture control systems both carbureted and fuel injection which do not

appear to be under really aggressive develJpment by the automobile industry

One should question why this is not occurring

I will skip the area of combustion modification because that really

comes under the new generation of engines The combustion modification is

an important approach and will be discussed by the next speaker

The area of exhaust system treatment the third area is the one about

which youve seen the most We early saw the use of air injection and then

improved air injection with thermal reactors Now were seeing oxidation

catalysts on essentially 100 of the U S cars sold in California There

are yet other possibilities for exhaust treatment for the control of

oxides of nitrogen based upon reduction catalysts or what is known as

threeway catalysts another variation of the reduction catalyst and

possibly also the use of particulate traps as a way of keeping lead in

gasoline if that proves a desirable thing to do (which does not appear to

be the case)

138

What about the 1975 California car Most of you probably have enough

interest in this vehicle that youve tried to figure out just what it does

But in case some of you have not been able to straighten its operation out

let me tell you as best I understand what the 1975 California car is

The cars from Detroit are 100 cataly~t eq11ipped There may be an excepshy[

l

1 tion sneaking through here and there but it looks like it is 100 These

are equipped with oxidation catalysts in a variety of configurations and

sizes the major difference being the pellet system which is used by

General Motors versus the monolith system which has been used by Ford and

Chrysler The pellet system appears to be better than the monolithic ~ l l system but it is not so obvious that there are huge differences between the

aocgtnow The catalysts come in a variety of sizes they are connected to

the engine in different ways sometimes there are two catalysts sometimes

a single catalyst (the single catalyst being on the 4 and 6-cylinder

engines) Some of the 8-cylinder engines have two catalysts some of them

have one catalyst All California cars have all of the exhaust going

through catalysts This is not true of some of the Federal cars in which

some of the exhaust goes through catalysts and some does not

Ninety percent of the California cars probably will have air pumps

Practically all the cars from Detroit have electronic ignition systems

which produce more energetic sparks and more reliable ignition The

exhaust gas recirculation (EGR) systems appear to have been improved

somewhat over 1974 but not as much as one would have hoped There were

some early designs of EGR systems which were fully proportional sophistishy

cated systems These do not appear to have come into final certification

so that there still is room for further improvement of the EGR system

The emissions levels in certification of these vehicles are extremely low

139

(Table I) Just how the automc1bile industry selects the emission levels

at which they tune their vehicles has been of great interest The

hydrocarbon and CO levels in certification (with deterioration factors

applied--so this is the effective emissions of the certification vehicles

at the end of 50000 miles) are approximately one-half the California

standards The oxides of nitrogen emissions are approximately two-thirds

of the California standards This safety factor is put in by the automoshy

bile industry to allow for differences between the certification vehicles

and the production vehicles to ensure that they did not get into a situation

of recall of production vehicles which would be very expensive

There appears to have been a great deal of sophistication developed by

the automobile industry in being able to tune their vehicles to specific

emission levels General Motors appears to have done better tuning than

the other manufacturers This leads to the rather interesting result

that a significant number of the 1975 California vehicles meet the 1977

emission standards (Table II) that is approximately 10 of the U S cars

certified for California already meet the 1977 emission standards This

does not mean to say that the industry could immediately put all of their

production into such vehicles and meet the 1977 emission standards because

of a concern about the safety factor for the certification versus producshy

tion vehicles Thirty-four percent of the foreign vehicles certified for

1975 in California meet the 1977 emission standards The 1977 emission

standards are 041 grn hydrocarbon~ 34 gm carbon monoxid~ and 20 gm

oxides of nitrogen This does confirm that the oxidation catalysts are a

more than adequate technology for meeting the 1977 emission standards and

only minor refinements and adjustments to those systems are required to go

ahead with the 1977 emission standards There are some other arguments

against this optimistic viewpoint and Ill deal with those later

140

There is a great uniformity in the deBigns which the U S manufacturshy

ers have selected for the 1975 California vehicles For those of you who

do not live in California about 80 of thl~ vehicles in the rest of the

country will be catalyst equipped General Motors is going with 100

catalysts apparently to realize the fuel economy benefit of their system

which more than pays for the cost of the catalyst system We have the very

interesting situation that the more stringent 1975 emission standards have

not only reduced the emissions of the 1975 vheicles with respect to the

1973-1974 vehicles but have also reduced the cost of operating the car

and have improved fuel economy The idea that emissions control and fuel

economy and economical operation are always one at odds with the other is

simply not true Compared to the previous years vehicles the more

stringent emissions standards of 1975 have brought improvements to fuel

economy because they forced the introduction of more advanced technology

The fuel savings which have been realized produce a net decrease in operashy

tional costs over the lifetime of the car This is not to say that pollution

control doesnt cost something If you were to compare the 1975 vehicle

with a completely uncontrolled vehicle tht~re would indeed be an incremental

cost associated with the 1975 vehicle

The foreign manufacturers have demonstrated a greater variety of

approaches in meeting the 1975 California standards but again they are

producing mostly catalyst equipped vehicles There is a widespread use of

fuel injection by the foreign manufacturers especially the Europeans

apparently because this is the easiest appmiddotroach for them and they realize

that only a fraction of their production comes to the United States

Volkswagen for example apparently has gone to 100 fuel injection on its

air cooled engines to be sold in California Mazda will continue to sell

141

rotary engine vehicles and thereby be the only rotary engine vehicle

manufacturer and marketer in the United States General Motorsgt elimination

of therotary engine stated for reasons of emissions is probably more

influenced by problems with fml economy although the two are a bit

difficult to separate Mazda is meeting the 1975 emissions standards and

in fact can meet the 1977 emission standards It has not solved its fuel

economy difficulties on the 1975 cars they will do better in 1976 All

evidence points to a fuel economy penalty for the rotary engine Nonetheshy

less we do have this option available because of the Japanese Also the

foreign manufacturers are providing us with a small number of diesel

engine cars These are of great interest because of definite fuel economy

advantages The diesel engine vehicles also meet the 1977 emissions

standards right now Also in J975 well 3ee the CVCC engine marketed by

Honda

The costs of the 1975 vehicles over tae lifetime of the vehicle are

definitely lower than the costs of the 197~ vehicles The National Academy

of Sciences estimate averaged over all vehicles is that in comparison to

the 1970 vehicles the lifetime cost of emission control system including

maintenance and fuel economy costs is aboJt $250 per vehicle greater in

1975 than 1970 Since the 1974 vehicles w2re about $500 more expensive

there has been a net saving in going from 1974 to 1975 I think the

conclusion we should draw for 1975 is that the auto industry has done a

pretty good job in meeting these standards This is something which they

said they couldnt do a few years ago something which they said that if

they could do it would be much more expewdve than it has turned out to

be

The same technology can be applied to 1977 models with no technological

difficulty and only slight refinements of the systems The fuel economy

142

penalties as estimated by the National Academy of Sciences are small 3

or less in going to the 1977 standards This estimate does assume further

advancements by the auto industry to improve fuel economy--primarily

improved exhaust gas recirculation systems It is unfortunate that this

issue of fuel economy has become so mixed up with the air pollution question

because the two are only slightly related If one is really concerned about

fuel economy and there isnt too much evidence that the auto industry or

the American public really is too concerned right now there is only one

way to have a drastic effect on fuel economy and that is to decrease the

vehicle weight Until that is done with gains on the order of 50 or

more to worry about 3 or 5 differences in fuel economy related to emission

control systems is simply to focus upon the wrong issue

Now what are the problem areas What remains to be done The

problems certainly arent over with the introduction of the 1975 vehicles

Problem Area Number One Field performance What is going to happen

to these vehicles when they get into actual service Past experience with

the 1971 through 1973 vehicles has been rather poor in that EPA and

California surveillance data show that these vehicles are not meeting the

standards Many of them did not meet the standards when they were new

The situation in general is getting worse at least for CO and hydrocarbons

that is with time the emission levels of CO and hydrocarbons for the 1971 I through 1973 vehicles is degrading There is no in-service experience of

this sort with the 1975 vehicles yet The certification data look quite I promising but the test procedures especially for durability are not ithe same as what occurs in actual use It is generally stated that the

1actual use situation for the catalysts will be more severe than the EPA

test procedure A larger number of cold starts are involved in actual use

than in the EPA test procedure and thermal cycling will probably have an

143

adverse effect on the lifetime of the cata]_yst This is not so obvious

It is also likely that the higher temperature duty cycle in actual use will

improve the performance of the catalyst in that it will help to regenerate

the catalyst through the removal of contaminants as long as one does not

get into an overheat situation The National Academy of Sciences estimate

was that the number of catalyst failures tn the first 50000 miles would

be on the order of about 7 Thats a very difficult number to estimate in

the absence of any real data A 7 failure still leaves a net gain in

emissions control even if nothing is done about this failure This points

to the problem of what happens after 50000 miles The EPA certification

procedure and control program only addresses the first 50000 miles The

second 50000 miles or slightly less for the average car is the responsishy

bility of the states Unfortunately then~ seems to be very little progress

in the area of mandatory inspection and ma-Lntenance--very little thought

being given to whether the replacement ofthe catalyst at 50000 miles

if it has failed is going to be required and how that is going to be

brought about The area of field performance remains a major problem

area one which obviously needs to be monitored as the California Air

Resources Board has been doing in the past but probably even more carefully

because the unknowns are higher with the catalyst systems

Problem Area Number Two Evaporative hydrocarbons from automobiles

It was identified at least 18 months ago that the evaporative emission

control systems are not working that the evaporative emissions are on the

order of 10 times greater than generally thought In the Los Angeles

area cars which are supposed to be under good evaporative emissions

controls are emitting approximately 19 grams per mile of hydrocarbons

through evaporation This apparently has to do with the test procedure used

144

The EPA is pursuing this The California Air Resources Board does have some

consideration going on for this but it appears that the level of activity

in resolving this problem is simply not adequate If we are to go ahead

to 04 of a gram per mile exhaust emissions standards for hydrocarbons

then it just doesnt make sense to let 19 grams per mile equivalent escape

through evaporative sources

Problem Area Number Three What about the secondary effects of the

catalyst control systems Specifically this is the sulfate emissions

problem and I really do not know the answer to that Our appraisal is

that it is not going to be an immediate problem so we can find out what

the problem is in time to solve it The way to solve it now since the

automobile industry is committed to catalysts and it is unreasonable

to expect that they will reverse that technology in any short period of

time is take the sulfur out of the gasoline The cost of removing sulfur

from gasoline is apparently less than one cent per gallon Therefore if

it becomes necessary to be concerned with sulfate emissions the way to

meet the problem is to take the sulfur out of gasoline Obviously sulfate

emissions need to be monitored very carefully to see what happens The

final appraisal is certainly not now available Another secondary effect

of the catalysts is the introduction of significant quantities of platinum

into an environment where it hasnt existed before Not only through

exhaust emissions which appear to be small but also through the disposal

problem of the catalytic reactors Since the quantity of platinum involved

is quite small the argument is sometimes used that platinum does not

represent much of a problem The fact that the amount of platinum in the

catalyst is so small may also mean that its not economical to recover it

This is probably unfortunate because then the disposal of these catalysts

l Jj

145

I becomes important I will not speak to the medical issues because

am not qualified The evidence is that theuro~ platinum will be emitted in a

form which does not enter into biological cycles--but this is no assurance

that it couldnt later be transformed in such a form What is obviously

needed is a very careful monitoring program which hopefully was started

before the catalysts were put into service If it wasnt then it should

be started today

Problem Area Number Four NO control The big problem with NO X X

control is that nobody seems to know or to be willing to establish what

the emission control level should be It is essential that this be tied

down rapidly and that it be fixed for a reiatively long period of time

because the NO level is going to have a VE~ry important ef feet upon the X

development of advanced engine technology The 20 gm level has been

attained in California with some loss of fuel economy through the use of

EGR and it is not unreasonable in our estimation to go to 15 grams per

mile with very little loss in fuel economy To go to 04 gram per mile

with present technology requires the use of one of two catalytic systems

either the reduction catalyst in tandem with the oxidation catalyst or what

is known as the three-way catalyst Both of these systems require technoshy

logical gains The state of development appears to be roughly that of the

oxidation catalyst two years ago The auto industry will probably say

that it is not quite that advanced but that if it were required to go to

04 gram per mile in 1978 that it could be done With the catalyst systems

the fuel economy penalties would not be great in fact the improvement to

the engine which would be required to make the system work would again

probably even allow a slight improvement in fuel economy What the 04

gram per mile NO catalyst system would appear to do however is to X

146

eliminate the possibility of the introduction of stratified charge engines

both the CVCC and the direction injection system and also diesel engines

It is in the context of the advantages of these advanced engines to meet

emission standards with improved fuel economy that one should be very

cautious about the 04 grammile oxides of nitrogen standards for automoshy

biles My own personal opinion is that the number should not be that

stringent that a number of 1 or 15 gm is appropriate Such a level

would require advancements but would not incur great penalties

Other items which I view as problem areas are less technically

involved and therefore require fewer comments

bull Nonregulated pollutants--again thls is a matter of keeping track

of particulates aldehydes hydrocarbon composition to make

certain that important pollutants ire not being overlooked or

that emission control systems are not increasing the output of

some of these pollutants

bull Fuel economy The pressures of fuel economy are going to be used

as arguments against going ahead wlth emissions control Mostly

these two can be resolved simultaneously We should simply ask

the automobile industry to work harder at this

bull Final problem area New fuels Again it does not appear that

the introduction of new fuels will come about as an emissions

control approach but that they may be introduced because of the

changing fuel availability patterns and the energy crisis These

fuels should be watched carefully for their impact upon emissions

This does middotappear to be an area in which a great deal of study is

going on at the present time It is one problem area perhaps in

which the amount of wprk being done is adequate to the problem

which is involved

147

In sunnnary then the appraisal of the 1975 systems is that they are

a big advancement they will be a lot better than most of us thought and

that we should give the automobile industry credit for the job theyve

done in coming up with their emissions control systems

With that boost for the auto industry which Im very unaccustomed

to Ill entertain your questions

-------=-~ ~~~ U- ~a1

~_~a--~-~ -J~ ~ -~r- _ --=~-- -___ja--~ __1~~ ~-~----=

AIR

1-4 FUEL----1

I I ENGINE

I II

_________ EXHAUST SYSTEM I bull EXHAUST

I I I

+ MIXTURE CONTROL COMBUSTION MODIFICATION EXHAUST TREATMENT

FuelAir Metering Ignition Air Jnjection FuelAir Mixing Chamber Geometry Thermal Reactor Fuel Vaporization Spark Timing Oxidation Catalyst Mixture Distribution Staged Combustion Reduction Catalyst Fuel Characteristics Ex tern almiddot Combustion Three Way Catalyst Exhaust Gas Redrculation Particulate Trap

FIGURE 1 Approaches to the Control of Engine Emissions

~ i 00

149

TABLE I

Average Emissions of 1975 Certification Vehicles (As Corrected Using the 50000-Mile Deterioration Factor)

Emissions in gmi Fraction of Standard HC CO NO HC CO NO

Federal 1975 X X

AMC 065 67 25 043 045 080

Chrysler 074 77 25 049 051 082

Ford 081 92 24 054 061 078

GM 083 80 23 055 053 074

Weighted Average 080 82 24 053 055 076

California 1975

AMC 042 49 17 047 054 087

Chrysler 048 61 16 053 067 082

Ford 052 56 13 058 062 067

GM 065 55 16 0 72 061 082

Weighted Average 058 56 16 064 062 078

kWeighted average assumes the following market shares AMC 3 Chrysler 16 Ford 27 and GM 54

150

TABLE II

Total Number of Vehicles Certified for California 1975 Standard and the Number (and percentage) of These Able to Meet

Certain More Stringent Standards

Calif 1975 Federal 1977 Hypothesized Hypothes ized 099020 04J420 049020 093420

i ~

Manufacturer no () no () no () no ()

AMC 16 (100) 1 ( 6) ti ( 38) 3 (19)

Chrysler 21 (100) 2 ( 9) ( 33) 0 ( O)

Ford 26 (100) 4 (15) -middot ( 15) 5 (19)

l GM 46 (100) 1 ( 2) -1 ( 9) 5 (11)

Foreign 62 (100) 21 (34) 3H (61) 28 (45)

1J

f

-l

151

CURRENT STATUS OF ALTERNATIVE AUTOM)BIIE ENGINE TECHNOLCXY

by

Henry K Newhall Project Leader Fuels Division

Chevron Research CanpanyRicbmmd California

I

iH1middot

10 1ntroduction and General Background

I

11 General

The term stratified ct1arge englne has been used for many

years in connection with a variety of unconventional engine

combustion systems Common to nearly all such systems is

the combustion of fuel-air mixtures havlng a significant

gradation or stratification in fuel- concentration within the

engine combustion chamber Henee the term nstratifled charge

Historically the objective of stratified charge engine designs

has been to permit spark ignition engine operation with average

or overall fuel-air ratios lean beyond the ignition limits of

conventional combustion systems The advantages of this type

of operation will be enumerated shortly Attempts at achieving

this objective date back to the first or second decade of this

century 1

More recently the stratified charge engine has been recognized

as a potential means for control of vehicle pollutant emissions

with minimum loss of fuel economy As a consequence the

various stratified charge concepts have been the focus of

renewed interest

152

12 Advantages and Disadvantages of Lean Mixture Operation

Fuel-lean combustion as achieved in a number of the stratified

charge engine designs receiving current attention has both

advantages and disadvantages wnen considered from the comshy

bined standpoints of emissionsmiddot control vehicle performance

and fuel economy

Advantages of lean mixture operation include the following

Excess oxygen contained in lean mixture combustion

gases helps to promote complete oxidation of hydroshy

carbons (HG) and carbon monoxide (CO) both in the

engine cylinder and in the exhaust system

Lean mixture combustion results in reduced peak

engine cycle temperatures and can therefore yield

lowered nitrogen oxide (NOx) emissions

Thermodynamic properties of lean mixture combustion

products are favorable from the standpoint of engine

cycle thermal efficiency (reduced extent cf dissociashy

tion and higher effective specific heats ratio)

Lean mixture operation caG reduce or eliminate the

need for air throttling as a means of engine load

control The consequent reduction in pumping losses

can result in significantly improved part load fuel

economy

153

Disadvantages of lean mixture operation include the following

Relatively low combustion gas temperatures during

the engine cycle expansion and exhaust processes

are inherent i~ lean mixture operation As a conseshy

quence hydrocarbon oxidation reactions are retarded

and unburned hydrocarbon exhaust emissions can be

excessive

Engine modifications aimed at raising exhaust temperashy

i tures for improved HC emissions control (retarded middot~

ignition timing lowered compression ratlo protrtacted combustion) necessarily impair engine fuel economy1 I

1j bull If lean mixture operation is to be maintained over ~

the entire engine load range maximum power output t l and hence vehicle performance are significantly

impaired

Lean mixture exhaust gases are not amenable to treatshy

ment by existing reducing catalysts for NOx emissions

control

Lean mixture combustion if not carefully controlled

can result in formation of undesirable odorant

materials that appear ln significant concentrations

in the engine exhaust Diesel exhaust odor is typical

of this problem and is thought to derive from lean mixshy

ture regions of the combustion chamber

154

Measures required for control of NOx emissions

to low levels (as example EGR) can accentuate

the above HC and odorant emissions problems

Successful developmentmiddotor the several stratified charge

engine designs now receiving serious attention will depend

very much on the balance that can be achieved among the

foregoing favorable and unfavorable features of lean comshy

bustion This balance will of course depend ultimately on

the standards or goals that are set for emissions control

fuel economy vehicle performance and cost Of particular

importance are the relationships between three factors -

UBHC emissions NOx emissions and fuel economy

13 Stratified Charge Engine Concepts

Charge stratification permitting lean mixture operation has

been achieved in a number of ways using differing concepts

and design configurations

Irrespective of the means used for achieving charge stratifishy

cation two distinct types of combustion process can be idenshy

tified One approach involves ignition of a small and

localized quantity of flammable mixture which in turn serves

to ignite a much larger quantity of adjoining or sur~rounding

fuel-lean mixture - too lean for ignition under normal cirshy

cumstances Requisite m1xture stratification has been achieved

155

in several different ways rangiDg from use of fuel injection

djrectly into open combustion chambers to use of dual

combustion chambers divided physically into rich and lean

mixture regions Under most operating conditions the

overall or average fuel-air ratio is fuel-lean and the

advantages enumerated above for lean operation can be realized

A second approach involves timed staging of the combustion

process An initial rich mj_xture stage in which major comshy

bustion reactions are completed is followed by rapid mixing

of rich mixture combustion products with an excess of air

Mixing and the resultant temperature reduction can in

principle occur so rapidly that minimum opportunity for NO

formation exists and as a consequence NOx emissions are

low Sufficient excess air is made available to encourage

complete oxidation of hydrocarbons and CO in the engine

cylinder and exhaust system The staged combustion concept

has been specifically exploited 1n so-called divided-chamber

or large volume prechamber engine designs But lt will be

seen that staging is also inherent to some degree in other

types of stratified charge engines

The foregoing would indicate that stratified charge engines

can be categorized either as lean burn engines or staged

combustion engines In reality the division between conshy

cepts is not so clear cut Many engines encompass features

of both concepts

156

14 Scope of This Report

During the past several years a large number of engine designs

falling into the broad category of stratified charge engines

have been proposed Many of these have been evaluated by comshy

petent organizations and have been found lacking in one or a

number of important areas A much smaller number of stratified

charge engine designs have shown promise for improved emissions

control and fuel economy with acceptable performance durashy

bility and production feasibility These are currently

receiving intensive research andor development efforts by

major organizations - both domestic and foreign

The purpose of this report is not to enumerate and describe the

many variations of stratified charge engine design that have

been proposed in recent years Rather it is intended to focus

on those engines that are receiving serious development efforts

and for which a reasonably Jarge and sound body of experimental

data has evolved It is hoped that this approach will lead to

a reliable appraisal of the potential for stratified charge

engine systems

20 Open-Chamber Stratified Charge Engines

21 General

From the standpoint of mechanical design stratified charge

engines can be conveniently divided into two types open-chamber

and dual-chamber The open-chamber stratjfied charge engine

has a long history of research lnterest Those crigines

157

reaching the most advanced stages of development are probably

the Ford-programmed c~mbustion process (PROC0) 2 3 and Texacos

controlled combustion process (TCCS) 4 5 Both engines employ a

combination of inlet aar swirl and direct timed combustion

chamber fuel injection to achieve a local fuel-rich ignitable

mixture near the point of ignition _For both engines the overshy

all mixture ratio under most operating conditions is fuel lean

Aside from these general design features that are common to

the two engiries details of their respective engine_cycle proshy

cesses are quite different and these differences reflect

strongly in comparisons of engine performance and emissions

characteristics

22 The Ford PROCO Engin~

221 Description

The Ford PROCO engine is an outgrowth of a stratified charge

development program initiated by Ford in the late 1950s The

development objective at that time was an engine having dieselshy

like fuel economy but with performance noise levels and

driveability comparable to those of conventional engines In

the 1960s objectives were broadened to include exhaust

emissions control

A recent developmental version of the PROCO engine is shown in

Figure 2-1 Fuel is injected directly into the combustion chamber

during the compression stroke resulting in vaporjzation and

formation of a rich mixture cloud or kernel in the immediate

158

vicinity of the spark plug(s) A flame initiated in this rich

mixture region propagates outwardly to the increasingly fuelshy

lean regions of the chamber At the same time high air swirl

velocities resulting from special orientation of the air inlet

system help to promote rapid mixing of fuel-rich combustion

products with excess air contained in the lean region Air

swirl is augmented by the squ1sh action of the piston as it

approaches the combustion chamber roof at the end of the comshy

pression stroke The effect of rapid mixing can be viewed as

promoting a second stage of cori1bustion in which rlch mixture

zone products mix with air contained in lean regions Charge

stratification permits operation with very lean fuel-air mixshy

tures with attendent fuel economy and emissj_ons advantages In

addition charge stratification and direct fuel injection pershy

mit use of high compression ratios with gasolines of moderate

octane quality - again giving a substantial fuel economy

advantage

Present engine operation includes enrichment under maximum

power demand conditions to mixture ratios richer than

stoichiometric Performance therefore closely matches

that of conventionally powered vehicles

Nearly all PROCO development plans at the present time include

use of oxidizing catalysts for HC emissions control For a

given HC emissions standard oxidizing catalyts permit use

of leaner air-fuel ratios (lower exhaust temperatures)

1

l

159

together with fuel injection and ignition timing charactershy

istics optimized for improved fuel economy

222 Emissions and Fuel Economy

Figure 2-2 is a plot of PROCO vehicle fuel economy versus NOx

emissions based or1 the Federal CVS-CH test procedure Also

included are corresponding HC and CO emissions levels Only

the most recent test data have been plotted since these are

most representative of current program directions and also

reflect most accurately current emphasis on improved vehicle

fuel economy 6 7 For comparison purposes average fuel

economies for 1974 production vehicles weighing 4500 pounds

and 5000 pounds have been plotted~ (The CVS-C values

reported in Reference 8 have been adjusted by 5 to obtain

estimated CVS-CH values)

Data points to the left on Figure 2-2 at the o4 gmile

NOx level represent efforts to achieve statutory 1977

emissions levels 6 While the NOx target of o4 gmile was

met the requisite use of exhaust gas recirculation (EGR)

resulted in HC emissions above the statutory level

A redefined NOx target of 2 gn1ile has resulted in the recent

data points appearing in the upper right hand region of

Figure 2-2 7 The HC and CO emissions values listed are

without exhaust oxidation catalysts Assuming catalyst middotl

conversion efficiencies of 50-60 at the end of 50000 miles

of operation HC and CO levels will approach but not meet

160

statutory levels It is clear that excellent fuel economies

have been obtained at the indlcated levels of emissions

control - some 40 to 45 improved re1at1ve to 1974 produc-

tj_on vehicle averages for the same weight class

The cross-hatched horizontal band appearing across the upper

part of Figure 2-2 represents the reductions in NOx emissions

achieveble with use of EGR if HC emissions are unrestricted

The statutory 04 gmile level can apparently be achieved

with this engine with little or no loss of fuel economy but

with significant increases in HC emissions The HC increase

is ascribed to the quenching effect of EGR in lean-middotmixture

regions of the combustion chamber

223 Fuel Requirements

Current PROCO engines operated v1ith 11 1 compression ratio

yield a significant fuel economy advantage over conventional

production engines at current compression ratios According

to Ford engineers the PROCO engine at this compression

ratio j_s satisfied by typical fu1J-boi1ing commercial gasoshy

lines of 91 RON rating Conventional engines are limited to

compression ratios of about 81 and possibly less for

operation on similar fuels

Results of preliminary experiments indicate that the PROCO

engine may be less sensitive to fuel volatility than convenshy

tional engines - m1 important ff1ctor in flextb1 llty from the

standpoint of the fuel supplier

161

224 Present Status

Present development objectives are two-fold

Develop calibrations for alternate emissions target

levels carefully defining the fueleconofuy pbtenshy

tial associated with each level of emissions control

Convert engine and auxiliary systems to designs

feasible for high volume production

23 The Texaco TCCS Stratified Charge Engine

231 General Description

Like the Ford PROCO engine Texacos TCCS system involves_

coordinated air swirl and direct combustion chamber fuel

injection to achieve charge stratification Inlet portshy

induced cylinder air swirl rates typically approach ten times

the rotational engine speed A sectional view of the TCCS

combustion chamber is shown in Figure 2-3

Unlike the PROCO engine fuel injection in the TCCS engine

begins very late in the compression stroke - just before th~

desired time of ignition As shown in Figure 2-4 the first

portion of fuel injected is immediately swept by the swirling

air into the spark plug region where ignition occurs and a

flame front is established The continuing stream of injected

fuel mixes with swirling air and is swept into the flame

region In many respects the Texaco process resembles the

162

spray burning typical of dj_esel combustion ~r1th the difshy

ference that ignition is achieved by energy from an elec-

tric spark rather than by high compression temperatures

The Texaco engine like the diesel engine does not have a

significant fuel octane requirement Further use of positive

spark ignition obviates fuel I

cetane requirements character-

istic of diesel engines The resultant flexibility of the

TCCS engine regarding fuel requirements is a si~1ificant

attribute

In contrast to the TCCS system Fords PROCO system employs

relatively early injection vaporization and mixing of fuel

with air The combustion process more closely resembles the

premixed flame propagation typical of conventional gasoline

engines The PROCO engine therefore has a definite fuel

octane requirement and cannot be considered a multifuel

system

The TCCS engine operates with hi__gh compression ratios and

with little or no inlet air throttling except at idle conshy

ditions As a consequence fuel economy is excellent--both

at full load and under part load operating conditions

232 Exhaust Emissions and Fuel Economv

Low exhaust temperatures characteristlc of the TCCS system

have necessitated use of exhaust oxidation catalysts for

control of HC emissions to low lf~Vels A11 recent development

163

programs have therefore included use of exhaust oxidation

catalysts and most of the data reported here r~present tests

with catalysts installed or with engines tuned for use with

catalysts

Figures 2-5 and 2-6 present fuel economy data at several

exhaust emissions levels for two vehicles--a US Army M-151

vehicle with naturally aspirated 4-cylinder TCCS conversion

and a Plymouth Cricket with turbocharged 4-cylinder TCCS

engine 9 10 1urbocharging has been used to advantage to

increase maximum power output Also plotted in these figures

I are average fuel economies for 1974 production vehicles of

similar weight 8

I When optimized for maximum fuel economy the rrccs vehicles

can meet NOx levels of about 2 gmile It should be noted

that these are relatively lightueight vehicles and that

increasing vehicle weight to the 4000-5000 pound level could

result in significantly increased NOx emissions Figur~s 2-5

and 2-6 both show that engine modifications for reduced NOx

levels including retarded combustion timing EGR and increased

exhaust back pressure result in substantial fuel economy

penalties

For the naturally aspirated engine reducing NOx emissions

from the 2 gmile level to O l~ gmile incurred a fuel

economy penalty of 20 Reducing NOx from the tllrbocharged

164

engine from 15 gmile to 04 gmile gave a 25 fuel economy

penalty Fuel economies for both engines appear to decrease

uniformly as NOx emissions are lowered

For the current TCCS systems most of the fuel economy penalty

associated with emissions control can be ascribed to control

of NOx emissions although several of the measures used for

NOx control (retarded cornbusticn timing and increased exhaust

back pressure) also help to reduce HG emissions HC and CO

emissions ari effectively controlled with oxidation catalysts

resulting in relatively minor reductions in engine efficiency

233 TCCS Fuel Reauirements

The TCCS engine is unique among current stratified charge

systems in its multifuel capability Successful operation

with a nuraber of fuels ranging from gasoline to No 2 diesel

Table 2-I

Emissions and Fuel Economy of Turbocharged TCCS Engine-Powered Vehicle 1

Fuel

Emissions gMile 2 Fuel Economy

mng 2HC co NOx

Gasoline

JP-4

100-600

No 2 Diesel

033

026

014

027

104

109

072

J bull l ~

-

061

050

059

060

197

202

213

230

1M-151 vehicle 8 degrees coffibustion retard 16 light load EGR tw0 catalysts (Ref 10)

2 CVS-CH 2750 pounds tnert1a welght

165

l

has been demonstrated Table ~-I lists emissions levels and

fuel economies obtained with a turbocharged TCCS-powered

M-151 vehicle when operated on each of four different fuels 10

These fuels encompass wide ranges in gravity volatjlity

octane number and cetane leve 1 as middotshown in Table 2-II

Table 2-II

Fuel Specifications for TCCS Emissions Tests (Reference 10)

Gravity 0 API Sulfur

OFDistillation~

Gasolj_ne 100-600 JP-4 No 2

Diesel

88 -

86 124 233 342 388

0024 912

-

486 012

110 170 358 544 615

0002 57 356

541 0020

136 230 314 459 505

-middot --

369 0065

390 435 508 562 594

--

lta 9

IBP 10 50 90 EP

TEL gGal Research Octane Cetane No

Generally the emissions levels were little affected by the

wide variations in fuel properties Vehicle fuel economy

varied in proportion to fuel energy content

As stated above the TCCS engine is unique in its multifuel

capability The results of Tables 2-I and 2-II demonshy

strate that the engine has neither 8ign1ficant fuel octane

nor cetane requirements and further that it can tolerate

166

wide variations j_n fuel volati1tty rhe flexibility offered

by this type of system could be of major importance in

future years

234 Durability Performance Production Readiness

Emissions control system durability has been demonstrated by

mileage accumulation tests Ignltion system service is more

severe than for conventional engines due to heterogeneity of

the fuel-air mixture and also to the high compression ratios

involved The ignition system has been the subject of

intensive development and significant progress in system

reliability has been made

A preproduction prototype engine employing the TCCS process is

now being developed by the Hercules Division of White Motors

Corporation under contract to the US Army Tank Automotive

Command Southwest Research Inr)titute will conduct reliability

tests on the White-developed enGines when installed in Military

vehlcles

30 Small Volume Prechambcr Eng1nes (3-Valve Prechamber Engines Jet Ignition Engines Torch Ignition Engines)

31 General

A number of designs achieve charge stratification through

division of the combustion region into two adjacent chambers

The emissions reduction potentiampl for two types of dualshy

chamber engines has been demonstrated F1 rst ~ j n B desJgn

trad1t1on~JJy caJJld the nrreebrnber engine a 2m211 auxil1ary

167

or ignition chamber equipped w1th a spark plug communicates

with the much larger main combustion chamber located in the

space above the piston (Figure 3-1) The prechamber which

typically contains 5-15 of the total combustion volume

is supplied with a small quantity of fuel-rich ignitable

fuel-air mixture while a large quantity of very lean and

normally unignitable mixture is applied to the main chamber

above the piston Expansion of high temperature flame

products from the prechamber leads to ignition and burning

of the lean maj_n chamber fuel-a_r charge Ignitionmiddot and

combustion in the lean main chamber region are promoted both

by the high temperatures of prechamber gases and bythe

mixing that accompanies the jet-like motion of prechamber

products into the main chamber

I jl

I i j

I

Operation with lean overall mixtures tends to limit peak comshy

bustion temperatures thus minimizing the formation of nitric

oxide Further lean mixture combustion products contain

sufficient oxygen for complete oxidation of HC and CO in the

engine cylinder and exhaust system

It should be reemphasized here that a iraditional problem

with lean mixture engines has been low exhaust temperatures

which tend to quench HC oxidation reactions leading to

excessive emissions

Control of HC emissions to low levels requires a retarded or

slowly developing combustion process The consequent extenshy

sion of heat release j nto 1ate porttt)ns of the engtne cycle

168

tends to raise exhaust gas temperatures thus promoting

complete oxidation of hydrocarbons and carbon monoxide

32 Historical Background and Current Status

321 Early Developm9nt Objectives and Engine Def igns

The prechamber stratified charge engine has existed in various

forms for many years Early work by Ricardo 1 indicated that

the engine could perform very efficiently within a limited

range of carefully controlled operating conditions Both

fuel-injected and carbureted prechambcr engines have been

built A fuel-injected design Lnittally conceived by

Brodersen 11 was the subject of extensive study at the

University of Rochester for nearly a decade 12 13 Unforshy

tunately the University of Rochester work was undertaken prior

to widespread recognition of the automobile emissions problem

and as a consequence emission characteristics of the

Brodersen engine were not determined Another prechamber

engine receiving attention in the early 1960s is that conshy

ceived by R M Heintz 14 bull The objectives of this design

were reduced HC emissions incr0ased fuel economy and more

flexible fuel requirements

Experiments with a prechamber engine design called the torch

ignition enginen were reported n the USSR by Nilov 15

and later by Kerimov and Mekhtier 16 This designation

refers to the torchlike jet of hot comhust1on gases issuing

169

from the precombustion chamber upon j_gnj_ tion In a recent

publication 17 Varshaoski et al have presented emissions

data obtained with a torch ignition engine These data show

significant pollutant reductions relative to conventional

engines however their interpretation in terms of requireshy

ments based on the Federal emissions test procedure is not

clear

l

3 2 2 Current DeveloJ)ments

A carbureted middotthree-valve prechamber engine the Honda CVCC

system has received considerable recent attention as a

potential low emissions power plant 18 This system is

illustrated in Figure 3-2 Hondas current design employs a

conventional engine block and piston assembly Only_ the

cylinder head and fuel inlet system differ from current

automotive practice Each cylinder is equipped with a small

precombustion chamber communicating by means of an orifice

with the main combustion chambe situated above the piston lj

ij_ A small inlet valve is located in each precharnber Larger

inlet and exhaust valves typical of conventlonal automotive

practice are located in the main combustion chamber Proper

proportioning of fuel-air mixture between prechamber and

main chamber is achieved by a combination of throttle conshy

trol and appropriate inlet valve timing A relatively slow

and uniform burning process gjvjng rise to elevated combusshy

tion temperatures late in the expansion stroke and during

the exhaust procezs is achieved H1 gh tewperaturr--s in thin

part of the engine cycle ar-e necessary to promote complete

170

oxidation of HC and CO It si1ould be no~ed that these

elevated exhaust temperatures are necessarily obtained at

the expense of a fuel economy penalty

To reduce HC and CO emissions to required levels it has been

necessary for Honda to employ specially designed inlet and

exhaust systems Supply of extremely rich fuel-air mixtures

to the precombustion chambers requires extensive inlet manifold

heating to provide adequate fuel vaporization This is accomshy

plished with a heat exchange system between inlet and exhaust

streams

To promote maximum oxidation of HC and CO in the lean mixture

CVCC engine exhaust gases it has been necessary to conserve

as much exhaust heat as possible and also to increase exhaust

manifold residence time This has been done by using a relashy

tively large exhaust manifold fitted with an internal heat

shield or liner to minimize heat losses In additj_on the

exhaust ports are equipped with thin metallic liners to

minimize loss of heat from exhaust gases to the cylinder

head casting

Engines similar in concept to the Honda CVCC system are under

development by other companies including Ttyota and Nissan

in Japan and General Motors and Fo~d in the United States

Honda presently markets a CVCC-powered vehicle tn tTapan and

plans US introduction in 1975 Othe~ manufactur~rs

includlnr General Motors and Forgtd 1n thr U S havf~ stated

171

that CVCC-type engines could be manufactured for use in limited

numbers of vehicles by as early as 1977 or 1978

33 Emissions and Fuel Economywith CVCC-Type Engines

331 Recent Emissions Test Results

Results of emissions tests with the Honda engine have been very

promising The emissions levels shown in Table 3-I are typical

and demonstate that the Honda engine can meet statutory 1975-1976

HC and CO stindards and can approach the statutory 1976 NOx

standard 19 Of particular importance durability of this

system appears excellent as evidenced by the high mileage

emissions levels reported in Table 3-I Any deterioration of

l emissions after 50000 miles of engine operation was slight

and apparently insignificant

I Table 3-I

Honda Compound Vortex-Controlled Combustion-Powered Vehicle 1 Emissions

Fuel Economy

Emissions 2 mpg gMile 1972

HC 1975 FTP FTPco NOv

210 50000-Mile Car+ No 2034 Low Mileage Car 3 No 3652 018 212 221089

024 065 198 1976 Standards

213175 20o41 34 - -04o411977 Standards 34 - -

1Honda Civic vehicles 2 1975 CVS C-H procedure with 2000-lb inertia weight3Average of five tests aAverage of four tests

172

Recently the EPA has tested a larger vehicle conve~ted to the

Honda system 20 This vehicle a 1973 Chevrolet Impala with

a 350-CID V-8 engine was equipped with cylinder heads and

induction system built by Honda The vehicle met the present

1976 interim Federal emissions standards though NOx levels

were substantially higher than for the much lighter weight

Honda Civic vehicles

Results of development tests conducted by General Motors are

shown in Table 3-II 21 These tests involved a 5000-pound

Chevrolet Impala with stratified charge engine conversion

HC and CO emissions were below 1977 statutory limits while

NOx emissions ranged from 15 to 2 gmile Average CVS-CH

fuel ec9nomy was 112 miles per gallon

Table 3-II

Emissions and Fuel Economy for Chevrolet Impala Strmiddotatified

Charge Engine Conversion (Ref 21)

Test

Exhaust Emlssions

gMile 1 Fuel

Economy mpgHC co NOx

1 2 3 4 5

Average

020 026 020 029 0 18

023

25 29 31 32 28

29

17 15 19 1 6 19

17

108 117 114 109 111

112

1cvs-CH 5000-lb inertia weight

173

I

332 HC Control Has a Significant Impact on Fuel Economy

In Figure 3-3 fuel economy data for several levels of hydroshy

carbon emissions from QVCC-type stratified charge engines

are plotted 22 23 ~ 24 At the 1 gmile HC level stratified

charge engine fuel economy appears better than the average

fuel economy for 1973-74 production vehicles of equivalent

weight Reduction of HC emissions below the 1-gram level

necessitates lowered compression ratios andor retarded

ignition timing with a consequent loss of efficiencymiddot For

the light-weight (2000-pound) vehicles the O~ gmile IIC

emissions standard can be met with a fuel economy of 25 mpg

a level approximately equal to the average of 1973 producshy

tion vehicles in this weight class 8 For heavier cars the

HC emissions versus fuel economy trade-off appears less

favorable A fuel economy penalty of 10 relative to 1974

production vehicles in the 2750-pound weight class is

required to meet the statutory 04 gmile HC level

333 Effect of NOx Emissions Control on Fuel Economy

Data showing the effect of NOx emissions control appear in

Figure 3-~ 22 These data are based on modifications of a Honda

CVCC-powered Civic vehicle (2000-pound test weight) to meet

increasingly stringent NOx standards ranging from 12 gmile

to as low as 03 gmile For all tests HC and CO emissions

are within the statutory 1977 standards

NOx control as shown in Figure 3-4 has been effected by use

of exhaust gas recirculation 1n comb1nation w1th retarded

174

ignj_tion timing It is clear that control of rmx emissions

to levels below l to 1 5 gmile results in stgnificant fuel

economy penalties The penalty increases uniformly as NOx

emissions are reduced ~nd appears to be 25 or more as the

04 gmile NOx level is approached

It should be emphasized that the data of Fisure 3-4 apply

specifically to a 2000-pound vehicle With increased vehicle

weight NOx emissions control becomes more difficult and the

fuel economy penalty more severe The effect of vehicle

weight on NOx emissions is apparent when comparing the data

of Table 3-I for 2000-pound vehicles with that of Table 3-II

for a 5000-pound vehicle While HC and CO emissio~s for the

two vehicles are roughly comparable there is over a factor

of two difference in average NOx emissions

34 Fuel Requirements

To meet present and future US emissions control standards

compression ratio and maximum ignltion advance are limited

by HC emissions control rather than by the octane quality of

existing gasolines CVCC engines tuned to meet 1975 California

emissions standards appear to be easily satisfied with

presently available 91 RON commercial unleaded gasolines

CVCC engines are lead tolerant and have completed emissions

certification test programs using leaded gasolines However

with the low octane requirement of the CVCC engine as noted

above the economic benefits of lead antlknock compoundt ar-euromiddot

not realized

175

It is possible that fuel volatLLity characteristlcs may be of

importance in relation to vaporization within the high

temperature fuel-rich regions of the prechamber cup inlet

port and prechamber iQlet manifold However experimental

data on this question aomiddot not appear to be available at

present

~O Divided-Chamber Staged Combustion Engines (Large-Volume Prechamber Engines Fuel-Injected Blind Prechamber Engines)

41 General

Dual-chamber engines of a type often called divided-chamber

or large-volume prechamber engines employ a two-stage comshy

bustion process Here initial r~ich mixture combustion and

heat release (first stage of combustion) are followed by rapid

dilution of combustion products with relatively low temperature

air (second stage of combustion) The object of this engine

design is to effect the transitjon from overall rich combustion

products to overall lean products with sufficient speed that

time is not available for formation of significant quantities

of NO During the second low temperature lean stage of

combustion oxidation of HC and CO goes to completion

An experimental divided-chamber engine design that has been

built and tested is represented schematically in Figure ~-1 25 26

A dividing orifice (3) separates the primary combustion

chamber (1) from the secondary combustion chamber (2) which

includes the cylinder volume above the piston top A fuel

injector (4) supplies fuel to the primary chamber only

176

Injection timing is arranged such that fuel continuously

mixes with air entering the primary chamber during the

compression stroke At the end of compression as the

piston nears its top center position the primary chamber

contains an ignitable fuel-air mixture while the secondary

chamber adjacent to the piston top contains only air

Following ignition of the primary chamber mixture by a spark

plug (6) located near the dividing orifice high temperature

rich mixture combustion products expand rapidly into and mix

with the relatively cool air contained in the secondary

chamber The resulting dilution of combustion products with

attendant temperature reduction rapidly suppresses formation

of NO At the same time the presence of excess air in the

secondary chamber tends to promote complete oxidation of HC

and CO

42 Exhaust Emissions and Fuel Economy

Results of limited research conducted both by university and

industrial laboratories indicat~ that NOx reductions of as

much as 80-95 relative to conventional engines are possible

with the divided-chamber staged combustion process Typical

experimentally determined NOx emissions levels are presented

in Figure 4-2 27 Here NOx emissions for two different

divided-chamber configurations 8re compared with typical

emissions levels for conventional uncontrolled automobile

engines The volume ratio 8 appearing as a parameter in

Figure 4-2 represents the fraction of total combustion volume

contained in the primary chamber For a values approaching

I

i J_

177

1

05 or lower NOx emissions reach extremely low levels Howshy

ever maximum power output capability for a given engine size

decreases with decreasing 6 values Optimum primary chamber

volume must ultimately_represent a compromise between low

emissions levels and desired maximum power output

HC and particularly CO emissions from the divided-chamber

engine are substantially lower than eonventional engine

levels However further detailed work with combustion

chamber geometries and fuel injection systems will be necesshy

sary to fully evaluate the potential for reduction of these

emissions

i Recent tests by Ford Motor Company show that the large volume

prechamber engine may be capable of better HC emissions conshy

trol and fuel economy than their PROCO engine This is shown

by the laboratory engine test comparison of Table 4-I 19

Table 4-I

Single-Cylinder Low Emissions middot11 ~ _____En____g__~ne __middot _e_s_-_s_____

Engine

NO--X Reduction

Method

Em1ssions g1 hp-Hr

Fuel Economy

Lb1 hp-HrNOv HC- co

PROCO

Divided Chamber

PROCO

Divided Chamber

EGR

None

EGR

None

10 30

10 04

05 ~o

o J_o 75

130

25

l 1i bull 0

33

0377

0378

0383

0377

178

Fuel injection spray characteristics are critical to control

of HC emissions from this type of engine and Fords success

in this regard is probably due in part to use of the already

highly developed PROCO-gasoline injection system Figure 4-3

is a cutaway view of Fords adaptation of a 400-CID V-8 engine

to the divided-chamber system 2 e

Volkswagen (VW) has recently published results of a program

aimed at development of a large volume precharnber engine 29

In the Volkswagen adaptation the primary chamber which comshy

prises about 30 of the total clearance volume is fueled by a

direct timed injection system and auxiliary fuel for high

power output conditions is supplied to the cylinder region by

a carburetor

Table 4-II presents emissions data for both air-cooled and

water-cooled versions of VW s dtvided-middotchamber engine 3 0

Emissions levels while quite low do not meet the ultimate

1978 statutory US standards

179

Table 4-II

Volkswagen Jarge Volume _Jrechamber Er[ Lne Emissions

Exhaust Emissions

_ _gMile 1

___E_n_gi_n_e__t--H_C___c_o__N_O_x____E_ng__i_n_e_S_p_e_c_i_f_i_c_a_tmiddot_1_middoto_n_s__

20 50 09 841 compression ratio Air-Cooled 16-Liter

prechamber volume 28 of total clearance volume conventional exhaust manishyfold direct prechamber fuel injection

20-Liter 10 40 10 91 compression ratio Water-Cooled prechamber volume 28 of

total clearance volume simple exhaust manifold reactor direct prechamber fuel injection

1cvs c-H

Toyota also has experimented wlth ___a large volume prechamber

engine using direct prechamber fuel injection and has

reported emissions levels comparable to those of Table 4-II 31

43 Problem Areas

A number of major problems inherent in the large volume

prechamber engine remain to be 3olved I~ These problems include the following II

Fuel injection spray characteristics are critically

important to achieving acceptable HC emissions

The feasibility of producing asatisfactory injecshy

tion system hasnot been estab1ished

180

Combustion noise due to high turbulence levels and

hence high rates of heat release and pres[-ure rise

in the prechamber can be excessive It has been

shown that the-noise level can be modified through

careful chamber design and combustion event timing

If the engine is operated with prechamber fuel

injection as the sole fuel source maximum engine

power output is limited This might be overcome

by a~xiliary carburetion of the air inlet for maximum

power demand or possibly by turbocharging Either

approach adds to system complexity

The engine is charmiddotaeter1zed by low exhaust temperatures

typical of most lean mixture engines

References

1 Ricardo H R Recent Research Work on the Internal Combustion Engine 11 SAE Journal Vol 10 p 305-336 (1922)

2 Bishop I N and Simko A Society of Automotive Engineers Paper 680041 (1968)

3 Simko A Choma M A and Repco L L Society of Automotive Engineers Paper 720052 (1972)

4 Mitchell E Cobb JM and Frost R A Society of Automotive Engineers Paper 680042 (1968)

5 Mitchell E Alperstein M and Cobb JM Society of Automotive Engineers Paper 720051 (1972)

6 1975-77 Emission Control Program Status Report submitted to EPA by Ford Motor Company November 26 1973

181

if

7 consultant Report on Emissions Control of Engine Systems National Academy of Sciences Committee on Motor Vehicle Emissions Washington DC September 1974

8 Austin T C and Hellman K H Society of Automotive Engineers Paper 730790 (1973)

9 See Ref 7

10 Alperstein M Schafer G H and Villforth F J Iiil SAE Paper 740563 (1974)

11 US Patent No 2615437 and No 2690741 Method of Operating Internal Combustion Engines Neil O Broderson Rochester New York

12 Conta L~ D and Pandeli American Society of Mechanical Engineers Paper 59-SA-25 (1959)

13 Canta L D and Pandeli American Society of Mechanical Engineers Paper 60-WA-314 (1960)

14 US Patent No 2884913 0 Internal Combustion Engine R Mi Heintz i

15 Nilov N A Automobilnaya Promyshlennost No 8 (1958)

l 16 Kerimov N A and Metehtiev R I Automobilnoya Promyshlennost No 1 p8-11 (1967)

17 Varshaoski I L Konev B F and Klatskin V B Automobilnaya Promyshlennost No 4 (1970)

18 An Evaluation of Three Honda Compound Vortex Controlled Combustion (CVCC) Powered Vehicles Report B-11 issued by Test and Evaluation Branch Environmental Protection Agency December 1972

19 Automotive Spark Ignition Engine Emission Control Systems to Meet Requirements of the 1970 Clean Air Amendments report of the Emissions Control Systems Panel to the Committee on Motor Vehicle Emissions National Academy of Sciences May 1973

20 An Evaluation of a 300-CID Compound Vortex Controlled Combustion (CVCC) Powered Chevrolet Impala Report 74-13 DWP issued by Test and Evaluation Branch Environmental Protection Agency October 1973

21 See Ref 7

22 See Ref 7

23 See Ref 7

24 See Ref 7

182

25 Newhall H K and El-Messiri I A Combustion and Flame 14 p 155-158 (1970)

26 Newhall H K and El-Messiri I A Society of Automotive Engineers Transaction Ford 78 Paper 700491 (1970)

27 El-Messiri I A and Newhall H K Proc Intersociety Energy Conversion Engineering Conference p 63 (1971)

28 See Ref 7

29 Decker G and Brandstetter W MTZ Motortechnische Zeitschrift Vol 34 No 10 p 317-322 (1973)

30 See Ref 7

31 See Ref 7

183

Fig 2-1 FORD PROCO ENGINE

l

Ford Proco Engine Fuel Economy and Emissions _ 15 _ f--1

00 +

I ~ x X gt( X _ x A 7- ~ X x~ ~c - l4catalyst Feed u NOx vs ruel Econ with 1 C0-71 CJ) 14 x x Ynn H( RP c tr ir-t irm vltgtZ G I HC - C0-127 _ A txcessve c

13 Approx W EG R

~ C~~r 351 CID 5000 Lb Inertia Weight

Q 21 A L 0 u w II _j

LJ =gt LL

10

35i CD 4500 Lb Inertia Weight

~ 1974 Production Average Fuel Economy

4 soo _b r-r-r-----z~lt_~~---7--_~--r--1r-7-r1--~-rz7-w~~

150 0 0 Lb PU221ufrac122-1 I

LO 20 30

NOx EMISSIONS-GMSMILE (CVS-CH) Revised216174

0

HKN 71074

Fig 2-2

l

~___-~ ~--=---~ ~=---__---~1 f-=-----1__middot-_~J ~-----------1 ~bull-=-=- (-~-~ LJii-ZJj ~ ~~-~ ~~ -__c~~ 1--~~ ~----~--1 ---------s___-c--1 ~~~-~~~bull r~~-~--middot1 ____c__ J~ p- ~

Texaco TCCS Engine

Shrouded Intake Valve

~ Intakemiddot r~ )p__-- Fuel Nozzle Fuel Nozzte Port ~ -- -yen -_~

X f -J J ( ~1 I --- ~ f middotmiddotj_Ja 1(~-~_ frff 1-Cylinderv~ v_ r--L~ I (~~)J ~- Intake 1 - ------L- middotmiddot - middotmiddot -1 H0 ad middot --- - -- 1 Po rt I 1 I ~~ ) ~ ~ ~~~ -A- I ------

- I _ ---_ ~ P1ston-mgt-lt_ffrac12 T_77~~~--1 i- r_-~J N

- ~- i~-L - _ _ - IExhaust - - I ~ - 1-_ r- bullsect ~ ----lt_ ~ I PortJ~bJ lt 7A--7~ ~1 ~j --~ ~ yl ind er

-__~lli- klmiddot ~ro v_t_gt11J1bull Bti Or K__ - middot ~

I t--tL pgt-- Ultmiddot middot- - Spark Plugr- -1 --U2middot- ~-~

LHorizont al Projections of Nozzle and Spark Plug Centerlines

Fig 2-3 i--1 00 U1

---~---~-~ -------c- --~--- 7middot-r---c-- ~- -~~~==---~~~~~- srsr RZIIEF7 11t111-~-----==-----=-~--~-~~---c=rmiddot=

OPEN CHAMBER TYPE STRATI Fl ED CHARGE ENGINE i-shyCj

DIRECTIONAl~Fsw7 Q

NOZZLE P

I

~J~treg lt-_(__(lt-(11

c_-- _7- -

SPARK PLUG_ l 1__- -_ - l --_ ~ ----__ lt_ lt_ -- --

ltlt_I_--- _

~ gt - _____- -- --~ ~-l_- 1_~ -~- ~ ------

~~~ r_I FUEL SPRAY 2 FUEL-AIR MIXING ZONE ~- _ -------

FLAME FRONT AREA 4 COMBUSTION PRODUCTS

TCCS COMBUSTION SYSTEM

Fig 2-4

3

----==-----~ l~~----bulli r-~ ~-----=-- 1 ~~ ~ -~ ~~ ___-_=gt---l p--- --=-=-_-__71-~-~~ 1-0-- --=---=-- 4 L--_-_-~ P--- ~

25

-c u

f

Cl) 24 gt u _

tgt 23a ~

I

gt-~ 220 2 0 u w 21 _J

lJJ gt LL

2

Texaco TCCS Powered Cricket Vehicle

Max Econ Setting gt A L07 HC

141 CID JQf CR 084 CO 2500 Lb Inertia Wgt

50-so Retard_ 0_73 HC

12 co 051 HC ~ 061 HC

085COA 064CO Retard+ ESPRetard+

EGR

036 HC ~ 115 co Retard +ESP+ EGR

04 06 08 10 12 14 16 18 20 NOx EMISSIONS-GMSMILE (CVS-CH) HtltN1110114

I- 00 -JFig 2-5

-~ ~=- ~ - -i______c_J ~-====c= wr=- ~-~ p--w~~~ rr w -

25

-c u

I

(f)

gt u-lt a_

2

gt-I 20

~ 0 z 0 u LLI

_J

w tJ_

15

I- CJ) CJ)

Turbocharged Texaco TCCS Ml51 Vehicle

Max Econ Adjustment_ HC-3J catalyst Feed C0-70

141 CID 10~1 CR 2750 Inertia Weight 8deg Retard ~

~bull HC-3middot2 catalyst Feed ~~ _ C0-64

_ 5deg Retard HC-0 30 8degRetard LowEGV bullco-11 ~bull HC-3middot6 catalyst Feed WIW21

Med EGR C0-67 1974 Production 33 Average Fuel Economy ~

COmiddoti05 (2750Lb)

I

bull HC-035 co- 141 13deg Retard High EGR

04 10 20 NOx EMISSIONS -GMSMILE (CVS-CH) ~~ts~b~~~74

Fig 2-6

189

Fig 3-1

PRECHAMBER TYPE STRATIFIED CHARGE ENGINE

r Inlet

(Fuel-lean Mixture )

I 0 I

Spark -Prechamber (Fuel-rich mixture)

-Main Chamber

1] HON DA CVCC ENGINE CONCEPT

190

Fig 3-2 Honda CVCC Engine

28 -l u

1

UJ 26 -gt u-(9 CL 24 2-

f

gtshy0gt

22 z ~ _)

u w

20 _J

w ~ LL

18

J= ---- 4 --~~-_----a ~~ _-_bull --~~ 1~~1 ltiil~I ~ ~-r~ ~ -~ ~-~ ~J~-iii-1 ~~1 s _-_ __-

Fuel Economy vs HC Emissions for 3-Valve Prechamber Engines

e NOx-14 15 Liter

bull Honda CVCC 2000 LbsNOx - 12 A Datsun NVCCbull15 Liter

bull ~JOx -09 A 2500 Lbs J LL 1ter NOv -15

2750 Lbs -NOx -17

- I AiJOx -12

0 02 04 06 08 LO 0HYDROCARBON EMiSSlmiddotONS - Glv1 I MILE (CVS-CH) I-

Fig 3-3

J--1

1--Fuel Economy vs NOx Emissions IO N

-- for Honda CVCC Powered Vehiclesr 26 u

l VHc-023 U1 gt umiddot 24_-__

(_IJ o_

~ 22 l

gt-5~-0 z 20 C0-200 u A HC-033w I co -3o_j

_A HC-029w 18 J I C0-27 LL

_ HC-025

HC-017 co -2-3

C0-22

0 -- 02 04 06middot 08 10 12 NOx Ef11SSIONS -GlviS MILE (CVS-CH)

Fig 3-4 middot

I

I

i93

J J

Fig 4-1 Divided Chamber Engine

middot(4) Fuel Injector

1

f J

f ff

f

~ Ii

I f

i

I f ] [

~~

0 0 0 0

i ~ I

1jl

194

E Cl 0

C QJ

CJl 0 _

-1-

z

0

Vl (lJ

-0

X 0

-t-J

V1 ro c X

LLI

Fig ~-2

COMPARISON OF CONVENTIONAL AND DIVIDED COMBUSTION CHAMBER NOx EMISSIONS

5000 MBT Ignition Timing Wide Open Ttl rattle

4000 Conventional Charnber

3000

J = fraction of Total Combustion 2000 Volume in Primary Ct1arnber

Divided Chamber 13 = 0 85

1000

Divided Chamber fo = 0 52

05 06 0 7 08 09 10 11

O~erall Fuel-Air Equivalence Ratio

195

196

AIRBORNE SURVEYS IN URBAN AIR BASINS IMPLICATIONS FOR MODEL DEVELOPMENT

by

Donald L Blumenthal Manager of Program Development

Meteorology Research Inc Altadena California 91001

middotI would like to make several points today First ozonemiddotis basically

a regional long-range problem There is a lot of long range ozone transshy

port and this transport is a normal occurrence The second point is that

ozone is stable in the absence of scavengers Junge mentions in his book

that the residence time of ozone in the troposphere is on the order of a

month Third vertical variations in concentration and ventilation rate are i very important in modeling atmospheres such as Los Angeles Layers aloft

are ventilated down to the surface on occasion and surface pollutants are

ventilated up mountain slopes as Jim Edinger has pointed out before and

often ventilated out of the basin in upper winds Fourth the day to day

carry over of pollutants from one day to the next is a very important considshy

eration in the Los Angeles Basin Finally there is a definite background

level of ozone The geophysical literature says its about O 02 to O 03 ppm (

in various parts of the world Weve seen data varying from 003 to 005 ppm

The difference may be due to calibration differences In any case numbers

like 005 are pretty substantial background levels for ozone

I am going to illustrate the points listed above with some data from

Los Angeles Basin The data were collected during a two-year study funded

by the Air Resources Board some of the analyses were funded by EPA The

study examined the three dimensional distribution of pollutants in the Los

Angeles Basin using airborne sampling systems Coinvestigators on the

project were Dr Ted Smith and Warren White of Meteorology Research Inc (MRI)

197

The first slide shows one of the aircraft we used Its a Cessna 205

which had sampling inlets on the side of the aircraft Figure 2 shows the

instrument system on the inside of the aircraft We were measuring nitrogen

oxides ozone scattering coefficient with a nephelometer condensation nuclei

carbon monoxide and meteorological parameters such as temperature humidity

turbulance Altitude and position were also measured

Figure 4 shows that the typical sampling pattern was a series of spirals

from the top of the mixing layer over an airport virtually to ground level

then we would climb up to the next point on the route and spiral down again

We had three routes (A B C Figure 3) that we would fly We had two airshy

craft and we would fly two of these three routes three times a day any

given day that we could The day I will be talking about September 25~ 1973

we flew what was called the Riverside route (C) and the Los Angeles route

(A) The 25th of July 1973 you might remember was the day before the

federal office buildings were closed in the area here because of smog

Figure 5 shows the surface streamlines at 0300 Pacific Standard Time

about 4 oclock in the morning daylight time on July 25 This streamline

analysis points out the morning stagnation conditions which are a very normal

occurrence in the Los Angeles Basin You start out with very light winds

quite variable maybe a slight off shore flow early in the morning On this

particular day this kind of situation extended well into midday The sea

breeze did not really pick up until up around noon When you have this kind

of a situation and a low radiation inversion at night you have a

long period of accumulation of pollutants all over the Basin espt~cialJy

in the prime source area the southwest portion of the Basin

198

I

Figure 6 shows the streamline pattern at 1600--400 cclock in the

afternoon same day sea breezes develop and with them a transport pattern

that carries pollutants up to the northeast and out toward the eastern por-

tion of the Basin This is a very regular pattern which we see day after l middot

day On July 25 1973 it was a little bit exaggerated The sea breeze was

held off for awhile started a bit late and so there was a very long period

of accumulation in the southwest area and then transport across the Basin

Figure 7 is an average streamline pattern at 1600 PacHic Daylight Time

on low inversion days for August 1970 It is included to show that the pattern

shown before is very typical Flow starts in the western portion of the

Basin and goes right across to the eastern portion This is using surface

data There is a very high average wind velocity in Ontario about 13 m iles

per hour and 23 mph in Riverside This is the average for the whole month

of August at 1600 PDT on low inversion days There is a considerable amount

of transport across the Basin starting relatively slowly in the morning and

accelerating in the afternoon

Figure 8 shows a verticle cross section of the scattering coefficient

The darker areas indicate higher levels of particulates Scattering coefficshy

ient is inversely proportional to visibility In the crosshatched area

visibility is less than about 3 miles In plotting altitude versus distance

inland from the coast you have Santa Monica (SMO) on the coast El Monte (EMT)

Pomona (BRA) Rialto (RIA) Redlands (RED) The lower broken line is surface

ground level The heavy dashed line is the base of the subsidence inversion

that occurred on the two days during this episode The middle line is the

base of the marine inversion There is a large area over in the western

portion of the Basin where emissions accumulate for much of the day At

199

midday the sea breeze has just started ventilating the Santa Monica area

The layer between the inversions is a layer aloft which is fairly well separshy

ated from the surface layer Ozone concentrations for instance in the

layer aloft were on the order of 04 05 ppm using the ARB calibration

method Down in the surface layer they were quite a bit lower in the mornshy

ing due to scavenging

Figure 9 shows that by afternoon the sea breeze starts and you get

kind of a clean air front Sea breeze starts ventilating the whole Basin

the stuff that was over in the west is transported eastward and at approxishy

mately Brackett (BRA) at 1700 PDT there is a clean air front The high conshy

centrations that were over Los Angeles earlier are now centered near Upland

(CAB) The numbers shown over CAB are data taken from a vertical profile

spiral over Upland at about 1600 That turns out to be the time when there

was the worst ozone concentration of the day in the Basin and it did occur

at Upland It could well be a result of the very polluted mass from the

western Basin being transported over the Upland area The layer aloft has

been a bit undercut by the sea breeze and some of the polluted mass has been

around possibly as long as the night before There has been very little

transport in the area aloft ozone concentrations are still very high

Figure 10 shows a trajectory analysis of the air arriving at Upland at

1600 since that was the worst time of the day at Upland We developed a

trajectory envelope using surface wind data and winds aloft so the air

arriving at Upland at 1600 started out somewhere back within this envelope

for example at 1130 PDT We did not go earlier than 1130 because the winds

were pretty much light and variable before that The air that arrives at

Upland at 1600 has been over the western portion of the Basin for much of

200

the morning and q~ite a bit of the evening before Thus there is

a very long period of accumulation and then a transport a pulsing effect

where you have pollutants moved across the Basin

Figure 11 is an isopleth map of surface ozone concentrations Again all

data are corrected to agree with the ARB calibration method Again you can

see that for the hours between 1600 and 1700 using surface data the Upland

area has the highest surface ozone concentrations about 063 ppm The western

area has been well ventilated by the sea breezes and it is cleaned out

The transport is actually pretty much perpendicular to the isopleth line

just about like that

Figure 12 is a vertical profile taken over Upland Cable Airportat

roughly the time of maximum ozone concentration 1636 PDT We are plotting

pollutant concentration on the x-axis versus altitude in meters (since it was

done for an EPA report) Surface leveJ at Upland is a little over 400 meters

the Z line is ozone Ozone concentration within the surface mixing layer

is pegged on the instrument at somewhat above 05 ppm Above the surface

mixing layer it drops off considerably and eventually get down to background

The T line is temperature and you ean see the subsidence inversion

on this day is very nicely documented here and provides a very strong trap

in that area The B line is the scattering coefficient inversely proporshy

tional to visibility Within the surface mixing layer visibility is on the

order of 3 miles or less while up above the surface mixing layer just a few

hundred feet difference visibilities get up to 60 or 80 miles The X is

condensation nuclei the measure of the very fine particles below about 010

micron It is a measure of quite fresh emissions If you have a high condenshy

sation nuclei count there are very fresh combustion emissions If you have

I

201

an aged air mass the condensation nuclei coagulate and the count decreases

considerably You can see that there are still some fresh emissions within

this surface layer as well But up above the surface mixing layer all the

pollutant indicators decrease considerably

Figure 13 is the same type of vertical profile taken over El Monte

which is on the western side of the sea breeze front The sea breeze front

has passed El Monte at this time almost 1700 PDT and again there are

distinct differences between the mass below the mixing layer within the sea

breeze front (below 400 meters) the marine inversion (400 to 800 meters) and

the subsidence inversion The subsidence inversion occurs at about 800 meters

and there is an old layer of very polluted stuff aloft The surface concenshy

trations are lower because of the ventilation by the sea breeze Condensashy

tion nuclei count (X line) within the surface layer is quite high There

are still fresh emissions in the El Monte area The 11 Z line is ozone

about 02 ppm within the surface layer (200 m) but it is 05 ppm up above

the surface mixing layer The scattering coefficient (B line) is very

similar it is lower at the surface and increases to a visibility equivalent

of less than 3 miles above the surface mixing layer The condensation nuclei

count is high in the lower portion of this (eg at 600 m) hut decreases conshy

siderably above This portion of the upper layer (600 m) has been around

at least all morning and condensation nuclei have been scattered from the

area The portion of the upper layer below 600 m has probably just recently

been undercut by the sea breeze and there are still some condensation nuclei

left in it

Figure 14 illustrates a different method of looking at the flushing

problems in the Basin We have tried to develop an objective criteria based

on ground level ozone to show the cleansing of the basin using the time of

202

arrival of clean air We determine the time when the ozone concentrations

drop by a factor of two at any given point The 1600 line means that between

1500 and 1700 the ozone concentration at that point dropped a factor of two

This sort of isopleth chart of when the clean air arrives agrees quite well

with the trajectory analyses although the numbers are a little bit behind

the trajectory analyses for the polluted air Figure 14 again shows the

transport process that takes place across the Basin which is ventilated from

west to east At 1900 some of the fresh ocean air finally gets out to

Redlands

In Figure 15 in order to put this whole flux problem into some perspecshy

tive we looked at the numbers the actual amount of ozone flux across the

basin We calculated the mean trajectory from Torrance towards Redlands

using the surface and upper air data We looked at the flux from the western

basin to the eastern basin basically from Los Angeles and Orange Counties to

Riverside and San Bernardino Counties This is a calculation made at 1700 PDT

We used the winds aloft from Chino as well as the vertical profiles taken at

Pomona and Corona Averaging the ozone concentration throughout the mixing

layer and multiplying by an average wind speed we arrive at a number of 185

metric tons per hour being transported directly from one side of the Basin

to the other If you look at this in terms of actual concentration in the

eastern Basin and assume that the flow was constant for about an hour it

is eno_ugh to fill up the box shown in Figure 15 to 025 ppm ozone which

exceeds the air quality standard by a factor of three (using the ARB calibrashy

tion method) Thus there is a very significant transport of ozone or ozone

precursors from one portion of the Basin to the other side of the Basin One

thing to mention though is that the concentration would not be kept up on a

203

steady state basis because the transport is a result of the pulsing effect

I Illentioned earlier There is a lot of accumulati6n in the western Basin

and these accumulated pollutants are then transported across the Basin This

kind of transport did take place in a couple hours because we also have

measurements from 1500 PDT which give us similar flux numbers

Figure 16 is a trajectory envelope similar to Figure 10 calculated for

Upland at 1600 for the air arriving at Redlands about 600 oclock in the

afternoon I wanted to include this trajectory envelope to show that the

problem is not really simple You cannot say that the air at Redlands came

from Long Beach per se The air at Redlands if you look at the whole

envelope of possible trajectories using upper air data as well as surface

data could have come from anywhere between Downtown Los Angeles and over

the Pacific Ocean south of Long Beach

Another thing to recognize is that the wind actually changes direction

slightly as you go up and down through the mixing layer and the mixing layer

is exactly what it implies There is mixing within the mixing layer so if

you begin with a parcel of air near the surface this parcel may move to the

top of the mixing layer and go one direction for awhile it then may go back

down to the bottom of the mixing layer and move in another direction for

awhile The ratio of the length scales indicata3mixing layer depths of 1500

or 2000 ft and distances on the order of 70 miles This makes it very

difficult for tetroons to follow an air trajectory because they do not go

up and down They stay at one altitude and in one wind regime and yet the

wind regimes are different at different altitudes and the air is continually

mixed up and down through this layer You can often see this on time lapse

photographs

204

The question is where does the pollutant mass go after Redlands Figure

17 is a repeat of Jim Pitts slide from yesterday and it is data for the

same day that we did our analysis It shows the ozone peaks starting at

Pomona and Riverside and on July 25 1973 eventually getting out to Palm

Springs so there is quite a bit of long-range transport The ozone is

stable at 8 00 or 9 00 oclock at night There still are ozone concenshy

trations of 02 ppm it hasnt dissipated even at the surface Ozone does

dilute as the mass moves Other calculations we did were integrations

through the mixing layer of various pollutants such as ozone and CO along

with trajectories that we measured Th~se integrations show just what the

ground data show in Figure 17 The concentrations increase through the western

portion of the Basin and then show a decrease through the eastern portion

of the Basin CO tends to decrease faster than the ozone indicating a

continued production of ozone further east

Figure 18 is a streamline chart on a larger area map for the 16th of

August 1973 It shows the typical streamline patterns that occur for

ventilation from the Basin By mid-afternoon there is flow out through the

major passes to the north and towards Palm Springs (PSP) On this particushy

lar day we had data from Arrowhead showing that the air mass from the Basin

does indeed get up there

Figure 19 shows a vertical profile over Arrowhead early in the morning

16 August 1973 at a time when there was a north wind Ozone level was

about 005 ppm the scattering coefficient was quite low on the order of

probably 60 miles visibility or so Figure 20 is a vertical profile again

over Arrowhead late that afternoon when the winds had switched There is a

flow from the Los Angeles Basin into the Arrowhead area thus one sees a

205

vertical profile that shows a distinct increase near the surface in both the

ozone and the scattering coefficient and in the condensation nuclei Ahove

that you have fairly clean air The top of the polluted level is just about

the top of the mixing level over the Basin

I want to leave the transport now and discuss the complicated vertical

structure that can occur If you want to try to model something try this

one for instance Figure 21 is a vertical profile over Brackett Airport

Pomona about 830 in the morning on 26 July 1973 which is the day after

the episode shown earlier A bit of interpretation shows how complicated

th is can be If one looks at the temperature profile it would be very

difficult to pick out a mixing layer theres a little inversion here another

inversion there several more up here After looking at hundreds of these

profiles though you can start interpreting them What is happening is that

there is a surface mixing layer at about 500 m In this layer there is a

high condensation nuclei (X line) count due to morning traffic The San

Bernardino freeway is quite close to Brackett there is a relatively high

nitrogen oxide count about 02 ppm and the b-scat is fairly high Ozone (Z)

within the surface layer however at this time is quite low The layer beshy

tween 500 m and 700 rn turns out to be the Fontana complex plume Note the

very high b-scat level it is below 3 miles visibility the plume is very

visible especially at this time of the morning when it is fairly stab]e

There is a high nitrogen oxide level (800 m) a high condensation nuclei

level and again a deficit of ozone Above this layer (800 m) you have stuff

that has been left all night very low condensation nuclei indicating a very

aged air mass ozone concentrations about 016 ppm b-scat of about 04 It

has been around all night and not yet had a chance to mix down within the

206

surface layer In fact one good way of determining the surface mixing layer

early in the morning and at night is to look for the ozone deficit Another

thing to mention is that wind reversals occurred for each of these three

layers The winds were fairly light and westerly at the surface slightly

easterly in the 500 m 700 m layer and westerly above 800 m There is a

complicated situation early in the morning but the main problem is that by

the middle of the day there is good surface heating and the pollutants have

all been entrained and mixed down to the ground so in order to modeI what

happens on the second or third day of an episode you must be able to look

at both old pollutants as well as fresh emissions And you need to account

r for ozone that is actually transported down to the surface from layers aloft l

The next slide is a photograph (not included) which is another e xample

of some layers aloft This is due to upslope flow as explained by Jim Edinger

in his publications The mountains are heated during the day in turn heating

the air and making it buoyant there is upslope flow to a point where the

heating cannot overcome the subsidence inversion and the stuff comes right

out from the mountains and spreads out over the Basin The pollutants can

stay up there if the winds aloft are very light and on the subsequent day

will he re-entrained to the surface On the other hand if there are winds

aloft different from those in the surface mixing layer or the wind velocity

aloft is high there can be a very substantial ventilation process for the

Basin Pollutants can be ventilated up the slope and blown away in the upper

winds In the case of the entire July 25th episode winds aloft were quite

light and these upper layers remained

Figure 22 is a vertical profile of one of those upslope flow conditions

in the same location shown in the photograph but on a different day Again

207

there is a relatively high surface concentration of about 03 ppm of ozone

(Z line) a layer of clean air between 900 to 1100 m and then high concenshy

trations of ozone again above 1100 m It has gone up the slopes of the

mountains and then come back out Concentrations in the 1100 to 1300 m area

are just slightly lower than they were at 600 to 800 m area Notice however

that the condensation nuclei count (X line) is quite a bit lower mainly

because the stuff is much more aged above the 1000 m level than it is down

below 900 m

Figure 23 shows the stability of ozone the fact that it can stay around

all night long This is a vertical profile taken over Riverside about 2200

PDT 1000 oclock at night Above the surface mixing layer (600 m) there

are ozone concentrations of about 0 15 ppm (Z line) Within the surface

mixing layer (below 500 m) ozone is completely scavenged decreasing to

zero The nitrogen oxides within this surface layer are being contained and

are around 01 ppm from fresh emissions that occurred during the evening

Condensation nuclei near the surface are very high The temperature profile

is very stable You have a surface based radiation inversion which is a

little strange looking for a radiation inversion~ nevertheless it is quite

stable There is a definite restriction of the mixing--a very difficult

time getting air from below 500 m to above 500 m The ozone that exists in

the 700 m range is in air where the reactions have virtually gone to compleshy

tion and is very stable All the profiles on this night changed very little

the ozone peak stays there High concentrations stay around

Figure 24 is a cross section across theurban plume of the City of St

Louis I wanted to show that this occurrence is not limited to Los Angeles

We have seen ozone formation and transport in other urban plumes These data

l

208

were taken during a project sponsored by EPA in conjunction with R Husar of

Washington University and William Wilson of EPA The dark line on this is

the ozone concentration across the urban plume perpendicular to plume The

dashed line is the scattering coefficient The power plant plume is parallel

to the urban plume The data on the left were taken 35 kilometers down wind

about 1100 oclock in the morning The ozone concentration increases slightly

to 005 ppm in the urban plume there is a deficit of o in the power plant plume3

In the same urban plume same conditions 1500 CDT two hours later further

downwind there has been substantial increase in the ozone in the urban plume

itself The b-scat is very similar to what it was before but the ozone is

now increased quite substantially except in the power plant plume where

there is a strong deficit of ozone due to scavenging by nitrogen oxides So

the formation and transport of ozone and ozone precursors in urban plumes is

a regular occurrence that happens in more places than Los Angeles and as Bob

Neligan showed this morning it can happen over quite a bit longer distances

than we are showing here

To summarize the conclusions as they affect model development first

once ozone is formed in the absence of scavengers ozone is a very stable

compound It remains for long periods of time It can he transported for

very long distances Ozone is a regional problem which cannot be controlled

on a local basis To have effective ozone control middotone must have a regional

control strategy and probably regional type air pollution districts

A second conclusion is that the vertical distribution of pollutants can

be highly complex and models have to include more than just a simple wellshy

mixed surface layer

209

A third conclusion is that layers aloft can persist over night and can

be re-entrained within the surface mixing layer on subsequent days models

should be able to account for old pollution as well as fresh emissions Also

pollutant accumulation and transport can have distinct diurnal patterns that

are strongly dependent on the meteorology Models should be time dependent

and should start at the beginning of the accumulation period In other words

models ought to be able to run for 24 or 48 hours if they have to In this

case in Los Angeles there is often an accumulation of pollutants which starts

in one portion of the Basin at midnight and continues through the next mornshy

ing even before it starts to be transported

As far as recommendations go in many areas a lot of ambient data has

been collected and in some cases the data are actually ahead of some of the

models so I think a research program is needed in developing models that

will account for this vertical structure and the day to day carry over and

the models need to be extended to cover longer distances In addition more

smog chamber work is going to be needed in looking at the effects of carry

over and mixing old pollutants with fresh emissions How people go about

this I leave to the modelers and the smog chamber people They know more

about that than I do

I

210

I

~ INVERTER

AUDIO TAPE

MONIT0R

MONITOR OBSERVER SEAT

MON ITOR

NEPHELOMETFR FLfCTRONICS

j DIGITAL DATA LOGGER

CONDENSATION

VOR DME NEPHELOMETER TUBE

JUNCTION middoteox ASSORTED POWER

AIRBORNE

TEMPERATURE TURBULENCE

middot HUMIDITY

ALTITUDE BOX

__

middotE=-middot RECORDER ----r----------

NUCLEI KJNITOR

CONVERTER

SUPPLIES

INSTRUMENT PACKAGE (

lCO

03

Ndeg

-

-----NEPHELOMETER

BLOWER

Figure 2 Instrumentation Layout for Cessna 205

211

bullubullbullbullbull

Figure 3 Airborne Sampling Routes in the Los Angeles Basin

Figure 4 Vertie al Profile Flight Path

~-~ r~i ~~1 -- ~ ~ ~2-1~ LJ-----~ r~~ ~~ t~~--l

~ ALM l

0 RIA

ec 8v

M

~ Afo

-o

M 0

~IV

ltgt

IN J--1 N

SCALE II fi M I j_ ES 0 3 4 5 =-JSEJ--J~ _middot ~middot- - =- =

I

~

M

N~J

Figure 5 SURFACE STREAMLINE ANALYSIS - 0300 PST 25 July 1973

~~~ ~~-- cp1FJ=D -~~

~ 1

~ ~ 8c

8v

~25

PACIFIC OCEAN

diams Tt

0

9 I 4 5 10 I- m p H - -middotmiddot u 4H__8 middott_

D i6 J4 k W~D SPED llaquotl SNA NJ ~1

SCALE m ICtt84bullmh R v1s1a1L1n (mil 6 ~ CONTOURS REPRESENT

-- 10ml 16km (~() bull ~ ) ~ - 000 ft 3C5

Figure 6 S_cJRFACE WIND STREAMLINES - l 600 PDT JULY 2 S I 8 7 3

l - ~---i ~-=-___-----c---it~~-~~ r----=------1 ~-~~--cpc---_t__A --~ ---llil

~_ - ~-l-cL

34bull vi~-dff

bullbullbullbull bull ~ bull -1 bullbull - -_- L bull-J bull ~bull-bull-ii------~ bullmiddot r_ -~- ~ bullI ~_ bull bull bullbull bull I bull _ - bull -~-~ middotbullbullbull ~ ~ --middot -~- bullbullmiddot ~v ) ~ - -__rl v middotmiddot - 1- ~ -- middot middotmiddot - 1 91 frac12 - ~- lt( middot K i - middot bull - middot - bullmiddot~~-~lJ) obullmiddot~ ~-f- _J_~---Smiddot~middot-~----~~~---gt_middotfY-_middot-~middot --middot-~-~----fJ_middot- middotmiddotbullmiddot u-- bullmiddot ~ ~ -middot L~ bullbull

~bullbullbullbull bullbull l_bull bull bullbullbull EW bullbullbullbull-- ~ __bull f f - middotbull - J middot f bull S bull I ~ -r --

_ bullbull bull- _ bullbull-bull ~ ~ bull bull bull bull I bull bull bull bull bull bull gt - bull middotbulliJ -bull I bull bull _1 bullJ C-- ~-middot _ bull bullbull bullbull bull _____ ~ ~ l _ middot q bull 1 -middot middot ~~middot middot middotbull_ J ~gt - J bull-bullbullbullbull ) _ -middotmiddotbullmiddot J ~middotmiddotmiddot -bullmiddotbull fmiddot 7middot _middotmiddotmiddot bullmiddot(middot Ii~ middotmiddot~_--~middot 1middot__middotmiddotmiddotmiddot middot- gt_ -~ -~-- Imiddotbullmiddotbullbull_ -

- ()_I (w--_ bullbull__(i- bullOmiddotbull bull middotbull -bull-_jlJ middot bull lt 1(middot t gt bull - ~ rbull I bull middot middot- bull41-bull l~r v-middot~- middot middot middot bull_ - middotmiddot ~Jtj (middot~ ~middoti middot middot middot middot middot ~- ~ -tmiddot~ I - middot middot_- ~ - -~ middot_ _- ~bull - _ ~) i bull bullbull bull- middot_ bull middotbull __ ( bull 11bull bull ~ampmiddot ~ l bull bullQ bull - -1 bull JY1 bullbull ~ or bullbullbullbullbull bullbull-bullbull _ ~ - bull bull-bullbullbull middotimiddot middot 91 bull t bull - - tfaw lJ--r- bull bull _ bull middot- - l

f ~~middot--~ middotmiddott ~ltrgtmiddotmiddotJmiddot_bull - ~ - __ middot- LOS ANGELES BASIN - LOW LEVEL -__ jmiddot l-gt bull - bull J iI bullbull bull bull bull _ bullbull _ Jmiddot middotL~_1 middot middot bullbullmiddot ( C middot INVERSION MEAN WIND FLOW _ J

lmiddot - f bullbullbull~ - f 1bullbullbull _ ~)- bull middot- _---_- 7f-~bull~ REGIME _F_~ AUG_UST_~ ~600 P~--- l

-__L-~bull --ncmiddotbull~~-j--bullmiddot~bullmiddot_-bull _fJibullmiddot Imiddotmiddotmiddot-bullmiddot- bullbull ~ bullbullbullbullmiddotmiddotmiddot~middotbull ___ bullJ_ _middot~0))deg bullt t1yensmiddotmiddot ( middot middotmiddot middot middot ~ middot lbullbull1 t_c0 bull -middot---l lt ~middot~- deg bullbull --= bull bull bull I bull bull bull bull bull bull bull bull bullbull _~bull b ---) bullbull-bull ) bulll middotbull middot1middot ) bullT --f bull I bullr ~bullbullbull bullbullbull( - -bull-- ( -o-----_i bull-~-l- i l l J l~-- c middotmiddot _--1 ---I middotmiddot ---- ~bull-bull bulli_ ALT Elmiddot_ bullbullbullbull _- ~~middot bull middot bullbull _ bull middotbull bull~ ~bull middot bull -middot bull--ua_-- bullbull bull

-- 01--- middot_ -middotmiddot hmiddotmiddot __1 ~-- ~ fi~~- ___ - ____ _ -middotmiddotmiddotmiddot~ ) -~-J bull bullbull bull bull 0 uc- -l ~- ~ IT ~~ll ~ bull -middot -middotmiddotmiddotmiddotbullCCAmiddotmiddotmiddot-middot middot bullbullbullbullbull

) i- 5 ~-==-- __ __ - bullbullbull _ bull~ bullbull _ bull bull l T[h4 ------ - 0

i17- o~-lt -(i-_~ 11t~bull-omiddot ~- -- 13 0l~~~bull bull Jbullbull~bull ~ ~bullbullbull bull bull x- middot~---=-~~ -=aJlll8 bull Ibull bull ~~ middotbull rbull~---bull1-~middot-middot _ middotmiddotmiddot-middot 1 0 ~vrbullmiddot ~middot ~ (J~-middot _-_~) ) ~ bull middot

l middot _ POMA_ middot =~~~----ti~ jmiddotmiddotmiddot - middot bull [j

~A ii J0 Vfli middot bullHud __=bt_ bull

CImiddot ~-- ~- middot)middot PACIFIC OCEAN I middot ---- middotmiddot ~

__ middot__ ~ - _ 23~1 middotbull 8 4 1 middot middot ~ middot middot gt ~~- l ~ u middot

bull - bull- I ~------ --1~ i middotmiddotmiddot - n _c-118 1130

~ n r -t ~~gt25) cmiddotbullmiddot

~--lt- ~~- 1-~__( i - t ~ _ middot 0 igt(_J

11bull bull11 ~~ -~[ ~i~gt----gtmiddotmiddotmiddotmiddot--~l_ ~~ ELEVATION

IN FEET bullbull (_- middot bullbullbull -middot middotbull middot ~~ middotmiddot bulltbullbull _ffmiddotmiddot-middot v I )tylt~ -~bullbull1bullbullrbullbull ~-lt -~ ( I~

600~ A0 Cv(A (1829 m AND OVER) deg )_ rJ__~7 middot middot ~--middot L==1 _J bullbullbull - bull -middot~-- rgt ~ middot(Zmiddot- middotbullmiddot middot

Z~C)-tGOO (762 middot 1829 m) 9-N4 __J (r -- lf _ bull bullgt-~~~ ~ _ w _ _ I (1 bullmiddot( middot1 middot -----~~~- middot L-bullmiddotbullW bullbullbull3 STA r I0-4 lODEL

100i -2soo (305~762m) -- Ow - -~1_- i ~~--- bull v~rvt ~~ -middot )) ~--

II gt J (-_bullmiddot middot~ l bull bull tr 1 )~ gt ) bullbull-_bullI-middot -middot bull~0 3 Mor nuq1ENr Wlbull~O JIAtCTIO-bull bull - lbull C---gt bullbull )t bullbull -( I bullf I - 20-00 (61 bull 305 ml J( Jloa xxE- -bullbull00 - -- middot1

0-200 (0middot61m) Wl)7 AVBt~gpound ) bullmiddot-iiNL~ middotntmiddot_ 1 iJJlt( _1J- ~ VAq IA9 IL ITY 0 ~ 10 15 ltS lHPtl

~--_ bull bull I bullbullbullbull 1 ~) J)J ~ bull Is bullmiddot bullbullbullbullbull ~ 3 V IS A VAqlABLE OIR~CTIO- 0 8 16 2-4 km

(SPEEDS SHOWN IN mph 10 mphbull 16 h1llr) -- middot ktr~~~ lt~ ) -middot-SCALE

Figure 7 LOS ANGELES BASIN MEAN WIND FLOW FOR DAYS WITH LOW LEVEL INVERSIONS DURING AUGUST I 970 AT 1600 PDT

-~~~~-=======~middot~-~======~middot--=-==-===gt=---==____________=== ~--=-J~==-- -=-ee----=-------

500

N f-- V

- - - SUBSIDENCE INVERSION

----MARINE INVERSION

bullbull-bull-bullbullGROUND LEVEL

x WINOS ALOFT (kmht)

WESTERN middoteASIN EASTERN BASIN

LAX WINOS EMT IHOS I I

CNO WIHOS

s_ 04 13 1500- 05 02 08

I 06 069 middot

11-1--

04 04 i ~4

06 ~ 4--

I 2

1000 n1 1005 -_E

lll --1 lJ -----------~----

~11

--=i-+- c -- 9 _____ - ~ C

lt I

I 6 4 _r 31

I 6 5 ~~ ~_ bull ---middot- 64 ~li- - middot- bullc - middot-----------

10

SMO (1347 PDT)

EMT (1246 PDT)

BRA CAB (1459 PDT) (1335 PDT

RIA (1349 PDT)

RED (1406PDT)

Figure 8 VERTICAL CROSS-SECTION OF bscat FOR lvflDDAY

T t 10-4 -1)(l n1 s are m

JULY 25 1973

- c - -~

~--~ JC_-_1- ~1pi~ oamp----~JilliiiM~f~-U~ -~--- --~~~ ~~~

-=--~

-E-- O

_ lt

1500 05

06 15

09 __~

1000 --

~- ~---middotmiddot 29

500

oJ11

__a

07

I 07 I

I I

I

09

I

I

I

I 7 ---

11 -----

~ ----- 6

---------------lt- -~middot4 --------

20

29

-

10 10

11 07 08 08

10

08

~8 _____ Y-

N

- - bull SUBSIDENCE INVERSION

----MARINE INVERSION

-bull-bull-bull GROUND LEVEL

WES TERN BASIN EASTERN BASIN x WINOS ALOFT (kmhr)

t t

CNO WINOSILA WllltOS poundMT WINOS

SMO LA EMT BRA CAB RIA RED O (1736 PDT) (1655 PDT) (1707 PDT) (163 PDT) (1823PDT) 1805 PDT)

Figure 9 VERTICAL CROSS-SECTION OF b FOR AFTERlOON OF JULY 25 1973 scat

T bull 1o- 4 - l )(units are m

__~~---iii~~- ~- ~~______ ~~- --~~J---=-~ ~

N ~ -J

PACIFiC OCEAN

0 5 10 15 1111

E 8 4 I 0 8 6 2 ~ bull

SCALE

dh Mes

CONTOURS REPRESENT - 000 ft 305 m

0 SNA

c8s

ec 8v

amp R~b

Figure 10 TRAJECTORY ENVELOPE FOR AIR ARRI1G AT CABLE AIRPORT (CPLAD) 1600 PDT JULY 25 1973

~-~

q_- ~ ------1 H~~~ -~~--~ ___---___--i- __r-=-1--===12---1 ~ ___r~ _==---_ - ~- f~~ ~-- - -5plusmn-at -~middot~

ll~~r1 ri

40

ec 8v

-1 I

amp

0 HQ_

7 0

CAP LAAR) O

VER

PACIFIC OCEAN ~ 0

RLA

4

WHqR d

diams

H ~I

I l

0 COMA

3

L~

LAH

Fa_ f ~~

S ~ LA APCD VALUES ADJUSTED TO AGREE ~

lt

0

5 10 15 mi0 WITH ARB CALIBRATIONE-j I I CONTOURS REPRESENT NZJ ~ 0 a SCALE 6 24 km - 1000 ft 305m COS v~J

______ J 10 ro ( igtf t-i

coFigure 11 SURFACE OZONE CONCENTRATIONS (pphm) I 600- I 700 PDT JULY 25 1973 ~

~~~~~C-~ ------=--~-__-~--~~~=--- ----=--~

N

-E

D1600----------------------------- 1--

14001-------------------------------

1200

I Ground Elevation

1000 middot 445 m ] lampJ

sect ~~ 7 ) SURFACE i6~ 800 MIXED LAYER

~

~ [ J ~ ~ I OZONE CONCENTRATIONS~ 600 E E GREATER THAN

( 50 pohm

400 I C H T Z GROUND LEVEL

200

I PUUloCETER UNIT SnbullBOL

NOc N0 0 ppm01 02 03 04 05 03 z

40 --~45~~ 50 co pm C0 5 10 15 20 25 30 35 I I I I I I I I I I TEIIPERATURE oc T-5 b 5 10 15 20 25 30 35 40 45

I-- 100 RELATIVE HUlillOITY H0 10 20 30 40 50 60 70 60 90 b1eot IOmiddotm- 1 8

CN cmmiddot3 1 IO X0 I 2 3 4 ~ 6 7 8 9 10 URBJLENC-C cm213ue- E

Figure 12 VERTICAL PROFILE OVER CABLE (CAB) J CLY 2 5 l C)7 3 l 63 6 PDT

~ _~ ~--- -

--

1400 I bull bull

1200

1000-5 LampJ 0 ~ I- 800 ~ c(

sooLl

-1-=-1-~--t j --=~c-o-----i-bull 1-~~~ ilt~~ -~-1 lta-abull--~ -c-~---=---r F--- ---- I n_--middot- =~~ ai~IHJ

(~-It

1600 ___________________________________

C r 11 s Ground Elevation t~C E H I~lcc

- ~ 1 90 m

4001 bullc C H

C UNDrnCUTTNG svC ~ Ic- H

SEA BREEZEC II 200

C C

[C -PARAMETER ---UNIT SYMBOL

NOx N0 0 ppm01 02 03 04 05 03 z co ppm C0 5 10 15 20 25 30 35 40 45 50

-5 middot- -~20~----25 TEMPERATURE oc T0 5 10 15 30 35 40 45

100 RELATIVE HUIOITY H0 JO 20 30 40 50 60 70 80 90 bcot 10-4m-1 8

CN crrr3 10 0 I 2 3 4 5 6 7 8 9 10 X TURBULENCE cmZ-13 sec-1 E

N N

_-----=-G--~---

Figure 13 VER TICAL PROFILE AT EL MONTE (EMT) JULY 25 1971 1656 PDT SHOWING UNDERCUTTING BY THE SEA BREEZE

0

middot~_lt ~middotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotbullbull

-~

LACA

0 - )

i r=

-v2v

~

_middot~middot)( I bullbull

bullJ

K~Ji~middot

~~ 61iAS 0

EMT J~J---6~-11 ~orr

PACIFIC OCEAN

WEST 0

SMC

0RLA

14

L~8

R~A

~BL

16 ~ ~

0 5s Pcfrac14A c1i ~ )

wFJfo~J_) ltI~~~

_ff-Clf1ito J )

HILL~

~J U

~ _~~~

~

I o middot

1 1$ ~ 11yen ~middot ~I N

I

N I- I

t

0 --pomiddotmiddot bullmiddot i- 1LO middot Joomiddotmiddotmiddot -- middot middotmiddot -middotmiddot

_middotmiddot 0 middot middotbull MWS r

L4 ( 1 T bull bull __-- -A bullbullbullbull middot

0 i __ bullbull

17 t-J~ N7 a S I ~r ~ 1 rtd ~lt A-~ v- middot ~ - cXa 0

RIA 19

CLO

ltJ~

bull ~ 0

(

--

1

_ _

-2Wl

~s~o -- _)~J0JgtJ~ ___ Q

15 l1JI

0 15 r(A0

CAP

CLARR)~R 1900 1-shyPDT

II (_-L~X L2X I 0~ R[V

0 CCtwA

I

I18=00 POT~ l4 r1

fj

-11J - ----- 11=oomiddotmiddotpor

l~i middotmiddot- o

i

5 10 5 Tl o~1 middot--middotmiddotmiddot middotmiddot

_q it==i--__F-3 9 I I CONTOURS REPRESENT SNA NZJ ~1 o

_- I 0 8 16 24 km I - 1000 ft 305 m middot ~

7 14~CALE --- 2500 ft o2m V lr1 ) middot I i0 _ il o5

16QQ pol(middot v( ____________ _L

I i

Figure 14 APPROXIMATE TIME (PDT) OF ARRIVAL OF SEA BREEZE Jl-LY 25 1973 (Ogt_iective criterion based on ground level ozone concentrations)

~ -___~==~ ~~ - ~ =-~ f7r=~1 _j~-~ --c_~~

u-middot - middot middotmiddotmiddotmiddotmiddot

~- middotmiddot~ ~1 WESTERN BASIN r Joa_middotmiddotmiddotmiddot_ NOxEMISSION RATE ~- 95 METRIC TONShr

-----bull_ ~ ~middot~ I -OUR -----middot )omiddotmiddotmiddot - middot~ l21 (fTI

~ AT middot ~ middotbullmiddot- ~- ~ middot 4bull-middot

I EASTERN BASIN NOx EMISSION RATE 10 METRIC TONS hr

ri r bullbull

t10 Joa

) __ 8v -a_ -- -bull-I O ~AGA -_ ~S ___ _ middotmiddotmiddot -

~ ~v ai- omiddot-middot~-- - ) r -middotmiddotmiddot f middot( ---~ -l A ~ _ (- bull ___

it~ ~~~ middot-middot -- ~-~ ~~~ 0 0 AZU~

AVERAGE CONCEN7RCTi)N iN BOX (IF STEADY STATE)

IS 25 pphm

1 r f--Ji 7 ~Sv PAS ou )V~(~- ~ t i -~ Li_) 03 FLUX THROUGH f~

~ ~JI_~ - amp_ JiM O SHADED BOUNOA~middot~-~ ~~-s-- EMT 185 t 60 METRI~ bull ~ ~ TONShr 0 (m)

c~~~ 1t~CS A~JFP

1000 _29

-i32

_~o tUA

_

1

O~ ~

0 -__rJ( (r- J PACIFIC OCEAN LAX _ C-middotJbull _

l o M R No _

550m

r

A frac14

HAR O HJ LAH

_ o camptA REDLANDS 18QO POT ~ r

I bull ~

RB MEAN TRAJECT~~~y

0

TOA L~S

0 AN

I - ~ 8 OUNOARY ~ ~middotltdeg ~ ~ BETWEEN middot __ WES~ERN ANO- middot middot - ~

I gt I lt bullmiddot bull (EASTERN ~ i middotmiddot middot - - ~

S ~ ~~ ~ - middot-

rt1~1_--t------l

middot1-- BASIN ~-~

1-)~~--middot ~ ~l

~~ ~-bull bull J --

-is-eo -_

0 5 10

j=i r-i C

0 8 ltl

SCALE

5 mi

2~ un

CONTOURS REPRESENT - 1000 ft 3gt5 m

--middotmiddot 2500 ft 1 762 m

~

0SNA

cos 0

_ --~ ----- --- ( bullmiddotmiddotgt

- middotlt- ltgtmiddot t__ Q ~

1 1 rmiddot bullbullbullbullmiddot ~9

NZJ ~ middotmiddot - middot- Alr ---middotmiddot- middot middot( middotmiddotmiddotmiddotv ~ bullbullbullw bullbullbull bullmiddot 1 bullbullr~ ~-- -middot ~--v ~- - I -~

ESTIMATED OZONE FLUX FROM VESTER~ TO EASTER-J BASIN JULY 25 1973 I 700 PDT

C ~IV

N N N

I

l ~

-~~

I

iI

i I

I t

t

~ ---~ --

Figure 15

~Qa llfJD fl(~middot ~ 11f ~I I

l

Lfb ec~s0 CPK v2v 0

ALT 8v Ld~_----1

I

HO-

0 CA

middotLARRv O VE~

1330

ol(Di

A~U

0ENT

~lt

s~e ~ 1530

F8f 1730

~

rbull-~

oc (WljT) -_-~(~~c lt-rw---_

~~ ~-_i~cB~~~

2-~) - ~ ~ l~w-~~ p~- pound)_

0 ojI middot tl-1CfUp I ~ ) 1 ~ J~I i bull middotbull middot~-Li 1)- ) I

DiI ~- 0

i ) 0 l I I

t

A RALc~o JI

C

-~

0 r-iR

~IV 1230 1~

RE PO ~- I - Ftl

) 0 ---~gt- __L8s ~Zi diams ( T~ _middot_ ~~ ~

I AN ~~-~ j t bi 0

~ I

~ I L i

-_gt ji o 5 c 5 Tl middot 0 0 ~-i p__i=r 2=f I_ I 1 NZJSNA 1

1 8 2 4 km )

SCALE I 00 J_(1 CONTOURS REPRESENT cos f

1 0 I --- I - ))) 35

PACIFIC OCEAN

Figure 16 TRAJECTORY E~VELOPE FOR AIR ARRI1gtJG OVER REDL_)DS AT 1800 PDT JULY 23 l =i73

224

JULY 25 1973

LA DOWNTOWN

0sect040 a

~

~ 020 0 X z0 ~ LJ 0 ~ z

~5 040 330POMONA 0 ~ en~ 020 w z _J

w w 0 (9 z O----u-~~-__~_-~~~-------L-~-0--0-0~----- z

ltt~ 040 56 (I)z

0 0o _ RIVERSIDE _J0 20 t6 ~

0~ Qt---0-0--ltrO-ltgt-C~------~~~~ a

LL ~

Rate ~ IO mph___ (I) w

_J~ ~ ~

et~ lt(

3 040 PALM SPRINGS ~

j 020 ~

0------____-----L--___---------L---~--~

105

12 4 8 12 4 8 12 l~-s----am _ pm----1

HOUR OF DAY PST

Figure 17 Diurnal variation July 25 1973 of oxidant concentrations at air monitoring stations at Los Angeles Downtown Pomona Riverside and Palm Springs California Values are corrected data Los Angeles Downtown and Pomona x 11 and Riverside and Palm Springs X 08

CONO S t 1 fRESEIS7

~

~~ 0

ciffmiddotdK ~ ~v~~o

( ~s ~

bull ~r ~ bull 1--~~----Soootl ~ ~ ~ ~ lj i1 d t CJ ~ ampfrsmiddotflt- frac12 ~ middotL~Js _-- ~

_gtgt middot~ ~rroltf~-) ~ 0 s- r

middot-middot- r_~ ~~JtbO ~~bull~Jt ~~~ L r - bull _ ~ I= J 1 ~ ~ ~-~~bullJC ___ -_ middot ~ laquo -poundJ~ ~- middot1~ r-- - V--_1_ ~ I 1 S I

V ~ bullf-uv~ fi -~zumiddot -~middot~ LS gt -tmiddot-F Q~ ~-tv I_~ --- ONT p(_ s ~S ~~~-[ ( 0 c-_ --~ ~~~___d_) lt- ~ I -i-C - -

~----1-1 bull~~POMA ~V BN ) middot-~ f -- s - ~

~VA -middot- ~p AAL a 2~~ ~~middot01 r r ~ middot middot 0-- V

i LAX bull1

~ -~poundJ-i- ltllll _(__1-0~ ~t- degQ-0- ~~ _ _-__~~-qlK ( a_ II ~ ~p-~ ~J

N bull - - 0 r o_ _I ~ -~ ~middot ~ ~amp ~--= ~ ) s ~

- -~- - middotO _a - Tl --0- ov I lHOIO J I bull J -- ~ 6 ~ -__ 2 ~

(__ ~~ _- ~-~ middot8---fl~ -- ~ bull~-abullbull _~ ~-cgt ~ bull bull middot e bull bull l ~ 0

I 1A_ HZJ middoto~J

middot0 (~ ~ S TAA

- ~ - - - --0 () _-j J middotO=c==c-c==cc~~~ l ~~ ~ ~ bull-~---~ ~ bullbull -~ al1 ~ bull __ ~--middotmiddotmiddot

diams Skyforest _ Strawberry Mt Lookout

Figure 18 STRE ~[Ll)ES FOR 1600 PDT on 8 1673

~ ~--

vO 0

N N V1

au

91 V7

-1 ~ -=1 ~~ ~~~~l r=--~d- ---1 _J-_

~E1 ~L1-~f~

3100 ---------------------------------

2900r-----------------------------

T

e w 0

~ 5 Cl Ground Elevation

1560 m

T PARAMETER UNIT SnbullBOL

NOx N 01 02 03 04 05 03

ppm z co ppm C

10 15 20 25 30 35 40 --

45 50

170

I I I z

0 5

-5 - -0~ 5 10 15 20 25 30 35 40 45 TEMPERATURE oc T

0

0

10

I

20

2

30

3

40

4

50

5

60

6

70

7

80

8

90

9

100

o

RELATIVE HUMIDITY

bcot CN

TUR8ULENC~

110-4m-

cm-3 tobull 213 1 cm sec-

H

8 X E N

N OI

Figure 19 VER TI CAL PROFILE OVER ARROWHEAD u-RR_l A CG CST I 6 1973 939 PDT

3100----------------------------------

N2900r----------------------------- -i

N

2700i-------------------------------

2500

e 0 uJ 2300 gt ~ ct

2100

1900i---------------------+--------------

~le 1iation 1360 m) 17001 ~

- -PARA1jETER UNIT SYMBOL

T NOx N1500 o ppm01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50

TEWERATJRE oc T-5 middot --~o--- 5 10 15 20 25 30 35 40 45

IOO RELATIVE HUWIOIT Y H0 10 20 30 40 50 60 70 80 90 bcat 10-~- 1 8

CN cm- 3 104 X0 I 2 3 4 5 6 7 8 9 10 213 1 tURBliiENCE cm sec- E

Figure 20 VERTICAL PROFILE OVER ARROWHEA D -RR 1 --- -AUGlJST 16 I) 16--1S PDT

1-~i w--~i_f l-=--bullC- ---~-4

1600 bull t c- N 8 ff Tbull C[ 8 H 1 bull H z H T ~ C f N 1 H T bull C rn 1 C NE bull-~z Hi400 bull bull tf T bull N ~r --middot _P H -ybull EC N z__e H T i 8 z H Tbull C E HD Z H T POLLUTANTS REMAINING FROM bullt C Hbull L T PREVIOUS DAY1200 Et HO I II -middot-- bull Ct H 9 - H T

___ Hbull( E N 1 a tC N i--_ -1 H

C N Tbull Z HP poundIC C H z_ 1111 1

- bull C H Z l _H_ _J1000 )( cc H -z emiddot ksect bull C N ~ T

)( iz H 8 H TIAI -t XC z 7-- T0 bull pound N t H_8

t-gt

YCpound N 1800 l I-gtltbull - H (Jet

N i -r~Bltt t bull gt- t C X N H T

[ BUOYANT POINT SOURCE PLUMEH 1

N ~z-- -

C H

-bull SUPERIMPOSED ON POLLUTANTSC JZ X H T 600 -~ E c REMAINING FROM PREVIOUS OtY Cl JC t H H f bull cmiddot t HT -fl

C- X t fl _ REMNANT OF NOCTURNAL RADIATION INVERSION(I-----e-C f N K I T H

C Z [ T H x-8 400 _Zc r -H -K SURFACE MIXING LAYERz C II H K 8

C N T pound H M 8 _ I -t ff H E N -9 l

Ground Elevation 305 rn200

PARAMETER UNIT SYMBOL

_ I - I I I NOx N00 ppm01 02 03 04 05 03 z

co ppm C 0 5 IO 15 20 25 30 35 40 45 50

L middot1 TEMPERATURE oc T-5 0 5 IO 15 20 25 30 35 40 45

100 RELATIVE HUPAIDIT y H0 10 20 30 40 50 60 70 80 90 bscot o-4m- 1 B

CN cm-3 x 104 X0 2 3 4 5 6 7 8 9 10 TURBULENC~ cm213sec-1 E N

N co

Figure 21 VERTICAL PROFILE OVER BRACKETT (BRA) JULY 26 1973 0825 PDT SHOWING BUOYANT PLUME AND UNDERCUTTING BY RADIATION INVERSION

N N 01600

___bull C M C

C

1400~~~ t C [ middot H LAYER CAUSED BY

C C H C [ H UPSLOPE FLOWl

1200

1000 ] w

SURFACE MIXING LAYER 0 --= ~ -~~ 6 800~ er

C C

600t-i C C t C

I ~00

Ground Elevation 436 m 2001-------------------------------

PAIUWETU UNIT SYWBOL

NOx N ppm0 0 01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50 I I I I I I I I TEWPERAT1JftE degC T-o b 5 10 15 20 25 30 35 40 45

100 ~EIATIVE HUWIOITY H0 10 20 30 40 50 60 70 80 90 b1tt1 10-m- 8

CN enr3 110 X0 2 3 4 5 6 7 8 9 10 Tu RUL Erct cm23sec- E

Figt1re 22 VERTICAl PROFILE AT RIALTO (RIA) JlJL Y 19 1973 1738 PDT SHOWI=JG LAYER CAUSED BY UPSLOPE FLOW

~~-7 ~ ~- 1 ~iri ~~- ~~-~ ~t ~~ ~ =~middot-1

1200 I t 1 If J-

1000

I C ltTl a_ ~l- t

800

600

L gE __r H

H

400 j (~ c pound N C E I~

t EH -

1-1 M

H H

H M H H

H

H H

11 bull H M H

M H If

H H

H

- C t H ~ C poundmiddot H

I C E I(

200

1600--------------------------- t

T t t T l

l T t

T t_

t 1

l] w ) g f

Tt t

ltt ~ T

t J t T

t J

f 1

t

Klt

H M Cro1nd Elevation 250 m HT X

5Yl80LPAllAlETER ~

NOx N0 0 ppm01 02 03 04 05 03 z

co ppm C0 5 10 io 20 25 30 35 40 45 50

25~--- ---35~~-40 TEMPERATU~E oc T-5 0 5 lO 15 20 30 45

100 RELATIVE HUMIDITY H0 iO 20 30 40 50 60 70 80 90 bact 10--ltllm-1 B

CN cmmiddot3 11 04 X0 I 2 3 4 5 6 7 8 9 10 IURBULENCE cm2hioC-1 E

Figure 23 VERTICAL PROFILE OVER RIVERSIDE (RAL) N

JULY 26 1973 2239 PDT I)

middot==-=-=

0

bull

N w 1--

ii -s~~ l-obull

CJ ~

obull -obull obull

5 02~

bscat

Oa

4l o2J

-I 3 e I 0

--)(

~

Abullu 2

ll

ol

Traverse at 750 m msl 35 km Downwind (SW) of Arch - St Louis Mo 1117 - 1137 CDT

( Power Plant Plume -01 Ibull-[ ~ e

11 bull E I -)(I

I0bull I 1r~ l -

0

I I Io 1 u I

I r- l A bull I i I 1I

H1I I 4 t I II I I

11 I I

I I r I I I

I I qo 01 I I

I I bullJ~viI I middot ~

I

I I

~

Urban Plume

ood 0 10 20 30 40 50

kilometers

o~

02

01

s 1

P

0bull 01

00S~J1 I ti middotmiddot1 middotvmiddotmiddot~ J

Urban Plume

I y

oo 0 10 20 30 40 so

kilometers

Traverse at 750 m msl 46 km Downwind (SVV) of Arch - St Louis Mo 153 0 - J 549 CDT

---- bscat

o-

Power Plant Plume

1l~ 11I 1 t

ill~t fl Ibull I ii

I

lmiddotmiddotrI

I I I I t II

l vrI V

JV-f Jl bull

bull t I bull I

Figure 24

l

232 RELATIVE CONTRIBUTIONS OF STATIONARY ANDMOilILE

SOURCES TO OXIDANT FORMATION IN LOS ANGELES COUN1Y IMPLICATIONS FOR CONTROL STRATEGIES

by Robert G Lunche Air Pollution Control Officer

Los Angeles County Air Pollution Control District Los Angeles California

Introduction

The type of air pollution problem characteristic of the west coast of the

United States and particularly of Southern California has come to be known

as photochemical smog because it is the result of sunlight-energized atmospheric

reations involving oxides of nitrogen and reactive hydrocarbons Its manifesta-

tions- -eye irritation reduced visibility damage to vegetation and accumula-

tion of abnormally high concentrations of ozone or oxidant - -are by now well

known In fact the occurrence of high levels of oxidant which consists almost

entirely of ozone has become the primary indicator for the presence and relative

severity of photochemical smog

During the 25 years since photochemical smog in Los Angeles County was

first identified an extensive program has been underway for control of the responshy

sible contaminant emissions Initially during the 1950 s these programs concenshy

trated on controlling emissions of hydrocarbons from the stationary sources of this

contaminant In the early 60 s programs for the control of hydrocarbon emissions

from motor vehicles in California were begun An exhaust emission control proshy

gram for hydrocarbons and carbon monoxide from new vehicles was begun in 1966

C011trol of oxides of nitrogen emissions from motor vehicles began in 1971

As a result of the overall control program by 1974 emissions of reactive

hydrocarbons from stationary sources have been reduced 70fo from uncontrolled

levels and about the same percentage from mobile sources Oxides of nitrcgen emissions

233

from statjonary sources have been reduced about 53 while emissions from moshy

bile sources are still about 7 above uncontrolled levels due to the increase

in NOx from 1966-1970 models Additional controls already planned for the future

will by 1980 achieve reductions of reactive hydrocarbons from stationary sources

of about 87 from uncontrolled levels and from mobile sources about 93 By

1980 emissions of oxides of nitrogen from stationary sources will have been reshy

duced 53 and from mobile sources 63 from uncontrolled levels The past

present and projected emissions of these contaminants are shown in Figure 1

A I though compliance with the air quality standards has not yet been achieved-shy

and is not likely before 1980- -the results of these programs have been reflected rather

predictably in changes in certain of the manifestations of photochemical smog For

example eye irritation is less frequent and less severe and in some areas js

rarely felt at all any more and damage to vegetation has been markedly reduced

Ozone (or oxidant) concentrations have been decreasing in Southern California

coastal areas since _1964 in areas 10-15 miles from the coast since 1966 and in

inland areas 40-60 miles from the coast since 1970 or 1971 as shown on Figures

2 arrl 3- All of these positive effects have occurred despite the continuing growth

of the area indicating that themiddot control programs are gradually achieving their purpos

a return to clean air

This improvement is al~o refutation of the so-called Big Box -concept which

assumes that the total daily emissions in a given area are somehow uniformly disshy

tributed throughout that area--regardless of its size or of known facts about the

meteorology of the area or the spatial and temporal distribution of its emissions- -

234

and of control strategies based on that concept And since the improvement in

air quality refutes the control strategies based on reductions in total emissions

it thus confirms the value of more recent control strategies which emphasize conshy

trol of motor vehicle emissions and use of a source-effect area concept

Following is a brief listing of the evidence we intend to present as supporting

our views on just what control strategy is appropriate

Examination of relative contributions of HC and NOx from stationarybull and mobile sources demonstrates that motor vehicles are the overwhelming

f source of both contaminants~

I bull Observation of air monitoring data shows that the effects of photochem -

ical smog are not uniformly distributed t_hroughout the county

bull Study of the meteorology of LA County shows consistent paths of trans -

port for various air parcels and consistent relationships between the

areas most seriously affected by photochemical smog and high oxidant

concentrations and certain other areas

bull The upwind areas are found to be source areas--the downwind areas-shy

effect areas

bull Central L A is found to be the predominant source area for the effectI area in which the highest oxidant levels in the SCAB consistently occur

bull The predominant source of emissions in this source area is found to

be motor vehicles

bull Central LA has the highest traffic density I

ij bull Both pr~mary and secondary contaminant concentrations reflect the effects

of the new motor vehicle control program in a predictable fashion 11 I

A strategy based upon these findings is gradually being verified by atmosshybull pheric oxidant data~

235

The Evidence that Motor Vehicle Emissions Are the Principal Source of Oxidant

As seen from Figure 1 at the present time the total daily emissions of I-IC

and_ NOx from all sources in Los Angeles middotcounty are primarily due to the motor

vehicle The problem now is to find the spatial and temporal representation of

emissions which when examined in the light of the known meteorology and geogra -

phy of the Los Angeles region best describes the source of emissions responsible

for the highest observed oxidant readings

In the rollback models used by EPA and others the basin is treated as a

big box with uniformly distributed emissions and peak oxidant is considered to

be proportional to total basinwide hydrocarbon emissions

The fact is that the middotemitted contaminants from which the smog is formed

and the effects which characterize that smog are not evenly distributed throughout

the Los Angeles Basin in other words the basin area under the inversion is not one

large box filled to all corners with homogeneously distributed air contaminants and

photochemical smog

Refutation of Big Box Myth

Examination of atmospheric contaminant concentrations refutes the big box

concept It is found for example that concentrations of djrectly emitted contam -

inants measured at a particular sampling site reflect the emissions within a rather

limited area around that site For this reason contaminant concentration levels

vary from one location to another and each has a characteristic daily pattern which

reflects the daily pattern of emissions in that area

middot 236

The big box concept is further refuted by the fact that peak concentrations

of carbon monoxide and oxides of nitrogen in areas of high traffic density were

fairly static prior to 1966 Thus they did not reflect the 45-50 per cent growth

in motor vehicle registrations and gasoline consumption which occurred in Los

Angeles County between 1955 and 1965 and which caused comparable increases in

total daily emissions of such vehicle-related contaminants This demonstrates

that growth was outward rather than upward so that a larger area of the County

began to be affected by photochemical smog but no area experienced smog ofJ

greater severity than that originally affected by smog formed from the vehicular

emissions which accumulated each weekday in central Los Angeles and were trans-

1 I

ported later that day to the San Gabriel Valley

1 Meteorological Evidence

To verify the geographical dependence of emissions and resulting atmospheric

concentrations let us examine the meteorology of these large areas of Southern

California Both the County and the Basin have many meteorological sub-regions

in which the patterns of wind speed and direction may be similar but within

which the patterns of air transport are parallel with those of adjacent sub-regions

and the respective air parcels do not ever meet or join

The characteristic patterns of inversion height and wind speed and direction

in these sub-regions and their patterns of vehicular emissions together have

created a network of source areas- -those in which the reactant contaminants accu -1T

i ~ mulate in the morning and begin to react--and related receptor areas--those to which

~ the products and associated effects of the photochemical reactions of the contamshy)

inants originally emitted in the source areas are carried by the late morning and

237 middot

afternoon winds ( sea breeze)

Wind-flow patterns show that characteristic patterns of transport for related

source area-effect area combinations are separate and parallel not mixing or

joining Each source area has its own reactor pipeline to its own effect area

or areas

To illustrate this source area-effect area relationship the typical flow of

polluted air from downtown Los Angeles to Pasadena was selected as a worst

case situation for in-depth examination Figure 4 shows that the air in downtown

Los Angeles on the morning of smoggy days moves directly from the central area

to Pasadena

Vehicular traffic is the predominant emission source in both downtown Los

Angeles and Pasadena Thus the air in each locality should contain CO Also

since oxidant would form in the air parcel moving from Los Angeles to Pasadena

oxidant levels would be expected to be higher in Pasadena than in downtown Los

Angeles

Figure 5 shows these relationships for the period 1960-1972 The atmosshy

pheric CO level is similar for the two areas while oxidant levels were higher in

Pasadena than in Los Angeles throughout this time period This demonstrates

that a significant amount of oxidant formed in the air as it moved to Pasadena

containing both the unreactive CO and the photochemical reactants for producing

oxidant Both CO and oxidant show a marked downward trend in each locality since

1965 which emphasizes the effect of vehicle exhaust controls and the correlation

between the localities

238

On a day which is favorable to the formation and accumulation of photoshy

chemical smog a contaminated air parcel normally originates during the

6-9 a m period on a weekday from an area of dense traffic centered just

south and west of Downtown Los Angeles It is oxidant generated within that air

parcel which usually affects Central Los Angeles and the West San Gabriel

middotK IJ l J

Valley area around Pasadena

The traffic area in which this smog had its origin is about the most dense

in Los Angeles County and has been so for the past 25-30 years No area

has a higher effective density thampn-this Using carbon monoxide which

1

is almost entirely attributable to motor vehicles as an indicator of such emis-

sions it is found that the concentrations of emitted vehicular contaminants

middotr i

measured in Central Los Angeles during the past 15 years confirms both this lack

of change in effective density and the absence of any area of any greater effective

density when local differences in inversion are acknowledged

This area the Central Source Area is depicted in Figure 4 The size

and shape of the Central Source Area was ch~sen to be large enough to reduce to

an insignificant level any diffusion or transport into this area from any externally

l generated reactants This conclusion is based in part on the trajectory studies

previously referenced as well as an analysis of the diffusion and transport parashy

meters for the area

239

The Central Source Area has been identified as that geographical region

which contributes essentially all of the primary contaminant emissions giving

rise to the highatmospheric oxidant levels in the West San Gabriel Valley

The proportion of emissions in the CSA due to motor vehicles and that due to

stationary sources is shown in Table 1 For the County as a whole about 80 per

cent of _(6-9) AM reactive hydrocarbons are due to motor vehicle emissions and this

figure rises to 90 per cent for the CSA The same conclusion a pp lies to NOx

emissions The Central Source Area contains the greatest density of vehicle traffic

in the County and thus the greatest density of source emissions Thus it appears

that the source area with the highest density of emissions during the critical (6-9)

AM period is responsible for the highest afternoon oxidant levels observed in Los

A i1geles County and in the South Coast Air Basin These highest oxidant levels

are consistently observed to occur in the San Gabriel Valley This is true whether

the LAAPCD or the ARB oxidant calibration procedure is used

Further the atmospheric concentrations of the primary pollutants can be

identified as originating primarily from the motor vehicle and they reflect the

effects of the motor vehicle emission control program A vehtcular source area

can be identified by its atmospheric levels of CO and NOx Figure 6 compares

measured atmospheric levels with calculated atmospheric levels for CO NOx

and the CONOx ratio in the downtown area

TABLE 1 240

REACTIVE HYDROCARBON EMISSIONS

(6-9) AM

1970

LOS ANGELES COUN1Y middot CENTRAL SOURCE AREA middot SOURCE TONS PER CENT TONS PER CENT

Mobile 1260 81 3 135 91 2

Stationary 290 187 1 3 88

Total 1s~o 1000 148 1000

By 7 -Mode Gallonage

241

The calculated values shown in Figure 6 were derived from a baseline

survey of 1100 vehicles and continued surveillance tests both using the Calishy

fornia 7-Mode test cycle The baseline survey showed that motor vehicles withshy

out exhaust control systems had average exhaust emissions concentrations of 3 4

per cent CO and 1000 parts per million of NOx Baseline emissions data apply

to 1965 and earlier model vehicleg and surveillance data to 1966 and later modelsmiddot

Since it can be concluded from calculations and observations that the dilushy

tion of auto exhaust emissions in the atmosphere on a smoggy day in Los Angeles

is approximately 1000 to 1 the calculated values for CO and NOx prior to 1965 are

34 ppm CO and 1 ppm NOxo After 1965 the changing effect of controlled vehicles

in the total vehicle population is reflected in the calculated values

CO and NOx values measured in the atmosphere are also shown in Figure

6 and confirm the values calculated entirely as diluted vehicular emissions NOx

concentrations measured in the atmosphere tend to be consistently a little lower

than the calculated values probably because photochemical reactions remove some

NOx from the system

The data for CO and NOx calculated and measured show that emissions in

downtown Los Angeles originate almost exclusively from motor vehicles and that

atmospheric concentrations there reflect the average emissions from a representashy

tive vehicle population

The ARB has recently published a report entitled A Trend Study of Two

Indicator Hydrocarbons in the South Coast Air Basin Acetylene was used as a

242

specific indicator of automobile exhaust emissions and it was found to have de-

clined in concentration in the Los Angeles atmosphere at an annual rate of 12 5

per cent since 1970 To quote from this report The California implementation

plan requires an annual average reduction in these emissions (reactive organic

compounds) of 166 tons per day or 11 1 of the 1970 tonnage per year The per cent

reductions in the_ acetylene levels at Los Angeles and Azusa are greater than reshy

quired by the implementation plan Since acetylene is almost entirely associated

J with auto exhaust this demonstrates that the motor vehicle emission control

program is achieving its purpose

To summarize at this point it has been deomonstrated that high oxidant values

are due to motor vehicular emissions of NOx and HC because

NOx and HC are the principal reactants in the oxidant formation process

and they originate primarily from motor vehicle emissions and

The highest oxidant values are recorded in_ effect areas that receive air

from source areas where motor vehicles are clearly identified as the

dominant source of NOx and HC

243

Future Control Strategy

The APCD strategy for achieving and maintaining the oxidant air quality

standard is based upon the fact that high oxidant values are due to motor ve-

hicle emissions of hydrocarlxms arrl nitrogen oxides This strategy is as follows

1 Both Hydrocarbon and Nitrogen Oxides Emissions Must Be Considered To Achieve the Federal Oxidant Standard

There is wide agreement that NOx and HC are the principal reactants in

the oxidant formation process and that vehicular emissions are a major source

of NOx HC and CO

2 Effective Regulation of Atmospheric Concentrations of Both HC and NOx and of the Ratio Between Them is necessary for Attainment of the Federal Air Quality Standard for Oxidant

Basmiddoted on the abundance middotof available experimental evidence it is our firm

position that the most rational approach to solving the photochemical oxidant smog

problem in the South Coast Air Basin (SCAB) is to control the quantities of emissions

from motor vehicles of both smog precursors--Hcmiddot and NOx--their resulting atmosshy

pheric concentrations and the ratios between both contaminants which will result

from these controls

We arc also convinced that the oxidant and nitrogen dioxide air quality stanshy

dards can and will be met not by 1975 or 1977 but by the early 1980 s if the emisshy

sion control program as originally outlined by Ca~ifornia or a slight modification

of it proposed by the District is followed and enforced This should also provide

for continued compliance with these air quality standards at least through 1990

244

It will also allow time for a reappraisal in about 1978 of the whole situation relative

to the ultimate emission standards required and the best approach to their impleshy

mentation

Calculation of the degree of control necessary to attain the air quality

~ standards for oxidant and nitrogen dioxide involves indirect complex methods 1

aimed at determ_ining the degree of control of the primary contaminants directly

emitted by automobiles

The following evidence supports our proposed solution to the problem in

terms of both the atmospheric concentrations of the oxidant precursors NOx

and HC the ratio between them as reflected in their exhaust emission standards

and the resulting atmospheric concentrations of oxidant which comply with the air

quality standards

Chamber Results and Projections to the Atmosphere

The importance of environmental chamberwork cannot be minimized the

j need for and direction of the whole emission control program was based initially

j on the results of chamber experiments In order to understand the importance to

air quality of achieving both the correct low quantities of emissions and the right

ratio we can present several graphic portrayals of analyses of experimental labshy

oratory work together with their relationship to past present and future air quality

in terms of both morning primary reactant concentrations during the morning

traffic peak and the equivalent emissions which would produce them

245

Figure 7 shows maximum ozone levels that were obtained by irradiating

varying amounts of auto exhaust hydrocarbons and oxides of nitrogen in an environshy

mental chamber The corresponding ozone levels then can be found for any comshy

bination of BC and NOx concentrations Thus high ozone is produced with high

emissions of both hydrocarbons and oxides of nitrogen and low oxidant is formed with

low emissions However either low NOx or low HC emissions11 can also produce

low oxidant--graphic and clear evidence of the importance of the NOxHC ratio in

ozone formation Furthermore each and every possible combination of values for

NOx and HC has then a corresponding characteristic maximum chamber ozone

concentration

Using this graph we can estimate what ozone levels would result if certain

atmospheric mixtures of NOx and HC could be injected into the chamber and

irradiated Such estimates were made for 1960 and 1965 using atmospheric data

rlThe points labeles 1960 and 65 show the location of the highest levels of both

HC and NOx found in the air in those years in Downtown Los Angeles (OOLA) area

during the 6-9 AM traffic peak

It has been demonstrated by use of CO and NOx data and CONOx ratios

hnw well the characteristics of vehicle emissions are reflected in the atmosphere

We know what emissions from the average vehicle were then in 1960-1965 both

for HC and NOx so that we can mathematically relate emissions to atmospheric

concentrations for those years and so for future years also knowing or calculating

only what the characteristic emissions will be from the average vehicle

246

The NOx concentrations stayed about the same from 1960 through 1965 because

average vehicle emissions of that contaminant did not change during that time

Mobile source emissions can be shown to have contributed essentially all of this obshy

served result However blow by controls did reduce emissions of HC and the

concentrations dropped accordingly In 1965 the last year before exhaust controls

the point 65 indicates where we were then in terms of maximum ozone formation

to be expected in a chamber with the highest HC and NO concentrations found in the X

air that year Levels of ozone actually measured in the atmosphere however

are higher than those shown on the graph for high NOx and I-IC concentrations for

those years up to the present

The strategy to meet the oxidant standard is obvious--get atmospheric NOx

and HC concentrations out of the area on the chart that produces high ozone levels

and put them in tie areas with the lowest levels This can only be done by implementshy

ing appropriate emission standards

As can be seen that did not happen between 1965 and 1970 because manufacshy

turers used controls on new cars in California which while causing a decrease in

BC (and CO) allowed a large increase in NOx emissions Thus the path line of

the atmosphere on the chart goes up from 65 and diagonally to the left passing

through an area of higher ozone levels The atmospheric concentrations of oxidant

predictably increased during the years 1967 and 1968 By 1970 they dropped to lower

levels - -back to about the same as in 1965- -exactly as predicted by the model The

app14oximate location of the point for 1970 (70) was both predicted on the basis of

247

the mathematical model and confirmed by atm-ospheric measurements of

[)owntown Los Angeles morning summertime NOx and calculated HC values

Again it should be pointed out that those points show the highest possible

concentrations of NOx and HC Years with less restrictive weather conditions

(for accumulating high primary contaminant levels) would cause lower measured

maximum NOx and HC levels but the calculations would still yield the points

shown Thus we are taking the most pessimistic view

Future Projections

In 1973 we were at about the point labeled 73 and ozone levels were beginshy

ning to drop as expected middot It should be emphasized that ozone values plotted on

thi$ graph are for the chamber only- -not the atmosphere The future path the

points 7 4 and on to 90 represents our estimate of future atmospheric levels of

NO and BC expected if the exhaust emission standards are just met While that X -

is optimistic it is all we really can do since performance of future vehicle models

is unknown We will achieve maximum ozone levels at or below the standard by

about 1980-1985 This will only be true however if cars in compliance with the

California interim standards for HC and NOx continue to be added to the vehicle

population at the normal rate These standards provide the optimum ratio of NO X

to HC necessary to provide the nitric oxide (NO) needed for the reaction that re-

moves from the air both oxidant formed photochemically and oxidant which occurs

as natural background which alone may cause the standard to be exceeded This

ratio is about 112 or 2 parts NOx to 1 part HC

248

The optimum NOxHC ratio is a key element in the APCD strategy but will

require a finite time for its attainment Replacement of older cars by newer ones

equipped to meet the most stringent standards is the only reasonable mechanism

which can change it VMT reduction proposed as a prime strategy by EPA cannot

change this crl(ical ratio which is a basic characteristic of the population at any

given time

Validation of the Districts Control Strategy

Figure 8 compares (1) future chamber oxidant levels based upon the

future maximum concentrations of HC and NOx we expect each year with the

California control program (2) calculated atmospheric concentrations using ~ I

our chamber-to-atmasphere empirical translation and (3) actual measured atmos-f 1l pheric oxidant maxima This clearly sets forth the relationship among these three

factors

The chamber concentrations (lower curve) middotare the lowest values shown

The actual atmospheric data (points connected by heavy dotted and solid lines)

vary considerably from year to year partly because of the vagaries of the weather

In all cases the atmospheric oxidant values are higher than the chamber values

because of the addition of vehicle emissions as the air parcel travels from source

to receptor areas The calculated atmospheric data (thin dashed and solid curves)

are shown to be the highest generally exceeding or equalling the actual measured

data and of course always exceeding the chamber data Thus the model paints

the most pessimistic picture possible It can be seen that by about 19801 1985 atmos -

pheric levels should be at or below the Federal air quality standard of 0 08 ppm oxidant

249

3 Motor Vehicle Exhaust Control is the Only Requirement for Achieving the Oxidant Standard by 1980

We can show that the existing motor vehicle control program has resulted

in a significant reduction of oxidant concentrations in the air

The foregoing material explained the relationship between vehicula~ emis -

sions in source areas and the high oxidant levels measured in effect areas This

relationship is exemplified by the downward trend of oxidant levels in the atmosshy

phere and by the similar year-by-year trends of NO and HC emissions from the X

average motor vehicle A projection of these vehicle emissions factors shows that

the associated maximum oxidant level in the atmosphere will meet the oxidant standard

by about 1980-1985

Figure 9 compares by year the number of days that the oxidant air quality

standard was exceeded in three separate areas with the average NO and HC emissions X

per vehicle mile To comply with the air quality regulations the number of days that

this standard is exceeded must be reduced to one per year

The lines plotted on Figure 9 show that a definite relationship exists between

the emissions from the average motor vehicle and the number of days each year that

the oxidant concentration in the air exceeds the clean air standard

The oxidant trendlines for downtown Los Angeles Pasadena arrl Azusa are

all downward and the slopes are about the same This similarity is logical because

the process that results in the suppression of oxidant accumulation simply has been

displaced from one area to another This was a unique one time situation because

of the increase in NOx between 1966 and 1971 After 1971 all areas are down Thus

l

250

the same conclusion is reached that the oxidantstandard will be met in the 1980s

I whether air quality data or vehicle emissions trends are projected middot~ Ul-

This outlook is based on the APCD s belief that future growth in both the

Los Angeles area and SCAB will not create any locality with a traffic density greater

than any traffic density in the area to date For the past 25 years the area around

downtown Los Angeles has been the area of maximum traffic density and therefore

the emissions source area responsible for the maximum effect area measurements

It is assumed that the traffic density in any future source area will be no

greater than the traffic density in downtown Los Angeles Thus since the

vehicular emissions control program will achieve and maintain the air quality

standards in areas affected by vehicular emissions from downtown Los Angeles it

will also achieve and maintain them for any area of SCAB

Summary Conclusions and Recommendations

In conclusion we have shown that a source and effect area analysis of emisshy

sions and resulting oxidant is a more reasonable and accurate representation of

the Los Angeles area for air quality analysis than gross integration metho9s such

as the big box technique It has been shown that motor vehicles are the major and

almost sole contributor to the primary HC and NOx emissions in the downtown source

area which results in the high oxidant levels in the San Gabriel Valley in fact the

highest in SCAB An air quality model and vehicle emissions control strategy has

been suggested to meet the oxidant standard by mid-1980 s

251

We have shown that

bull Only by adjusting the ratio of NOxHC in the motor vehicle emissions to

permit accumulation of sufficient atmospheric NO to sea venge the normal

atmospheric background oxidant can the standard be attained

bull The APCD strategy which provides for implementation of the present

California interim emissions standards for NOx HC and CO for new

motor vehicles in California beginning with the 1975 model vehicles will

result in compliance with the CO N02 and oxidant air quality standards

by the mid 1980 s and will maintain this compliance until 1990 and

possibly longer

bull The effectiveness of the present California motor vehicle control program

is easily demonstrable using air quality data from several areas in Los

Angeles County 1960-1973

bull To assure achievement and maintenance of the air quality goals as now preshy

dicted there must be periodic assessments of the effectiveness of the

motor vehicle control program followed by corrective actions if necessary

What has been accomplished thus far is significant but much more remains

to be done so that the best possible representation of emissions and resulting air

quality may be available for use in this air basin A much better emission inventory

defining the spatial and temporal distribution of both mobile and stationary sources

is needed Better statbnary source information is needed to evaluate the local

effects of these emissions Further detailed studies are needed to establish the

252

true relationship between emissions data from vehicle test cycles and the actual

operation of vehicles neither the 7-mode nor the CVS procedure provides a true

representation of actual vehicle operation Further tracer studies to assess the

transport and dilution of mobile and stationary source emissions from selected

source areas are also needed

253

1111

IUD

a CC I w gt-

1111

1UO

IUD

I 990

IDJO

1180

1111

IUO

FIGURE I

HYDROCARBONS

STATIONARY SOURCES MOTOR VEHICLES

- --

8 12 II 20 742 2l IS 12 I 4

HUNDREDS

HYDROCARBON EMISSIONS STATIONARY SOURCES IN

OXIDES OF

0

OF TONSDAY

FROM MOTOO VEHICLES AND LOS ANGELES COUNTY

NITROGEN

STATIONARY SOURCES

MOTOR VEHICLES

011111111111111111110111bull1111111

IIIIIIHIIIIIIIIIHIUII

llillL Its rd

l1uu~111111u1111111

2 I O 1 J 3

HUND REDS OF TONSDAY

OXIDES OF NITROGEN EMISSIONS FROM MOTOR VEHICLES ANO STATIONARY SOURCES IN LOS ANGELES COUNTY

illl~ -~--~ i~-=i _J~l ~--~ bull_~L- I ~~~-~~--Z ~

6

6S-66 ox

ICS ~A~1 M

i ssmuwmmgt

bullI

e COROyent_

64 ~ IDB RIVERS~

ORAJfD

-

t t 10 miles

bullmiddotsame Avg Cone Both Years

Pigare 2

YEAR OP HIGHEST OXlDANI CONCENTRATIONS

Highest Average of Daily -Maiimum One-Hour Concentrations

During July August amp September 1963-1972

bullLj

I

64

70 s11 3RlU)U0

70

--__ 69bull

N V +=

middot Source Air Resources Board

-200o

t t 10 adlea

tDS ampIJtsect

-1~

-1611ASampXllmiddot bull - bull -z----~------

I ldmmprwJ

IIVERSIDI

~ - 70

OampY -1 U 70 bull L

I

N V1 V

middot-i___

-----------------------------------------------------------i----------------------------

Figure 3

CHANGE OP OXIDANT CONCENTRATIONS

Percent Change from the Highest Three-Year Average to the 1970-72 Average

Of Daily Maximum One-Hour Con~entrationa for JulY August amp September

Source Air Resources Board

256

FIGURE 4 TYPICAL FLOW OF POLLUTED Am PARCEIS CIUGINATING AT DIFFERENT LOCATIONS IN THE LOS ARE~S BASIN - STARTIOO 0900 PST

l I

OAT

TRAJECTORY SUWMATIOl4

----- SMOG ~AVS

I

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullNONbullSlfOG DAYS

ISTARTING Tl~ cgxpsy

~ HAW

(CA

257

FiGURE 5 ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AND OXIDANT IN DOWlflC1N LOS AIDELES (SOURCE AREA) AND PASADENA (EFFECT AREA) 1

1960-1972

LO CARBON MONOXIDE

30

Pasadena

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullbullbullbullbull Downtown Los Angeles

20

10

o_______________________________

OXIDANT

)

2 Down~ Los Angeles

1

o________________________ 1960 1962 196L 1966 1968 1970 1972

YEAR

bullbullbullbullbull

bullbullbullbullbullbullbull

258

FIGURE 6 COMPARISON 01 CALCULATED AND MEASURED ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AN1) OXIDES OF NITROOEN IN DCMNTOWN IDS AIJELES

196o-1972

CARBON MONOXIDE

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ~ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot _-- ---_ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ----middotmiddot-bullw-_~ ---bullbullbull

10

o_______________1111111_____

OXIDES OF NITROGEN25

20

15 bullbullbullbullbullmiddotmiddotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~

1-i 10 middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ---

oS o_______________________

RATIO CONOx

40

50

0 +raquo Cd

p 30

~ 20

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot bullbullbullbullbull middotmiddotmiddotmiddotmiddot-shybullbullbullbullbull 0 u

bullbullbullbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot 10

0 j

ilI 196o 1964 1968 1970 1972 I

YEAR

Measured~D-owntown Los Angeles (90th percentile ofmiddot daily] instantaneous maxima)

Calculated - Aver~ge vehicle emissions - Present control program

259

FIGURE 7

25

t i5

flJ

~ on ~ ~ Q) bO 100 Jo

+gt on z

o5

EFFECT OF CALIFORNIA 1 s AUTO EXHAUST CONTROL ffiOORA M ON MAXIMUM CHAMBER OZONE CONCENTRATION

- PPM

357bullbull

r 76 bull

11 l

30

20

CHAMBER OZONE MAXIMUM

50

10

o___________111111111111______111111111111_____________

0 05 10 15 20 25

Hydrocarbons m-2 (LB-15) - PPM (as Hexane)middot

--

bull bull bull

r--=--~1 ~a==-~ - _~l ~ y--===-- ~~--~-- ~ r---~~

o

o8

~ I

~ 0 H 8 o6 I

c~ ~ 0 z 0 0

8

~ o+ A H gtlto-

02

middoto

Figure 8 Calculated t1ax1mum Levels Instantaneous and Hourly Average

of Atmospheric Oxidant Compared to Measured Los Angeles County Maxima-with Projections to 1990

(California Standards)

~ -Calculated Inst ax ~

f Calculate Max Hr Avg 03

_ bullbull _ _ - i bull

0 bullbull -l bullbull a0Ieasured Inst Lax o3 bull middotmiddotmiddot~bull 0bull _ ____ V ~ ea~ured ~ Hr Avr o3

~~ r---

~ ~ NB r~ima for 197 4 amiddots of 121074--- -_ Chamber Ozone F ~_ _~

- 1L_

~ Federal Primarfo Air ~uality Standard ~6- -UaximumT- our Avera~elr~ppm-------------- --~ ------- -~- -~-- ~

I I I I I I I I I I I I I I I I I N1 O

1960 6i 64 66 ~i middot-o 72 74 76 79 middotso middot92 84 bullg s9 9o

TBAR (end)

0

261 FIGURE -OMPARISON OF ATMOSPHERIC OXIDANT TRENDS WITH AVERAGE NCJx AND

HC EMISSIONS (Grams per Mile from Average Vehicle)

JOO Number of days state oxidant standara wds equalled or exceeded

--- Azusa __ Pasadena ________ Downtown Los Angeles

20

15 u

___ Hydroc_arbons Oxides of Nitrogenbullmiddotmiddotmiddotmiddotmiddotbullbullmiddot 1975 and later-assume middotcalifornia ARB standards

o_ ___________________________11111____

1965 1970 1975middot 198omiddot 198S 1990

138

What about the 1975 California car Most of you probably have enough

interest in this vehicle that youve tried to figure out just what it does

But in case some of you have not been able to straighten its operation out

let me tell you as best I understand what the 1975 California car is

The cars from Detroit are 100 cataly~t eq11ipped There may be an excepshy[

l

1 tion sneaking through here and there but it looks like it is 100 These

are equipped with oxidation catalysts in a variety of configurations and

sizes the major difference being the pellet system which is used by

General Motors versus the monolith system which has been used by Ford and

Chrysler The pellet system appears to be better than the monolithic ~ l l system but it is not so obvious that there are huge differences between the

aocgtnow The catalysts come in a variety of sizes they are connected to

the engine in different ways sometimes there are two catalysts sometimes

a single catalyst (the single catalyst being on the 4 and 6-cylinder

engines) Some of the 8-cylinder engines have two catalysts some of them

have one catalyst All California cars have all of the exhaust going

through catalysts This is not true of some of the Federal cars in which

some of the exhaust goes through catalysts and some does not

Ninety percent of the California cars probably will have air pumps

Practically all the cars from Detroit have electronic ignition systems

which produce more energetic sparks and more reliable ignition The

exhaust gas recirculation (EGR) systems appear to have been improved

somewhat over 1974 but not as much as one would have hoped There were

some early designs of EGR systems which were fully proportional sophistishy

cated systems These do not appear to have come into final certification

so that there still is room for further improvement of the EGR system

The emissions levels in certification of these vehicles are extremely low

139

(Table I) Just how the automc1bile industry selects the emission levels

at which they tune their vehicles has been of great interest The

hydrocarbon and CO levels in certification (with deterioration factors

applied--so this is the effective emissions of the certification vehicles

at the end of 50000 miles) are approximately one-half the California

standards The oxides of nitrogen emissions are approximately two-thirds

of the California standards This safety factor is put in by the automoshy

bile industry to allow for differences between the certification vehicles

and the production vehicles to ensure that they did not get into a situation

of recall of production vehicles which would be very expensive

There appears to have been a great deal of sophistication developed by

the automobile industry in being able to tune their vehicles to specific

emission levels General Motors appears to have done better tuning than

the other manufacturers This leads to the rather interesting result

that a significant number of the 1975 California vehicles meet the 1977

emission standards (Table II) that is approximately 10 of the U S cars

certified for California already meet the 1977 emission standards This

does not mean to say that the industry could immediately put all of their

production into such vehicles and meet the 1977 emission standards because

of a concern about the safety factor for the certification versus producshy

tion vehicles Thirty-four percent of the foreign vehicles certified for

1975 in California meet the 1977 emission standards The 1977 emission

standards are 041 grn hydrocarbon~ 34 gm carbon monoxid~ and 20 gm

oxides of nitrogen This does confirm that the oxidation catalysts are a

more than adequate technology for meeting the 1977 emission standards and

only minor refinements and adjustments to those systems are required to go

ahead with the 1977 emission standards There are some other arguments

against this optimistic viewpoint and Ill deal with those later

140

There is a great uniformity in the deBigns which the U S manufacturshy

ers have selected for the 1975 California vehicles For those of you who

do not live in California about 80 of thl~ vehicles in the rest of the

country will be catalyst equipped General Motors is going with 100

catalysts apparently to realize the fuel economy benefit of their system

which more than pays for the cost of the catalyst system We have the very

interesting situation that the more stringent 1975 emission standards have

not only reduced the emissions of the 1975 vheicles with respect to the

1973-1974 vehicles but have also reduced the cost of operating the car

and have improved fuel economy The idea that emissions control and fuel

economy and economical operation are always one at odds with the other is

simply not true Compared to the previous years vehicles the more

stringent emissions standards of 1975 have brought improvements to fuel

economy because they forced the introduction of more advanced technology

The fuel savings which have been realized produce a net decrease in operashy

tional costs over the lifetime of the car This is not to say that pollution

control doesnt cost something If you were to compare the 1975 vehicle

with a completely uncontrolled vehicle tht~re would indeed be an incremental

cost associated with the 1975 vehicle

The foreign manufacturers have demonstrated a greater variety of

approaches in meeting the 1975 California standards but again they are

producing mostly catalyst equipped vehicles There is a widespread use of

fuel injection by the foreign manufacturers especially the Europeans

apparently because this is the easiest appmiddotroach for them and they realize

that only a fraction of their production comes to the United States

Volkswagen for example apparently has gone to 100 fuel injection on its

air cooled engines to be sold in California Mazda will continue to sell

141

rotary engine vehicles and thereby be the only rotary engine vehicle

manufacturer and marketer in the United States General Motorsgt elimination

of therotary engine stated for reasons of emissions is probably more

influenced by problems with fml economy although the two are a bit

difficult to separate Mazda is meeting the 1975 emissions standards and

in fact can meet the 1977 emission standards It has not solved its fuel

economy difficulties on the 1975 cars they will do better in 1976 All

evidence points to a fuel economy penalty for the rotary engine Nonetheshy

less we do have this option available because of the Japanese Also the

foreign manufacturers are providing us with a small number of diesel

engine cars These are of great interest because of definite fuel economy

advantages The diesel engine vehicles also meet the 1977 emissions

standards right now Also in J975 well 3ee the CVCC engine marketed by

Honda

The costs of the 1975 vehicles over tae lifetime of the vehicle are

definitely lower than the costs of the 197~ vehicles The National Academy

of Sciences estimate averaged over all vehicles is that in comparison to

the 1970 vehicles the lifetime cost of emission control system including

maintenance and fuel economy costs is aboJt $250 per vehicle greater in

1975 than 1970 Since the 1974 vehicles w2re about $500 more expensive

there has been a net saving in going from 1974 to 1975 I think the

conclusion we should draw for 1975 is that the auto industry has done a

pretty good job in meeting these standards This is something which they

said they couldnt do a few years ago something which they said that if

they could do it would be much more expewdve than it has turned out to

be

The same technology can be applied to 1977 models with no technological

difficulty and only slight refinements of the systems The fuel economy

142

penalties as estimated by the National Academy of Sciences are small 3

or less in going to the 1977 standards This estimate does assume further

advancements by the auto industry to improve fuel economy--primarily

improved exhaust gas recirculation systems It is unfortunate that this

issue of fuel economy has become so mixed up with the air pollution question

because the two are only slightly related If one is really concerned about

fuel economy and there isnt too much evidence that the auto industry or

the American public really is too concerned right now there is only one

way to have a drastic effect on fuel economy and that is to decrease the

vehicle weight Until that is done with gains on the order of 50 or

more to worry about 3 or 5 differences in fuel economy related to emission

control systems is simply to focus upon the wrong issue

Now what are the problem areas What remains to be done The

problems certainly arent over with the introduction of the 1975 vehicles

Problem Area Number One Field performance What is going to happen

to these vehicles when they get into actual service Past experience with

the 1971 through 1973 vehicles has been rather poor in that EPA and

California surveillance data show that these vehicles are not meeting the

standards Many of them did not meet the standards when they were new

The situation in general is getting worse at least for CO and hydrocarbons

that is with time the emission levels of CO and hydrocarbons for the 1971 I through 1973 vehicles is degrading There is no in-service experience of

this sort with the 1975 vehicles yet The certification data look quite I promising but the test procedures especially for durability are not ithe same as what occurs in actual use It is generally stated that the

1actual use situation for the catalysts will be more severe than the EPA

test procedure A larger number of cold starts are involved in actual use

than in the EPA test procedure and thermal cycling will probably have an

143

adverse effect on the lifetime of the cata]_yst This is not so obvious

It is also likely that the higher temperature duty cycle in actual use will

improve the performance of the catalyst in that it will help to regenerate

the catalyst through the removal of contaminants as long as one does not

get into an overheat situation The National Academy of Sciences estimate

was that the number of catalyst failures tn the first 50000 miles would

be on the order of about 7 Thats a very difficult number to estimate in

the absence of any real data A 7 failure still leaves a net gain in

emissions control even if nothing is done about this failure This points

to the problem of what happens after 50000 miles The EPA certification

procedure and control program only addresses the first 50000 miles The

second 50000 miles or slightly less for the average car is the responsishy

bility of the states Unfortunately then~ seems to be very little progress

in the area of mandatory inspection and ma-Lntenance--very little thought

being given to whether the replacement ofthe catalyst at 50000 miles

if it has failed is going to be required and how that is going to be

brought about The area of field performance remains a major problem

area one which obviously needs to be monitored as the California Air

Resources Board has been doing in the past but probably even more carefully

because the unknowns are higher with the catalyst systems

Problem Area Number Two Evaporative hydrocarbons from automobiles

It was identified at least 18 months ago that the evaporative emission

control systems are not working that the evaporative emissions are on the

order of 10 times greater than generally thought In the Los Angeles

area cars which are supposed to be under good evaporative emissions

controls are emitting approximately 19 grams per mile of hydrocarbons

through evaporation This apparently has to do with the test procedure used

144

The EPA is pursuing this The California Air Resources Board does have some

consideration going on for this but it appears that the level of activity

in resolving this problem is simply not adequate If we are to go ahead

to 04 of a gram per mile exhaust emissions standards for hydrocarbons

then it just doesnt make sense to let 19 grams per mile equivalent escape

through evaporative sources

Problem Area Number Three What about the secondary effects of the

catalyst control systems Specifically this is the sulfate emissions

problem and I really do not know the answer to that Our appraisal is

that it is not going to be an immediate problem so we can find out what

the problem is in time to solve it The way to solve it now since the

automobile industry is committed to catalysts and it is unreasonable

to expect that they will reverse that technology in any short period of

time is take the sulfur out of the gasoline The cost of removing sulfur

from gasoline is apparently less than one cent per gallon Therefore if

it becomes necessary to be concerned with sulfate emissions the way to

meet the problem is to take the sulfur out of gasoline Obviously sulfate

emissions need to be monitored very carefully to see what happens The

final appraisal is certainly not now available Another secondary effect

of the catalysts is the introduction of significant quantities of platinum

into an environment where it hasnt existed before Not only through

exhaust emissions which appear to be small but also through the disposal

problem of the catalytic reactors Since the quantity of platinum involved

is quite small the argument is sometimes used that platinum does not

represent much of a problem The fact that the amount of platinum in the

catalyst is so small may also mean that its not economical to recover it

This is probably unfortunate because then the disposal of these catalysts

l Jj

145

I becomes important I will not speak to the medical issues because

am not qualified The evidence is that theuro~ platinum will be emitted in a

form which does not enter into biological cycles--but this is no assurance

that it couldnt later be transformed in such a form What is obviously

needed is a very careful monitoring program which hopefully was started

before the catalysts were put into service If it wasnt then it should

be started today

Problem Area Number Four NO control The big problem with NO X X

control is that nobody seems to know or to be willing to establish what

the emission control level should be It is essential that this be tied

down rapidly and that it be fixed for a reiatively long period of time

because the NO level is going to have a VE~ry important ef feet upon the X

development of advanced engine technology The 20 gm level has been

attained in California with some loss of fuel economy through the use of

EGR and it is not unreasonable in our estimation to go to 15 grams per

mile with very little loss in fuel economy To go to 04 gram per mile

with present technology requires the use of one of two catalytic systems

either the reduction catalyst in tandem with the oxidation catalyst or what

is known as the three-way catalyst Both of these systems require technoshy

logical gains The state of development appears to be roughly that of the

oxidation catalyst two years ago The auto industry will probably say

that it is not quite that advanced but that if it were required to go to

04 gram per mile in 1978 that it could be done With the catalyst systems

the fuel economy penalties would not be great in fact the improvement to

the engine which would be required to make the system work would again

probably even allow a slight improvement in fuel economy What the 04

gram per mile NO catalyst system would appear to do however is to X

146

eliminate the possibility of the introduction of stratified charge engines

both the CVCC and the direction injection system and also diesel engines

It is in the context of the advantages of these advanced engines to meet

emission standards with improved fuel economy that one should be very

cautious about the 04 grammile oxides of nitrogen standards for automoshy

biles My own personal opinion is that the number should not be that

stringent that a number of 1 or 15 gm is appropriate Such a level

would require advancements but would not incur great penalties

Other items which I view as problem areas are less technically

involved and therefore require fewer comments

bull Nonregulated pollutants--again thls is a matter of keeping track

of particulates aldehydes hydrocarbon composition to make

certain that important pollutants ire not being overlooked or

that emission control systems are not increasing the output of

some of these pollutants

bull Fuel economy The pressures of fuel economy are going to be used

as arguments against going ahead wlth emissions control Mostly

these two can be resolved simultaneously We should simply ask

the automobile industry to work harder at this

bull Final problem area New fuels Again it does not appear that

the introduction of new fuels will come about as an emissions

control approach but that they may be introduced because of the

changing fuel availability patterns and the energy crisis These

fuels should be watched carefully for their impact upon emissions

This does middotappear to be an area in which a great deal of study is

going on at the present time It is one problem area perhaps in

which the amount of wprk being done is adequate to the problem

which is involved

147

In sunnnary then the appraisal of the 1975 systems is that they are

a big advancement they will be a lot better than most of us thought and

that we should give the automobile industry credit for the job theyve

done in coming up with their emissions control systems

With that boost for the auto industry which Im very unaccustomed

to Ill entertain your questions

-------=-~ ~~~ U- ~a1

~_~a--~-~ -J~ ~ -~r- _ --=~-- -___ja--~ __1~~ ~-~----=

AIR

1-4 FUEL----1

I I ENGINE

I II

_________ EXHAUST SYSTEM I bull EXHAUST

I I I

+ MIXTURE CONTROL COMBUSTION MODIFICATION EXHAUST TREATMENT

FuelAir Metering Ignition Air Jnjection FuelAir Mixing Chamber Geometry Thermal Reactor Fuel Vaporization Spark Timing Oxidation Catalyst Mixture Distribution Staged Combustion Reduction Catalyst Fuel Characteristics Ex tern almiddot Combustion Three Way Catalyst Exhaust Gas Redrculation Particulate Trap

FIGURE 1 Approaches to the Control of Engine Emissions

~ i 00

149

TABLE I

Average Emissions of 1975 Certification Vehicles (As Corrected Using the 50000-Mile Deterioration Factor)

Emissions in gmi Fraction of Standard HC CO NO HC CO NO

Federal 1975 X X

AMC 065 67 25 043 045 080

Chrysler 074 77 25 049 051 082

Ford 081 92 24 054 061 078

GM 083 80 23 055 053 074

Weighted Average 080 82 24 053 055 076

California 1975

AMC 042 49 17 047 054 087

Chrysler 048 61 16 053 067 082

Ford 052 56 13 058 062 067

GM 065 55 16 0 72 061 082

Weighted Average 058 56 16 064 062 078

kWeighted average assumes the following market shares AMC 3 Chrysler 16 Ford 27 and GM 54

150

TABLE II

Total Number of Vehicles Certified for California 1975 Standard and the Number (and percentage) of These Able to Meet

Certain More Stringent Standards

Calif 1975 Federal 1977 Hypothesized Hypothes ized 099020 04J420 049020 093420

i ~

Manufacturer no () no () no () no ()

AMC 16 (100) 1 ( 6) ti ( 38) 3 (19)

Chrysler 21 (100) 2 ( 9) ( 33) 0 ( O)

Ford 26 (100) 4 (15) -middot ( 15) 5 (19)

l GM 46 (100) 1 ( 2) -1 ( 9) 5 (11)

Foreign 62 (100) 21 (34) 3H (61) 28 (45)

1J

f

-l

151

CURRENT STATUS OF ALTERNATIVE AUTOM)BIIE ENGINE TECHNOLCXY

by

Henry K Newhall Project Leader Fuels Division

Chevron Research CanpanyRicbmmd California

I

iH1middot

10 1ntroduction and General Background

I

11 General

The term stratified ct1arge englne has been used for many

years in connection with a variety of unconventional engine

combustion systems Common to nearly all such systems is

the combustion of fuel-air mixtures havlng a significant

gradation or stratification in fuel- concentration within the

engine combustion chamber Henee the term nstratifled charge

Historically the objective of stratified charge engine designs

has been to permit spark ignition engine operation with average

or overall fuel-air ratios lean beyond the ignition limits of

conventional combustion systems The advantages of this type

of operation will be enumerated shortly Attempts at achieving

this objective date back to the first or second decade of this

century 1

More recently the stratified charge engine has been recognized

as a potential means for control of vehicle pollutant emissions

with minimum loss of fuel economy As a consequence the

various stratified charge concepts have been the focus of

renewed interest

152

12 Advantages and Disadvantages of Lean Mixture Operation

Fuel-lean combustion as achieved in a number of the stratified

charge engine designs receiving current attention has both

advantages and disadvantages wnen considered from the comshy

bined standpoints of emissionsmiddot control vehicle performance

and fuel economy

Advantages of lean mixture operation include the following

Excess oxygen contained in lean mixture combustion

gases helps to promote complete oxidation of hydroshy

carbons (HG) and carbon monoxide (CO) both in the

engine cylinder and in the exhaust system

Lean mixture combustion results in reduced peak

engine cycle temperatures and can therefore yield

lowered nitrogen oxide (NOx) emissions

Thermodynamic properties of lean mixture combustion

products are favorable from the standpoint of engine

cycle thermal efficiency (reduced extent cf dissociashy

tion and higher effective specific heats ratio)

Lean mixture operation caG reduce or eliminate the

need for air throttling as a means of engine load

control The consequent reduction in pumping losses

can result in significantly improved part load fuel

economy

153

Disadvantages of lean mixture operation include the following

Relatively low combustion gas temperatures during

the engine cycle expansion and exhaust processes

are inherent i~ lean mixture operation As a conseshy

quence hydrocarbon oxidation reactions are retarded

and unburned hydrocarbon exhaust emissions can be

excessive

Engine modifications aimed at raising exhaust temperashy

i tures for improved HC emissions control (retarded middot~

ignition timing lowered compression ratlo protrtacted combustion) necessarily impair engine fuel economy1 I

1j bull If lean mixture operation is to be maintained over ~

the entire engine load range maximum power output t l and hence vehicle performance are significantly

impaired

Lean mixture exhaust gases are not amenable to treatshy

ment by existing reducing catalysts for NOx emissions

control

Lean mixture combustion if not carefully controlled

can result in formation of undesirable odorant

materials that appear ln significant concentrations

in the engine exhaust Diesel exhaust odor is typical

of this problem and is thought to derive from lean mixshy

ture regions of the combustion chamber

154

Measures required for control of NOx emissions

to low levels (as example EGR) can accentuate

the above HC and odorant emissions problems

Successful developmentmiddotor the several stratified charge

engine designs now receiving serious attention will depend

very much on the balance that can be achieved among the

foregoing favorable and unfavorable features of lean comshy

bustion This balance will of course depend ultimately on

the standards or goals that are set for emissions control

fuel economy vehicle performance and cost Of particular

importance are the relationships between three factors -

UBHC emissions NOx emissions and fuel economy

13 Stratified Charge Engine Concepts

Charge stratification permitting lean mixture operation has

been achieved in a number of ways using differing concepts

and design configurations

Irrespective of the means used for achieving charge stratifishy

cation two distinct types of combustion process can be idenshy

tified One approach involves ignition of a small and

localized quantity of flammable mixture which in turn serves

to ignite a much larger quantity of adjoining or sur~rounding

fuel-lean mixture - too lean for ignition under normal cirshy

cumstances Requisite m1xture stratification has been achieved

155

in several different ways rangiDg from use of fuel injection

djrectly into open combustion chambers to use of dual

combustion chambers divided physically into rich and lean

mixture regions Under most operating conditions the

overall or average fuel-air ratio is fuel-lean and the

advantages enumerated above for lean operation can be realized

A second approach involves timed staging of the combustion

process An initial rich mj_xture stage in which major comshy

bustion reactions are completed is followed by rapid mixing

of rich mixture combustion products with an excess of air

Mixing and the resultant temperature reduction can in

principle occur so rapidly that minimum opportunity for NO

formation exists and as a consequence NOx emissions are

low Sufficient excess air is made available to encourage

complete oxidation of hydrocarbons and CO in the engine

cylinder and exhaust system The staged combustion concept

has been specifically exploited 1n so-called divided-chamber

or large volume prechamber engine designs But lt will be

seen that staging is also inherent to some degree in other

types of stratified charge engines

The foregoing would indicate that stratified charge engines

can be categorized either as lean burn engines or staged

combustion engines In reality the division between conshy

cepts is not so clear cut Many engines encompass features

of both concepts

156

14 Scope of This Report

During the past several years a large number of engine designs

falling into the broad category of stratified charge engines

have been proposed Many of these have been evaluated by comshy

petent organizations and have been found lacking in one or a

number of important areas A much smaller number of stratified

charge engine designs have shown promise for improved emissions

control and fuel economy with acceptable performance durashy

bility and production feasibility These are currently

receiving intensive research andor development efforts by

major organizations - both domestic and foreign

The purpose of this report is not to enumerate and describe the

many variations of stratified charge engine design that have

been proposed in recent years Rather it is intended to focus

on those engines that are receiving serious development efforts

and for which a reasonably Jarge and sound body of experimental

data has evolved It is hoped that this approach will lead to

a reliable appraisal of the potential for stratified charge

engine systems

20 Open-Chamber Stratified Charge Engines

21 General

From the standpoint of mechanical design stratified charge

engines can be conveniently divided into two types open-chamber

and dual-chamber The open-chamber stratjfied charge engine

has a long history of research lnterest Those crigines

157

reaching the most advanced stages of development are probably

the Ford-programmed c~mbustion process (PROC0) 2 3 and Texacos

controlled combustion process (TCCS) 4 5 Both engines employ a

combination of inlet aar swirl and direct timed combustion

chamber fuel injection to achieve a local fuel-rich ignitable

mixture near the point of ignition _For both engines the overshy

all mixture ratio under most operating conditions is fuel lean

Aside from these general design features that are common to

the two engiries details of their respective engine_cycle proshy

cesses are quite different and these differences reflect

strongly in comparisons of engine performance and emissions

characteristics

22 The Ford PROCO Engin~

221 Description

The Ford PROCO engine is an outgrowth of a stratified charge

development program initiated by Ford in the late 1950s The

development objective at that time was an engine having dieselshy

like fuel economy but with performance noise levels and

driveability comparable to those of conventional engines In

the 1960s objectives were broadened to include exhaust

emissions control

A recent developmental version of the PROCO engine is shown in

Figure 2-1 Fuel is injected directly into the combustion chamber

during the compression stroke resulting in vaporjzation and

formation of a rich mixture cloud or kernel in the immediate

158

vicinity of the spark plug(s) A flame initiated in this rich

mixture region propagates outwardly to the increasingly fuelshy

lean regions of the chamber At the same time high air swirl

velocities resulting from special orientation of the air inlet

system help to promote rapid mixing of fuel-rich combustion

products with excess air contained in the lean region Air

swirl is augmented by the squ1sh action of the piston as it

approaches the combustion chamber roof at the end of the comshy

pression stroke The effect of rapid mixing can be viewed as

promoting a second stage of cori1bustion in which rlch mixture

zone products mix with air contained in lean regions Charge

stratification permits operation with very lean fuel-air mixshy

tures with attendent fuel economy and emissj_ons advantages In

addition charge stratification and direct fuel injection pershy

mit use of high compression ratios with gasolines of moderate

octane quality - again giving a substantial fuel economy

advantage

Present engine operation includes enrichment under maximum

power demand conditions to mixture ratios richer than

stoichiometric Performance therefore closely matches

that of conventionally powered vehicles

Nearly all PROCO development plans at the present time include

use of oxidizing catalysts for HC emissions control For a

given HC emissions standard oxidizing catalyts permit use

of leaner air-fuel ratios (lower exhaust temperatures)

1

l

159

together with fuel injection and ignition timing charactershy

istics optimized for improved fuel economy

222 Emissions and Fuel Economy

Figure 2-2 is a plot of PROCO vehicle fuel economy versus NOx

emissions based or1 the Federal CVS-CH test procedure Also

included are corresponding HC and CO emissions levels Only

the most recent test data have been plotted since these are

most representative of current program directions and also

reflect most accurately current emphasis on improved vehicle

fuel economy 6 7 For comparison purposes average fuel

economies for 1974 production vehicles weighing 4500 pounds

and 5000 pounds have been plotted~ (The CVS-C values

reported in Reference 8 have been adjusted by 5 to obtain

estimated CVS-CH values)

Data points to the left on Figure 2-2 at the o4 gmile

NOx level represent efforts to achieve statutory 1977

emissions levels 6 While the NOx target of o4 gmile was

met the requisite use of exhaust gas recirculation (EGR)

resulted in HC emissions above the statutory level

A redefined NOx target of 2 gn1ile has resulted in the recent

data points appearing in the upper right hand region of

Figure 2-2 7 The HC and CO emissions values listed are

without exhaust oxidation catalysts Assuming catalyst middotl

conversion efficiencies of 50-60 at the end of 50000 miles

of operation HC and CO levels will approach but not meet

160

statutory levels It is clear that excellent fuel economies

have been obtained at the indlcated levels of emissions

control - some 40 to 45 improved re1at1ve to 1974 produc-

tj_on vehicle averages for the same weight class

The cross-hatched horizontal band appearing across the upper

part of Figure 2-2 represents the reductions in NOx emissions

achieveble with use of EGR if HC emissions are unrestricted

The statutory 04 gmile level can apparently be achieved

with this engine with little or no loss of fuel economy but

with significant increases in HC emissions The HC increase

is ascribed to the quenching effect of EGR in lean-middotmixture

regions of the combustion chamber

223 Fuel Requirements

Current PROCO engines operated v1ith 11 1 compression ratio

yield a significant fuel economy advantage over conventional

production engines at current compression ratios According

to Ford engineers the PROCO engine at this compression

ratio j_s satisfied by typical fu1J-boi1ing commercial gasoshy

lines of 91 RON rating Conventional engines are limited to

compression ratios of about 81 and possibly less for

operation on similar fuels

Results of preliminary experiments indicate that the PROCO

engine may be less sensitive to fuel volatility than convenshy

tional engines - m1 important ff1ctor in flextb1 llty from the

standpoint of the fuel supplier

161

224 Present Status

Present development objectives are two-fold

Develop calibrations for alternate emissions target

levels carefully defining the fueleconofuy pbtenshy

tial associated with each level of emissions control

Convert engine and auxiliary systems to designs

feasible for high volume production

23 The Texaco TCCS Stratified Charge Engine

231 General Description

Like the Ford PROCO engine Texacos TCCS system involves_

coordinated air swirl and direct combustion chamber fuel

injection to achieve charge stratification Inlet portshy

induced cylinder air swirl rates typically approach ten times

the rotational engine speed A sectional view of the TCCS

combustion chamber is shown in Figure 2-3

Unlike the PROCO engine fuel injection in the TCCS engine

begins very late in the compression stroke - just before th~

desired time of ignition As shown in Figure 2-4 the first

portion of fuel injected is immediately swept by the swirling

air into the spark plug region where ignition occurs and a

flame front is established The continuing stream of injected

fuel mixes with swirling air and is swept into the flame

region In many respects the Texaco process resembles the

162

spray burning typical of dj_esel combustion ~r1th the difshy

ference that ignition is achieved by energy from an elec-

tric spark rather than by high compression temperatures

The Texaco engine like the diesel engine does not have a

significant fuel octane requirement Further use of positive

spark ignition obviates fuel I

cetane requirements character-

istic of diesel engines The resultant flexibility of the

TCCS engine regarding fuel requirements is a si~1ificant

attribute

In contrast to the TCCS system Fords PROCO system employs

relatively early injection vaporization and mixing of fuel

with air The combustion process more closely resembles the

premixed flame propagation typical of conventional gasoline

engines The PROCO engine therefore has a definite fuel

octane requirement and cannot be considered a multifuel

system

The TCCS engine operates with hi__gh compression ratios and

with little or no inlet air throttling except at idle conshy

ditions As a consequence fuel economy is excellent--both

at full load and under part load operating conditions

232 Exhaust Emissions and Fuel Economv

Low exhaust temperatures characteristlc of the TCCS system

have necessitated use of exhaust oxidation catalysts for

control of HC emissions to low lf~Vels A11 recent development

163

programs have therefore included use of exhaust oxidation

catalysts and most of the data reported here r~present tests

with catalysts installed or with engines tuned for use with

catalysts

Figures 2-5 and 2-6 present fuel economy data at several

exhaust emissions levels for two vehicles--a US Army M-151

vehicle with naturally aspirated 4-cylinder TCCS conversion

and a Plymouth Cricket with turbocharged 4-cylinder TCCS

engine 9 10 1urbocharging has been used to advantage to

increase maximum power output Also plotted in these figures

I are average fuel economies for 1974 production vehicles of

similar weight 8

I When optimized for maximum fuel economy the rrccs vehicles

can meet NOx levels of about 2 gmile It should be noted

that these are relatively lightueight vehicles and that

increasing vehicle weight to the 4000-5000 pound level could

result in significantly increased NOx emissions Figur~s 2-5

and 2-6 both show that engine modifications for reduced NOx

levels including retarded combustion timing EGR and increased

exhaust back pressure result in substantial fuel economy

penalties

For the naturally aspirated engine reducing NOx emissions

from the 2 gmile level to O l~ gmile incurred a fuel

economy penalty of 20 Reducing NOx from the tllrbocharged

164

engine from 15 gmile to 04 gmile gave a 25 fuel economy

penalty Fuel economies for both engines appear to decrease

uniformly as NOx emissions are lowered

For the current TCCS systems most of the fuel economy penalty

associated with emissions control can be ascribed to control

of NOx emissions although several of the measures used for

NOx control (retarded cornbusticn timing and increased exhaust

back pressure) also help to reduce HG emissions HC and CO

emissions ari effectively controlled with oxidation catalysts

resulting in relatively minor reductions in engine efficiency

233 TCCS Fuel Reauirements

The TCCS engine is unique among current stratified charge

systems in its multifuel capability Successful operation

with a nuraber of fuels ranging from gasoline to No 2 diesel

Table 2-I

Emissions and Fuel Economy of Turbocharged TCCS Engine-Powered Vehicle 1

Fuel

Emissions gMile 2 Fuel Economy

mng 2HC co NOx

Gasoline

JP-4

100-600

No 2 Diesel

033

026

014

027

104

109

072

J bull l ~

-

061

050

059

060

197

202

213

230

1M-151 vehicle 8 degrees coffibustion retard 16 light load EGR tw0 catalysts (Ref 10)

2 CVS-CH 2750 pounds tnert1a welght

165

l

has been demonstrated Table ~-I lists emissions levels and

fuel economies obtained with a turbocharged TCCS-powered

M-151 vehicle when operated on each of four different fuels 10

These fuels encompass wide ranges in gravity volatjlity

octane number and cetane leve 1 as middotshown in Table 2-II

Table 2-II

Fuel Specifications for TCCS Emissions Tests (Reference 10)

Gravity 0 API Sulfur

OFDistillation~

Gasolj_ne 100-600 JP-4 No 2

Diesel

88 -

86 124 233 342 388

0024 912

-

486 012

110 170 358 544 615

0002 57 356

541 0020

136 230 314 459 505

-middot --

369 0065

390 435 508 562 594

--

lta 9

IBP 10 50 90 EP

TEL gGal Research Octane Cetane No

Generally the emissions levels were little affected by the

wide variations in fuel properties Vehicle fuel economy

varied in proportion to fuel energy content

As stated above the TCCS engine is unique in its multifuel

capability The results of Tables 2-I and 2-II demonshy

strate that the engine has neither 8ign1ficant fuel octane

nor cetane requirements and further that it can tolerate

166

wide variations j_n fuel volati1tty rhe flexibility offered

by this type of system could be of major importance in

future years

234 Durability Performance Production Readiness

Emissions control system durability has been demonstrated by

mileage accumulation tests Ignltion system service is more

severe than for conventional engines due to heterogeneity of

the fuel-air mixture and also to the high compression ratios

involved The ignition system has been the subject of

intensive development and significant progress in system

reliability has been made

A preproduction prototype engine employing the TCCS process is

now being developed by the Hercules Division of White Motors

Corporation under contract to the US Army Tank Automotive

Command Southwest Research Inr)titute will conduct reliability

tests on the White-developed enGines when installed in Military

vehlcles

30 Small Volume Prechambcr Eng1nes (3-Valve Prechamber Engines Jet Ignition Engines Torch Ignition Engines)

31 General

A number of designs achieve charge stratification through

division of the combustion region into two adjacent chambers

The emissions reduction potentiampl for two types of dualshy

chamber engines has been demonstrated F1 rst ~ j n B desJgn

trad1t1on~JJy caJJld the nrreebrnber engine a 2m211 auxil1ary

167

or ignition chamber equipped w1th a spark plug communicates

with the much larger main combustion chamber located in the

space above the piston (Figure 3-1) The prechamber which

typically contains 5-15 of the total combustion volume

is supplied with a small quantity of fuel-rich ignitable

fuel-air mixture while a large quantity of very lean and

normally unignitable mixture is applied to the main chamber

above the piston Expansion of high temperature flame

products from the prechamber leads to ignition and burning

of the lean maj_n chamber fuel-a_r charge Ignitionmiddot and

combustion in the lean main chamber region are promoted both

by the high temperatures of prechamber gases and bythe

mixing that accompanies the jet-like motion of prechamber

products into the main chamber

I jl

I i j

I

Operation with lean overall mixtures tends to limit peak comshy

bustion temperatures thus minimizing the formation of nitric

oxide Further lean mixture combustion products contain

sufficient oxygen for complete oxidation of HC and CO in the

engine cylinder and exhaust system

It should be reemphasized here that a iraditional problem

with lean mixture engines has been low exhaust temperatures

which tend to quench HC oxidation reactions leading to

excessive emissions

Control of HC emissions to low levels requires a retarded or

slowly developing combustion process The consequent extenshy

sion of heat release j nto 1ate porttt)ns of the engtne cycle

168

tends to raise exhaust gas temperatures thus promoting

complete oxidation of hydrocarbons and carbon monoxide

32 Historical Background and Current Status

321 Early Developm9nt Objectives and Engine Def igns

The prechamber stratified charge engine has existed in various

forms for many years Early work by Ricardo 1 indicated that

the engine could perform very efficiently within a limited

range of carefully controlled operating conditions Both

fuel-injected and carbureted prechambcr engines have been

built A fuel-injected design Lnittally conceived by

Brodersen 11 was the subject of extensive study at the

University of Rochester for nearly a decade 12 13 Unforshy

tunately the University of Rochester work was undertaken prior

to widespread recognition of the automobile emissions problem

and as a consequence emission characteristics of the

Brodersen engine were not determined Another prechamber

engine receiving attention in the early 1960s is that conshy

ceived by R M Heintz 14 bull The objectives of this design

were reduced HC emissions incr0ased fuel economy and more

flexible fuel requirements

Experiments with a prechamber engine design called the torch

ignition enginen were reported n the USSR by Nilov 15

and later by Kerimov and Mekhtier 16 This designation

refers to the torchlike jet of hot comhust1on gases issuing

169

from the precombustion chamber upon j_gnj_ tion In a recent

publication 17 Varshaoski et al have presented emissions

data obtained with a torch ignition engine These data show

significant pollutant reductions relative to conventional

engines however their interpretation in terms of requireshy

ments based on the Federal emissions test procedure is not

clear

l

3 2 2 Current DeveloJ)ments

A carbureted middotthree-valve prechamber engine the Honda CVCC

system has received considerable recent attention as a

potential low emissions power plant 18 This system is

illustrated in Figure 3-2 Hondas current design employs a

conventional engine block and piston assembly Only_ the

cylinder head and fuel inlet system differ from current

automotive practice Each cylinder is equipped with a small

precombustion chamber communicating by means of an orifice

with the main combustion chambe situated above the piston lj

ij_ A small inlet valve is located in each precharnber Larger

inlet and exhaust valves typical of conventlonal automotive

practice are located in the main combustion chamber Proper

proportioning of fuel-air mixture between prechamber and

main chamber is achieved by a combination of throttle conshy

trol and appropriate inlet valve timing A relatively slow

and uniform burning process gjvjng rise to elevated combusshy

tion temperatures late in the expansion stroke and during

the exhaust procezs is achieved H1 gh tewperaturr--s in thin

part of the engine cycle ar-e necessary to promote complete

170

oxidation of HC and CO It si1ould be no~ed that these

elevated exhaust temperatures are necessarily obtained at

the expense of a fuel economy penalty

To reduce HC and CO emissions to required levels it has been

necessary for Honda to employ specially designed inlet and

exhaust systems Supply of extremely rich fuel-air mixtures

to the precombustion chambers requires extensive inlet manifold

heating to provide adequate fuel vaporization This is accomshy

plished with a heat exchange system between inlet and exhaust

streams

To promote maximum oxidation of HC and CO in the lean mixture

CVCC engine exhaust gases it has been necessary to conserve

as much exhaust heat as possible and also to increase exhaust

manifold residence time This has been done by using a relashy

tively large exhaust manifold fitted with an internal heat

shield or liner to minimize heat losses In additj_on the

exhaust ports are equipped with thin metallic liners to

minimize loss of heat from exhaust gases to the cylinder

head casting

Engines similar in concept to the Honda CVCC system are under

development by other companies including Ttyota and Nissan

in Japan and General Motors and Fo~d in the United States

Honda presently markets a CVCC-powered vehicle tn tTapan and

plans US introduction in 1975 Othe~ manufactur~rs

includlnr General Motors and Forgtd 1n thr U S havf~ stated

171

that CVCC-type engines could be manufactured for use in limited

numbers of vehicles by as early as 1977 or 1978

33 Emissions and Fuel Economywith CVCC-Type Engines

331 Recent Emissions Test Results

Results of emissions tests with the Honda engine have been very

promising The emissions levels shown in Table 3-I are typical

and demonstate that the Honda engine can meet statutory 1975-1976

HC and CO stindards and can approach the statutory 1976 NOx

standard 19 Of particular importance durability of this

system appears excellent as evidenced by the high mileage

emissions levels reported in Table 3-I Any deterioration of

l emissions after 50000 miles of engine operation was slight

and apparently insignificant

I Table 3-I

Honda Compound Vortex-Controlled Combustion-Powered Vehicle 1 Emissions

Fuel Economy

Emissions 2 mpg gMile 1972

HC 1975 FTP FTPco NOv

210 50000-Mile Car+ No 2034 Low Mileage Car 3 No 3652 018 212 221089

024 065 198 1976 Standards

213175 20o41 34 - -04o411977 Standards 34 - -

1Honda Civic vehicles 2 1975 CVS C-H procedure with 2000-lb inertia weight3Average of five tests aAverage of four tests

172

Recently the EPA has tested a larger vehicle conve~ted to the

Honda system 20 This vehicle a 1973 Chevrolet Impala with

a 350-CID V-8 engine was equipped with cylinder heads and

induction system built by Honda The vehicle met the present

1976 interim Federal emissions standards though NOx levels

were substantially higher than for the much lighter weight

Honda Civic vehicles

Results of development tests conducted by General Motors are

shown in Table 3-II 21 These tests involved a 5000-pound

Chevrolet Impala with stratified charge engine conversion

HC and CO emissions were below 1977 statutory limits while

NOx emissions ranged from 15 to 2 gmile Average CVS-CH

fuel ec9nomy was 112 miles per gallon

Table 3-II

Emissions and Fuel Economy for Chevrolet Impala Strmiddotatified

Charge Engine Conversion (Ref 21)

Test

Exhaust Emlssions

gMile 1 Fuel

Economy mpgHC co NOx

1 2 3 4 5

Average

020 026 020 029 0 18

023

25 29 31 32 28

29

17 15 19 1 6 19

17

108 117 114 109 111

112

1cvs-CH 5000-lb inertia weight

173

I

332 HC Control Has a Significant Impact on Fuel Economy

In Figure 3-3 fuel economy data for several levels of hydroshy

carbon emissions from QVCC-type stratified charge engines

are plotted 22 23 ~ 24 At the 1 gmile HC level stratified

charge engine fuel economy appears better than the average

fuel economy for 1973-74 production vehicles of equivalent

weight Reduction of HC emissions below the 1-gram level

necessitates lowered compression ratios andor retarded

ignition timing with a consequent loss of efficiencymiddot For

the light-weight (2000-pound) vehicles the O~ gmile IIC

emissions standard can be met with a fuel economy of 25 mpg

a level approximately equal to the average of 1973 producshy

tion vehicles in this weight class 8 For heavier cars the

HC emissions versus fuel economy trade-off appears less

favorable A fuel economy penalty of 10 relative to 1974

production vehicles in the 2750-pound weight class is

required to meet the statutory 04 gmile HC level

333 Effect of NOx Emissions Control on Fuel Economy

Data showing the effect of NOx emissions control appear in

Figure 3-~ 22 These data are based on modifications of a Honda

CVCC-powered Civic vehicle (2000-pound test weight) to meet

increasingly stringent NOx standards ranging from 12 gmile

to as low as 03 gmile For all tests HC and CO emissions

are within the statutory 1977 standards

NOx control as shown in Figure 3-4 has been effected by use

of exhaust gas recirculation 1n comb1nation w1th retarded

174

ignj_tion timing It is clear that control of rmx emissions

to levels below l to 1 5 gmile results in stgnificant fuel

economy penalties The penalty increases uniformly as NOx

emissions are reduced ~nd appears to be 25 or more as the

04 gmile NOx level is approached

It should be emphasized that the data of Fisure 3-4 apply

specifically to a 2000-pound vehicle With increased vehicle

weight NOx emissions control becomes more difficult and the

fuel economy penalty more severe The effect of vehicle

weight on NOx emissions is apparent when comparing the data

of Table 3-I for 2000-pound vehicles with that of Table 3-II

for a 5000-pound vehicle While HC and CO emissio~s for the

two vehicles are roughly comparable there is over a factor

of two difference in average NOx emissions

34 Fuel Requirements

To meet present and future US emissions control standards

compression ratio and maximum ignltion advance are limited

by HC emissions control rather than by the octane quality of

existing gasolines CVCC engines tuned to meet 1975 California

emissions standards appear to be easily satisfied with

presently available 91 RON commercial unleaded gasolines

CVCC engines are lead tolerant and have completed emissions

certification test programs using leaded gasolines However

with the low octane requirement of the CVCC engine as noted

above the economic benefits of lead antlknock compoundt ar-euromiddot

not realized

175

It is possible that fuel volatLLity characteristlcs may be of

importance in relation to vaporization within the high

temperature fuel-rich regions of the prechamber cup inlet

port and prechamber iQlet manifold However experimental

data on this question aomiddot not appear to be available at

present

~O Divided-Chamber Staged Combustion Engines (Large-Volume Prechamber Engines Fuel-Injected Blind Prechamber Engines)

41 General

Dual-chamber engines of a type often called divided-chamber

or large-volume prechamber engines employ a two-stage comshy

bustion process Here initial r~ich mixture combustion and

heat release (first stage of combustion) are followed by rapid

dilution of combustion products with relatively low temperature

air (second stage of combustion) The object of this engine

design is to effect the transitjon from overall rich combustion

products to overall lean products with sufficient speed that

time is not available for formation of significant quantities

of NO During the second low temperature lean stage of

combustion oxidation of HC and CO goes to completion

An experimental divided-chamber engine design that has been

built and tested is represented schematically in Figure ~-1 25 26

A dividing orifice (3) separates the primary combustion

chamber (1) from the secondary combustion chamber (2) which

includes the cylinder volume above the piston top A fuel

injector (4) supplies fuel to the primary chamber only

176

Injection timing is arranged such that fuel continuously

mixes with air entering the primary chamber during the

compression stroke At the end of compression as the

piston nears its top center position the primary chamber

contains an ignitable fuel-air mixture while the secondary

chamber adjacent to the piston top contains only air

Following ignition of the primary chamber mixture by a spark

plug (6) located near the dividing orifice high temperature

rich mixture combustion products expand rapidly into and mix

with the relatively cool air contained in the secondary

chamber The resulting dilution of combustion products with

attendant temperature reduction rapidly suppresses formation

of NO At the same time the presence of excess air in the

secondary chamber tends to promote complete oxidation of HC

and CO

42 Exhaust Emissions and Fuel Economy

Results of limited research conducted both by university and

industrial laboratories indicat~ that NOx reductions of as

much as 80-95 relative to conventional engines are possible

with the divided-chamber staged combustion process Typical

experimentally determined NOx emissions levels are presented

in Figure 4-2 27 Here NOx emissions for two different

divided-chamber configurations 8re compared with typical

emissions levels for conventional uncontrolled automobile

engines The volume ratio 8 appearing as a parameter in

Figure 4-2 represents the fraction of total combustion volume

contained in the primary chamber For a values approaching

I

i J_

177

1

05 or lower NOx emissions reach extremely low levels Howshy

ever maximum power output capability for a given engine size

decreases with decreasing 6 values Optimum primary chamber

volume must ultimately_represent a compromise between low

emissions levels and desired maximum power output

HC and particularly CO emissions from the divided-chamber

engine are substantially lower than eonventional engine

levels However further detailed work with combustion

chamber geometries and fuel injection systems will be necesshy

sary to fully evaluate the potential for reduction of these

emissions

i Recent tests by Ford Motor Company show that the large volume

prechamber engine may be capable of better HC emissions conshy

trol and fuel economy than their PROCO engine This is shown

by the laboratory engine test comparison of Table 4-I 19

Table 4-I

Single-Cylinder Low Emissions middot11 ~ _____En____g__~ne __middot _e_s_-_s_____

Engine

NO--X Reduction

Method

Em1ssions g1 hp-Hr

Fuel Economy

Lb1 hp-HrNOv HC- co

PROCO

Divided Chamber

PROCO

Divided Chamber

EGR

None

EGR

None

10 30

10 04

05 ~o

o J_o 75

130

25

l 1i bull 0

33

0377

0378

0383

0377

178

Fuel injection spray characteristics are critical to control

of HC emissions from this type of engine and Fords success

in this regard is probably due in part to use of the already

highly developed PROCO-gasoline injection system Figure 4-3

is a cutaway view of Fords adaptation of a 400-CID V-8 engine

to the divided-chamber system 2 e

Volkswagen (VW) has recently published results of a program

aimed at development of a large volume precharnber engine 29

In the Volkswagen adaptation the primary chamber which comshy

prises about 30 of the total clearance volume is fueled by a

direct timed injection system and auxiliary fuel for high

power output conditions is supplied to the cylinder region by

a carburetor

Table 4-II presents emissions data for both air-cooled and

water-cooled versions of VW s dtvided-middotchamber engine 3 0

Emissions levels while quite low do not meet the ultimate

1978 statutory US standards

179

Table 4-II

Volkswagen Jarge Volume _Jrechamber Er[ Lne Emissions

Exhaust Emissions

_ _gMile 1

___E_n_gi_n_e__t--H_C___c_o__N_O_x____E_ng__i_n_e_S_p_e_c_i_f_i_c_a_tmiddot_1_middoto_n_s__

20 50 09 841 compression ratio Air-Cooled 16-Liter

prechamber volume 28 of total clearance volume conventional exhaust manishyfold direct prechamber fuel injection

20-Liter 10 40 10 91 compression ratio Water-Cooled prechamber volume 28 of

total clearance volume simple exhaust manifold reactor direct prechamber fuel injection

1cvs c-H

Toyota also has experimented wlth ___a large volume prechamber

engine using direct prechamber fuel injection and has

reported emissions levels comparable to those of Table 4-II 31

43 Problem Areas

A number of major problems inherent in the large volume

prechamber engine remain to be 3olved I~ These problems include the following II

Fuel injection spray characteristics are critically

important to achieving acceptable HC emissions

The feasibility of producing asatisfactory injecshy

tion system hasnot been estab1ished

180

Combustion noise due to high turbulence levels and

hence high rates of heat release and pres[-ure rise

in the prechamber can be excessive It has been

shown that the-noise level can be modified through

careful chamber design and combustion event timing

If the engine is operated with prechamber fuel

injection as the sole fuel source maximum engine

power output is limited This might be overcome

by a~xiliary carburetion of the air inlet for maximum

power demand or possibly by turbocharging Either

approach adds to system complexity

The engine is charmiddotaeter1zed by low exhaust temperatures

typical of most lean mixture engines

References

1 Ricardo H R Recent Research Work on the Internal Combustion Engine 11 SAE Journal Vol 10 p 305-336 (1922)

2 Bishop I N and Simko A Society of Automotive Engineers Paper 680041 (1968)

3 Simko A Choma M A and Repco L L Society of Automotive Engineers Paper 720052 (1972)

4 Mitchell E Cobb JM and Frost R A Society of Automotive Engineers Paper 680042 (1968)

5 Mitchell E Alperstein M and Cobb JM Society of Automotive Engineers Paper 720051 (1972)

6 1975-77 Emission Control Program Status Report submitted to EPA by Ford Motor Company November 26 1973

181

if

7 consultant Report on Emissions Control of Engine Systems National Academy of Sciences Committee on Motor Vehicle Emissions Washington DC September 1974

8 Austin T C and Hellman K H Society of Automotive Engineers Paper 730790 (1973)

9 See Ref 7

10 Alperstein M Schafer G H and Villforth F J Iiil SAE Paper 740563 (1974)

11 US Patent No 2615437 and No 2690741 Method of Operating Internal Combustion Engines Neil O Broderson Rochester New York

12 Conta L~ D and Pandeli American Society of Mechanical Engineers Paper 59-SA-25 (1959)

13 Canta L D and Pandeli American Society of Mechanical Engineers Paper 60-WA-314 (1960)

14 US Patent No 2884913 0 Internal Combustion Engine R Mi Heintz i

15 Nilov N A Automobilnaya Promyshlennost No 8 (1958)

l 16 Kerimov N A and Metehtiev R I Automobilnoya Promyshlennost No 1 p8-11 (1967)

17 Varshaoski I L Konev B F and Klatskin V B Automobilnaya Promyshlennost No 4 (1970)

18 An Evaluation of Three Honda Compound Vortex Controlled Combustion (CVCC) Powered Vehicles Report B-11 issued by Test and Evaluation Branch Environmental Protection Agency December 1972

19 Automotive Spark Ignition Engine Emission Control Systems to Meet Requirements of the 1970 Clean Air Amendments report of the Emissions Control Systems Panel to the Committee on Motor Vehicle Emissions National Academy of Sciences May 1973

20 An Evaluation of a 300-CID Compound Vortex Controlled Combustion (CVCC) Powered Chevrolet Impala Report 74-13 DWP issued by Test and Evaluation Branch Environmental Protection Agency October 1973

21 See Ref 7

22 See Ref 7

23 See Ref 7

24 See Ref 7

182

25 Newhall H K and El-Messiri I A Combustion and Flame 14 p 155-158 (1970)

26 Newhall H K and El-Messiri I A Society of Automotive Engineers Transaction Ford 78 Paper 700491 (1970)

27 El-Messiri I A and Newhall H K Proc Intersociety Energy Conversion Engineering Conference p 63 (1971)

28 See Ref 7

29 Decker G and Brandstetter W MTZ Motortechnische Zeitschrift Vol 34 No 10 p 317-322 (1973)

30 See Ref 7

31 See Ref 7

183

Fig 2-1 FORD PROCO ENGINE

l

Ford Proco Engine Fuel Economy and Emissions _ 15 _ f--1

00 +

I ~ x X gt( X _ x A 7- ~ X x~ ~c - l4catalyst Feed u NOx vs ruel Econ with 1 C0-71 CJ) 14 x x Ynn H( RP c tr ir-t irm vltgtZ G I HC - C0-127 _ A txcessve c

13 Approx W EG R

~ C~~r 351 CID 5000 Lb Inertia Weight

Q 21 A L 0 u w II _j

LJ =gt LL

10

35i CD 4500 Lb Inertia Weight

~ 1974 Production Average Fuel Economy

4 soo _b r-r-r-----z~lt_~~---7--_~--r--1r-7-r1--~-rz7-w~~

150 0 0 Lb PU221ufrac122-1 I

LO 20 30

NOx EMISSIONS-GMSMILE (CVS-CH) Revised216174

0

HKN 71074

Fig 2-2

l

~___-~ ~--=---~ ~=---__---~1 f-=-----1__middot-_~J ~-----------1 ~bull-=-=- (-~-~ LJii-ZJj ~ ~~-~ ~~ -__c~~ 1--~~ ~----~--1 ---------s___-c--1 ~~~-~~~bull r~~-~--middot1 ____c__ J~ p- ~

Texaco TCCS Engine

Shrouded Intake Valve

~ Intakemiddot r~ )p__-- Fuel Nozzle Fuel Nozzte Port ~ -- -yen -_~

X f -J J ( ~1 I --- ~ f middotmiddotj_Ja 1(~-~_ frff 1-Cylinderv~ v_ r--L~ I (~~)J ~- Intake 1 - ------L- middotmiddot - middotmiddot -1 H0 ad middot --- - -- 1 Po rt I 1 I ~~ ) ~ ~ ~~~ -A- I ------

- I _ ---_ ~ P1ston-mgt-lt_ffrac12 T_77~~~--1 i- r_-~J N

- ~- i~-L - _ _ - IExhaust - - I ~ - 1-_ r- bullsect ~ ----lt_ ~ I PortJ~bJ lt 7A--7~ ~1 ~j --~ ~ yl ind er

-__~lli- klmiddot ~ro v_t_gt11J1bull Bti Or K__ - middot ~

I t--tL pgt-- Ultmiddot middot- - Spark Plugr- -1 --U2middot- ~-~

LHorizont al Projections of Nozzle and Spark Plug Centerlines

Fig 2-3 i--1 00 U1

---~---~-~ -------c- --~--- 7middot-r---c-- ~- -~~~==---~~~~~- srsr RZIIEF7 11t111-~-----==-----=-~--~-~~---c=rmiddot=

OPEN CHAMBER TYPE STRATI Fl ED CHARGE ENGINE i-shyCj

DIRECTIONAl~Fsw7 Q

NOZZLE P

I

~J~treg lt-_(__(lt-(11

c_-- _7- -

SPARK PLUG_ l 1__- -_ - l --_ ~ ----__ lt_ lt_ -- --

ltlt_I_--- _

~ gt - _____- -- --~ ~-l_- 1_~ -~- ~ ------

~~~ r_I FUEL SPRAY 2 FUEL-AIR MIXING ZONE ~- _ -------

FLAME FRONT AREA 4 COMBUSTION PRODUCTS

TCCS COMBUSTION SYSTEM

Fig 2-4

3

----==-----~ l~~----bulli r-~ ~-----=-- 1 ~~ ~ -~ ~~ ___-_=gt---l p--- --=-=-_-__71-~-~~ 1-0-- --=---=-- 4 L--_-_-~ P--- ~

25

-c u

f

Cl) 24 gt u _

tgt 23a ~

I

gt-~ 220 2 0 u w 21 _J

lJJ gt LL

2

Texaco TCCS Powered Cricket Vehicle

Max Econ Setting gt A L07 HC

141 CID JQf CR 084 CO 2500 Lb Inertia Wgt

50-so Retard_ 0_73 HC

12 co 051 HC ~ 061 HC

085COA 064CO Retard+ ESPRetard+

EGR

036 HC ~ 115 co Retard +ESP+ EGR

04 06 08 10 12 14 16 18 20 NOx EMISSIONS-GMSMILE (CVS-CH) HtltN1110114

I- 00 -JFig 2-5

-~ ~=- ~ - -i______c_J ~-====c= wr=- ~-~ p--w~~~ rr w -

25

-c u

I

(f)

gt u-lt a_

2

gt-I 20

~ 0 z 0 u LLI

_J

w tJ_

15

I- CJ) CJ)

Turbocharged Texaco TCCS Ml51 Vehicle

Max Econ Adjustment_ HC-3J catalyst Feed C0-70

141 CID 10~1 CR 2750 Inertia Weight 8deg Retard ~

~bull HC-3middot2 catalyst Feed ~~ _ C0-64

_ 5deg Retard HC-0 30 8degRetard LowEGV bullco-11 ~bull HC-3middot6 catalyst Feed WIW21

Med EGR C0-67 1974 Production 33 Average Fuel Economy ~

COmiddoti05 (2750Lb)

I

bull HC-035 co- 141 13deg Retard High EGR

04 10 20 NOx EMISSIONS -GMSMILE (CVS-CH) ~~ts~b~~~74

Fig 2-6

189

Fig 3-1

PRECHAMBER TYPE STRATIFIED CHARGE ENGINE

r Inlet

(Fuel-lean Mixture )

I 0 I

Spark -Prechamber (Fuel-rich mixture)

-Main Chamber

1] HON DA CVCC ENGINE CONCEPT

190

Fig 3-2 Honda CVCC Engine

28 -l u

1

UJ 26 -gt u-(9 CL 24 2-

f

gtshy0gt

22 z ~ _)

u w

20 _J

w ~ LL

18

J= ---- 4 --~~-_----a ~~ _-_bull --~~ 1~~1 ltiil~I ~ ~-r~ ~ -~ ~-~ ~J~-iii-1 ~~1 s _-_ __-

Fuel Economy vs HC Emissions for 3-Valve Prechamber Engines

e NOx-14 15 Liter

bull Honda CVCC 2000 LbsNOx - 12 A Datsun NVCCbull15 Liter

bull ~JOx -09 A 2500 Lbs J LL 1ter NOv -15

2750 Lbs -NOx -17

- I AiJOx -12

0 02 04 06 08 LO 0HYDROCARBON EMiSSlmiddotONS - Glv1 I MILE (CVS-CH) I-

Fig 3-3

J--1

1--Fuel Economy vs NOx Emissions IO N

-- for Honda CVCC Powered Vehiclesr 26 u

l VHc-023 U1 gt umiddot 24_-__

(_IJ o_

~ 22 l

gt-5~-0 z 20 C0-200 u A HC-033w I co -3o_j

_A HC-029w 18 J I C0-27 LL

_ HC-025

HC-017 co -2-3

C0-22

0 -- 02 04 06middot 08 10 12 NOx Ef11SSIONS -GlviS MILE (CVS-CH)

Fig 3-4 middot

I

I

i93

J J

Fig 4-1 Divided Chamber Engine

middot(4) Fuel Injector

1

f J

f ff

f

~ Ii

I f

i

I f ] [

~~

0 0 0 0

i ~ I

1jl

194

E Cl 0

C QJ

CJl 0 _

-1-

z

0

Vl (lJ

-0

X 0

-t-J

V1 ro c X

LLI

Fig ~-2

COMPARISON OF CONVENTIONAL AND DIVIDED COMBUSTION CHAMBER NOx EMISSIONS

5000 MBT Ignition Timing Wide Open Ttl rattle

4000 Conventional Charnber

3000

J = fraction of Total Combustion 2000 Volume in Primary Ct1arnber

Divided Chamber 13 = 0 85

1000

Divided Chamber fo = 0 52

05 06 0 7 08 09 10 11

O~erall Fuel-Air Equivalence Ratio

195

196

AIRBORNE SURVEYS IN URBAN AIR BASINS IMPLICATIONS FOR MODEL DEVELOPMENT

by

Donald L Blumenthal Manager of Program Development

Meteorology Research Inc Altadena California 91001

middotI would like to make several points today First ozonemiddotis basically

a regional long-range problem There is a lot of long range ozone transshy

port and this transport is a normal occurrence The second point is that

ozone is stable in the absence of scavengers Junge mentions in his book

that the residence time of ozone in the troposphere is on the order of a

month Third vertical variations in concentration and ventilation rate are i very important in modeling atmospheres such as Los Angeles Layers aloft

are ventilated down to the surface on occasion and surface pollutants are

ventilated up mountain slopes as Jim Edinger has pointed out before and

often ventilated out of the basin in upper winds Fourth the day to day

carry over of pollutants from one day to the next is a very important considshy

eration in the Los Angeles Basin Finally there is a definite background

level of ozone The geophysical literature says its about O 02 to O 03 ppm (

in various parts of the world Weve seen data varying from 003 to 005 ppm

The difference may be due to calibration differences In any case numbers

like 005 are pretty substantial background levels for ozone

I am going to illustrate the points listed above with some data from

Los Angeles Basin The data were collected during a two-year study funded

by the Air Resources Board some of the analyses were funded by EPA The

study examined the three dimensional distribution of pollutants in the Los

Angeles Basin using airborne sampling systems Coinvestigators on the

project were Dr Ted Smith and Warren White of Meteorology Research Inc (MRI)

197

The first slide shows one of the aircraft we used Its a Cessna 205

which had sampling inlets on the side of the aircraft Figure 2 shows the

instrument system on the inside of the aircraft We were measuring nitrogen

oxides ozone scattering coefficient with a nephelometer condensation nuclei

carbon monoxide and meteorological parameters such as temperature humidity

turbulance Altitude and position were also measured

Figure 4 shows that the typical sampling pattern was a series of spirals

from the top of the mixing layer over an airport virtually to ground level

then we would climb up to the next point on the route and spiral down again

We had three routes (A B C Figure 3) that we would fly We had two airshy

craft and we would fly two of these three routes three times a day any

given day that we could The day I will be talking about September 25~ 1973

we flew what was called the Riverside route (C) and the Los Angeles route

(A) The 25th of July 1973 you might remember was the day before the

federal office buildings were closed in the area here because of smog

Figure 5 shows the surface streamlines at 0300 Pacific Standard Time

about 4 oclock in the morning daylight time on July 25 This streamline

analysis points out the morning stagnation conditions which are a very normal

occurrence in the Los Angeles Basin You start out with very light winds

quite variable maybe a slight off shore flow early in the morning On this

particular day this kind of situation extended well into midday The sea

breeze did not really pick up until up around noon When you have this kind

of a situation and a low radiation inversion at night you have a

long period of accumulation of pollutants all over the Basin espt~cialJy

in the prime source area the southwest portion of the Basin

198

I

Figure 6 shows the streamline pattern at 1600--400 cclock in the

afternoon same day sea breezes develop and with them a transport pattern

that carries pollutants up to the northeast and out toward the eastern por-

tion of the Basin This is a very regular pattern which we see day after l middot

day On July 25 1973 it was a little bit exaggerated The sea breeze was

held off for awhile started a bit late and so there was a very long period

of accumulation in the southwest area and then transport across the Basin

Figure 7 is an average streamline pattern at 1600 PacHic Daylight Time

on low inversion days for August 1970 It is included to show that the pattern

shown before is very typical Flow starts in the western portion of the

Basin and goes right across to the eastern portion This is using surface

data There is a very high average wind velocity in Ontario about 13 m iles

per hour and 23 mph in Riverside This is the average for the whole month

of August at 1600 PDT on low inversion days There is a considerable amount

of transport across the Basin starting relatively slowly in the morning and

accelerating in the afternoon

Figure 8 shows a verticle cross section of the scattering coefficient

The darker areas indicate higher levels of particulates Scattering coefficshy

ient is inversely proportional to visibility In the crosshatched area

visibility is less than about 3 miles In plotting altitude versus distance

inland from the coast you have Santa Monica (SMO) on the coast El Monte (EMT)

Pomona (BRA) Rialto (RIA) Redlands (RED) The lower broken line is surface

ground level The heavy dashed line is the base of the subsidence inversion

that occurred on the two days during this episode The middle line is the

base of the marine inversion There is a large area over in the western

portion of the Basin where emissions accumulate for much of the day At

199

midday the sea breeze has just started ventilating the Santa Monica area

The layer between the inversions is a layer aloft which is fairly well separshy

ated from the surface layer Ozone concentrations for instance in the

layer aloft were on the order of 04 05 ppm using the ARB calibration

method Down in the surface layer they were quite a bit lower in the mornshy

ing due to scavenging

Figure 9 shows that by afternoon the sea breeze starts and you get

kind of a clean air front Sea breeze starts ventilating the whole Basin

the stuff that was over in the west is transported eastward and at approxishy

mately Brackett (BRA) at 1700 PDT there is a clean air front The high conshy

centrations that were over Los Angeles earlier are now centered near Upland

(CAB) The numbers shown over CAB are data taken from a vertical profile

spiral over Upland at about 1600 That turns out to be the time when there

was the worst ozone concentration of the day in the Basin and it did occur

at Upland It could well be a result of the very polluted mass from the

western Basin being transported over the Upland area The layer aloft has

been a bit undercut by the sea breeze and some of the polluted mass has been

around possibly as long as the night before There has been very little

transport in the area aloft ozone concentrations are still very high

Figure 10 shows a trajectory analysis of the air arriving at Upland at

1600 since that was the worst time of the day at Upland We developed a

trajectory envelope using surface wind data and winds aloft so the air

arriving at Upland at 1600 started out somewhere back within this envelope

for example at 1130 PDT We did not go earlier than 1130 because the winds

were pretty much light and variable before that The air that arrives at

Upland at 1600 has been over the western portion of the Basin for much of

200

the morning and q~ite a bit of the evening before Thus there is

a very long period of accumulation and then a transport a pulsing effect

where you have pollutants moved across the Basin

Figure 11 is an isopleth map of surface ozone concentrations Again all

data are corrected to agree with the ARB calibration method Again you can

see that for the hours between 1600 and 1700 using surface data the Upland

area has the highest surface ozone concentrations about 063 ppm The western

area has been well ventilated by the sea breezes and it is cleaned out

The transport is actually pretty much perpendicular to the isopleth line

just about like that

Figure 12 is a vertical profile taken over Upland Cable Airportat

roughly the time of maximum ozone concentration 1636 PDT We are plotting

pollutant concentration on the x-axis versus altitude in meters (since it was

done for an EPA report) Surface leveJ at Upland is a little over 400 meters

the Z line is ozone Ozone concentration within the surface mixing layer

is pegged on the instrument at somewhat above 05 ppm Above the surface

mixing layer it drops off considerably and eventually get down to background

The T line is temperature and you ean see the subsidence inversion

on this day is very nicely documented here and provides a very strong trap

in that area The B line is the scattering coefficient inversely proporshy

tional to visibility Within the surface mixing layer visibility is on the

order of 3 miles or less while up above the surface mixing layer just a few

hundred feet difference visibilities get up to 60 or 80 miles The X is

condensation nuclei the measure of the very fine particles below about 010

micron It is a measure of quite fresh emissions If you have a high condenshy

sation nuclei count there are very fresh combustion emissions If you have

I

201

an aged air mass the condensation nuclei coagulate and the count decreases

considerably You can see that there are still some fresh emissions within

this surface layer as well But up above the surface mixing layer all the

pollutant indicators decrease considerably

Figure 13 is the same type of vertical profile taken over El Monte

which is on the western side of the sea breeze front The sea breeze front

has passed El Monte at this time almost 1700 PDT and again there are

distinct differences between the mass below the mixing layer within the sea

breeze front (below 400 meters) the marine inversion (400 to 800 meters) and

the subsidence inversion The subsidence inversion occurs at about 800 meters

and there is an old layer of very polluted stuff aloft The surface concenshy

trations are lower because of the ventilation by the sea breeze Condensashy

tion nuclei count (X line) within the surface layer is quite high There

are still fresh emissions in the El Monte area The 11 Z line is ozone

about 02 ppm within the surface layer (200 m) but it is 05 ppm up above

the surface mixing layer The scattering coefficient (B line) is very

similar it is lower at the surface and increases to a visibility equivalent

of less than 3 miles above the surface mixing layer The condensation nuclei

count is high in the lower portion of this (eg at 600 m) hut decreases conshy

siderably above This portion of the upper layer (600 m) has been around

at least all morning and condensation nuclei have been scattered from the

area The portion of the upper layer below 600 m has probably just recently

been undercut by the sea breeze and there are still some condensation nuclei

left in it

Figure 14 illustrates a different method of looking at the flushing

problems in the Basin We have tried to develop an objective criteria based

on ground level ozone to show the cleansing of the basin using the time of

202

arrival of clean air We determine the time when the ozone concentrations

drop by a factor of two at any given point The 1600 line means that between

1500 and 1700 the ozone concentration at that point dropped a factor of two

This sort of isopleth chart of when the clean air arrives agrees quite well

with the trajectory analyses although the numbers are a little bit behind

the trajectory analyses for the polluted air Figure 14 again shows the

transport process that takes place across the Basin which is ventilated from

west to east At 1900 some of the fresh ocean air finally gets out to

Redlands

In Figure 15 in order to put this whole flux problem into some perspecshy

tive we looked at the numbers the actual amount of ozone flux across the

basin We calculated the mean trajectory from Torrance towards Redlands

using the surface and upper air data We looked at the flux from the western

basin to the eastern basin basically from Los Angeles and Orange Counties to

Riverside and San Bernardino Counties This is a calculation made at 1700 PDT

We used the winds aloft from Chino as well as the vertical profiles taken at

Pomona and Corona Averaging the ozone concentration throughout the mixing

layer and multiplying by an average wind speed we arrive at a number of 185

metric tons per hour being transported directly from one side of the Basin

to the other If you look at this in terms of actual concentration in the

eastern Basin and assume that the flow was constant for about an hour it

is eno_ugh to fill up the box shown in Figure 15 to 025 ppm ozone which

exceeds the air quality standard by a factor of three (using the ARB calibrashy

tion method) Thus there is a very significant transport of ozone or ozone

precursors from one portion of the Basin to the other side of the Basin One

thing to mention though is that the concentration would not be kept up on a

203

steady state basis because the transport is a result of the pulsing effect

I Illentioned earlier There is a lot of accumulati6n in the western Basin

and these accumulated pollutants are then transported across the Basin This

kind of transport did take place in a couple hours because we also have

measurements from 1500 PDT which give us similar flux numbers

Figure 16 is a trajectory envelope similar to Figure 10 calculated for

Upland at 1600 for the air arriving at Redlands about 600 oclock in the

afternoon I wanted to include this trajectory envelope to show that the

problem is not really simple You cannot say that the air at Redlands came

from Long Beach per se The air at Redlands if you look at the whole

envelope of possible trajectories using upper air data as well as surface

data could have come from anywhere between Downtown Los Angeles and over

the Pacific Ocean south of Long Beach

Another thing to recognize is that the wind actually changes direction

slightly as you go up and down through the mixing layer and the mixing layer

is exactly what it implies There is mixing within the mixing layer so if

you begin with a parcel of air near the surface this parcel may move to the

top of the mixing layer and go one direction for awhile it then may go back

down to the bottom of the mixing layer and move in another direction for

awhile The ratio of the length scales indicata3mixing layer depths of 1500

or 2000 ft and distances on the order of 70 miles This makes it very

difficult for tetroons to follow an air trajectory because they do not go

up and down They stay at one altitude and in one wind regime and yet the

wind regimes are different at different altitudes and the air is continually

mixed up and down through this layer You can often see this on time lapse

photographs

204

The question is where does the pollutant mass go after Redlands Figure

17 is a repeat of Jim Pitts slide from yesterday and it is data for the

same day that we did our analysis It shows the ozone peaks starting at

Pomona and Riverside and on July 25 1973 eventually getting out to Palm

Springs so there is quite a bit of long-range transport The ozone is

stable at 8 00 or 9 00 oclock at night There still are ozone concenshy

trations of 02 ppm it hasnt dissipated even at the surface Ozone does

dilute as the mass moves Other calculations we did were integrations

through the mixing layer of various pollutants such as ozone and CO along

with trajectories that we measured Th~se integrations show just what the

ground data show in Figure 17 The concentrations increase through the western

portion of the Basin and then show a decrease through the eastern portion

of the Basin CO tends to decrease faster than the ozone indicating a

continued production of ozone further east

Figure 18 is a streamline chart on a larger area map for the 16th of

August 1973 It shows the typical streamline patterns that occur for

ventilation from the Basin By mid-afternoon there is flow out through the

major passes to the north and towards Palm Springs (PSP) On this particushy

lar day we had data from Arrowhead showing that the air mass from the Basin

does indeed get up there

Figure 19 shows a vertical profile over Arrowhead early in the morning

16 August 1973 at a time when there was a north wind Ozone level was

about 005 ppm the scattering coefficient was quite low on the order of

probably 60 miles visibility or so Figure 20 is a vertical profile again

over Arrowhead late that afternoon when the winds had switched There is a

flow from the Los Angeles Basin into the Arrowhead area thus one sees a

205

vertical profile that shows a distinct increase near the surface in both the

ozone and the scattering coefficient and in the condensation nuclei Ahove

that you have fairly clean air The top of the polluted level is just about

the top of the mixing level over the Basin

I want to leave the transport now and discuss the complicated vertical

structure that can occur If you want to try to model something try this

one for instance Figure 21 is a vertical profile over Brackett Airport

Pomona about 830 in the morning on 26 July 1973 which is the day after

the episode shown earlier A bit of interpretation shows how complicated

th is can be If one looks at the temperature profile it would be very

difficult to pick out a mixing layer theres a little inversion here another

inversion there several more up here After looking at hundreds of these

profiles though you can start interpreting them What is happening is that

there is a surface mixing layer at about 500 m In this layer there is a

high condensation nuclei (X line) count due to morning traffic The San

Bernardino freeway is quite close to Brackett there is a relatively high

nitrogen oxide count about 02 ppm and the b-scat is fairly high Ozone (Z)

within the surface layer however at this time is quite low The layer beshy

tween 500 m and 700 rn turns out to be the Fontana complex plume Note the

very high b-scat level it is below 3 miles visibility the plume is very

visible especially at this time of the morning when it is fairly stab]e

There is a high nitrogen oxide level (800 m) a high condensation nuclei

level and again a deficit of ozone Above this layer (800 m) you have stuff

that has been left all night very low condensation nuclei indicating a very

aged air mass ozone concentrations about 016 ppm b-scat of about 04 It

has been around all night and not yet had a chance to mix down within the

206

surface layer In fact one good way of determining the surface mixing layer

early in the morning and at night is to look for the ozone deficit Another

thing to mention is that wind reversals occurred for each of these three

layers The winds were fairly light and westerly at the surface slightly

easterly in the 500 m 700 m layer and westerly above 800 m There is a

complicated situation early in the morning but the main problem is that by

the middle of the day there is good surface heating and the pollutants have

all been entrained and mixed down to the ground so in order to modeI what

happens on the second or third day of an episode you must be able to look

at both old pollutants as well as fresh emissions And you need to account

r for ozone that is actually transported down to the surface from layers aloft l

The next slide is a photograph (not included) which is another e xample

of some layers aloft This is due to upslope flow as explained by Jim Edinger

in his publications The mountains are heated during the day in turn heating

the air and making it buoyant there is upslope flow to a point where the

heating cannot overcome the subsidence inversion and the stuff comes right

out from the mountains and spreads out over the Basin The pollutants can

stay up there if the winds aloft are very light and on the subsequent day

will he re-entrained to the surface On the other hand if there are winds

aloft different from those in the surface mixing layer or the wind velocity

aloft is high there can be a very substantial ventilation process for the

Basin Pollutants can be ventilated up the slope and blown away in the upper

winds In the case of the entire July 25th episode winds aloft were quite

light and these upper layers remained

Figure 22 is a vertical profile of one of those upslope flow conditions

in the same location shown in the photograph but on a different day Again

207

there is a relatively high surface concentration of about 03 ppm of ozone

(Z line) a layer of clean air between 900 to 1100 m and then high concenshy

trations of ozone again above 1100 m It has gone up the slopes of the

mountains and then come back out Concentrations in the 1100 to 1300 m area

are just slightly lower than they were at 600 to 800 m area Notice however

that the condensation nuclei count (X line) is quite a bit lower mainly

because the stuff is much more aged above the 1000 m level than it is down

below 900 m

Figure 23 shows the stability of ozone the fact that it can stay around

all night long This is a vertical profile taken over Riverside about 2200

PDT 1000 oclock at night Above the surface mixing layer (600 m) there

are ozone concentrations of about 0 15 ppm (Z line) Within the surface

mixing layer (below 500 m) ozone is completely scavenged decreasing to

zero The nitrogen oxides within this surface layer are being contained and

are around 01 ppm from fresh emissions that occurred during the evening

Condensation nuclei near the surface are very high The temperature profile

is very stable You have a surface based radiation inversion which is a

little strange looking for a radiation inversion~ nevertheless it is quite

stable There is a definite restriction of the mixing--a very difficult

time getting air from below 500 m to above 500 m The ozone that exists in

the 700 m range is in air where the reactions have virtually gone to compleshy

tion and is very stable All the profiles on this night changed very little

the ozone peak stays there High concentrations stay around

Figure 24 is a cross section across theurban plume of the City of St

Louis I wanted to show that this occurrence is not limited to Los Angeles

We have seen ozone formation and transport in other urban plumes These data

l

208

were taken during a project sponsored by EPA in conjunction with R Husar of

Washington University and William Wilson of EPA The dark line on this is

the ozone concentration across the urban plume perpendicular to plume The

dashed line is the scattering coefficient The power plant plume is parallel

to the urban plume The data on the left were taken 35 kilometers down wind

about 1100 oclock in the morning The ozone concentration increases slightly

to 005 ppm in the urban plume there is a deficit of o in the power plant plume3

In the same urban plume same conditions 1500 CDT two hours later further

downwind there has been substantial increase in the ozone in the urban plume

itself The b-scat is very similar to what it was before but the ozone is

now increased quite substantially except in the power plant plume where

there is a strong deficit of ozone due to scavenging by nitrogen oxides So

the formation and transport of ozone and ozone precursors in urban plumes is

a regular occurrence that happens in more places than Los Angeles and as Bob

Neligan showed this morning it can happen over quite a bit longer distances

than we are showing here

To summarize the conclusions as they affect model development first

once ozone is formed in the absence of scavengers ozone is a very stable

compound It remains for long periods of time It can he transported for

very long distances Ozone is a regional problem which cannot be controlled

on a local basis To have effective ozone control middotone must have a regional

control strategy and probably regional type air pollution districts

A second conclusion is that the vertical distribution of pollutants can

be highly complex and models have to include more than just a simple wellshy

mixed surface layer

209

A third conclusion is that layers aloft can persist over night and can

be re-entrained within the surface mixing layer on subsequent days models

should be able to account for old pollution as well as fresh emissions Also

pollutant accumulation and transport can have distinct diurnal patterns that

are strongly dependent on the meteorology Models should be time dependent

and should start at the beginning of the accumulation period In other words

models ought to be able to run for 24 or 48 hours if they have to In this

case in Los Angeles there is often an accumulation of pollutants which starts

in one portion of the Basin at midnight and continues through the next mornshy

ing even before it starts to be transported

As far as recommendations go in many areas a lot of ambient data has

been collected and in some cases the data are actually ahead of some of the

models so I think a research program is needed in developing models that

will account for this vertical structure and the day to day carry over and

the models need to be extended to cover longer distances In addition more

smog chamber work is going to be needed in looking at the effects of carry

over and mixing old pollutants with fresh emissions How people go about

this I leave to the modelers and the smog chamber people They know more

about that than I do

I

210

I

~ INVERTER

AUDIO TAPE

MONIT0R

MONITOR OBSERVER SEAT

MON ITOR

NEPHELOMETFR FLfCTRONICS

j DIGITAL DATA LOGGER

CONDENSATION

VOR DME NEPHELOMETER TUBE

JUNCTION middoteox ASSORTED POWER

AIRBORNE

TEMPERATURE TURBULENCE

middot HUMIDITY

ALTITUDE BOX

__

middotE=-middot RECORDER ----r----------

NUCLEI KJNITOR

CONVERTER

SUPPLIES

INSTRUMENT PACKAGE (

lCO

03

Ndeg

-

-----NEPHELOMETER

BLOWER

Figure 2 Instrumentation Layout for Cessna 205

211

bullubullbullbullbull

Figure 3 Airborne Sampling Routes in the Los Angeles Basin

Figure 4 Vertie al Profile Flight Path

~-~ r~i ~~1 -- ~ ~ ~2-1~ LJ-----~ r~~ ~~ t~~--l

~ ALM l

0 RIA

ec 8v

M

~ Afo

-o

M 0

~IV

ltgt

IN J--1 N

SCALE II fi M I j_ ES 0 3 4 5 =-JSEJ--J~ _middot ~middot- - =- =

I

~

M

N~J

Figure 5 SURFACE STREAMLINE ANALYSIS - 0300 PST 25 July 1973

~~~ ~~-- cp1FJ=D -~~

~ 1

~ ~ 8c

8v

~25

PACIFIC OCEAN

diams Tt

0

9 I 4 5 10 I- m p H - -middotmiddot u 4H__8 middott_

D i6 J4 k W~D SPED llaquotl SNA NJ ~1

SCALE m ICtt84bullmh R v1s1a1L1n (mil 6 ~ CONTOURS REPRESENT

-- 10ml 16km (~() bull ~ ) ~ - 000 ft 3C5

Figure 6 S_cJRFACE WIND STREAMLINES - l 600 PDT JULY 2 S I 8 7 3

l - ~---i ~-=-___-----c---it~~-~~ r----=------1 ~-~~--cpc---_t__A --~ ---llil

~_ - ~-l-cL

34bull vi~-dff

bullbullbullbull bull ~ bull -1 bullbull - -_- L bull-J bull ~bull-bull-ii------~ bullmiddot r_ -~- ~ bullI ~_ bull bull bullbull bull I bull _ - bull -~-~ middotbullbullbull ~ ~ --middot -~- bullbullmiddot ~v ) ~ - -__rl v middotmiddot - 1- ~ -- middot middotmiddot - 1 91 frac12 - ~- lt( middot K i - middot bull - middot - bullmiddot~~-~lJ) obullmiddot~ ~-f- _J_~---Smiddot~middot-~----~~~---gt_middotfY-_middot-~middot --middot-~-~----fJ_middot- middotmiddotbullmiddot u-- bullmiddot ~ ~ -middot L~ bullbull

~bullbullbullbull bullbull l_bull bull bullbullbull EW bullbullbullbull-- ~ __bull f f - middotbull - J middot f bull S bull I ~ -r --

_ bullbull bull- _ bullbull-bull ~ ~ bull bull bull bull I bull bull bull bull bull bull gt - bull middotbulliJ -bull I bull bull _1 bullJ C-- ~-middot _ bull bullbull bullbull bull _____ ~ ~ l _ middot q bull 1 -middot middot ~~middot middot middotbull_ J ~gt - J bull-bullbullbullbull ) _ -middotmiddotbullmiddot J ~middotmiddotmiddot -bullmiddotbull fmiddot 7middot _middotmiddotmiddot bullmiddot(middot Ii~ middotmiddot~_--~middot 1middot__middotmiddotmiddotmiddot middot- gt_ -~ -~-- Imiddotbullmiddotbullbull_ -

- ()_I (w--_ bullbull__(i- bullOmiddotbull bull middotbull -bull-_jlJ middot bull lt 1(middot t gt bull - ~ rbull I bull middot middot- bull41-bull l~r v-middot~- middot middot middot bull_ - middotmiddot ~Jtj (middot~ ~middoti middot middot middot middot middot ~- ~ -tmiddot~ I - middot middot_- ~ - -~ middot_ _- ~bull - _ ~) i bull bullbull bull- middot_ bull middotbull __ ( bull 11bull bull ~ampmiddot ~ l bull bullQ bull - -1 bull JY1 bullbull ~ or bullbullbullbullbull bullbull-bullbull _ ~ - bull bull-bullbullbull middotimiddot middot 91 bull t bull - - tfaw lJ--r- bull bull _ bull middot- - l

f ~~middot--~ middotmiddott ~ltrgtmiddotmiddotJmiddot_bull - ~ - __ middot- LOS ANGELES BASIN - LOW LEVEL -__ jmiddot l-gt bull - bull J iI bullbull bull bull bull _ bullbull _ Jmiddot middotL~_1 middot middot bullbullmiddot ( C middot INVERSION MEAN WIND FLOW _ J

lmiddot - f bullbullbull~ - f 1bullbullbull _ ~)- bull middot- _---_- 7f-~bull~ REGIME _F_~ AUG_UST_~ ~600 P~--- l

-__L-~bull --ncmiddotbull~~-j--bullmiddot~bullmiddot_-bull _fJibullmiddot Imiddotmiddotmiddot-bullmiddot- bullbull ~ bullbullbullbullmiddotmiddotmiddot~middotbull ___ bullJ_ _middot~0))deg bullt t1yensmiddotmiddot ( middot middotmiddot middot middot ~ middot lbullbull1 t_c0 bull -middot---l lt ~middot~- deg bullbull --= bull bull bull I bull bull bull bull bull bull bull bull bullbull _~bull b ---) bullbull-bull ) bulll middotbull middot1middot ) bullT --f bull I bullr ~bullbullbull bullbullbull( - -bull-- ( -o-----_i bull-~-l- i l l J l~-- c middotmiddot _--1 ---I middotmiddot ---- ~bull-bull bulli_ ALT Elmiddot_ bullbullbullbull _- ~~middot bull middot bullbull _ bull middotbull bull~ ~bull middot bull -middot bull--ua_-- bullbull bull

-- 01--- middot_ -middotmiddot hmiddotmiddot __1 ~-- ~ fi~~- ___ - ____ _ -middotmiddotmiddotmiddot~ ) -~-J bull bullbull bull bull 0 uc- -l ~- ~ IT ~~ll ~ bull -middot -middotmiddotmiddotmiddotbullCCAmiddotmiddotmiddot-middot middot bullbullbullbullbull

) i- 5 ~-==-- __ __ - bullbullbull _ bull~ bullbull _ bull bull l T[h4 ------ - 0

i17- o~-lt -(i-_~ 11t~bull-omiddot ~- -- 13 0l~~~bull bull Jbullbull~bull ~ ~bullbullbull bull bull x- middot~---=-~~ -=aJlll8 bull Ibull bull ~~ middotbull rbull~---bull1-~middot-middot _ middotmiddotmiddot-middot 1 0 ~vrbullmiddot ~middot ~ (J~-middot _-_~) ) ~ bull middot

l middot _ POMA_ middot =~~~----ti~ jmiddotmiddotmiddot - middot bull [j

~A ii J0 Vfli middot bullHud __=bt_ bull

CImiddot ~-- ~- middot)middot PACIFIC OCEAN I middot ---- middotmiddot ~

__ middot__ ~ - _ 23~1 middotbull 8 4 1 middot middot ~ middot middot gt ~~- l ~ u middot

bull - bull- I ~------ --1~ i middotmiddotmiddot - n _c-118 1130

~ n r -t ~~gt25) cmiddotbullmiddot

~--lt- ~~- 1-~__( i - t ~ _ middot 0 igt(_J

11bull bull11 ~~ -~[ ~i~gt----gtmiddotmiddotmiddotmiddot--~l_ ~~ ELEVATION

IN FEET bullbull (_- middot bullbullbull -middot middotbull middot ~~ middotmiddot bulltbullbull _ffmiddotmiddot-middot v I )tylt~ -~bullbull1bullbullrbullbull ~-lt -~ ( I~

600~ A0 Cv(A (1829 m AND OVER) deg )_ rJ__~7 middot middot ~--middot L==1 _J bullbullbull - bull -middot~-- rgt ~ middot(Zmiddot- middotbullmiddot middot

Z~C)-tGOO (762 middot 1829 m) 9-N4 __J (r -- lf _ bull bullgt-~~~ ~ _ w _ _ I (1 bullmiddot( middot1 middot -----~~~- middot L-bullmiddotbullW bullbullbull3 STA r I0-4 lODEL

100i -2soo (305~762m) -- Ow - -~1_- i ~~--- bull v~rvt ~~ -middot )) ~--

II gt J (-_bullmiddot middot~ l bull bull tr 1 )~ gt ) bullbull-_bullI-middot -middot bull~0 3 Mor nuq1ENr Wlbull~O JIAtCTIO-bull bull - lbull C---gt bullbull )t bullbull -( I bullf I - 20-00 (61 bull 305 ml J( Jloa xxE- -bullbull00 - -- middot1

0-200 (0middot61m) Wl)7 AVBt~gpound ) bullmiddot-iiNL~ middotntmiddot_ 1 iJJlt( _1J- ~ VAq IA9 IL ITY 0 ~ 10 15 ltS lHPtl

~--_ bull bull I bullbullbullbull 1 ~) J)J ~ bull Is bullmiddot bullbullbullbullbull ~ 3 V IS A VAqlABLE OIR~CTIO- 0 8 16 2-4 km

(SPEEDS SHOWN IN mph 10 mphbull 16 h1llr) -- middot ktr~~~ lt~ ) -middot-SCALE

Figure 7 LOS ANGELES BASIN MEAN WIND FLOW FOR DAYS WITH LOW LEVEL INVERSIONS DURING AUGUST I 970 AT 1600 PDT

-~~~~-=======~middot~-~======~middot--=-==-===gt=---==____________=== ~--=-J~==-- -=-ee----=-------

500

N f-- V

- - - SUBSIDENCE INVERSION

----MARINE INVERSION

bullbull-bull-bullbullGROUND LEVEL

x WINOS ALOFT (kmht)

WESTERN middoteASIN EASTERN BASIN

LAX WINOS EMT IHOS I I

CNO WIHOS

s_ 04 13 1500- 05 02 08

I 06 069 middot

11-1--

04 04 i ~4

06 ~ 4--

I 2

1000 n1 1005 -_E

lll --1 lJ -----------~----

~11

--=i-+- c -- 9 _____ - ~ C

lt I

I 6 4 _r 31

I 6 5 ~~ ~_ bull ---middot- 64 ~li- - middot- bullc - middot-----------

10

SMO (1347 PDT)

EMT (1246 PDT)

BRA CAB (1459 PDT) (1335 PDT

RIA (1349 PDT)

RED (1406PDT)

Figure 8 VERTICAL CROSS-SECTION OF bscat FOR lvflDDAY

T t 10-4 -1)(l n1 s are m

JULY 25 1973

- c - -~

~--~ JC_-_1- ~1pi~ oamp----~JilliiiM~f~-U~ -~--- --~~~ ~~~

-=--~

-E-- O

_ lt

1500 05

06 15

09 __~

1000 --

~- ~---middotmiddot 29

500

oJ11

__a

07

I 07 I

I I

I

09

I

I

I

I 7 ---

11 -----

~ ----- 6

---------------lt- -~middot4 --------

20

29

-

10 10

11 07 08 08

10

08

~8 _____ Y-

N

- - bull SUBSIDENCE INVERSION

----MARINE INVERSION

-bull-bull-bull GROUND LEVEL

WES TERN BASIN EASTERN BASIN x WINOS ALOFT (kmhr)

t t

CNO WINOSILA WllltOS poundMT WINOS

SMO LA EMT BRA CAB RIA RED O (1736 PDT) (1655 PDT) (1707 PDT) (163 PDT) (1823PDT) 1805 PDT)

Figure 9 VERTICAL CROSS-SECTION OF b FOR AFTERlOON OF JULY 25 1973 scat

T bull 1o- 4 - l )(units are m

__~~---iii~~- ~- ~~______ ~~- --~~J---=-~ ~

N ~ -J

PACIFiC OCEAN

0 5 10 15 1111

E 8 4 I 0 8 6 2 ~ bull

SCALE

dh Mes

CONTOURS REPRESENT - 000 ft 305 m

0 SNA

c8s

ec 8v

amp R~b

Figure 10 TRAJECTORY ENVELOPE FOR AIR ARRI1G AT CABLE AIRPORT (CPLAD) 1600 PDT JULY 25 1973

~-~

q_- ~ ------1 H~~~ -~~--~ ___---___--i- __r-=-1--===12---1 ~ ___r~ _==---_ - ~- f~~ ~-- - -5plusmn-at -~middot~

ll~~r1 ri

40

ec 8v

-1 I

amp

0 HQ_

7 0

CAP LAAR) O

VER

PACIFIC OCEAN ~ 0

RLA

4

WHqR d

diams

H ~I

I l

0 COMA

3

L~

LAH

Fa_ f ~~

S ~ LA APCD VALUES ADJUSTED TO AGREE ~

lt

0

5 10 15 mi0 WITH ARB CALIBRATIONE-j I I CONTOURS REPRESENT NZJ ~ 0 a SCALE 6 24 km - 1000 ft 305m COS v~J

______ J 10 ro ( igtf t-i

coFigure 11 SURFACE OZONE CONCENTRATIONS (pphm) I 600- I 700 PDT JULY 25 1973 ~

~~~~~C-~ ------=--~-__-~--~~~=--- ----=--~

N

-E

D1600----------------------------- 1--

14001-------------------------------

1200

I Ground Elevation

1000 middot 445 m ] lampJ

sect ~~ 7 ) SURFACE i6~ 800 MIXED LAYER

~

~ [ J ~ ~ I OZONE CONCENTRATIONS~ 600 E E GREATER THAN

( 50 pohm

400 I C H T Z GROUND LEVEL

200

I PUUloCETER UNIT SnbullBOL

NOc N0 0 ppm01 02 03 04 05 03 z

40 --~45~~ 50 co pm C0 5 10 15 20 25 30 35 I I I I I I I I I I TEIIPERATURE oc T-5 b 5 10 15 20 25 30 35 40 45

I-- 100 RELATIVE HUlillOITY H0 10 20 30 40 50 60 70 60 90 b1eot IOmiddotm- 1 8

CN cmmiddot3 1 IO X0 I 2 3 4 ~ 6 7 8 9 10 URBJLENC-C cm213ue- E

Figure 12 VERTICAL PROFILE OVER CABLE (CAB) J CLY 2 5 l C)7 3 l 63 6 PDT

~ _~ ~--- -

--

1400 I bull bull

1200

1000-5 LampJ 0 ~ I- 800 ~ c(

sooLl

-1-=-1-~--t j --=~c-o-----i-bull 1-~~~ ilt~~ -~-1 lta-abull--~ -c-~---=---r F--- ---- I n_--middot- =~~ ai~IHJ

(~-It

1600 ___________________________________

C r 11 s Ground Elevation t~C E H I~lcc

- ~ 1 90 m

4001 bullc C H

C UNDrnCUTTNG svC ~ Ic- H

SEA BREEZEC II 200

C C

[C -PARAMETER ---UNIT SYMBOL

NOx N0 0 ppm01 02 03 04 05 03 z co ppm C0 5 10 15 20 25 30 35 40 45 50

-5 middot- -~20~----25 TEMPERATURE oc T0 5 10 15 30 35 40 45

100 RELATIVE HUIOITY H0 JO 20 30 40 50 60 70 80 90 bcot 10-4m-1 8

CN crrr3 10 0 I 2 3 4 5 6 7 8 9 10 X TURBULENCE cmZ-13 sec-1 E

N N

_-----=-G--~---

Figure 13 VER TICAL PROFILE AT EL MONTE (EMT) JULY 25 1971 1656 PDT SHOWING UNDERCUTTING BY THE SEA BREEZE

0

middot~_lt ~middotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotbullbull

-~

LACA

0 - )

i r=

-v2v

~

_middot~middot)( I bullbull

bullJ

K~Ji~middot

~~ 61iAS 0

EMT J~J---6~-11 ~orr

PACIFIC OCEAN

WEST 0

SMC

0RLA

14

L~8

R~A

~BL

16 ~ ~

0 5s Pcfrac14A c1i ~ )

wFJfo~J_) ltI~~~

_ff-Clf1ito J )

HILL~

~J U

~ _~~~

~

I o middot

1 1$ ~ 11yen ~middot ~I N

I

N I- I

t

0 --pomiddotmiddot bullmiddot i- 1LO middot Joomiddotmiddotmiddot -- middot middotmiddot -middotmiddot

_middotmiddot 0 middot middotbull MWS r

L4 ( 1 T bull bull __-- -A bullbullbullbull middot

0 i __ bullbull

17 t-J~ N7 a S I ~r ~ 1 rtd ~lt A-~ v- middot ~ - cXa 0

RIA 19

CLO

ltJ~

bull ~ 0

(

--

1

_ _

-2Wl

~s~o -- _)~J0JgtJ~ ___ Q

15 l1JI

0 15 r(A0

CAP

CLARR)~R 1900 1-shyPDT

II (_-L~X L2X I 0~ R[V

0 CCtwA

I

I18=00 POT~ l4 r1

fj

-11J - ----- 11=oomiddotmiddotpor

l~i middotmiddot- o

i

5 10 5 Tl o~1 middot--middotmiddotmiddot middotmiddot

_q it==i--__F-3 9 I I CONTOURS REPRESENT SNA NZJ ~1 o

_- I 0 8 16 24 km I - 1000 ft 305 m middot ~

7 14~CALE --- 2500 ft o2m V lr1 ) middot I i0 _ il o5

16QQ pol(middot v( ____________ _L

I i

Figure 14 APPROXIMATE TIME (PDT) OF ARRIVAL OF SEA BREEZE Jl-LY 25 1973 (Ogt_iective criterion based on ground level ozone concentrations)

~ -___~==~ ~~ - ~ =-~ f7r=~1 _j~-~ --c_~~

u-middot - middot middotmiddotmiddotmiddotmiddot

~- middotmiddot~ ~1 WESTERN BASIN r Joa_middotmiddotmiddotmiddot_ NOxEMISSION RATE ~- 95 METRIC TONShr

-----bull_ ~ ~middot~ I -OUR -----middot )omiddotmiddotmiddot - middot~ l21 (fTI

~ AT middot ~ middotbullmiddot- ~- ~ middot 4bull-middot

I EASTERN BASIN NOx EMISSION RATE 10 METRIC TONS hr

ri r bullbull

t10 Joa

) __ 8v -a_ -- -bull-I O ~AGA -_ ~S ___ _ middotmiddotmiddot -

~ ~v ai- omiddot-middot~-- - ) r -middotmiddotmiddot f middot( ---~ -l A ~ _ (- bull ___

it~ ~~~ middot-middot -- ~-~ ~~~ 0 0 AZU~

AVERAGE CONCEN7RCTi)N iN BOX (IF STEADY STATE)

IS 25 pphm

1 r f--Ji 7 ~Sv PAS ou )V~(~- ~ t i -~ Li_) 03 FLUX THROUGH f~

~ ~JI_~ - amp_ JiM O SHADED BOUNOA~middot~-~ ~~-s-- EMT 185 t 60 METRI~ bull ~ ~ TONShr 0 (m)

c~~~ 1t~CS A~JFP

1000 _29

-i32

_~o tUA

_

1

O~ ~

0 -__rJ( (r- J PACIFIC OCEAN LAX _ C-middotJbull _

l o M R No _

550m

r

A frac14

HAR O HJ LAH

_ o camptA REDLANDS 18QO POT ~ r

I bull ~

RB MEAN TRAJECT~~~y

0

TOA L~S

0 AN

I - ~ 8 OUNOARY ~ ~middotltdeg ~ ~ BETWEEN middot __ WES~ERN ANO- middot middot - ~

I gt I lt bullmiddot bull (EASTERN ~ i middotmiddot middot - - ~

S ~ ~~ ~ - middot-

rt1~1_--t------l

middot1-- BASIN ~-~

1-)~~--middot ~ ~l

~~ ~-bull bull J --

-is-eo -_

0 5 10

j=i r-i C

0 8 ltl

SCALE

5 mi

2~ un

CONTOURS REPRESENT - 1000 ft 3gt5 m

--middotmiddot 2500 ft 1 762 m

~

0SNA

cos 0

_ --~ ----- --- ( bullmiddotmiddotgt

- middotlt- ltgtmiddot t__ Q ~

1 1 rmiddot bullbullbullbullmiddot ~9

NZJ ~ middotmiddot - middot- Alr ---middotmiddot- middot middot( middotmiddotmiddotmiddotv ~ bullbullbullw bullbullbull bullmiddot 1 bullbullr~ ~-- -middot ~--v ~- - I -~

ESTIMATED OZONE FLUX FROM VESTER~ TO EASTER-J BASIN JULY 25 1973 I 700 PDT

C ~IV

N N N

I

l ~

-~~

I

iI

i I

I t

t

~ ---~ --

Figure 15

~Qa llfJD fl(~middot ~ 11f ~I I

l

Lfb ec~s0 CPK v2v 0

ALT 8v Ld~_----1

I

HO-

0 CA

middotLARRv O VE~

1330

ol(Di

A~U

0ENT

~lt

s~e ~ 1530

F8f 1730

~

rbull-~

oc (WljT) -_-~(~~c lt-rw---_

~~ ~-_i~cB~~~

2-~) - ~ ~ l~w-~~ p~- pound)_

0 ojI middot tl-1CfUp I ~ ) 1 ~ J~I i bull middotbull middot~-Li 1)- ) I

DiI ~- 0

i ) 0 l I I

t

A RALc~o JI

C

-~

0 r-iR

~IV 1230 1~

RE PO ~- I - Ftl

) 0 ---~gt- __L8s ~Zi diams ( T~ _middot_ ~~ ~

I AN ~~-~ j t bi 0

~ I

~ I L i

-_gt ji o 5 c 5 Tl middot 0 0 ~-i p__i=r 2=f I_ I 1 NZJSNA 1

1 8 2 4 km )

SCALE I 00 J_(1 CONTOURS REPRESENT cos f

1 0 I --- I - ))) 35

PACIFIC OCEAN

Figure 16 TRAJECTORY E~VELOPE FOR AIR ARRI1gtJG OVER REDL_)DS AT 1800 PDT JULY 23 l =i73

224

JULY 25 1973

LA DOWNTOWN

0sect040 a

~

~ 020 0 X z0 ~ LJ 0 ~ z

~5 040 330POMONA 0 ~ en~ 020 w z _J

w w 0 (9 z O----u-~~-__~_-~~~-------L-~-0--0-0~----- z

ltt~ 040 56 (I)z

0 0o _ RIVERSIDE _J0 20 t6 ~

0~ Qt---0-0--ltrO-ltgt-C~------~~~~ a

LL ~

Rate ~ IO mph___ (I) w

_J~ ~ ~

et~ lt(

3 040 PALM SPRINGS ~

j 020 ~

0------____-----L--___---------L---~--~

105

12 4 8 12 4 8 12 l~-s----am _ pm----1

HOUR OF DAY PST

Figure 17 Diurnal variation July 25 1973 of oxidant concentrations at air monitoring stations at Los Angeles Downtown Pomona Riverside and Palm Springs California Values are corrected data Los Angeles Downtown and Pomona x 11 and Riverside and Palm Springs X 08

CONO S t 1 fRESEIS7

~

~~ 0

ciffmiddotdK ~ ~v~~o

( ~s ~

bull ~r ~ bull 1--~~----Soootl ~ ~ ~ ~ lj i1 d t CJ ~ ampfrsmiddotflt- frac12 ~ middotL~Js _-- ~

_gtgt middot~ ~rroltf~-) ~ 0 s- r

middot-middot- r_~ ~~JtbO ~~bull~Jt ~~~ L r - bull _ ~ I= J 1 ~ ~ ~-~~bullJC ___ -_ middot ~ laquo -poundJ~ ~- middot1~ r-- - V--_1_ ~ I 1 S I

V ~ bullf-uv~ fi -~zumiddot -~middot~ LS gt -tmiddot-F Q~ ~-tv I_~ --- ONT p(_ s ~S ~~~-[ ( 0 c-_ --~ ~~~___d_) lt- ~ I -i-C - -

~----1-1 bull~~POMA ~V BN ) middot-~ f -- s - ~

~VA -middot- ~p AAL a 2~~ ~~middot01 r r ~ middot middot 0-- V

i LAX bull1

~ -~poundJ-i- ltllll _(__1-0~ ~t- degQ-0- ~~ _ _-__~~-qlK ( a_ II ~ ~p-~ ~J

N bull - - 0 r o_ _I ~ -~ ~middot ~ ~amp ~--= ~ ) s ~

- -~- - middotO _a - Tl --0- ov I lHOIO J I bull J -- ~ 6 ~ -__ 2 ~

(__ ~~ _- ~-~ middot8---fl~ -- ~ bull~-abullbull _~ ~-cgt ~ bull bull middot e bull bull l ~ 0

I 1A_ HZJ middoto~J

middot0 (~ ~ S TAA

- ~ - - - --0 () _-j J middotO=c==c-c==cc~~~ l ~~ ~ ~ bull-~---~ ~ bullbull -~ al1 ~ bull __ ~--middotmiddotmiddot

diams Skyforest _ Strawberry Mt Lookout

Figure 18 STRE ~[Ll)ES FOR 1600 PDT on 8 1673

~ ~--

vO 0

N N V1

au

91 V7

-1 ~ -=1 ~~ ~~~~l r=--~d- ---1 _J-_

~E1 ~L1-~f~

3100 ---------------------------------

2900r-----------------------------

T

e w 0

~ 5 Cl Ground Elevation

1560 m

T PARAMETER UNIT SnbullBOL

NOx N 01 02 03 04 05 03

ppm z co ppm C

10 15 20 25 30 35 40 --

45 50

170

I I I z

0 5

-5 - -0~ 5 10 15 20 25 30 35 40 45 TEMPERATURE oc T

0

0

10

I

20

2

30

3

40

4

50

5

60

6

70

7

80

8

90

9

100

o

RELATIVE HUMIDITY

bcot CN

TUR8ULENC~

110-4m-

cm-3 tobull 213 1 cm sec-

H

8 X E N

N OI

Figure 19 VER TI CAL PROFILE OVER ARROWHEAD u-RR_l A CG CST I 6 1973 939 PDT

3100----------------------------------

N2900r----------------------------- -i

N

2700i-------------------------------

2500

e 0 uJ 2300 gt ~ ct

2100

1900i---------------------+--------------

~le 1iation 1360 m) 17001 ~

- -PARA1jETER UNIT SYMBOL

T NOx N1500 o ppm01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50

TEWERATJRE oc T-5 middot --~o--- 5 10 15 20 25 30 35 40 45

IOO RELATIVE HUWIOIT Y H0 10 20 30 40 50 60 70 80 90 bcat 10-~- 1 8

CN cm- 3 104 X0 I 2 3 4 5 6 7 8 9 10 213 1 tURBliiENCE cm sec- E

Figure 20 VERTICAL PROFILE OVER ARROWHEA D -RR 1 --- -AUGlJST 16 I) 16--1S PDT

1-~i w--~i_f l-=--bullC- ---~-4

1600 bull t c- N 8 ff Tbull C[ 8 H 1 bull H z H T ~ C f N 1 H T bull C rn 1 C NE bull-~z Hi400 bull bull tf T bull N ~r --middot _P H -ybull EC N z__e H T i 8 z H Tbull C E HD Z H T POLLUTANTS REMAINING FROM bullt C Hbull L T PREVIOUS DAY1200 Et HO I II -middot-- bull Ct H 9 - H T

___ Hbull( E N 1 a tC N i--_ -1 H

C N Tbull Z HP poundIC C H z_ 1111 1

- bull C H Z l _H_ _J1000 )( cc H -z emiddot ksect bull C N ~ T

)( iz H 8 H TIAI -t XC z 7-- T0 bull pound N t H_8

t-gt

YCpound N 1800 l I-gtltbull - H (Jet

N i -r~Bltt t bull gt- t C X N H T

[ BUOYANT POINT SOURCE PLUMEH 1

N ~z-- -

C H

-bull SUPERIMPOSED ON POLLUTANTSC JZ X H T 600 -~ E c REMAINING FROM PREVIOUS OtY Cl JC t H H f bull cmiddot t HT -fl

C- X t fl _ REMNANT OF NOCTURNAL RADIATION INVERSION(I-----e-C f N K I T H

C Z [ T H x-8 400 _Zc r -H -K SURFACE MIXING LAYERz C II H K 8

C N T pound H M 8 _ I -t ff H E N -9 l

Ground Elevation 305 rn200

PARAMETER UNIT SYMBOL

_ I - I I I NOx N00 ppm01 02 03 04 05 03 z

co ppm C 0 5 IO 15 20 25 30 35 40 45 50

L middot1 TEMPERATURE oc T-5 0 5 IO 15 20 25 30 35 40 45

100 RELATIVE HUPAIDIT y H0 10 20 30 40 50 60 70 80 90 bscot o-4m- 1 B

CN cm-3 x 104 X0 2 3 4 5 6 7 8 9 10 TURBULENC~ cm213sec-1 E N

N co

Figure 21 VERTICAL PROFILE OVER BRACKETT (BRA) JULY 26 1973 0825 PDT SHOWING BUOYANT PLUME AND UNDERCUTTING BY RADIATION INVERSION

N N 01600

___bull C M C

C

1400~~~ t C [ middot H LAYER CAUSED BY

C C H C [ H UPSLOPE FLOWl

1200

1000 ] w

SURFACE MIXING LAYER 0 --= ~ -~~ 6 800~ er

C C

600t-i C C t C

I ~00

Ground Elevation 436 m 2001-------------------------------

PAIUWETU UNIT SYWBOL

NOx N ppm0 0 01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50 I I I I I I I I TEWPERAT1JftE degC T-o b 5 10 15 20 25 30 35 40 45

100 ~EIATIVE HUWIOITY H0 10 20 30 40 50 60 70 80 90 b1tt1 10-m- 8

CN enr3 110 X0 2 3 4 5 6 7 8 9 10 Tu RUL Erct cm23sec- E

Figt1re 22 VERTICAl PROFILE AT RIALTO (RIA) JlJL Y 19 1973 1738 PDT SHOWI=JG LAYER CAUSED BY UPSLOPE FLOW

~~-7 ~ ~- 1 ~iri ~~- ~~-~ ~t ~~ ~ =~middot-1

1200 I t 1 If J-

1000

I C ltTl a_ ~l- t

800

600

L gE __r H

H

400 j (~ c pound N C E I~

t EH -

1-1 M

H H

H M H H

H

H H

11 bull H M H

M H If

H H

H

- C t H ~ C poundmiddot H

I C E I(

200

1600--------------------------- t

T t t T l

l T t

T t_

t 1

l] w ) g f

Tt t

ltt ~ T

t J t T

t J

f 1

t

Klt

H M Cro1nd Elevation 250 m HT X

5Yl80LPAllAlETER ~

NOx N0 0 ppm01 02 03 04 05 03 z

co ppm C0 5 10 io 20 25 30 35 40 45 50

25~--- ---35~~-40 TEMPERATU~E oc T-5 0 5 lO 15 20 30 45

100 RELATIVE HUMIDITY H0 iO 20 30 40 50 60 70 80 90 bact 10--ltllm-1 B

CN cmmiddot3 11 04 X0 I 2 3 4 5 6 7 8 9 10 IURBULENCE cm2hioC-1 E

Figure 23 VERTICAL PROFILE OVER RIVERSIDE (RAL) N

JULY 26 1973 2239 PDT I)

middot==-=-=

0

bull

N w 1--

ii -s~~ l-obull

CJ ~

obull -obull obull

5 02~

bscat

Oa

4l o2J

-I 3 e I 0

--)(

~

Abullu 2

ll

ol

Traverse at 750 m msl 35 km Downwind (SW) of Arch - St Louis Mo 1117 - 1137 CDT

( Power Plant Plume -01 Ibull-[ ~ e

11 bull E I -)(I

I0bull I 1r~ l -

0

I I Io 1 u I

I r- l A bull I i I 1I

H1I I 4 t I II I I

11 I I

I I r I I I

I I qo 01 I I

I I bullJ~viI I middot ~

I

I I

~

Urban Plume

ood 0 10 20 30 40 50

kilometers

o~

02

01

s 1

P

0bull 01

00S~J1 I ti middotmiddot1 middotvmiddotmiddot~ J

Urban Plume

I y

oo 0 10 20 30 40 so

kilometers

Traverse at 750 m msl 46 km Downwind (SVV) of Arch - St Louis Mo 153 0 - J 549 CDT

---- bscat

o-

Power Plant Plume

1l~ 11I 1 t

ill~t fl Ibull I ii

I

lmiddotmiddotrI

I I I I t II

l vrI V

JV-f Jl bull

bull t I bull I

Figure 24

l

232 RELATIVE CONTRIBUTIONS OF STATIONARY ANDMOilILE

SOURCES TO OXIDANT FORMATION IN LOS ANGELES COUN1Y IMPLICATIONS FOR CONTROL STRATEGIES

by Robert G Lunche Air Pollution Control Officer

Los Angeles County Air Pollution Control District Los Angeles California

Introduction

The type of air pollution problem characteristic of the west coast of the

United States and particularly of Southern California has come to be known

as photochemical smog because it is the result of sunlight-energized atmospheric

reations involving oxides of nitrogen and reactive hydrocarbons Its manifesta-

tions- -eye irritation reduced visibility damage to vegetation and accumula-

tion of abnormally high concentrations of ozone or oxidant - -are by now well

known In fact the occurrence of high levels of oxidant which consists almost

entirely of ozone has become the primary indicator for the presence and relative

severity of photochemical smog

During the 25 years since photochemical smog in Los Angeles County was

first identified an extensive program has been underway for control of the responshy

sible contaminant emissions Initially during the 1950 s these programs concenshy

trated on controlling emissions of hydrocarbons from the stationary sources of this

contaminant In the early 60 s programs for the control of hydrocarbon emissions

from motor vehicles in California were begun An exhaust emission control proshy

gram for hydrocarbons and carbon monoxide from new vehicles was begun in 1966

C011trol of oxides of nitrogen emissions from motor vehicles began in 1971

As a result of the overall control program by 1974 emissions of reactive

hydrocarbons from stationary sources have been reduced 70fo from uncontrolled

levels and about the same percentage from mobile sources Oxides of nitrcgen emissions

233

from statjonary sources have been reduced about 53 while emissions from moshy

bile sources are still about 7 above uncontrolled levels due to the increase

in NOx from 1966-1970 models Additional controls already planned for the future

will by 1980 achieve reductions of reactive hydrocarbons from stationary sources

of about 87 from uncontrolled levels and from mobile sources about 93 By

1980 emissions of oxides of nitrogen from stationary sources will have been reshy

duced 53 and from mobile sources 63 from uncontrolled levels The past

present and projected emissions of these contaminants are shown in Figure 1

A I though compliance with the air quality standards has not yet been achieved-shy

and is not likely before 1980- -the results of these programs have been reflected rather

predictably in changes in certain of the manifestations of photochemical smog For

example eye irritation is less frequent and less severe and in some areas js

rarely felt at all any more and damage to vegetation has been markedly reduced

Ozone (or oxidant) concentrations have been decreasing in Southern California

coastal areas since _1964 in areas 10-15 miles from the coast since 1966 and in

inland areas 40-60 miles from the coast since 1970 or 1971 as shown on Figures

2 arrl 3- All of these positive effects have occurred despite the continuing growth

of the area indicating that themiddot control programs are gradually achieving their purpos

a return to clean air

This improvement is al~o refutation of the so-called Big Box -concept which

assumes that the total daily emissions in a given area are somehow uniformly disshy

tributed throughout that area--regardless of its size or of known facts about the

meteorology of the area or the spatial and temporal distribution of its emissions- -

234

and of control strategies based on that concept And since the improvement in

air quality refutes the control strategies based on reductions in total emissions

it thus confirms the value of more recent control strategies which emphasize conshy

trol of motor vehicle emissions and use of a source-effect area concept

Following is a brief listing of the evidence we intend to present as supporting

our views on just what control strategy is appropriate

Examination of relative contributions of HC and NOx from stationarybull and mobile sources demonstrates that motor vehicles are the overwhelming

f source of both contaminants~

I bull Observation of air monitoring data shows that the effects of photochem -

ical smog are not uniformly distributed t_hroughout the county

bull Study of the meteorology of LA County shows consistent paths of trans -

port for various air parcels and consistent relationships between the

areas most seriously affected by photochemical smog and high oxidant

concentrations and certain other areas

bull The upwind areas are found to be source areas--the downwind areas-shy

effect areas

bull Central L A is found to be the predominant source area for the effectI area in which the highest oxidant levels in the SCAB consistently occur

bull The predominant source of emissions in this source area is found to

be motor vehicles

bull Central LA has the highest traffic density I

ij bull Both pr~mary and secondary contaminant concentrations reflect the effects

of the new motor vehicle control program in a predictable fashion 11 I

A strategy based upon these findings is gradually being verified by atmosshybull pheric oxidant data~

235

The Evidence that Motor Vehicle Emissions Are the Principal Source of Oxidant

As seen from Figure 1 at the present time the total daily emissions of I-IC

and_ NOx from all sources in Los Angeles middotcounty are primarily due to the motor

vehicle The problem now is to find the spatial and temporal representation of

emissions which when examined in the light of the known meteorology and geogra -

phy of the Los Angeles region best describes the source of emissions responsible

for the highest observed oxidant readings

In the rollback models used by EPA and others the basin is treated as a

big box with uniformly distributed emissions and peak oxidant is considered to

be proportional to total basinwide hydrocarbon emissions

The fact is that the middotemitted contaminants from which the smog is formed

and the effects which characterize that smog are not evenly distributed throughout

the Los Angeles Basin in other words the basin area under the inversion is not one

large box filled to all corners with homogeneously distributed air contaminants and

photochemical smog

Refutation of Big Box Myth

Examination of atmospheric contaminant concentrations refutes the big box

concept It is found for example that concentrations of djrectly emitted contam -

inants measured at a particular sampling site reflect the emissions within a rather

limited area around that site For this reason contaminant concentration levels

vary from one location to another and each has a characteristic daily pattern which

reflects the daily pattern of emissions in that area

middot 236

The big box concept is further refuted by the fact that peak concentrations

of carbon monoxide and oxides of nitrogen in areas of high traffic density were

fairly static prior to 1966 Thus they did not reflect the 45-50 per cent growth

in motor vehicle registrations and gasoline consumption which occurred in Los

Angeles County between 1955 and 1965 and which caused comparable increases in

total daily emissions of such vehicle-related contaminants This demonstrates

that growth was outward rather than upward so that a larger area of the County

began to be affected by photochemical smog but no area experienced smog ofJ

greater severity than that originally affected by smog formed from the vehicular

emissions which accumulated each weekday in central Los Angeles and were trans-

1 I

ported later that day to the San Gabriel Valley

1 Meteorological Evidence

To verify the geographical dependence of emissions and resulting atmospheric

concentrations let us examine the meteorology of these large areas of Southern

California Both the County and the Basin have many meteorological sub-regions

in which the patterns of wind speed and direction may be similar but within

which the patterns of air transport are parallel with those of adjacent sub-regions

and the respective air parcels do not ever meet or join

The characteristic patterns of inversion height and wind speed and direction

in these sub-regions and their patterns of vehicular emissions together have

created a network of source areas- -those in which the reactant contaminants accu -1T

i ~ mulate in the morning and begin to react--and related receptor areas--those to which

~ the products and associated effects of the photochemical reactions of the contamshy)

inants originally emitted in the source areas are carried by the late morning and

237 middot

afternoon winds ( sea breeze)

Wind-flow patterns show that characteristic patterns of transport for related

source area-effect area combinations are separate and parallel not mixing or

joining Each source area has its own reactor pipeline to its own effect area

or areas

To illustrate this source area-effect area relationship the typical flow of

polluted air from downtown Los Angeles to Pasadena was selected as a worst

case situation for in-depth examination Figure 4 shows that the air in downtown

Los Angeles on the morning of smoggy days moves directly from the central area

to Pasadena

Vehicular traffic is the predominant emission source in both downtown Los

Angeles and Pasadena Thus the air in each locality should contain CO Also

since oxidant would form in the air parcel moving from Los Angeles to Pasadena

oxidant levels would be expected to be higher in Pasadena than in downtown Los

Angeles

Figure 5 shows these relationships for the period 1960-1972 The atmosshy

pheric CO level is similar for the two areas while oxidant levels were higher in

Pasadena than in Los Angeles throughout this time period This demonstrates

that a significant amount of oxidant formed in the air as it moved to Pasadena

containing both the unreactive CO and the photochemical reactants for producing

oxidant Both CO and oxidant show a marked downward trend in each locality since

1965 which emphasizes the effect of vehicle exhaust controls and the correlation

between the localities

238

On a day which is favorable to the formation and accumulation of photoshy

chemical smog a contaminated air parcel normally originates during the

6-9 a m period on a weekday from an area of dense traffic centered just

south and west of Downtown Los Angeles It is oxidant generated within that air

parcel which usually affects Central Los Angeles and the West San Gabriel

middotK IJ l J

Valley area around Pasadena

The traffic area in which this smog had its origin is about the most dense

in Los Angeles County and has been so for the past 25-30 years No area

has a higher effective density thampn-this Using carbon monoxide which

1

is almost entirely attributable to motor vehicles as an indicator of such emis-

sions it is found that the concentrations of emitted vehicular contaminants

middotr i

measured in Central Los Angeles during the past 15 years confirms both this lack

of change in effective density and the absence of any area of any greater effective

density when local differences in inversion are acknowledged

This area the Central Source Area is depicted in Figure 4 The size

and shape of the Central Source Area was ch~sen to be large enough to reduce to

an insignificant level any diffusion or transport into this area from any externally

l generated reactants This conclusion is based in part on the trajectory studies

previously referenced as well as an analysis of the diffusion and transport parashy

meters for the area

239

The Central Source Area has been identified as that geographical region

which contributes essentially all of the primary contaminant emissions giving

rise to the highatmospheric oxidant levels in the West San Gabriel Valley

The proportion of emissions in the CSA due to motor vehicles and that due to

stationary sources is shown in Table 1 For the County as a whole about 80 per

cent of _(6-9) AM reactive hydrocarbons are due to motor vehicle emissions and this

figure rises to 90 per cent for the CSA The same conclusion a pp lies to NOx

emissions The Central Source Area contains the greatest density of vehicle traffic

in the County and thus the greatest density of source emissions Thus it appears

that the source area with the highest density of emissions during the critical (6-9)

AM period is responsible for the highest afternoon oxidant levels observed in Los

A i1geles County and in the South Coast Air Basin These highest oxidant levels

are consistently observed to occur in the San Gabriel Valley This is true whether

the LAAPCD or the ARB oxidant calibration procedure is used

Further the atmospheric concentrations of the primary pollutants can be

identified as originating primarily from the motor vehicle and they reflect the

effects of the motor vehicle emission control program A vehtcular source area

can be identified by its atmospheric levels of CO and NOx Figure 6 compares

measured atmospheric levels with calculated atmospheric levels for CO NOx

and the CONOx ratio in the downtown area

TABLE 1 240

REACTIVE HYDROCARBON EMISSIONS

(6-9) AM

1970

LOS ANGELES COUN1Y middot CENTRAL SOURCE AREA middot SOURCE TONS PER CENT TONS PER CENT

Mobile 1260 81 3 135 91 2

Stationary 290 187 1 3 88

Total 1s~o 1000 148 1000

By 7 -Mode Gallonage

241

The calculated values shown in Figure 6 were derived from a baseline

survey of 1100 vehicles and continued surveillance tests both using the Calishy

fornia 7-Mode test cycle The baseline survey showed that motor vehicles withshy

out exhaust control systems had average exhaust emissions concentrations of 3 4

per cent CO and 1000 parts per million of NOx Baseline emissions data apply

to 1965 and earlier model vehicleg and surveillance data to 1966 and later modelsmiddot

Since it can be concluded from calculations and observations that the dilushy

tion of auto exhaust emissions in the atmosphere on a smoggy day in Los Angeles

is approximately 1000 to 1 the calculated values for CO and NOx prior to 1965 are

34 ppm CO and 1 ppm NOxo After 1965 the changing effect of controlled vehicles

in the total vehicle population is reflected in the calculated values

CO and NOx values measured in the atmosphere are also shown in Figure

6 and confirm the values calculated entirely as diluted vehicular emissions NOx

concentrations measured in the atmosphere tend to be consistently a little lower

than the calculated values probably because photochemical reactions remove some

NOx from the system

The data for CO and NOx calculated and measured show that emissions in

downtown Los Angeles originate almost exclusively from motor vehicles and that

atmospheric concentrations there reflect the average emissions from a representashy

tive vehicle population

The ARB has recently published a report entitled A Trend Study of Two

Indicator Hydrocarbons in the South Coast Air Basin Acetylene was used as a

242

specific indicator of automobile exhaust emissions and it was found to have de-

clined in concentration in the Los Angeles atmosphere at an annual rate of 12 5

per cent since 1970 To quote from this report The California implementation

plan requires an annual average reduction in these emissions (reactive organic

compounds) of 166 tons per day or 11 1 of the 1970 tonnage per year The per cent

reductions in the_ acetylene levels at Los Angeles and Azusa are greater than reshy

quired by the implementation plan Since acetylene is almost entirely associated

J with auto exhaust this demonstrates that the motor vehicle emission control

program is achieving its purpose

To summarize at this point it has been deomonstrated that high oxidant values

are due to motor vehicular emissions of NOx and HC because

NOx and HC are the principal reactants in the oxidant formation process

and they originate primarily from motor vehicle emissions and

The highest oxidant values are recorded in_ effect areas that receive air

from source areas where motor vehicles are clearly identified as the

dominant source of NOx and HC

243

Future Control Strategy

The APCD strategy for achieving and maintaining the oxidant air quality

standard is based upon the fact that high oxidant values are due to motor ve-

hicle emissions of hydrocarlxms arrl nitrogen oxides This strategy is as follows

1 Both Hydrocarbon and Nitrogen Oxides Emissions Must Be Considered To Achieve the Federal Oxidant Standard

There is wide agreement that NOx and HC are the principal reactants in

the oxidant formation process and that vehicular emissions are a major source

of NOx HC and CO

2 Effective Regulation of Atmospheric Concentrations of Both HC and NOx and of the Ratio Between Them is necessary for Attainment of the Federal Air Quality Standard for Oxidant

Basmiddoted on the abundance middotof available experimental evidence it is our firm

position that the most rational approach to solving the photochemical oxidant smog

problem in the South Coast Air Basin (SCAB) is to control the quantities of emissions

from motor vehicles of both smog precursors--Hcmiddot and NOx--their resulting atmosshy

pheric concentrations and the ratios between both contaminants which will result

from these controls

We arc also convinced that the oxidant and nitrogen dioxide air quality stanshy

dards can and will be met not by 1975 or 1977 but by the early 1980 s if the emisshy

sion control program as originally outlined by Ca~ifornia or a slight modification

of it proposed by the District is followed and enforced This should also provide

for continued compliance with these air quality standards at least through 1990

244

It will also allow time for a reappraisal in about 1978 of the whole situation relative

to the ultimate emission standards required and the best approach to their impleshy

mentation

Calculation of the degree of control necessary to attain the air quality

~ standards for oxidant and nitrogen dioxide involves indirect complex methods 1

aimed at determ_ining the degree of control of the primary contaminants directly

emitted by automobiles

The following evidence supports our proposed solution to the problem in

terms of both the atmospheric concentrations of the oxidant precursors NOx

and HC the ratio between them as reflected in their exhaust emission standards

and the resulting atmospheric concentrations of oxidant which comply with the air

quality standards

Chamber Results and Projections to the Atmosphere

The importance of environmental chamberwork cannot be minimized the

j need for and direction of the whole emission control program was based initially

j on the results of chamber experiments In order to understand the importance to

air quality of achieving both the correct low quantities of emissions and the right

ratio we can present several graphic portrayals of analyses of experimental labshy

oratory work together with their relationship to past present and future air quality

in terms of both morning primary reactant concentrations during the morning

traffic peak and the equivalent emissions which would produce them

245

Figure 7 shows maximum ozone levels that were obtained by irradiating

varying amounts of auto exhaust hydrocarbons and oxides of nitrogen in an environshy

mental chamber The corresponding ozone levels then can be found for any comshy

bination of BC and NOx concentrations Thus high ozone is produced with high

emissions of both hydrocarbons and oxides of nitrogen and low oxidant is formed with

low emissions However either low NOx or low HC emissions11 can also produce

low oxidant--graphic and clear evidence of the importance of the NOxHC ratio in

ozone formation Furthermore each and every possible combination of values for

NOx and HC has then a corresponding characteristic maximum chamber ozone

concentration

Using this graph we can estimate what ozone levels would result if certain

atmospheric mixtures of NOx and HC could be injected into the chamber and

irradiated Such estimates were made for 1960 and 1965 using atmospheric data

rlThe points labeles 1960 and 65 show the location of the highest levels of both

HC and NOx found in the air in those years in Downtown Los Angeles (OOLA) area

during the 6-9 AM traffic peak

It has been demonstrated by use of CO and NOx data and CONOx ratios

hnw well the characteristics of vehicle emissions are reflected in the atmosphere

We know what emissions from the average vehicle were then in 1960-1965 both

for HC and NOx so that we can mathematically relate emissions to atmospheric

concentrations for those years and so for future years also knowing or calculating

only what the characteristic emissions will be from the average vehicle

246

The NOx concentrations stayed about the same from 1960 through 1965 because

average vehicle emissions of that contaminant did not change during that time

Mobile source emissions can be shown to have contributed essentially all of this obshy

served result However blow by controls did reduce emissions of HC and the

concentrations dropped accordingly In 1965 the last year before exhaust controls

the point 65 indicates where we were then in terms of maximum ozone formation

to be expected in a chamber with the highest HC and NO concentrations found in the X

air that year Levels of ozone actually measured in the atmosphere however

are higher than those shown on the graph for high NOx and I-IC concentrations for

those years up to the present

The strategy to meet the oxidant standard is obvious--get atmospheric NOx

and HC concentrations out of the area on the chart that produces high ozone levels

and put them in tie areas with the lowest levels This can only be done by implementshy

ing appropriate emission standards

As can be seen that did not happen between 1965 and 1970 because manufacshy

turers used controls on new cars in California which while causing a decrease in

BC (and CO) allowed a large increase in NOx emissions Thus the path line of

the atmosphere on the chart goes up from 65 and diagonally to the left passing

through an area of higher ozone levels The atmospheric concentrations of oxidant

predictably increased during the years 1967 and 1968 By 1970 they dropped to lower

levels - -back to about the same as in 1965- -exactly as predicted by the model The

app14oximate location of the point for 1970 (70) was both predicted on the basis of

247

the mathematical model and confirmed by atm-ospheric measurements of

[)owntown Los Angeles morning summertime NOx and calculated HC values

Again it should be pointed out that those points show the highest possible

concentrations of NOx and HC Years with less restrictive weather conditions

(for accumulating high primary contaminant levels) would cause lower measured

maximum NOx and HC levels but the calculations would still yield the points

shown Thus we are taking the most pessimistic view

Future Projections

In 1973 we were at about the point labeled 73 and ozone levels were beginshy

ning to drop as expected middot It should be emphasized that ozone values plotted on

thi$ graph are for the chamber only- -not the atmosphere The future path the

points 7 4 and on to 90 represents our estimate of future atmospheric levels of

NO and BC expected if the exhaust emission standards are just met While that X -

is optimistic it is all we really can do since performance of future vehicle models

is unknown We will achieve maximum ozone levels at or below the standard by

about 1980-1985 This will only be true however if cars in compliance with the

California interim standards for HC and NOx continue to be added to the vehicle

population at the normal rate These standards provide the optimum ratio of NO X

to HC necessary to provide the nitric oxide (NO) needed for the reaction that re-

moves from the air both oxidant formed photochemically and oxidant which occurs

as natural background which alone may cause the standard to be exceeded This

ratio is about 112 or 2 parts NOx to 1 part HC

248

The optimum NOxHC ratio is a key element in the APCD strategy but will

require a finite time for its attainment Replacement of older cars by newer ones

equipped to meet the most stringent standards is the only reasonable mechanism

which can change it VMT reduction proposed as a prime strategy by EPA cannot

change this crl(ical ratio which is a basic characteristic of the population at any

given time

Validation of the Districts Control Strategy

Figure 8 compares (1) future chamber oxidant levels based upon the

future maximum concentrations of HC and NOx we expect each year with the

California control program (2) calculated atmospheric concentrations using ~ I

our chamber-to-atmasphere empirical translation and (3) actual measured atmos-f 1l pheric oxidant maxima This clearly sets forth the relationship among these three

factors

The chamber concentrations (lower curve) middotare the lowest values shown

The actual atmospheric data (points connected by heavy dotted and solid lines)

vary considerably from year to year partly because of the vagaries of the weather

In all cases the atmospheric oxidant values are higher than the chamber values

because of the addition of vehicle emissions as the air parcel travels from source

to receptor areas The calculated atmospheric data (thin dashed and solid curves)

are shown to be the highest generally exceeding or equalling the actual measured

data and of course always exceeding the chamber data Thus the model paints

the most pessimistic picture possible It can be seen that by about 19801 1985 atmos -

pheric levels should be at or below the Federal air quality standard of 0 08 ppm oxidant

249

3 Motor Vehicle Exhaust Control is the Only Requirement for Achieving the Oxidant Standard by 1980

We can show that the existing motor vehicle control program has resulted

in a significant reduction of oxidant concentrations in the air

The foregoing material explained the relationship between vehicula~ emis -

sions in source areas and the high oxidant levels measured in effect areas This

relationship is exemplified by the downward trend of oxidant levels in the atmosshy

phere and by the similar year-by-year trends of NO and HC emissions from the X

average motor vehicle A projection of these vehicle emissions factors shows that

the associated maximum oxidant level in the atmosphere will meet the oxidant standard

by about 1980-1985

Figure 9 compares by year the number of days that the oxidant air quality

standard was exceeded in three separate areas with the average NO and HC emissions X

per vehicle mile To comply with the air quality regulations the number of days that

this standard is exceeded must be reduced to one per year

The lines plotted on Figure 9 show that a definite relationship exists between

the emissions from the average motor vehicle and the number of days each year that

the oxidant concentration in the air exceeds the clean air standard

The oxidant trendlines for downtown Los Angeles Pasadena arrl Azusa are

all downward and the slopes are about the same This similarity is logical because

the process that results in the suppression of oxidant accumulation simply has been

displaced from one area to another This was a unique one time situation because

of the increase in NOx between 1966 and 1971 After 1971 all areas are down Thus

l

250

the same conclusion is reached that the oxidantstandard will be met in the 1980s

I whether air quality data or vehicle emissions trends are projected middot~ Ul-

This outlook is based on the APCD s belief that future growth in both the

Los Angeles area and SCAB will not create any locality with a traffic density greater

than any traffic density in the area to date For the past 25 years the area around

downtown Los Angeles has been the area of maximum traffic density and therefore

the emissions source area responsible for the maximum effect area measurements

It is assumed that the traffic density in any future source area will be no

greater than the traffic density in downtown Los Angeles Thus since the

vehicular emissions control program will achieve and maintain the air quality

standards in areas affected by vehicular emissions from downtown Los Angeles it

will also achieve and maintain them for any area of SCAB

Summary Conclusions and Recommendations

In conclusion we have shown that a source and effect area analysis of emisshy

sions and resulting oxidant is a more reasonable and accurate representation of

the Los Angeles area for air quality analysis than gross integration metho9s such

as the big box technique It has been shown that motor vehicles are the major and

almost sole contributor to the primary HC and NOx emissions in the downtown source

area which results in the high oxidant levels in the San Gabriel Valley in fact the

highest in SCAB An air quality model and vehicle emissions control strategy has

been suggested to meet the oxidant standard by mid-1980 s

251

We have shown that

bull Only by adjusting the ratio of NOxHC in the motor vehicle emissions to

permit accumulation of sufficient atmospheric NO to sea venge the normal

atmospheric background oxidant can the standard be attained

bull The APCD strategy which provides for implementation of the present

California interim emissions standards for NOx HC and CO for new

motor vehicles in California beginning with the 1975 model vehicles will

result in compliance with the CO N02 and oxidant air quality standards

by the mid 1980 s and will maintain this compliance until 1990 and

possibly longer

bull The effectiveness of the present California motor vehicle control program

is easily demonstrable using air quality data from several areas in Los

Angeles County 1960-1973

bull To assure achievement and maintenance of the air quality goals as now preshy

dicted there must be periodic assessments of the effectiveness of the

motor vehicle control program followed by corrective actions if necessary

What has been accomplished thus far is significant but much more remains

to be done so that the best possible representation of emissions and resulting air

quality may be available for use in this air basin A much better emission inventory

defining the spatial and temporal distribution of both mobile and stationary sources

is needed Better statbnary source information is needed to evaluate the local

effects of these emissions Further detailed studies are needed to establish the

252

true relationship between emissions data from vehicle test cycles and the actual

operation of vehicles neither the 7-mode nor the CVS procedure provides a true

representation of actual vehicle operation Further tracer studies to assess the

transport and dilution of mobile and stationary source emissions from selected

source areas are also needed

253

1111

IUD

a CC I w gt-

1111

1UO

IUD

I 990

IDJO

1180

1111

IUO

FIGURE I

HYDROCARBONS

STATIONARY SOURCES MOTOR VEHICLES

- --

8 12 II 20 742 2l IS 12 I 4

HUNDREDS

HYDROCARBON EMISSIONS STATIONARY SOURCES IN

OXIDES OF

0

OF TONSDAY

FROM MOTOO VEHICLES AND LOS ANGELES COUNTY

NITROGEN

STATIONARY SOURCES

MOTOR VEHICLES

011111111111111111110111bull1111111

IIIIIIHIIIIIIIIIHIUII

llillL Its rd

l1uu~111111u1111111

2 I O 1 J 3

HUND REDS OF TONSDAY

OXIDES OF NITROGEN EMISSIONS FROM MOTOR VEHICLES ANO STATIONARY SOURCES IN LOS ANGELES COUNTY

illl~ -~--~ i~-=i _J~l ~--~ bull_~L- I ~~~-~~--Z ~

6

6S-66 ox

ICS ~A~1 M

i ssmuwmmgt

bullI

e COROyent_

64 ~ IDB RIVERS~

ORAJfD

-

t t 10 miles

bullmiddotsame Avg Cone Both Years

Pigare 2

YEAR OP HIGHEST OXlDANI CONCENTRATIONS

Highest Average of Daily -Maiimum One-Hour Concentrations

During July August amp September 1963-1972

bullLj

I

64

70 s11 3RlU)U0

70

--__ 69bull

N V +=

middot Source Air Resources Board

-200o

t t 10 adlea

tDS ampIJtsect

-1~

-1611ASampXllmiddot bull - bull -z----~------

I ldmmprwJ

IIVERSIDI

~ - 70

OampY -1 U 70 bull L

I

N V1 V

middot-i___

-----------------------------------------------------------i----------------------------

Figure 3

CHANGE OP OXIDANT CONCENTRATIONS

Percent Change from the Highest Three-Year Average to the 1970-72 Average

Of Daily Maximum One-Hour Con~entrationa for JulY August amp September

Source Air Resources Board

256

FIGURE 4 TYPICAL FLOW OF POLLUTED Am PARCEIS CIUGINATING AT DIFFERENT LOCATIONS IN THE LOS ARE~S BASIN - STARTIOO 0900 PST

l I

OAT

TRAJECTORY SUWMATIOl4

----- SMOG ~AVS

I

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullNONbullSlfOG DAYS

ISTARTING Tl~ cgxpsy

~ HAW

(CA

257

FiGURE 5 ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AND OXIDANT IN DOWlflC1N LOS AIDELES (SOURCE AREA) AND PASADENA (EFFECT AREA) 1

1960-1972

LO CARBON MONOXIDE

30

Pasadena

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullbullbullbullbull Downtown Los Angeles

20

10

o_______________________________

OXIDANT

)

2 Down~ Los Angeles

1

o________________________ 1960 1962 196L 1966 1968 1970 1972

YEAR

bullbullbullbullbull

bullbullbullbullbullbullbull

258

FIGURE 6 COMPARISON 01 CALCULATED AND MEASURED ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AN1) OXIDES OF NITROOEN IN DCMNTOWN IDS AIJELES

196o-1972

CARBON MONOXIDE

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ~ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot _-- ---_ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ----middotmiddot-bullw-_~ ---bullbullbull

10

o_______________1111111_____

OXIDES OF NITROGEN25

20

15 bullbullbullbullbullmiddotmiddotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~

1-i 10 middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ---

oS o_______________________

RATIO CONOx

40

50

0 +raquo Cd

p 30

~ 20

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot bullbullbullbullbull middotmiddotmiddotmiddotmiddot-shybullbullbullbullbull 0 u

bullbullbullbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot 10

0 j

ilI 196o 1964 1968 1970 1972 I

YEAR

Measured~D-owntown Los Angeles (90th percentile ofmiddot daily] instantaneous maxima)

Calculated - Aver~ge vehicle emissions - Present control program

259

FIGURE 7

25

t i5

flJ

~ on ~ ~ Q) bO 100 Jo

+gt on z

o5

EFFECT OF CALIFORNIA 1 s AUTO EXHAUST CONTROL ffiOORA M ON MAXIMUM CHAMBER OZONE CONCENTRATION

- PPM

357bullbull

r 76 bull

11 l

30

20

CHAMBER OZONE MAXIMUM

50

10

o___________111111111111______111111111111_____________

0 05 10 15 20 25

Hydrocarbons m-2 (LB-15) - PPM (as Hexane)middot

--

bull bull bull

r--=--~1 ~a==-~ - _~l ~ y--===-- ~~--~-- ~ r---~~

o

o8

~ I

~ 0 H 8 o6 I

c~ ~ 0 z 0 0

8

~ o+ A H gtlto-

02

middoto

Figure 8 Calculated t1ax1mum Levels Instantaneous and Hourly Average

of Atmospheric Oxidant Compared to Measured Los Angeles County Maxima-with Projections to 1990

(California Standards)

~ -Calculated Inst ax ~

f Calculate Max Hr Avg 03

_ bullbull _ _ - i bull

0 bullbull -l bullbull a0Ieasured Inst Lax o3 bull middotmiddotmiddot~bull 0bull _ ____ V ~ ea~ured ~ Hr Avr o3

~~ r---

~ ~ NB r~ima for 197 4 amiddots of 121074--- -_ Chamber Ozone F ~_ _~

- 1L_

~ Federal Primarfo Air ~uality Standard ~6- -UaximumT- our Avera~elr~ppm-------------- --~ ------- -~- -~-- ~

I I I I I I I I I I I I I I I I I N1 O

1960 6i 64 66 ~i middot-o 72 74 76 79 middotso middot92 84 bullg s9 9o

TBAR (end)

0

261 FIGURE -OMPARISON OF ATMOSPHERIC OXIDANT TRENDS WITH AVERAGE NCJx AND

HC EMISSIONS (Grams per Mile from Average Vehicle)

JOO Number of days state oxidant standara wds equalled or exceeded

--- Azusa __ Pasadena ________ Downtown Los Angeles

20

15 u

___ Hydroc_arbons Oxides of Nitrogenbullmiddotmiddotmiddotmiddotmiddotbullbullmiddot 1975 and later-assume middotcalifornia ARB standards

o_ ___________________________11111____

1965 1970 1975middot 198omiddot 198S 1990

139

(Table I) Just how the automc1bile industry selects the emission levels

at which they tune their vehicles has been of great interest The

hydrocarbon and CO levels in certification (with deterioration factors

applied--so this is the effective emissions of the certification vehicles

at the end of 50000 miles) are approximately one-half the California

standards The oxides of nitrogen emissions are approximately two-thirds

of the California standards This safety factor is put in by the automoshy

bile industry to allow for differences between the certification vehicles

and the production vehicles to ensure that they did not get into a situation

of recall of production vehicles which would be very expensive

There appears to have been a great deal of sophistication developed by

the automobile industry in being able to tune their vehicles to specific

emission levels General Motors appears to have done better tuning than

the other manufacturers This leads to the rather interesting result

that a significant number of the 1975 California vehicles meet the 1977

emission standards (Table II) that is approximately 10 of the U S cars

certified for California already meet the 1977 emission standards This

does not mean to say that the industry could immediately put all of their

production into such vehicles and meet the 1977 emission standards because

of a concern about the safety factor for the certification versus producshy

tion vehicles Thirty-four percent of the foreign vehicles certified for

1975 in California meet the 1977 emission standards The 1977 emission

standards are 041 grn hydrocarbon~ 34 gm carbon monoxid~ and 20 gm

oxides of nitrogen This does confirm that the oxidation catalysts are a

more than adequate technology for meeting the 1977 emission standards and

only minor refinements and adjustments to those systems are required to go

ahead with the 1977 emission standards There are some other arguments

against this optimistic viewpoint and Ill deal with those later

140

There is a great uniformity in the deBigns which the U S manufacturshy

ers have selected for the 1975 California vehicles For those of you who

do not live in California about 80 of thl~ vehicles in the rest of the

country will be catalyst equipped General Motors is going with 100

catalysts apparently to realize the fuel economy benefit of their system

which more than pays for the cost of the catalyst system We have the very

interesting situation that the more stringent 1975 emission standards have

not only reduced the emissions of the 1975 vheicles with respect to the

1973-1974 vehicles but have also reduced the cost of operating the car

and have improved fuel economy The idea that emissions control and fuel

economy and economical operation are always one at odds with the other is

simply not true Compared to the previous years vehicles the more

stringent emissions standards of 1975 have brought improvements to fuel

economy because they forced the introduction of more advanced technology

The fuel savings which have been realized produce a net decrease in operashy

tional costs over the lifetime of the car This is not to say that pollution

control doesnt cost something If you were to compare the 1975 vehicle

with a completely uncontrolled vehicle tht~re would indeed be an incremental

cost associated with the 1975 vehicle

The foreign manufacturers have demonstrated a greater variety of

approaches in meeting the 1975 California standards but again they are

producing mostly catalyst equipped vehicles There is a widespread use of

fuel injection by the foreign manufacturers especially the Europeans

apparently because this is the easiest appmiddotroach for them and they realize

that only a fraction of their production comes to the United States

Volkswagen for example apparently has gone to 100 fuel injection on its

air cooled engines to be sold in California Mazda will continue to sell

141

rotary engine vehicles and thereby be the only rotary engine vehicle

manufacturer and marketer in the United States General Motorsgt elimination

of therotary engine stated for reasons of emissions is probably more

influenced by problems with fml economy although the two are a bit

difficult to separate Mazda is meeting the 1975 emissions standards and

in fact can meet the 1977 emission standards It has not solved its fuel

economy difficulties on the 1975 cars they will do better in 1976 All

evidence points to a fuel economy penalty for the rotary engine Nonetheshy

less we do have this option available because of the Japanese Also the

foreign manufacturers are providing us with a small number of diesel

engine cars These are of great interest because of definite fuel economy

advantages The diesel engine vehicles also meet the 1977 emissions

standards right now Also in J975 well 3ee the CVCC engine marketed by

Honda

The costs of the 1975 vehicles over tae lifetime of the vehicle are

definitely lower than the costs of the 197~ vehicles The National Academy

of Sciences estimate averaged over all vehicles is that in comparison to

the 1970 vehicles the lifetime cost of emission control system including

maintenance and fuel economy costs is aboJt $250 per vehicle greater in

1975 than 1970 Since the 1974 vehicles w2re about $500 more expensive

there has been a net saving in going from 1974 to 1975 I think the

conclusion we should draw for 1975 is that the auto industry has done a

pretty good job in meeting these standards This is something which they

said they couldnt do a few years ago something which they said that if

they could do it would be much more expewdve than it has turned out to

be

The same technology can be applied to 1977 models with no technological

difficulty and only slight refinements of the systems The fuel economy

142

penalties as estimated by the National Academy of Sciences are small 3

or less in going to the 1977 standards This estimate does assume further

advancements by the auto industry to improve fuel economy--primarily

improved exhaust gas recirculation systems It is unfortunate that this

issue of fuel economy has become so mixed up with the air pollution question

because the two are only slightly related If one is really concerned about

fuel economy and there isnt too much evidence that the auto industry or

the American public really is too concerned right now there is only one

way to have a drastic effect on fuel economy and that is to decrease the

vehicle weight Until that is done with gains on the order of 50 or

more to worry about 3 or 5 differences in fuel economy related to emission

control systems is simply to focus upon the wrong issue

Now what are the problem areas What remains to be done The

problems certainly arent over with the introduction of the 1975 vehicles

Problem Area Number One Field performance What is going to happen

to these vehicles when they get into actual service Past experience with

the 1971 through 1973 vehicles has been rather poor in that EPA and

California surveillance data show that these vehicles are not meeting the

standards Many of them did not meet the standards when they were new

The situation in general is getting worse at least for CO and hydrocarbons

that is with time the emission levels of CO and hydrocarbons for the 1971 I through 1973 vehicles is degrading There is no in-service experience of

this sort with the 1975 vehicles yet The certification data look quite I promising but the test procedures especially for durability are not ithe same as what occurs in actual use It is generally stated that the

1actual use situation for the catalysts will be more severe than the EPA

test procedure A larger number of cold starts are involved in actual use

than in the EPA test procedure and thermal cycling will probably have an

143

adverse effect on the lifetime of the cata]_yst This is not so obvious

It is also likely that the higher temperature duty cycle in actual use will

improve the performance of the catalyst in that it will help to regenerate

the catalyst through the removal of contaminants as long as one does not

get into an overheat situation The National Academy of Sciences estimate

was that the number of catalyst failures tn the first 50000 miles would

be on the order of about 7 Thats a very difficult number to estimate in

the absence of any real data A 7 failure still leaves a net gain in

emissions control even if nothing is done about this failure This points

to the problem of what happens after 50000 miles The EPA certification

procedure and control program only addresses the first 50000 miles The

second 50000 miles or slightly less for the average car is the responsishy

bility of the states Unfortunately then~ seems to be very little progress

in the area of mandatory inspection and ma-Lntenance--very little thought

being given to whether the replacement ofthe catalyst at 50000 miles

if it has failed is going to be required and how that is going to be

brought about The area of field performance remains a major problem

area one which obviously needs to be monitored as the California Air

Resources Board has been doing in the past but probably even more carefully

because the unknowns are higher with the catalyst systems

Problem Area Number Two Evaporative hydrocarbons from automobiles

It was identified at least 18 months ago that the evaporative emission

control systems are not working that the evaporative emissions are on the

order of 10 times greater than generally thought In the Los Angeles

area cars which are supposed to be under good evaporative emissions

controls are emitting approximately 19 grams per mile of hydrocarbons

through evaporation This apparently has to do with the test procedure used

144

The EPA is pursuing this The California Air Resources Board does have some

consideration going on for this but it appears that the level of activity

in resolving this problem is simply not adequate If we are to go ahead

to 04 of a gram per mile exhaust emissions standards for hydrocarbons

then it just doesnt make sense to let 19 grams per mile equivalent escape

through evaporative sources

Problem Area Number Three What about the secondary effects of the

catalyst control systems Specifically this is the sulfate emissions

problem and I really do not know the answer to that Our appraisal is

that it is not going to be an immediate problem so we can find out what

the problem is in time to solve it The way to solve it now since the

automobile industry is committed to catalysts and it is unreasonable

to expect that they will reverse that technology in any short period of

time is take the sulfur out of the gasoline The cost of removing sulfur

from gasoline is apparently less than one cent per gallon Therefore if

it becomes necessary to be concerned with sulfate emissions the way to

meet the problem is to take the sulfur out of gasoline Obviously sulfate

emissions need to be monitored very carefully to see what happens The

final appraisal is certainly not now available Another secondary effect

of the catalysts is the introduction of significant quantities of platinum

into an environment where it hasnt existed before Not only through

exhaust emissions which appear to be small but also through the disposal

problem of the catalytic reactors Since the quantity of platinum involved

is quite small the argument is sometimes used that platinum does not

represent much of a problem The fact that the amount of platinum in the

catalyst is so small may also mean that its not economical to recover it

This is probably unfortunate because then the disposal of these catalysts

l Jj

145

I becomes important I will not speak to the medical issues because

am not qualified The evidence is that theuro~ platinum will be emitted in a

form which does not enter into biological cycles--but this is no assurance

that it couldnt later be transformed in such a form What is obviously

needed is a very careful monitoring program which hopefully was started

before the catalysts were put into service If it wasnt then it should

be started today

Problem Area Number Four NO control The big problem with NO X X

control is that nobody seems to know or to be willing to establish what

the emission control level should be It is essential that this be tied

down rapidly and that it be fixed for a reiatively long period of time

because the NO level is going to have a VE~ry important ef feet upon the X

development of advanced engine technology The 20 gm level has been

attained in California with some loss of fuel economy through the use of

EGR and it is not unreasonable in our estimation to go to 15 grams per

mile with very little loss in fuel economy To go to 04 gram per mile

with present technology requires the use of one of two catalytic systems

either the reduction catalyst in tandem with the oxidation catalyst or what

is known as the three-way catalyst Both of these systems require technoshy

logical gains The state of development appears to be roughly that of the

oxidation catalyst two years ago The auto industry will probably say

that it is not quite that advanced but that if it were required to go to

04 gram per mile in 1978 that it could be done With the catalyst systems

the fuel economy penalties would not be great in fact the improvement to

the engine which would be required to make the system work would again

probably even allow a slight improvement in fuel economy What the 04

gram per mile NO catalyst system would appear to do however is to X

146

eliminate the possibility of the introduction of stratified charge engines

both the CVCC and the direction injection system and also diesel engines

It is in the context of the advantages of these advanced engines to meet

emission standards with improved fuel economy that one should be very

cautious about the 04 grammile oxides of nitrogen standards for automoshy

biles My own personal opinion is that the number should not be that

stringent that a number of 1 or 15 gm is appropriate Such a level

would require advancements but would not incur great penalties

Other items which I view as problem areas are less technically

involved and therefore require fewer comments

bull Nonregulated pollutants--again thls is a matter of keeping track

of particulates aldehydes hydrocarbon composition to make

certain that important pollutants ire not being overlooked or

that emission control systems are not increasing the output of

some of these pollutants

bull Fuel economy The pressures of fuel economy are going to be used

as arguments against going ahead wlth emissions control Mostly

these two can be resolved simultaneously We should simply ask

the automobile industry to work harder at this

bull Final problem area New fuels Again it does not appear that

the introduction of new fuels will come about as an emissions

control approach but that they may be introduced because of the

changing fuel availability patterns and the energy crisis These

fuels should be watched carefully for their impact upon emissions

This does middotappear to be an area in which a great deal of study is

going on at the present time It is one problem area perhaps in

which the amount of wprk being done is adequate to the problem

which is involved

147

In sunnnary then the appraisal of the 1975 systems is that they are

a big advancement they will be a lot better than most of us thought and

that we should give the automobile industry credit for the job theyve

done in coming up with their emissions control systems

With that boost for the auto industry which Im very unaccustomed

to Ill entertain your questions

-------=-~ ~~~ U- ~a1

~_~a--~-~ -J~ ~ -~r- _ --=~-- -___ja--~ __1~~ ~-~----=

AIR

1-4 FUEL----1

I I ENGINE

I II

_________ EXHAUST SYSTEM I bull EXHAUST

I I I

+ MIXTURE CONTROL COMBUSTION MODIFICATION EXHAUST TREATMENT

FuelAir Metering Ignition Air Jnjection FuelAir Mixing Chamber Geometry Thermal Reactor Fuel Vaporization Spark Timing Oxidation Catalyst Mixture Distribution Staged Combustion Reduction Catalyst Fuel Characteristics Ex tern almiddot Combustion Three Way Catalyst Exhaust Gas Redrculation Particulate Trap

FIGURE 1 Approaches to the Control of Engine Emissions

~ i 00

149

TABLE I

Average Emissions of 1975 Certification Vehicles (As Corrected Using the 50000-Mile Deterioration Factor)

Emissions in gmi Fraction of Standard HC CO NO HC CO NO

Federal 1975 X X

AMC 065 67 25 043 045 080

Chrysler 074 77 25 049 051 082

Ford 081 92 24 054 061 078

GM 083 80 23 055 053 074

Weighted Average 080 82 24 053 055 076

California 1975

AMC 042 49 17 047 054 087

Chrysler 048 61 16 053 067 082

Ford 052 56 13 058 062 067

GM 065 55 16 0 72 061 082

Weighted Average 058 56 16 064 062 078

kWeighted average assumes the following market shares AMC 3 Chrysler 16 Ford 27 and GM 54

150

TABLE II

Total Number of Vehicles Certified for California 1975 Standard and the Number (and percentage) of These Able to Meet

Certain More Stringent Standards

Calif 1975 Federal 1977 Hypothesized Hypothes ized 099020 04J420 049020 093420

i ~

Manufacturer no () no () no () no ()

AMC 16 (100) 1 ( 6) ti ( 38) 3 (19)

Chrysler 21 (100) 2 ( 9) ( 33) 0 ( O)

Ford 26 (100) 4 (15) -middot ( 15) 5 (19)

l GM 46 (100) 1 ( 2) -1 ( 9) 5 (11)

Foreign 62 (100) 21 (34) 3H (61) 28 (45)

1J

f

-l

151

CURRENT STATUS OF ALTERNATIVE AUTOM)BIIE ENGINE TECHNOLCXY

by

Henry K Newhall Project Leader Fuels Division

Chevron Research CanpanyRicbmmd California

I

iH1middot

10 1ntroduction and General Background

I

11 General

The term stratified ct1arge englne has been used for many

years in connection with a variety of unconventional engine

combustion systems Common to nearly all such systems is

the combustion of fuel-air mixtures havlng a significant

gradation or stratification in fuel- concentration within the

engine combustion chamber Henee the term nstratifled charge

Historically the objective of stratified charge engine designs

has been to permit spark ignition engine operation with average

or overall fuel-air ratios lean beyond the ignition limits of

conventional combustion systems The advantages of this type

of operation will be enumerated shortly Attempts at achieving

this objective date back to the first or second decade of this

century 1

More recently the stratified charge engine has been recognized

as a potential means for control of vehicle pollutant emissions

with minimum loss of fuel economy As a consequence the

various stratified charge concepts have been the focus of

renewed interest

152

12 Advantages and Disadvantages of Lean Mixture Operation

Fuel-lean combustion as achieved in a number of the stratified

charge engine designs receiving current attention has both

advantages and disadvantages wnen considered from the comshy

bined standpoints of emissionsmiddot control vehicle performance

and fuel economy

Advantages of lean mixture operation include the following

Excess oxygen contained in lean mixture combustion

gases helps to promote complete oxidation of hydroshy

carbons (HG) and carbon monoxide (CO) both in the

engine cylinder and in the exhaust system

Lean mixture combustion results in reduced peak

engine cycle temperatures and can therefore yield

lowered nitrogen oxide (NOx) emissions

Thermodynamic properties of lean mixture combustion

products are favorable from the standpoint of engine

cycle thermal efficiency (reduced extent cf dissociashy

tion and higher effective specific heats ratio)

Lean mixture operation caG reduce or eliminate the

need for air throttling as a means of engine load

control The consequent reduction in pumping losses

can result in significantly improved part load fuel

economy

153

Disadvantages of lean mixture operation include the following

Relatively low combustion gas temperatures during

the engine cycle expansion and exhaust processes

are inherent i~ lean mixture operation As a conseshy

quence hydrocarbon oxidation reactions are retarded

and unburned hydrocarbon exhaust emissions can be

excessive

Engine modifications aimed at raising exhaust temperashy

i tures for improved HC emissions control (retarded middot~

ignition timing lowered compression ratlo protrtacted combustion) necessarily impair engine fuel economy1 I

1j bull If lean mixture operation is to be maintained over ~

the entire engine load range maximum power output t l and hence vehicle performance are significantly

impaired

Lean mixture exhaust gases are not amenable to treatshy

ment by existing reducing catalysts for NOx emissions

control

Lean mixture combustion if not carefully controlled

can result in formation of undesirable odorant

materials that appear ln significant concentrations

in the engine exhaust Diesel exhaust odor is typical

of this problem and is thought to derive from lean mixshy

ture regions of the combustion chamber

154

Measures required for control of NOx emissions

to low levels (as example EGR) can accentuate

the above HC and odorant emissions problems

Successful developmentmiddotor the several stratified charge

engine designs now receiving serious attention will depend

very much on the balance that can be achieved among the

foregoing favorable and unfavorable features of lean comshy

bustion This balance will of course depend ultimately on

the standards or goals that are set for emissions control

fuel economy vehicle performance and cost Of particular

importance are the relationships between three factors -

UBHC emissions NOx emissions and fuel economy

13 Stratified Charge Engine Concepts

Charge stratification permitting lean mixture operation has

been achieved in a number of ways using differing concepts

and design configurations

Irrespective of the means used for achieving charge stratifishy

cation two distinct types of combustion process can be idenshy

tified One approach involves ignition of a small and

localized quantity of flammable mixture which in turn serves

to ignite a much larger quantity of adjoining or sur~rounding

fuel-lean mixture - too lean for ignition under normal cirshy

cumstances Requisite m1xture stratification has been achieved

155

in several different ways rangiDg from use of fuel injection

djrectly into open combustion chambers to use of dual

combustion chambers divided physically into rich and lean

mixture regions Under most operating conditions the

overall or average fuel-air ratio is fuel-lean and the

advantages enumerated above for lean operation can be realized

A second approach involves timed staging of the combustion

process An initial rich mj_xture stage in which major comshy

bustion reactions are completed is followed by rapid mixing

of rich mixture combustion products with an excess of air

Mixing and the resultant temperature reduction can in

principle occur so rapidly that minimum opportunity for NO

formation exists and as a consequence NOx emissions are

low Sufficient excess air is made available to encourage

complete oxidation of hydrocarbons and CO in the engine

cylinder and exhaust system The staged combustion concept

has been specifically exploited 1n so-called divided-chamber

or large volume prechamber engine designs But lt will be

seen that staging is also inherent to some degree in other

types of stratified charge engines

The foregoing would indicate that stratified charge engines

can be categorized either as lean burn engines or staged

combustion engines In reality the division between conshy

cepts is not so clear cut Many engines encompass features

of both concepts

156

14 Scope of This Report

During the past several years a large number of engine designs

falling into the broad category of stratified charge engines

have been proposed Many of these have been evaluated by comshy

petent organizations and have been found lacking in one or a

number of important areas A much smaller number of stratified

charge engine designs have shown promise for improved emissions

control and fuel economy with acceptable performance durashy

bility and production feasibility These are currently

receiving intensive research andor development efforts by

major organizations - both domestic and foreign

The purpose of this report is not to enumerate and describe the

many variations of stratified charge engine design that have

been proposed in recent years Rather it is intended to focus

on those engines that are receiving serious development efforts

and for which a reasonably Jarge and sound body of experimental

data has evolved It is hoped that this approach will lead to

a reliable appraisal of the potential for stratified charge

engine systems

20 Open-Chamber Stratified Charge Engines

21 General

From the standpoint of mechanical design stratified charge

engines can be conveniently divided into two types open-chamber

and dual-chamber The open-chamber stratjfied charge engine

has a long history of research lnterest Those crigines

157

reaching the most advanced stages of development are probably

the Ford-programmed c~mbustion process (PROC0) 2 3 and Texacos

controlled combustion process (TCCS) 4 5 Both engines employ a

combination of inlet aar swirl and direct timed combustion

chamber fuel injection to achieve a local fuel-rich ignitable

mixture near the point of ignition _For both engines the overshy

all mixture ratio under most operating conditions is fuel lean

Aside from these general design features that are common to

the two engiries details of their respective engine_cycle proshy

cesses are quite different and these differences reflect

strongly in comparisons of engine performance and emissions

characteristics

22 The Ford PROCO Engin~

221 Description

The Ford PROCO engine is an outgrowth of a stratified charge

development program initiated by Ford in the late 1950s The

development objective at that time was an engine having dieselshy

like fuel economy but with performance noise levels and

driveability comparable to those of conventional engines In

the 1960s objectives were broadened to include exhaust

emissions control

A recent developmental version of the PROCO engine is shown in

Figure 2-1 Fuel is injected directly into the combustion chamber

during the compression stroke resulting in vaporjzation and

formation of a rich mixture cloud or kernel in the immediate

158

vicinity of the spark plug(s) A flame initiated in this rich

mixture region propagates outwardly to the increasingly fuelshy

lean regions of the chamber At the same time high air swirl

velocities resulting from special orientation of the air inlet

system help to promote rapid mixing of fuel-rich combustion

products with excess air contained in the lean region Air

swirl is augmented by the squ1sh action of the piston as it

approaches the combustion chamber roof at the end of the comshy

pression stroke The effect of rapid mixing can be viewed as

promoting a second stage of cori1bustion in which rlch mixture

zone products mix with air contained in lean regions Charge

stratification permits operation with very lean fuel-air mixshy

tures with attendent fuel economy and emissj_ons advantages In

addition charge stratification and direct fuel injection pershy

mit use of high compression ratios with gasolines of moderate

octane quality - again giving a substantial fuel economy

advantage

Present engine operation includes enrichment under maximum

power demand conditions to mixture ratios richer than

stoichiometric Performance therefore closely matches

that of conventionally powered vehicles

Nearly all PROCO development plans at the present time include

use of oxidizing catalysts for HC emissions control For a

given HC emissions standard oxidizing catalyts permit use

of leaner air-fuel ratios (lower exhaust temperatures)

1

l

159

together with fuel injection and ignition timing charactershy

istics optimized for improved fuel economy

222 Emissions and Fuel Economy

Figure 2-2 is a plot of PROCO vehicle fuel economy versus NOx

emissions based or1 the Federal CVS-CH test procedure Also

included are corresponding HC and CO emissions levels Only

the most recent test data have been plotted since these are

most representative of current program directions and also

reflect most accurately current emphasis on improved vehicle

fuel economy 6 7 For comparison purposes average fuel

economies for 1974 production vehicles weighing 4500 pounds

and 5000 pounds have been plotted~ (The CVS-C values

reported in Reference 8 have been adjusted by 5 to obtain

estimated CVS-CH values)

Data points to the left on Figure 2-2 at the o4 gmile

NOx level represent efforts to achieve statutory 1977

emissions levels 6 While the NOx target of o4 gmile was

met the requisite use of exhaust gas recirculation (EGR)

resulted in HC emissions above the statutory level

A redefined NOx target of 2 gn1ile has resulted in the recent

data points appearing in the upper right hand region of

Figure 2-2 7 The HC and CO emissions values listed are

without exhaust oxidation catalysts Assuming catalyst middotl

conversion efficiencies of 50-60 at the end of 50000 miles

of operation HC and CO levels will approach but not meet

160

statutory levels It is clear that excellent fuel economies

have been obtained at the indlcated levels of emissions

control - some 40 to 45 improved re1at1ve to 1974 produc-

tj_on vehicle averages for the same weight class

The cross-hatched horizontal band appearing across the upper

part of Figure 2-2 represents the reductions in NOx emissions

achieveble with use of EGR if HC emissions are unrestricted

The statutory 04 gmile level can apparently be achieved

with this engine with little or no loss of fuel economy but

with significant increases in HC emissions The HC increase

is ascribed to the quenching effect of EGR in lean-middotmixture

regions of the combustion chamber

223 Fuel Requirements

Current PROCO engines operated v1ith 11 1 compression ratio

yield a significant fuel economy advantage over conventional

production engines at current compression ratios According

to Ford engineers the PROCO engine at this compression

ratio j_s satisfied by typical fu1J-boi1ing commercial gasoshy

lines of 91 RON rating Conventional engines are limited to

compression ratios of about 81 and possibly less for

operation on similar fuels

Results of preliminary experiments indicate that the PROCO

engine may be less sensitive to fuel volatility than convenshy

tional engines - m1 important ff1ctor in flextb1 llty from the

standpoint of the fuel supplier

161

224 Present Status

Present development objectives are two-fold

Develop calibrations for alternate emissions target

levels carefully defining the fueleconofuy pbtenshy

tial associated with each level of emissions control

Convert engine and auxiliary systems to designs

feasible for high volume production

23 The Texaco TCCS Stratified Charge Engine

231 General Description

Like the Ford PROCO engine Texacos TCCS system involves_

coordinated air swirl and direct combustion chamber fuel

injection to achieve charge stratification Inlet portshy

induced cylinder air swirl rates typically approach ten times

the rotational engine speed A sectional view of the TCCS

combustion chamber is shown in Figure 2-3

Unlike the PROCO engine fuel injection in the TCCS engine

begins very late in the compression stroke - just before th~

desired time of ignition As shown in Figure 2-4 the first

portion of fuel injected is immediately swept by the swirling

air into the spark plug region where ignition occurs and a

flame front is established The continuing stream of injected

fuel mixes with swirling air and is swept into the flame

region In many respects the Texaco process resembles the

162

spray burning typical of dj_esel combustion ~r1th the difshy

ference that ignition is achieved by energy from an elec-

tric spark rather than by high compression temperatures

The Texaco engine like the diesel engine does not have a

significant fuel octane requirement Further use of positive

spark ignition obviates fuel I

cetane requirements character-

istic of diesel engines The resultant flexibility of the

TCCS engine regarding fuel requirements is a si~1ificant

attribute

In contrast to the TCCS system Fords PROCO system employs

relatively early injection vaporization and mixing of fuel

with air The combustion process more closely resembles the

premixed flame propagation typical of conventional gasoline

engines The PROCO engine therefore has a definite fuel

octane requirement and cannot be considered a multifuel

system

The TCCS engine operates with hi__gh compression ratios and

with little or no inlet air throttling except at idle conshy

ditions As a consequence fuel economy is excellent--both

at full load and under part load operating conditions

232 Exhaust Emissions and Fuel Economv

Low exhaust temperatures characteristlc of the TCCS system

have necessitated use of exhaust oxidation catalysts for

control of HC emissions to low lf~Vels A11 recent development

163

programs have therefore included use of exhaust oxidation

catalysts and most of the data reported here r~present tests

with catalysts installed or with engines tuned for use with

catalysts

Figures 2-5 and 2-6 present fuel economy data at several

exhaust emissions levels for two vehicles--a US Army M-151

vehicle with naturally aspirated 4-cylinder TCCS conversion

and a Plymouth Cricket with turbocharged 4-cylinder TCCS

engine 9 10 1urbocharging has been used to advantage to

increase maximum power output Also plotted in these figures

I are average fuel economies for 1974 production vehicles of

similar weight 8

I When optimized for maximum fuel economy the rrccs vehicles

can meet NOx levels of about 2 gmile It should be noted

that these are relatively lightueight vehicles and that

increasing vehicle weight to the 4000-5000 pound level could

result in significantly increased NOx emissions Figur~s 2-5

and 2-6 both show that engine modifications for reduced NOx

levels including retarded combustion timing EGR and increased

exhaust back pressure result in substantial fuel economy

penalties

For the naturally aspirated engine reducing NOx emissions

from the 2 gmile level to O l~ gmile incurred a fuel

economy penalty of 20 Reducing NOx from the tllrbocharged

164

engine from 15 gmile to 04 gmile gave a 25 fuel economy

penalty Fuel economies for both engines appear to decrease

uniformly as NOx emissions are lowered

For the current TCCS systems most of the fuel economy penalty

associated with emissions control can be ascribed to control

of NOx emissions although several of the measures used for

NOx control (retarded cornbusticn timing and increased exhaust

back pressure) also help to reduce HG emissions HC and CO

emissions ari effectively controlled with oxidation catalysts

resulting in relatively minor reductions in engine efficiency

233 TCCS Fuel Reauirements

The TCCS engine is unique among current stratified charge

systems in its multifuel capability Successful operation

with a nuraber of fuels ranging from gasoline to No 2 diesel

Table 2-I

Emissions and Fuel Economy of Turbocharged TCCS Engine-Powered Vehicle 1

Fuel

Emissions gMile 2 Fuel Economy

mng 2HC co NOx

Gasoline

JP-4

100-600

No 2 Diesel

033

026

014

027

104

109

072

J bull l ~

-

061

050

059

060

197

202

213

230

1M-151 vehicle 8 degrees coffibustion retard 16 light load EGR tw0 catalysts (Ref 10)

2 CVS-CH 2750 pounds tnert1a welght

165

l

has been demonstrated Table ~-I lists emissions levels and

fuel economies obtained with a turbocharged TCCS-powered

M-151 vehicle when operated on each of four different fuels 10

These fuels encompass wide ranges in gravity volatjlity

octane number and cetane leve 1 as middotshown in Table 2-II

Table 2-II

Fuel Specifications for TCCS Emissions Tests (Reference 10)

Gravity 0 API Sulfur

OFDistillation~

Gasolj_ne 100-600 JP-4 No 2

Diesel

88 -

86 124 233 342 388

0024 912

-

486 012

110 170 358 544 615

0002 57 356

541 0020

136 230 314 459 505

-middot --

369 0065

390 435 508 562 594

--

lta 9

IBP 10 50 90 EP

TEL gGal Research Octane Cetane No

Generally the emissions levels were little affected by the

wide variations in fuel properties Vehicle fuel economy

varied in proportion to fuel energy content

As stated above the TCCS engine is unique in its multifuel

capability The results of Tables 2-I and 2-II demonshy

strate that the engine has neither 8ign1ficant fuel octane

nor cetane requirements and further that it can tolerate

166

wide variations j_n fuel volati1tty rhe flexibility offered

by this type of system could be of major importance in

future years

234 Durability Performance Production Readiness

Emissions control system durability has been demonstrated by

mileage accumulation tests Ignltion system service is more

severe than for conventional engines due to heterogeneity of

the fuel-air mixture and also to the high compression ratios

involved The ignition system has been the subject of

intensive development and significant progress in system

reliability has been made

A preproduction prototype engine employing the TCCS process is

now being developed by the Hercules Division of White Motors

Corporation under contract to the US Army Tank Automotive

Command Southwest Research Inr)titute will conduct reliability

tests on the White-developed enGines when installed in Military

vehlcles

30 Small Volume Prechambcr Eng1nes (3-Valve Prechamber Engines Jet Ignition Engines Torch Ignition Engines)

31 General

A number of designs achieve charge stratification through

division of the combustion region into two adjacent chambers

The emissions reduction potentiampl for two types of dualshy

chamber engines has been demonstrated F1 rst ~ j n B desJgn

trad1t1on~JJy caJJld the nrreebrnber engine a 2m211 auxil1ary

167

or ignition chamber equipped w1th a spark plug communicates

with the much larger main combustion chamber located in the

space above the piston (Figure 3-1) The prechamber which

typically contains 5-15 of the total combustion volume

is supplied with a small quantity of fuel-rich ignitable

fuel-air mixture while a large quantity of very lean and

normally unignitable mixture is applied to the main chamber

above the piston Expansion of high temperature flame

products from the prechamber leads to ignition and burning

of the lean maj_n chamber fuel-a_r charge Ignitionmiddot and

combustion in the lean main chamber region are promoted both

by the high temperatures of prechamber gases and bythe

mixing that accompanies the jet-like motion of prechamber

products into the main chamber

I jl

I i j

I

Operation with lean overall mixtures tends to limit peak comshy

bustion temperatures thus minimizing the formation of nitric

oxide Further lean mixture combustion products contain

sufficient oxygen for complete oxidation of HC and CO in the

engine cylinder and exhaust system

It should be reemphasized here that a iraditional problem

with lean mixture engines has been low exhaust temperatures

which tend to quench HC oxidation reactions leading to

excessive emissions

Control of HC emissions to low levels requires a retarded or

slowly developing combustion process The consequent extenshy

sion of heat release j nto 1ate porttt)ns of the engtne cycle

168

tends to raise exhaust gas temperatures thus promoting

complete oxidation of hydrocarbons and carbon monoxide

32 Historical Background and Current Status

321 Early Developm9nt Objectives and Engine Def igns

The prechamber stratified charge engine has existed in various

forms for many years Early work by Ricardo 1 indicated that

the engine could perform very efficiently within a limited

range of carefully controlled operating conditions Both

fuel-injected and carbureted prechambcr engines have been

built A fuel-injected design Lnittally conceived by

Brodersen 11 was the subject of extensive study at the

University of Rochester for nearly a decade 12 13 Unforshy

tunately the University of Rochester work was undertaken prior

to widespread recognition of the automobile emissions problem

and as a consequence emission characteristics of the

Brodersen engine were not determined Another prechamber

engine receiving attention in the early 1960s is that conshy

ceived by R M Heintz 14 bull The objectives of this design

were reduced HC emissions incr0ased fuel economy and more

flexible fuel requirements

Experiments with a prechamber engine design called the torch

ignition enginen were reported n the USSR by Nilov 15

and later by Kerimov and Mekhtier 16 This designation

refers to the torchlike jet of hot comhust1on gases issuing

169

from the precombustion chamber upon j_gnj_ tion In a recent

publication 17 Varshaoski et al have presented emissions

data obtained with a torch ignition engine These data show

significant pollutant reductions relative to conventional

engines however their interpretation in terms of requireshy

ments based on the Federal emissions test procedure is not

clear

l

3 2 2 Current DeveloJ)ments

A carbureted middotthree-valve prechamber engine the Honda CVCC

system has received considerable recent attention as a

potential low emissions power plant 18 This system is

illustrated in Figure 3-2 Hondas current design employs a

conventional engine block and piston assembly Only_ the

cylinder head and fuel inlet system differ from current

automotive practice Each cylinder is equipped with a small

precombustion chamber communicating by means of an orifice

with the main combustion chambe situated above the piston lj

ij_ A small inlet valve is located in each precharnber Larger

inlet and exhaust valves typical of conventlonal automotive

practice are located in the main combustion chamber Proper

proportioning of fuel-air mixture between prechamber and

main chamber is achieved by a combination of throttle conshy

trol and appropriate inlet valve timing A relatively slow

and uniform burning process gjvjng rise to elevated combusshy

tion temperatures late in the expansion stroke and during

the exhaust procezs is achieved H1 gh tewperaturr--s in thin

part of the engine cycle ar-e necessary to promote complete

170

oxidation of HC and CO It si1ould be no~ed that these

elevated exhaust temperatures are necessarily obtained at

the expense of a fuel economy penalty

To reduce HC and CO emissions to required levels it has been

necessary for Honda to employ specially designed inlet and

exhaust systems Supply of extremely rich fuel-air mixtures

to the precombustion chambers requires extensive inlet manifold

heating to provide adequate fuel vaporization This is accomshy

plished with a heat exchange system between inlet and exhaust

streams

To promote maximum oxidation of HC and CO in the lean mixture

CVCC engine exhaust gases it has been necessary to conserve

as much exhaust heat as possible and also to increase exhaust

manifold residence time This has been done by using a relashy

tively large exhaust manifold fitted with an internal heat

shield or liner to minimize heat losses In additj_on the

exhaust ports are equipped with thin metallic liners to

minimize loss of heat from exhaust gases to the cylinder

head casting

Engines similar in concept to the Honda CVCC system are under

development by other companies including Ttyota and Nissan

in Japan and General Motors and Fo~d in the United States

Honda presently markets a CVCC-powered vehicle tn tTapan and

plans US introduction in 1975 Othe~ manufactur~rs

includlnr General Motors and Forgtd 1n thr U S havf~ stated

171

that CVCC-type engines could be manufactured for use in limited

numbers of vehicles by as early as 1977 or 1978

33 Emissions and Fuel Economywith CVCC-Type Engines

331 Recent Emissions Test Results

Results of emissions tests with the Honda engine have been very

promising The emissions levels shown in Table 3-I are typical

and demonstate that the Honda engine can meet statutory 1975-1976

HC and CO stindards and can approach the statutory 1976 NOx

standard 19 Of particular importance durability of this

system appears excellent as evidenced by the high mileage

emissions levels reported in Table 3-I Any deterioration of

l emissions after 50000 miles of engine operation was slight

and apparently insignificant

I Table 3-I

Honda Compound Vortex-Controlled Combustion-Powered Vehicle 1 Emissions

Fuel Economy

Emissions 2 mpg gMile 1972

HC 1975 FTP FTPco NOv

210 50000-Mile Car+ No 2034 Low Mileage Car 3 No 3652 018 212 221089

024 065 198 1976 Standards

213175 20o41 34 - -04o411977 Standards 34 - -

1Honda Civic vehicles 2 1975 CVS C-H procedure with 2000-lb inertia weight3Average of five tests aAverage of four tests

172

Recently the EPA has tested a larger vehicle conve~ted to the

Honda system 20 This vehicle a 1973 Chevrolet Impala with

a 350-CID V-8 engine was equipped with cylinder heads and

induction system built by Honda The vehicle met the present

1976 interim Federal emissions standards though NOx levels

were substantially higher than for the much lighter weight

Honda Civic vehicles

Results of development tests conducted by General Motors are

shown in Table 3-II 21 These tests involved a 5000-pound

Chevrolet Impala with stratified charge engine conversion

HC and CO emissions were below 1977 statutory limits while

NOx emissions ranged from 15 to 2 gmile Average CVS-CH

fuel ec9nomy was 112 miles per gallon

Table 3-II

Emissions and Fuel Economy for Chevrolet Impala Strmiddotatified

Charge Engine Conversion (Ref 21)

Test

Exhaust Emlssions

gMile 1 Fuel

Economy mpgHC co NOx

1 2 3 4 5

Average

020 026 020 029 0 18

023

25 29 31 32 28

29

17 15 19 1 6 19

17

108 117 114 109 111

112

1cvs-CH 5000-lb inertia weight

173

I

332 HC Control Has a Significant Impact on Fuel Economy

In Figure 3-3 fuel economy data for several levels of hydroshy

carbon emissions from QVCC-type stratified charge engines

are plotted 22 23 ~ 24 At the 1 gmile HC level stratified

charge engine fuel economy appears better than the average

fuel economy for 1973-74 production vehicles of equivalent

weight Reduction of HC emissions below the 1-gram level

necessitates lowered compression ratios andor retarded

ignition timing with a consequent loss of efficiencymiddot For

the light-weight (2000-pound) vehicles the O~ gmile IIC

emissions standard can be met with a fuel economy of 25 mpg

a level approximately equal to the average of 1973 producshy

tion vehicles in this weight class 8 For heavier cars the

HC emissions versus fuel economy trade-off appears less

favorable A fuel economy penalty of 10 relative to 1974

production vehicles in the 2750-pound weight class is

required to meet the statutory 04 gmile HC level

333 Effect of NOx Emissions Control on Fuel Economy

Data showing the effect of NOx emissions control appear in

Figure 3-~ 22 These data are based on modifications of a Honda

CVCC-powered Civic vehicle (2000-pound test weight) to meet

increasingly stringent NOx standards ranging from 12 gmile

to as low as 03 gmile For all tests HC and CO emissions

are within the statutory 1977 standards

NOx control as shown in Figure 3-4 has been effected by use

of exhaust gas recirculation 1n comb1nation w1th retarded

174

ignj_tion timing It is clear that control of rmx emissions

to levels below l to 1 5 gmile results in stgnificant fuel

economy penalties The penalty increases uniformly as NOx

emissions are reduced ~nd appears to be 25 or more as the

04 gmile NOx level is approached

It should be emphasized that the data of Fisure 3-4 apply

specifically to a 2000-pound vehicle With increased vehicle

weight NOx emissions control becomes more difficult and the

fuel economy penalty more severe The effect of vehicle

weight on NOx emissions is apparent when comparing the data

of Table 3-I for 2000-pound vehicles with that of Table 3-II

for a 5000-pound vehicle While HC and CO emissio~s for the

two vehicles are roughly comparable there is over a factor

of two difference in average NOx emissions

34 Fuel Requirements

To meet present and future US emissions control standards

compression ratio and maximum ignltion advance are limited

by HC emissions control rather than by the octane quality of

existing gasolines CVCC engines tuned to meet 1975 California

emissions standards appear to be easily satisfied with

presently available 91 RON commercial unleaded gasolines

CVCC engines are lead tolerant and have completed emissions

certification test programs using leaded gasolines However

with the low octane requirement of the CVCC engine as noted

above the economic benefits of lead antlknock compoundt ar-euromiddot

not realized

175

It is possible that fuel volatLLity characteristlcs may be of

importance in relation to vaporization within the high

temperature fuel-rich regions of the prechamber cup inlet

port and prechamber iQlet manifold However experimental

data on this question aomiddot not appear to be available at

present

~O Divided-Chamber Staged Combustion Engines (Large-Volume Prechamber Engines Fuel-Injected Blind Prechamber Engines)

41 General

Dual-chamber engines of a type often called divided-chamber

or large-volume prechamber engines employ a two-stage comshy

bustion process Here initial r~ich mixture combustion and

heat release (first stage of combustion) are followed by rapid

dilution of combustion products with relatively low temperature

air (second stage of combustion) The object of this engine

design is to effect the transitjon from overall rich combustion

products to overall lean products with sufficient speed that

time is not available for formation of significant quantities

of NO During the second low temperature lean stage of

combustion oxidation of HC and CO goes to completion

An experimental divided-chamber engine design that has been

built and tested is represented schematically in Figure ~-1 25 26

A dividing orifice (3) separates the primary combustion

chamber (1) from the secondary combustion chamber (2) which

includes the cylinder volume above the piston top A fuel

injector (4) supplies fuel to the primary chamber only

176

Injection timing is arranged such that fuel continuously

mixes with air entering the primary chamber during the

compression stroke At the end of compression as the

piston nears its top center position the primary chamber

contains an ignitable fuel-air mixture while the secondary

chamber adjacent to the piston top contains only air

Following ignition of the primary chamber mixture by a spark

plug (6) located near the dividing orifice high temperature

rich mixture combustion products expand rapidly into and mix

with the relatively cool air contained in the secondary

chamber The resulting dilution of combustion products with

attendant temperature reduction rapidly suppresses formation

of NO At the same time the presence of excess air in the

secondary chamber tends to promote complete oxidation of HC

and CO

42 Exhaust Emissions and Fuel Economy

Results of limited research conducted both by university and

industrial laboratories indicat~ that NOx reductions of as

much as 80-95 relative to conventional engines are possible

with the divided-chamber staged combustion process Typical

experimentally determined NOx emissions levels are presented

in Figure 4-2 27 Here NOx emissions for two different

divided-chamber configurations 8re compared with typical

emissions levels for conventional uncontrolled automobile

engines The volume ratio 8 appearing as a parameter in

Figure 4-2 represents the fraction of total combustion volume

contained in the primary chamber For a values approaching

I

i J_

177

1

05 or lower NOx emissions reach extremely low levels Howshy

ever maximum power output capability for a given engine size

decreases with decreasing 6 values Optimum primary chamber

volume must ultimately_represent a compromise between low

emissions levels and desired maximum power output

HC and particularly CO emissions from the divided-chamber

engine are substantially lower than eonventional engine

levels However further detailed work with combustion

chamber geometries and fuel injection systems will be necesshy

sary to fully evaluate the potential for reduction of these

emissions

i Recent tests by Ford Motor Company show that the large volume

prechamber engine may be capable of better HC emissions conshy

trol and fuel economy than their PROCO engine This is shown

by the laboratory engine test comparison of Table 4-I 19

Table 4-I

Single-Cylinder Low Emissions middot11 ~ _____En____g__~ne __middot _e_s_-_s_____

Engine

NO--X Reduction

Method

Em1ssions g1 hp-Hr

Fuel Economy

Lb1 hp-HrNOv HC- co

PROCO

Divided Chamber

PROCO

Divided Chamber

EGR

None

EGR

None

10 30

10 04

05 ~o

o J_o 75

130

25

l 1i bull 0

33

0377

0378

0383

0377

178

Fuel injection spray characteristics are critical to control

of HC emissions from this type of engine and Fords success

in this regard is probably due in part to use of the already

highly developed PROCO-gasoline injection system Figure 4-3

is a cutaway view of Fords adaptation of a 400-CID V-8 engine

to the divided-chamber system 2 e

Volkswagen (VW) has recently published results of a program

aimed at development of a large volume precharnber engine 29

In the Volkswagen adaptation the primary chamber which comshy

prises about 30 of the total clearance volume is fueled by a

direct timed injection system and auxiliary fuel for high

power output conditions is supplied to the cylinder region by

a carburetor

Table 4-II presents emissions data for both air-cooled and

water-cooled versions of VW s dtvided-middotchamber engine 3 0

Emissions levels while quite low do not meet the ultimate

1978 statutory US standards

179

Table 4-II

Volkswagen Jarge Volume _Jrechamber Er[ Lne Emissions

Exhaust Emissions

_ _gMile 1

___E_n_gi_n_e__t--H_C___c_o__N_O_x____E_ng__i_n_e_S_p_e_c_i_f_i_c_a_tmiddot_1_middoto_n_s__

20 50 09 841 compression ratio Air-Cooled 16-Liter

prechamber volume 28 of total clearance volume conventional exhaust manishyfold direct prechamber fuel injection

20-Liter 10 40 10 91 compression ratio Water-Cooled prechamber volume 28 of

total clearance volume simple exhaust manifold reactor direct prechamber fuel injection

1cvs c-H

Toyota also has experimented wlth ___a large volume prechamber

engine using direct prechamber fuel injection and has

reported emissions levels comparable to those of Table 4-II 31

43 Problem Areas

A number of major problems inherent in the large volume

prechamber engine remain to be 3olved I~ These problems include the following II

Fuel injection spray characteristics are critically

important to achieving acceptable HC emissions

The feasibility of producing asatisfactory injecshy

tion system hasnot been estab1ished

180

Combustion noise due to high turbulence levels and

hence high rates of heat release and pres[-ure rise

in the prechamber can be excessive It has been

shown that the-noise level can be modified through

careful chamber design and combustion event timing

If the engine is operated with prechamber fuel

injection as the sole fuel source maximum engine

power output is limited This might be overcome

by a~xiliary carburetion of the air inlet for maximum

power demand or possibly by turbocharging Either

approach adds to system complexity

The engine is charmiddotaeter1zed by low exhaust temperatures

typical of most lean mixture engines

References

1 Ricardo H R Recent Research Work on the Internal Combustion Engine 11 SAE Journal Vol 10 p 305-336 (1922)

2 Bishop I N and Simko A Society of Automotive Engineers Paper 680041 (1968)

3 Simko A Choma M A and Repco L L Society of Automotive Engineers Paper 720052 (1972)

4 Mitchell E Cobb JM and Frost R A Society of Automotive Engineers Paper 680042 (1968)

5 Mitchell E Alperstein M and Cobb JM Society of Automotive Engineers Paper 720051 (1972)

6 1975-77 Emission Control Program Status Report submitted to EPA by Ford Motor Company November 26 1973

181

if

7 consultant Report on Emissions Control of Engine Systems National Academy of Sciences Committee on Motor Vehicle Emissions Washington DC September 1974

8 Austin T C and Hellman K H Society of Automotive Engineers Paper 730790 (1973)

9 See Ref 7

10 Alperstein M Schafer G H and Villforth F J Iiil SAE Paper 740563 (1974)

11 US Patent No 2615437 and No 2690741 Method of Operating Internal Combustion Engines Neil O Broderson Rochester New York

12 Conta L~ D and Pandeli American Society of Mechanical Engineers Paper 59-SA-25 (1959)

13 Canta L D and Pandeli American Society of Mechanical Engineers Paper 60-WA-314 (1960)

14 US Patent No 2884913 0 Internal Combustion Engine R Mi Heintz i

15 Nilov N A Automobilnaya Promyshlennost No 8 (1958)

l 16 Kerimov N A and Metehtiev R I Automobilnoya Promyshlennost No 1 p8-11 (1967)

17 Varshaoski I L Konev B F and Klatskin V B Automobilnaya Promyshlennost No 4 (1970)

18 An Evaluation of Three Honda Compound Vortex Controlled Combustion (CVCC) Powered Vehicles Report B-11 issued by Test and Evaluation Branch Environmental Protection Agency December 1972

19 Automotive Spark Ignition Engine Emission Control Systems to Meet Requirements of the 1970 Clean Air Amendments report of the Emissions Control Systems Panel to the Committee on Motor Vehicle Emissions National Academy of Sciences May 1973

20 An Evaluation of a 300-CID Compound Vortex Controlled Combustion (CVCC) Powered Chevrolet Impala Report 74-13 DWP issued by Test and Evaluation Branch Environmental Protection Agency October 1973

21 See Ref 7

22 See Ref 7

23 See Ref 7

24 See Ref 7

182

25 Newhall H K and El-Messiri I A Combustion and Flame 14 p 155-158 (1970)

26 Newhall H K and El-Messiri I A Society of Automotive Engineers Transaction Ford 78 Paper 700491 (1970)

27 El-Messiri I A and Newhall H K Proc Intersociety Energy Conversion Engineering Conference p 63 (1971)

28 See Ref 7

29 Decker G and Brandstetter W MTZ Motortechnische Zeitschrift Vol 34 No 10 p 317-322 (1973)

30 See Ref 7

31 See Ref 7

183

Fig 2-1 FORD PROCO ENGINE

l

Ford Proco Engine Fuel Economy and Emissions _ 15 _ f--1

00 +

I ~ x X gt( X _ x A 7- ~ X x~ ~c - l4catalyst Feed u NOx vs ruel Econ with 1 C0-71 CJ) 14 x x Ynn H( RP c tr ir-t irm vltgtZ G I HC - C0-127 _ A txcessve c

13 Approx W EG R

~ C~~r 351 CID 5000 Lb Inertia Weight

Q 21 A L 0 u w II _j

LJ =gt LL

10

35i CD 4500 Lb Inertia Weight

~ 1974 Production Average Fuel Economy

4 soo _b r-r-r-----z~lt_~~---7--_~--r--1r-7-r1--~-rz7-w~~

150 0 0 Lb PU221ufrac122-1 I

LO 20 30

NOx EMISSIONS-GMSMILE (CVS-CH) Revised216174

0

HKN 71074

Fig 2-2

l

~___-~ ~--=---~ ~=---__---~1 f-=-----1__middot-_~J ~-----------1 ~bull-=-=- (-~-~ LJii-ZJj ~ ~~-~ ~~ -__c~~ 1--~~ ~----~--1 ---------s___-c--1 ~~~-~~~bull r~~-~--middot1 ____c__ J~ p- ~

Texaco TCCS Engine

Shrouded Intake Valve

~ Intakemiddot r~ )p__-- Fuel Nozzle Fuel Nozzte Port ~ -- -yen -_~

X f -J J ( ~1 I --- ~ f middotmiddotj_Ja 1(~-~_ frff 1-Cylinderv~ v_ r--L~ I (~~)J ~- Intake 1 - ------L- middotmiddot - middotmiddot -1 H0 ad middot --- - -- 1 Po rt I 1 I ~~ ) ~ ~ ~~~ -A- I ------

- I _ ---_ ~ P1ston-mgt-lt_ffrac12 T_77~~~--1 i- r_-~J N

- ~- i~-L - _ _ - IExhaust - - I ~ - 1-_ r- bullsect ~ ----lt_ ~ I PortJ~bJ lt 7A--7~ ~1 ~j --~ ~ yl ind er

-__~lli- klmiddot ~ro v_t_gt11J1bull Bti Or K__ - middot ~

I t--tL pgt-- Ultmiddot middot- - Spark Plugr- -1 --U2middot- ~-~

LHorizont al Projections of Nozzle and Spark Plug Centerlines

Fig 2-3 i--1 00 U1

---~---~-~ -------c- --~--- 7middot-r---c-- ~- -~~~==---~~~~~- srsr RZIIEF7 11t111-~-----==-----=-~--~-~~---c=rmiddot=

OPEN CHAMBER TYPE STRATI Fl ED CHARGE ENGINE i-shyCj

DIRECTIONAl~Fsw7 Q

NOZZLE P

I

~J~treg lt-_(__(lt-(11

c_-- _7- -

SPARK PLUG_ l 1__- -_ - l --_ ~ ----__ lt_ lt_ -- --

ltlt_I_--- _

~ gt - _____- -- --~ ~-l_- 1_~ -~- ~ ------

~~~ r_I FUEL SPRAY 2 FUEL-AIR MIXING ZONE ~- _ -------

FLAME FRONT AREA 4 COMBUSTION PRODUCTS

TCCS COMBUSTION SYSTEM

Fig 2-4

3

----==-----~ l~~----bulli r-~ ~-----=-- 1 ~~ ~ -~ ~~ ___-_=gt---l p--- --=-=-_-__71-~-~~ 1-0-- --=---=-- 4 L--_-_-~ P--- ~

25

-c u

f

Cl) 24 gt u _

tgt 23a ~

I

gt-~ 220 2 0 u w 21 _J

lJJ gt LL

2

Texaco TCCS Powered Cricket Vehicle

Max Econ Setting gt A L07 HC

141 CID JQf CR 084 CO 2500 Lb Inertia Wgt

50-so Retard_ 0_73 HC

12 co 051 HC ~ 061 HC

085COA 064CO Retard+ ESPRetard+

EGR

036 HC ~ 115 co Retard +ESP+ EGR

04 06 08 10 12 14 16 18 20 NOx EMISSIONS-GMSMILE (CVS-CH) HtltN1110114

I- 00 -JFig 2-5

-~ ~=- ~ - -i______c_J ~-====c= wr=- ~-~ p--w~~~ rr w -

25

-c u

I

(f)

gt u-lt a_

2

gt-I 20

~ 0 z 0 u LLI

_J

w tJ_

15

I- CJ) CJ)

Turbocharged Texaco TCCS Ml51 Vehicle

Max Econ Adjustment_ HC-3J catalyst Feed C0-70

141 CID 10~1 CR 2750 Inertia Weight 8deg Retard ~

~bull HC-3middot2 catalyst Feed ~~ _ C0-64

_ 5deg Retard HC-0 30 8degRetard LowEGV bullco-11 ~bull HC-3middot6 catalyst Feed WIW21

Med EGR C0-67 1974 Production 33 Average Fuel Economy ~

COmiddoti05 (2750Lb)

I

bull HC-035 co- 141 13deg Retard High EGR

04 10 20 NOx EMISSIONS -GMSMILE (CVS-CH) ~~ts~b~~~74

Fig 2-6

189

Fig 3-1

PRECHAMBER TYPE STRATIFIED CHARGE ENGINE

r Inlet

(Fuel-lean Mixture )

I 0 I

Spark -Prechamber (Fuel-rich mixture)

-Main Chamber

1] HON DA CVCC ENGINE CONCEPT

190

Fig 3-2 Honda CVCC Engine

28 -l u

1

UJ 26 -gt u-(9 CL 24 2-

f

gtshy0gt

22 z ~ _)

u w

20 _J

w ~ LL

18

J= ---- 4 --~~-_----a ~~ _-_bull --~~ 1~~1 ltiil~I ~ ~-r~ ~ -~ ~-~ ~J~-iii-1 ~~1 s _-_ __-

Fuel Economy vs HC Emissions for 3-Valve Prechamber Engines

e NOx-14 15 Liter

bull Honda CVCC 2000 LbsNOx - 12 A Datsun NVCCbull15 Liter

bull ~JOx -09 A 2500 Lbs J LL 1ter NOv -15

2750 Lbs -NOx -17

- I AiJOx -12

0 02 04 06 08 LO 0HYDROCARBON EMiSSlmiddotONS - Glv1 I MILE (CVS-CH) I-

Fig 3-3

J--1

1--Fuel Economy vs NOx Emissions IO N

-- for Honda CVCC Powered Vehiclesr 26 u

l VHc-023 U1 gt umiddot 24_-__

(_IJ o_

~ 22 l

gt-5~-0 z 20 C0-200 u A HC-033w I co -3o_j

_A HC-029w 18 J I C0-27 LL

_ HC-025

HC-017 co -2-3

C0-22

0 -- 02 04 06middot 08 10 12 NOx Ef11SSIONS -GlviS MILE (CVS-CH)

Fig 3-4 middot

I

I

i93

J J

Fig 4-1 Divided Chamber Engine

middot(4) Fuel Injector

1

f J

f ff

f

~ Ii

I f

i

I f ] [

~~

0 0 0 0

i ~ I

1jl

194

E Cl 0

C QJ

CJl 0 _

-1-

z

0

Vl (lJ

-0

X 0

-t-J

V1 ro c X

LLI

Fig ~-2

COMPARISON OF CONVENTIONAL AND DIVIDED COMBUSTION CHAMBER NOx EMISSIONS

5000 MBT Ignition Timing Wide Open Ttl rattle

4000 Conventional Charnber

3000

J = fraction of Total Combustion 2000 Volume in Primary Ct1arnber

Divided Chamber 13 = 0 85

1000

Divided Chamber fo = 0 52

05 06 0 7 08 09 10 11

O~erall Fuel-Air Equivalence Ratio

195

196

AIRBORNE SURVEYS IN URBAN AIR BASINS IMPLICATIONS FOR MODEL DEVELOPMENT

by

Donald L Blumenthal Manager of Program Development

Meteorology Research Inc Altadena California 91001

middotI would like to make several points today First ozonemiddotis basically

a regional long-range problem There is a lot of long range ozone transshy

port and this transport is a normal occurrence The second point is that

ozone is stable in the absence of scavengers Junge mentions in his book

that the residence time of ozone in the troposphere is on the order of a

month Third vertical variations in concentration and ventilation rate are i very important in modeling atmospheres such as Los Angeles Layers aloft

are ventilated down to the surface on occasion and surface pollutants are

ventilated up mountain slopes as Jim Edinger has pointed out before and

often ventilated out of the basin in upper winds Fourth the day to day

carry over of pollutants from one day to the next is a very important considshy

eration in the Los Angeles Basin Finally there is a definite background

level of ozone The geophysical literature says its about O 02 to O 03 ppm (

in various parts of the world Weve seen data varying from 003 to 005 ppm

The difference may be due to calibration differences In any case numbers

like 005 are pretty substantial background levels for ozone

I am going to illustrate the points listed above with some data from

Los Angeles Basin The data were collected during a two-year study funded

by the Air Resources Board some of the analyses were funded by EPA The

study examined the three dimensional distribution of pollutants in the Los

Angeles Basin using airborne sampling systems Coinvestigators on the

project were Dr Ted Smith and Warren White of Meteorology Research Inc (MRI)

197

The first slide shows one of the aircraft we used Its a Cessna 205

which had sampling inlets on the side of the aircraft Figure 2 shows the

instrument system on the inside of the aircraft We were measuring nitrogen

oxides ozone scattering coefficient with a nephelometer condensation nuclei

carbon monoxide and meteorological parameters such as temperature humidity

turbulance Altitude and position were also measured

Figure 4 shows that the typical sampling pattern was a series of spirals

from the top of the mixing layer over an airport virtually to ground level

then we would climb up to the next point on the route and spiral down again

We had three routes (A B C Figure 3) that we would fly We had two airshy

craft and we would fly two of these three routes three times a day any

given day that we could The day I will be talking about September 25~ 1973

we flew what was called the Riverside route (C) and the Los Angeles route

(A) The 25th of July 1973 you might remember was the day before the

federal office buildings were closed in the area here because of smog

Figure 5 shows the surface streamlines at 0300 Pacific Standard Time

about 4 oclock in the morning daylight time on July 25 This streamline

analysis points out the morning stagnation conditions which are a very normal

occurrence in the Los Angeles Basin You start out with very light winds

quite variable maybe a slight off shore flow early in the morning On this

particular day this kind of situation extended well into midday The sea

breeze did not really pick up until up around noon When you have this kind

of a situation and a low radiation inversion at night you have a

long period of accumulation of pollutants all over the Basin espt~cialJy

in the prime source area the southwest portion of the Basin

198

I

Figure 6 shows the streamline pattern at 1600--400 cclock in the

afternoon same day sea breezes develop and with them a transport pattern

that carries pollutants up to the northeast and out toward the eastern por-

tion of the Basin This is a very regular pattern which we see day after l middot

day On July 25 1973 it was a little bit exaggerated The sea breeze was

held off for awhile started a bit late and so there was a very long period

of accumulation in the southwest area and then transport across the Basin

Figure 7 is an average streamline pattern at 1600 PacHic Daylight Time

on low inversion days for August 1970 It is included to show that the pattern

shown before is very typical Flow starts in the western portion of the

Basin and goes right across to the eastern portion This is using surface

data There is a very high average wind velocity in Ontario about 13 m iles

per hour and 23 mph in Riverside This is the average for the whole month

of August at 1600 PDT on low inversion days There is a considerable amount

of transport across the Basin starting relatively slowly in the morning and

accelerating in the afternoon

Figure 8 shows a verticle cross section of the scattering coefficient

The darker areas indicate higher levels of particulates Scattering coefficshy

ient is inversely proportional to visibility In the crosshatched area

visibility is less than about 3 miles In plotting altitude versus distance

inland from the coast you have Santa Monica (SMO) on the coast El Monte (EMT)

Pomona (BRA) Rialto (RIA) Redlands (RED) The lower broken line is surface

ground level The heavy dashed line is the base of the subsidence inversion

that occurred on the two days during this episode The middle line is the

base of the marine inversion There is a large area over in the western

portion of the Basin where emissions accumulate for much of the day At

199

midday the sea breeze has just started ventilating the Santa Monica area

The layer between the inversions is a layer aloft which is fairly well separshy

ated from the surface layer Ozone concentrations for instance in the

layer aloft were on the order of 04 05 ppm using the ARB calibration

method Down in the surface layer they were quite a bit lower in the mornshy

ing due to scavenging

Figure 9 shows that by afternoon the sea breeze starts and you get

kind of a clean air front Sea breeze starts ventilating the whole Basin

the stuff that was over in the west is transported eastward and at approxishy

mately Brackett (BRA) at 1700 PDT there is a clean air front The high conshy

centrations that were over Los Angeles earlier are now centered near Upland

(CAB) The numbers shown over CAB are data taken from a vertical profile

spiral over Upland at about 1600 That turns out to be the time when there

was the worst ozone concentration of the day in the Basin and it did occur

at Upland It could well be a result of the very polluted mass from the

western Basin being transported over the Upland area The layer aloft has

been a bit undercut by the sea breeze and some of the polluted mass has been

around possibly as long as the night before There has been very little

transport in the area aloft ozone concentrations are still very high

Figure 10 shows a trajectory analysis of the air arriving at Upland at

1600 since that was the worst time of the day at Upland We developed a

trajectory envelope using surface wind data and winds aloft so the air

arriving at Upland at 1600 started out somewhere back within this envelope

for example at 1130 PDT We did not go earlier than 1130 because the winds

were pretty much light and variable before that The air that arrives at

Upland at 1600 has been over the western portion of the Basin for much of

200

the morning and q~ite a bit of the evening before Thus there is

a very long period of accumulation and then a transport a pulsing effect

where you have pollutants moved across the Basin

Figure 11 is an isopleth map of surface ozone concentrations Again all

data are corrected to agree with the ARB calibration method Again you can

see that for the hours between 1600 and 1700 using surface data the Upland

area has the highest surface ozone concentrations about 063 ppm The western

area has been well ventilated by the sea breezes and it is cleaned out

The transport is actually pretty much perpendicular to the isopleth line

just about like that

Figure 12 is a vertical profile taken over Upland Cable Airportat

roughly the time of maximum ozone concentration 1636 PDT We are plotting

pollutant concentration on the x-axis versus altitude in meters (since it was

done for an EPA report) Surface leveJ at Upland is a little over 400 meters

the Z line is ozone Ozone concentration within the surface mixing layer

is pegged on the instrument at somewhat above 05 ppm Above the surface

mixing layer it drops off considerably and eventually get down to background

The T line is temperature and you ean see the subsidence inversion

on this day is very nicely documented here and provides a very strong trap

in that area The B line is the scattering coefficient inversely proporshy

tional to visibility Within the surface mixing layer visibility is on the

order of 3 miles or less while up above the surface mixing layer just a few

hundred feet difference visibilities get up to 60 or 80 miles The X is

condensation nuclei the measure of the very fine particles below about 010

micron It is a measure of quite fresh emissions If you have a high condenshy

sation nuclei count there are very fresh combustion emissions If you have

I

201

an aged air mass the condensation nuclei coagulate and the count decreases

considerably You can see that there are still some fresh emissions within

this surface layer as well But up above the surface mixing layer all the

pollutant indicators decrease considerably

Figure 13 is the same type of vertical profile taken over El Monte

which is on the western side of the sea breeze front The sea breeze front

has passed El Monte at this time almost 1700 PDT and again there are

distinct differences between the mass below the mixing layer within the sea

breeze front (below 400 meters) the marine inversion (400 to 800 meters) and

the subsidence inversion The subsidence inversion occurs at about 800 meters

and there is an old layer of very polluted stuff aloft The surface concenshy

trations are lower because of the ventilation by the sea breeze Condensashy

tion nuclei count (X line) within the surface layer is quite high There

are still fresh emissions in the El Monte area The 11 Z line is ozone

about 02 ppm within the surface layer (200 m) but it is 05 ppm up above

the surface mixing layer The scattering coefficient (B line) is very

similar it is lower at the surface and increases to a visibility equivalent

of less than 3 miles above the surface mixing layer The condensation nuclei

count is high in the lower portion of this (eg at 600 m) hut decreases conshy

siderably above This portion of the upper layer (600 m) has been around

at least all morning and condensation nuclei have been scattered from the

area The portion of the upper layer below 600 m has probably just recently

been undercut by the sea breeze and there are still some condensation nuclei

left in it

Figure 14 illustrates a different method of looking at the flushing

problems in the Basin We have tried to develop an objective criteria based

on ground level ozone to show the cleansing of the basin using the time of

202

arrival of clean air We determine the time when the ozone concentrations

drop by a factor of two at any given point The 1600 line means that between

1500 and 1700 the ozone concentration at that point dropped a factor of two

This sort of isopleth chart of when the clean air arrives agrees quite well

with the trajectory analyses although the numbers are a little bit behind

the trajectory analyses for the polluted air Figure 14 again shows the

transport process that takes place across the Basin which is ventilated from

west to east At 1900 some of the fresh ocean air finally gets out to

Redlands

In Figure 15 in order to put this whole flux problem into some perspecshy

tive we looked at the numbers the actual amount of ozone flux across the

basin We calculated the mean trajectory from Torrance towards Redlands

using the surface and upper air data We looked at the flux from the western

basin to the eastern basin basically from Los Angeles and Orange Counties to

Riverside and San Bernardino Counties This is a calculation made at 1700 PDT

We used the winds aloft from Chino as well as the vertical profiles taken at

Pomona and Corona Averaging the ozone concentration throughout the mixing

layer and multiplying by an average wind speed we arrive at a number of 185

metric tons per hour being transported directly from one side of the Basin

to the other If you look at this in terms of actual concentration in the

eastern Basin and assume that the flow was constant for about an hour it

is eno_ugh to fill up the box shown in Figure 15 to 025 ppm ozone which

exceeds the air quality standard by a factor of three (using the ARB calibrashy

tion method) Thus there is a very significant transport of ozone or ozone

precursors from one portion of the Basin to the other side of the Basin One

thing to mention though is that the concentration would not be kept up on a

203

steady state basis because the transport is a result of the pulsing effect

I Illentioned earlier There is a lot of accumulati6n in the western Basin

and these accumulated pollutants are then transported across the Basin This

kind of transport did take place in a couple hours because we also have

measurements from 1500 PDT which give us similar flux numbers

Figure 16 is a trajectory envelope similar to Figure 10 calculated for

Upland at 1600 for the air arriving at Redlands about 600 oclock in the

afternoon I wanted to include this trajectory envelope to show that the

problem is not really simple You cannot say that the air at Redlands came

from Long Beach per se The air at Redlands if you look at the whole

envelope of possible trajectories using upper air data as well as surface

data could have come from anywhere between Downtown Los Angeles and over

the Pacific Ocean south of Long Beach

Another thing to recognize is that the wind actually changes direction

slightly as you go up and down through the mixing layer and the mixing layer

is exactly what it implies There is mixing within the mixing layer so if

you begin with a parcel of air near the surface this parcel may move to the

top of the mixing layer and go one direction for awhile it then may go back

down to the bottom of the mixing layer and move in another direction for

awhile The ratio of the length scales indicata3mixing layer depths of 1500

or 2000 ft and distances on the order of 70 miles This makes it very

difficult for tetroons to follow an air trajectory because they do not go

up and down They stay at one altitude and in one wind regime and yet the

wind regimes are different at different altitudes and the air is continually

mixed up and down through this layer You can often see this on time lapse

photographs

204

The question is where does the pollutant mass go after Redlands Figure

17 is a repeat of Jim Pitts slide from yesterday and it is data for the

same day that we did our analysis It shows the ozone peaks starting at

Pomona and Riverside and on July 25 1973 eventually getting out to Palm

Springs so there is quite a bit of long-range transport The ozone is

stable at 8 00 or 9 00 oclock at night There still are ozone concenshy

trations of 02 ppm it hasnt dissipated even at the surface Ozone does

dilute as the mass moves Other calculations we did were integrations

through the mixing layer of various pollutants such as ozone and CO along

with trajectories that we measured Th~se integrations show just what the

ground data show in Figure 17 The concentrations increase through the western

portion of the Basin and then show a decrease through the eastern portion

of the Basin CO tends to decrease faster than the ozone indicating a

continued production of ozone further east

Figure 18 is a streamline chart on a larger area map for the 16th of

August 1973 It shows the typical streamline patterns that occur for

ventilation from the Basin By mid-afternoon there is flow out through the

major passes to the north and towards Palm Springs (PSP) On this particushy

lar day we had data from Arrowhead showing that the air mass from the Basin

does indeed get up there

Figure 19 shows a vertical profile over Arrowhead early in the morning

16 August 1973 at a time when there was a north wind Ozone level was

about 005 ppm the scattering coefficient was quite low on the order of

probably 60 miles visibility or so Figure 20 is a vertical profile again

over Arrowhead late that afternoon when the winds had switched There is a

flow from the Los Angeles Basin into the Arrowhead area thus one sees a

205

vertical profile that shows a distinct increase near the surface in both the

ozone and the scattering coefficient and in the condensation nuclei Ahove

that you have fairly clean air The top of the polluted level is just about

the top of the mixing level over the Basin

I want to leave the transport now and discuss the complicated vertical

structure that can occur If you want to try to model something try this

one for instance Figure 21 is a vertical profile over Brackett Airport

Pomona about 830 in the morning on 26 July 1973 which is the day after

the episode shown earlier A bit of interpretation shows how complicated

th is can be If one looks at the temperature profile it would be very

difficult to pick out a mixing layer theres a little inversion here another

inversion there several more up here After looking at hundreds of these

profiles though you can start interpreting them What is happening is that

there is a surface mixing layer at about 500 m In this layer there is a

high condensation nuclei (X line) count due to morning traffic The San

Bernardino freeway is quite close to Brackett there is a relatively high

nitrogen oxide count about 02 ppm and the b-scat is fairly high Ozone (Z)

within the surface layer however at this time is quite low The layer beshy

tween 500 m and 700 rn turns out to be the Fontana complex plume Note the

very high b-scat level it is below 3 miles visibility the plume is very

visible especially at this time of the morning when it is fairly stab]e

There is a high nitrogen oxide level (800 m) a high condensation nuclei

level and again a deficit of ozone Above this layer (800 m) you have stuff

that has been left all night very low condensation nuclei indicating a very

aged air mass ozone concentrations about 016 ppm b-scat of about 04 It

has been around all night and not yet had a chance to mix down within the

206

surface layer In fact one good way of determining the surface mixing layer

early in the morning and at night is to look for the ozone deficit Another

thing to mention is that wind reversals occurred for each of these three

layers The winds were fairly light and westerly at the surface slightly

easterly in the 500 m 700 m layer and westerly above 800 m There is a

complicated situation early in the morning but the main problem is that by

the middle of the day there is good surface heating and the pollutants have

all been entrained and mixed down to the ground so in order to modeI what

happens on the second or third day of an episode you must be able to look

at both old pollutants as well as fresh emissions And you need to account

r for ozone that is actually transported down to the surface from layers aloft l

The next slide is a photograph (not included) which is another e xample

of some layers aloft This is due to upslope flow as explained by Jim Edinger

in his publications The mountains are heated during the day in turn heating

the air and making it buoyant there is upslope flow to a point where the

heating cannot overcome the subsidence inversion and the stuff comes right

out from the mountains and spreads out over the Basin The pollutants can

stay up there if the winds aloft are very light and on the subsequent day

will he re-entrained to the surface On the other hand if there are winds

aloft different from those in the surface mixing layer or the wind velocity

aloft is high there can be a very substantial ventilation process for the

Basin Pollutants can be ventilated up the slope and blown away in the upper

winds In the case of the entire July 25th episode winds aloft were quite

light and these upper layers remained

Figure 22 is a vertical profile of one of those upslope flow conditions

in the same location shown in the photograph but on a different day Again

207

there is a relatively high surface concentration of about 03 ppm of ozone

(Z line) a layer of clean air between 900 to 1100 m and then high concenshy

trations of ozone again above 1100 m It has gone up the slopes of the

mountains and then come back out Concentrations in the 1100 to 1300 m area

are just slightly lower than they were at 600 to 800 m area Notice however

that the condensation nuclei count (X line) is quite a bit lower mainly

because the stuff is much more aged above the 1000 m level than it is down

below 900 m

Figure 23 shows the stability of ozone the fact that it can stay around

all night long This is a vertical profile taken over Riverside about 2200

PDT 1000 oclock at night Above the surface mixing layer (600 m) there

are ozone concentrations of about 0 15 ppm (Z line) Within the surface

mixing layer (below 500 m) ozone is completely scavenged decreasing to

zero The nitrogen oxides within this surface layer are being contained and

are around 01 ppm from fresh emissions that occurred during the evening

Condensation nuclei near the surface are very high The temperature profile

is very stable You have a surface based radiation inversion which is a

little strange looking for a radiation inversion~ nevertheless it is quite

stable There is a definite restriction of the mixing--a very difficult

time getting air from below 500 m to above 500 m The ozone that exists in

the 700 m range is in air where the reactions have virtually gone to compleshy

tion and is very stable All the profiles on this night changed very little

the ozone peak stays there High concentrations stay around

Figure 24 is a cross section across theurban plume of the City of St

Louis I wanted to show that this occurrence is not limited to Los Angeles

We have seen ozone formation and transport in other urban plumes These data

l

208

were taken during a project sponsored by EPA in conjunction with R Husar of

Washington University and William Wilson of EPA The dark line on this is

the ozone concentration across the urban plume perpendicular to plume The

dashed line is the scattering coefficient The power plant plume is parallel

to the urban plume The data on the left were taken 35 kilometers down wind

about 1100 oclock in the morning The ozone concentration increases slightly

to 005 ppm in the urban plume there is a deficit of o in the power plant plume3

In the same urban plume same conditions 1500 CDT two hours later further

downwind there has been substantial increase in the ozone in the urban plume

itself The b-scat is very similar to what it was before but the ozone is

now increased quite substantially except in the power plant plume where

there is a strong deficit of ozone due to scavenging by nitrogen oxides So

the formation and transport of ozone and ozone precursors in urban plumes is

a regular occurrence that happens in more places than Los Angeles and as Bob

Neligan showed this morning it can happen over quite a bit longer distances

than we are showing here

To summarize the conclusions as they affect model development first

once ozone is formed in the absence of scavengers ozone is a very stable

compound It remains for long periods of time It can he transported for

very long distances Ozone is a regional problem which cannot be controlled

on a local basis To have effective ozone control middotone must have a regional

control strategy and probably regional type air pollution districts

A second conclusion is that the vertical distribution of pollutants can

be highly complex and models have to include more than just a simple wellshy

mixed surface layer

209

A third conclusion is that layers aloft can persist over night and can

be re-entrained within the surface mixing layer on subsequent days models

should be able to account for old pollution as well as fresh emissions Also

pollutant accumulation and transport can have distinct diurnal patterns that

are strongly dependent on the meteorology Models should be time dependent

and should start at the beginning of the accumulation period In other words

models ought to be able to run for 24 or 48 hours if they have to In this

case in Los Angeles there is often an accumulation of pollutants which starts

in one portion of the Basin at midnight and continues through the next mornshy

ing even before it starts to be transported

As far as recommendations go in many areas a lot of ambient data has

been collected and in some cases the data are actually ahead of some of the

models so I think a research program is needed in developing models that

will account for this vertical structure and the day to day carry over and

the models need to be extended to cover longer distances In addition more

smog chamber work is going to be needed in looking at the effects of carry

over and mixing old pollutants with fresh emissions How people go about

this I leave to the modelers and the smog chamber people They know more

about that than I do

I

210

I

~ INVERTER

AUDIO TAPE

MONIT0R

MONITOR OBSERVER SEAT

MON ITOR

NEPHELOMETFR FLfCTRONICS

j DIGITAL DATA LOGGER

CONDENSATION

VOR DME NEPHELOMETER TUBE

JUNCTION middoteox ASSORTED POWER

AIRBORNE

TEMPERATURE TURBULENCE

middot HUMIDITY

ALTITUDE BOX

__

middotE=-middot RECORDER ----r----------

NUCLEI KJNITOR

CONVERTER

SUPPLIES

INSTRUMENT PACKAGE (

lCO

03

Ndeg

-

-----NEPHELOMETER

BLOWER

Figure 2 Instrumentation Layout for Cessna 205

211

bullubullbullbullbull

Figure 3 Airborne Sampling Routes in the Los Angeles Basin

Figure 4 Vertie al Profile Flight Path

~-~ r~i ~~1 -- ~ ~ ~2-1~ LJ-----~ r~~ ~~ t~~--l

~ ALM l

0 RIA

ec 8v

M

~ Afo

-o

M 0

~IV

ltgt

IN J--1 N

SCALE II fi M I j_ ES 0 3 4 5 =-JSEJ--J~ _middot ~middot- - =- =

I

~

M

N~J

Figure 5 SURFACE STREAMLINE ANALYSIS - 0300 PST 25 July 1973

~~~ ~~-- cp1FJ=D -~~

~ 1

~ ~ 8c

8v

~25

PACIFIC OCEAN

diams Tt

0

9 I 4 5 10 I- m p H - -middotmiddot u 4H__8 middott_

D i6 J4 k W~D SPED llaquotl SNA NJ ~1

SCALE m ICtt84bullmh R v1s1a1L1n (mil 6 ~ CONTOURS REPRESENT

-- 10ml 16km (~() bull ~ ) ~ - 000 ft 3C5

Figure 6 S_cJRFACE WIND STREAMLINES - l 600 PDT JULY 2 S I 8 7 3

l - ~---i ~-=-___-----c---it~~-~~ r----=------1 ~-~~--cpc---_t__A --~ ---llil

~_ - ~-l-cL

34bull vi~-dff

bullbullbullbull bull ~ bull -1 bullbull - -_- L bull-J bull ~bull-bull-ii------~ bullmiddot r_ -~- ~ bullI ~_ bull bull bullbull bull I bull _ - bull -~-~ middotbullbullbull ~ ~ --middot -~- bullbullmiddot ~v ) ~ - -__rl v middotmiddot - 1- ~ -- middot middotmiddot - 1 91 frac12 - ~- lt( middot K i - middot bull - middot - bullmiddot~~-~lJ) obullmiddot~ ~-f- _J_~---Smiddot~middot-~----~~~---gt_middotfY-_middot-~middot --middot-~-~----fJ_middot- middotmiddotbullmiddot u-- bullmiddot ~ ~ -middot L~ bullbull

~bullbullbullbull bullbull l_bull bull bullbullbull EW bullbullbullbull-- ~ __bull f f - middotbull - J middot f bull S bull I ~ -r --

_ bullbull bull- _ bullbull-bull ~ ~ bull bull bull bull I bull bull bull bull bull bull gt - bull middotbulliJ -bull I bull bull _1 bullJ C-- ~-middot _ bull bullbull bullbull bull _____ ~ ~ l _ middot q bull 1 -middot middot ~~middot middot middotbull_ J ~gt - J bull-bullbullbullbull ) _ -middotmiddotbullmiddot J ~middotmiddotmiddot -bullmiddotbull fmiddot 7middot _middotmiddotmiddot bullmiddot(middot Ii~ middotmiddot~_--~middot 1middot__middotmiddotmiddotmiddot middot- gt_ -~ -~-- Imiddotbullmiddotbullbull_ -

- ()_I (w--_ bullbull__(i- bullOmiddotbull bull middotbull -bull-_jlJ middot bull lt 1(middot t gt bull - ~ rbull I bull middot middot- bull41-bull l~r v-middot~- middot middot middot bull_ - middotmiddot ~Jtj (middot~ ~middoti middot middot middot middot middot ~- ~ -tmiddot~ I - middot middot_- ~ - -~ middot_ _- ~bull - _ ~) i bull bullbull bull- middot_ bull middotbull __ ( bull 11bull bull ~ampmiddot ~ l bull bullQ bull - -1 bull JY1 bullbull ~ or bullbullbullbullbull bullbull-bullbull _ ~ - bull bull-bullbullbull middotimiddot middot 91 bull t bull - - tfaw lJ--r- bull bull _ bull middot- - l

f ~~middot--~ middotmiddott ~ltrgtmiddotmiddotJmiddot_bull - ~ - __ middot- LOS ANGELES BASIN - LOW LEVEL -__ jmiddot l-gt bull - bull J iI bullbull bull bull bull _ bullbull _ Jmiddot middotL~_1 middot middot bullbullmiddot ( C middot INVERSION MEAN WIND FLOW _ J

lmiddot - f bullbullbull~ - f 1bullbullbull _ ~)- bull middot- _---_- 7f-~bull~ REGIME _F_~ AUG_UST_~ ~600 P~--- l

-__L-~bull --ncmiddotbull~~-j--bullmiddot~bullmiddot_-bull _fJibullmiddot Imiddotmiddotmiddot-bullmiddot- bullbull ~ bullbullbullbullmiddotmiddotmiddot~middotbull ___ bullJ_ _middot~0))deg bullt t1yensmiddotmiddot ( middot middotmiddot middot middot ~ middot lbullbull1 t_c0 bull -middot---l lt ~middot~- deg bullbull --= bull bull bull I bull bull bull bull bull bull bull bull bullbull _~bull b ---) bullbull-bull ) bulll middotbull middot1middot ) bullT --f bull I bullr ~bullbullbull bullbullbull( - -bull-- ( -o-----_i bull-~-l- i l l J l~-- c middotmiddot _--1 ---I middotmiddot ---- ~bull-bull bulli_ ALT Elmiddot_ bullbullbullbull _- ~~middot bull middot bullbull _ bull middotbull bull~ ~bull middot bull -middot bull--ua_-- bullbull bull

-- 01--- middot_ -middotmiddot hmiddotmiddot __1 ~-- ~ fi~~- ___ - ____ _ -middotmiddotmiddotmiddot~ ) -~-J bull bullbull bull bull 0 uc- -l ~- ~ IT ~~ll ~ bull -middot -middotmiddotmiddotmiddotbullCCAmiddotmiddotmiddot-middot middot bullbullbullbullbull

) i- 5 ~-==-- __ __ - bullbullbull _ bull~ bullbull _ bull bull l T[h4 ------ - 0

i17- o~-lt -(i-_~ 11t~bull-omiddot ~- -- 13 0l~~~bull bull Jbullbull~bull ~ ~bullbullbull bull bull x- middot~---=-~~ -=aJlll8 bull Ibull bull ~~ middotbull rbull~---bull1-~middot-middot _ middotmiddotmiddot-middot 1 0 ~vrbullmiddot ~middot ~ (J~-middot _-_~) ) ~ bull middot

l middot _ POMA_ middot =~~~----ti~ jmiddotmiddotmiddot - middot bull [j

~A ii J0 Vfli middot bullHud __=bt_ bull

CImiddot ~-- ~- middot)middot PACIFIC OCEAN I middot ---- middotmiddot ~

__ middot__ ~ - _ 23~1 middotbull 8 4 1 middot middot ~ middot middot gt ~~- l ~ u middot

bull - bull- I ~------ --1~ i middotmiddotmiddot - n _c-118 1130

~ n r -t ~~gt25) cmiddotbullmiddot

~--lt- ~~- 1-~__( i - t ~ _ middot 0 igt(_J

11bull bull11 ~~ -~[ ~i~gt----gtmiddotmiddotmiddotmiddot--~l_ ~~ ELEVATION

IN FEET bullbull (_- middot bullbullbull -middot middotbull middot ~~ middotmiddot bulltbullbull _ffmiddotmiddot-middot v I )tylt~ -~bullbull1bullbullrbullbull ~-lt -~ ( I~

600~ A0 Cv(A (1829 m AND OVER) deg )_ rJ__~7 middot middot ~--middot L==1 _J bullbullbull - bull -middot~-- rgt ~ middot(Zmiddot- middotbullmiddot middot

Z~C)-tGOO (762 middot 1829 m) 9-N4 __J (r -- lf _ bull bullgt-~~~ ~ _ w _ _ I (1 bullmiddot( middot1 middot -----~~~- middot L-bullmiddotbullW bullbullbull3 STA r I0-4 lODEL

100i -2soo (305~762m) -- Ow - -~1_- i ~~--- bull v~rvt ~~ -middot )) ~--

II gt J (-_bullmiddot middot~ l bull bull tr 1 )~ gt ) bullbull-_bullI-middot -middot bull~0 3 Mor nuq1ENr Wlbull~O JIAtCTIO-bull bull - lbull C---gt bullbull )t bullbull -( I bullf I - 20-00 (61 bull 305 ml J( Jloa xxE- -bullbull00 - -- middot1

0-200 (0middot61m) Wl)7 AVBt~gpound ) bullmiddot-iiNL~ middotntmiddot_ 1 iJJlt( _1J- ~ VAq IA9 IL ITY 0 ~ 10 15 ltS lHPtl

~--_ bull bull I bullbullbullbull 1 ~) J)J ~ bull Is bullmiddot bullbullbullbullbull ~ 3 V IS A VAqlABLE OIR~CTIO- 0 8 16 2-4 km

(SPEEDS SHOWN IN mph 10 mphbull 16 h1llr) -- middot ktr~~~ lt~ ) -middot-SCALE

Figure 7 LOS ANGELES BASIN MEAN WIND FLOW FOR DAYS WITH LOW LEVEL INVERSIONS DURING AUGUST I 970 AT 1600 PDT

-~~~~-=======~middot~-~======~middot--=-==-===gt=---==____________=== ~--=-J~==-- -=-ee----=-------

500

N f-- V

- - - SUBSIDENCE INVERSION

----MARINE INVERSION

bullbull-bull-bullbullGROUND LEVEL

x WINOS ALOFT (kmht)

WESTERN middoteASIN EASTERN BASIN

LAX WINOS EMT IHOS I I

CNO WIHOS

s_ 04 13 1500- 05 02 08

I 06 069 middot

11-1--

04 04 i ~4

06 ~ 4--

I 2

1000 n1 1005 -_E

lll --1 lJ -----------~----

~11

--=i-+- c -- 9 _____ - ~ C

lt I

I 6 4 _r 31

I 6 5 ~~ ~_ bull ---middot- 64 ~li- - middot- bullc - middot-----------

10

SMO (1347 PDT)

EMT (1246 PDT)

BRA CAB (1459 PDT) (1335 PDT

RIA (1349 PDT)

RED (1406PDT)

Figure 8 VERTICAL CROSS-SECTION OF bscat FOR lvflDDAY

T t 10-4 -1)(l n1 s are m

JULY 25 1973

- c - -~

~--~ JC_-_1- ~1pi~ oamp----~JilliiiM~f~-U~ -~--- --~~~ ~~~

-=--~

-E-- O

_ lt

1500 05

06 15

09 __~

1000 --

~- ~---middotmiddot 29

500

oJ11

__a

07

I 07 I

I I

I

09

I

I

I

I 7 ---

11 -----

~ ----- 6

---------------lt- -~middot4 --------

20

29

-

10 10

11 07 08 08

10

08

~8 _____ Y-

N

- - bull SUBSIDENCE INVERSION

----MARINE INVERSION

-bull-bull-bull GROUND LEVEL

WES TERN BASIN EASTERN BASIN x WINOS ALOFT (kmhr)

t t

CNO WINOSILA WllltOS poundMT WINOS

SMO LA EMT BRA CAB RIA RED O (1736 PDT) (1655 PDT) (1707 PDT) (163 PDT) (1823PDT) 1805 PDT)

Figure 9 VERTICAL CROSS-SECTION OF b FOR AFTERlOON OF JULY 25 1973 scat

T bull 1o- 4 - l )(units are m

__~~---iii~~- ~- ~~______ ~~- --~~J---=-~ ~

N ~ -J

PACIFiC OCEAN

0 5 10 15 1111

E 8 4 I 0 8 6 2 ~ bull

SCALE

dh Mes

CONTOURS REPRESENT - 000 ft 305 m

0 SNA

c8s

ec 8v

amp R~b

Figure 10 TRAJECTORY ENVELOPE FOR AIR ARRI1G AT CABLE AIRPORT (CPLAD) 1600 PDT JULY 25 1973

~-~

q_- ~ ------1 H~~~ -~~--~ ___---___--i- __r-=-1--===12---1 ~ ___r~ _==---_ - ~- f~~ ~-- - -5plusmn-at -~middot~

ll~~r1 ri

40

ec 8v

-1 I

amp

0 HQ_

7 0

CAP LAAR) O

VER

PACIFIC OCEAN ~ 0

RLA

4

WHqR d

diams

H ~I

I l

0 COMA

3

L~

LAH

Fa_ f ~~

S ~ LA APCD VALUES ADJUSTED TO AGREE ~

lt

0

5 10 15 mi0 WITH ARB CALIBRATIONE-j I I CONTOURS REPRESENT NZJ ~ 0 a SCALE 6 24 km - 1000 ft 305m COS v~J

______ J 10 ro ( igtf t-i

coFigure 11 SURFACE OZONE CONCENTRATIONS (pphm) I 600- I 700 PDT JULY 25 1973 ~

~~~~~C-~ ------=--~-__-~--~~~=--- ----=--~

N

-E

D1600----------------------------- 1--

14001-------------------------------

1200

I Ground Elevation

1000 middot 445 m ] lampJ

sect ~~ 7 ) SURFACE i6~ 800 MIXED LAYER

~

~ [ J ~ ~ I OZONE CONCENTRATIONS~ 600 E E GREATER THAN

( 50 pohm

400 I C H T Z GROUND LEVEL

200

I PUUloCETER UNIT SnbullBOL

NOc N0 0 ppm01 02 03 04 05 03 z

40 --~45~~ 50 co pm C0 5 10 15 20 25 30 35 I I I I I I I I I I TEIIPERATURE oc T-5 b 5 10 15 20 25 30 35 40 45

I-- 100 RELATIVE HUlillOITY H0 10 20 30 40 50 60 70 60 90 b1eot IOmiddotm- 1 8

CN cmmiddot3 1 IO X0 I 2 3 4 ~ 6 7 8 9 10 URBJLENC-C cm213ue- E

Figure 12 VERTICAL PROFILE OVER CABLE (CAB) J CLY 2 5 l C)7 3 l 63 6 PDT

~ _~ ~--- -

--

1400 I bull bull

1200

1000-5 LampJ 0 ~ I- 800 ~ c(

sooLl

-1-=-1-~--t j --=~c-o-----i-bull 1-~~~ ilt~~ -~-1 lta-abull--~ -c-~---=---r F--- ---- I n_--middot- =~~ ai~IHJ

(~-It

1600 ___________________________________

C r 11 s Ground Elevation t~C E H I~lcc

- ~ 1 90 m

4001 bullc C H

C UNDrnCUTTNG svC ~ Ic- H

SEA BREEZEC II 200

C C

[C -PARAMETER ---UNIT SYMBOL

NOx N0 0 ppm01 02 03 04 05 03 z co ppm C0 5 10 15 20 25 30 35 40 45 50

-5 middot- -~20~----25 TEMPERATURE oc T0 5 10 15 30 35 40 45

100 RELATIVE HUIOITY H0 JO 20 30 40 50 60 70 80 90 bcot 10-4m-1 8

CN crrr3 10 0 I 2 3 4 5 6 7 8 9 10 X TURBULENCE cmZ-13 sec-1 E

N N

_-----=-G--~---

Figure 13 VER TICAL PROFILE AT EL MONTE (EMT) JULY 25 1971 1656 PDT SHOWING UNDERCUTTING BY THE SEA BREEZE

0

middot~_lt ~middotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotbullbull

-~

LACA

0 - )

i r=

-v2v

~

_middot~middot)( I bullbull

bullJ

K~Ji~middot

~~ 61iAS 0

EMT J~J---6~-11 ~orr

PACIFIC OCEAN

WEST 0

SMC

0RLA

14

L~8

R~A

~BL

16 ~ ~

0 5s Pcfrac14A c1i ~ )

wFJfo~J_) ltI~~~

_ff-Clf1ito J )

HILL~

~J U

~ _~~~

~

I o middot

1 1$ ~ 11yen ~middot ~I N

I

N I- I

t

0 --pomiddotmiddot bullmiddot i- 1LO middot Joomiddotmiddotmiddot -- middot middotmiddot -middotmiddot

_middotmiddot 0 middot middotbull MWS r

L4 ( 1 T bull bull __-- -A bullbullbullbull middot

0 i __ bullbull

17 t-J~ N7 a S I ~r ~ 1 rtd ~lt A-~ v- middot ~ - cXa 0

RIA 19

CLO

ltJ~

bull ~ 0

(

--

1

_ _

-2Wl

~s~o -- _)~J0JgtJ~ ___ Q

15 l1JI

0 15 r(A0

CAP

CLARR)~R 1900 1-shyPDT

II (_-L~X L2X I 0~ R[V

0 CCtwA

I

I18=00 POT~ l4 r1

fj

-11J - ----- 11=oomiddotmiddotpor

l~i middotmiddot- o

i

5 10 5 Tl o~1 middot--middotmiddotmiddot middotmiddot

_q it==i--__F-3 9 I I CONTOURS REPRESENT SNA NZJ ~1 o

_- I 0 8 16 24 km I - 1000 ft 305 m middot ~

7 14~CALE --- 2500 ft o2m V lr1 ) middot I i0 _ il o5

16QQ pol(middot v( ____________ _L

I i

Figure 14 APPROXIMATE TIME (PDT) OF ARRIVAL OF SEA BREEZE Jl-LY 25 1973 (Ogt_iective criterion based on ground level ozone concentrations)

~ -___~==~ ~~ - ~ =-~ f7r=~1 _j~-~ --c_~~

u-middot - middot middotmiddotmiddotmiddotmiddot

~- middotmiddot~ ~1 WESTERN BASIN r Joa_middotmiddotmiddotmiddot_ NOxEMISSION RATE ~- 95 METRIC TONShr

-----bull_ ~ ~middot~ I -OUR -----middot )omiddotmiddotmiddot - middot~ l21 (fTI

~ AT middot ~ middotbullmiddot- ~- ~ middot 4bull-middot

I EASTERN BASIN NOx EMISSION RATE 10 METRIC TONS hr

ri r bullbull

t10 Joa

) __ 8v -a_ -- -bull-I O ~AGA -_ ~S ___ _ middotmiddotmiddot -

~ ~v ai- omiddot-middot~-- - ) r -middotmiddotmiddot f middot( ---~ -l A ~ _ (- bull ___

it~ ~~~ middot-middot -- ~-~ ~~~ 0 0 AZU~

AVERAGE CONCEN7RCTi)N iN BOX (IF STEADY STATE)

IS 25 pphm

1 r f--Ji 7 ~Sv PAS ou )V~(~- ~ t i -~ Li_) 03 FLUX THROUGH f~

~ ~JI_~ - amp_ JiM O SHADED BOUNOA~middot~-~ ~~-s-- EMT 185 t 60 METRI~ bull ~ ~ TONShr 0 (m)

c~~~ 1t~CS A~JFP

1000 _29

-i32

_~o tUA

_

1

O~ ~

0 -__rJ( (r- J PACIFIC OCEAN LAX _ C-middotJbull _

l o M R No _

550m

r

A frac14

HAR O HJ LAH

_ o camptA REDLANDS 18QO POT ~ r

I bull ~

RB MEAN TRAJECT~~~y

0

TOA L~S

0 AN

I - ~ 8 OUNOARY ~ ~middotltdeg ~ ~ BETWEEN middot __ WES~ERN ANO- middot middot - ~

I gt I lt bullmiddot bull (EASTERN ~ i middotmiddot middot - - ~

S ~ ~~ ~ - middot-

rt1~1_--t------l

middot1-- BASIN ~-~

1-)~~--middot ~ ~l

~~ ~-bull bull J --

-is-eo -_

0 5 10

j=i r-i C

0 8 ltl

SCALE

5 mi

2~ un

CONTOURS REPRESENT - 1000 ft 3gt5 m

--middotmiddot 2500 ft 1 762 m

~

0SNA

cos 0

_ --~ ----- --- ( bullmiddotmiddotgt

- middotlt- ltgtmiddot t__ Q ~

1 1 rmiddot bullbullbullbullmiddot ~9

NZJ ~ middotmiddot - middot- Alr ---middotmiddot- middot middot( middotmiddotmiddotmiddotv ~ bullbullbullw bullbullbull bullmiddot 1 bullbullr~ ~-- -middot ~--v ~- - I -~

ESTIMATED OZONE FLUX FROM VESTER~ TO EASTER-J BASIN JULY 25 1973 I 700 PDT

C ~IV

N N N

I

l ~

-~~

I

iI

i I

I t

t

~ ---~ --

Figure 15

~Qa llfJD fl(~middot ~ 11f ~I I

l

Lfb ec~s0 CPK v2v 0

ALT 8v Ld~_----1

I

HO-

0 CA

middotLARRv O VE~

1330

ol(Di

A~U

0ENT

~lt

s~e ~ 1530

F8f 1730

~

rbull-~

oc (WljT) -_-~(~~c lt-rw---_

~~ ~-_i~cB~~~

2-~) - ~ ~ l~w-~~ p~- pound)_

0 ojI middot tl-1CfUp I ~ ) 1 ~ J~I i bull middotbull middot~-Li 1)- ) I

DiI ~- 0

i ) 0 l I I

t

A RALc~o JI

C

-~

0 r-iR

~IV 1230 1~

RE PO ~- I - Ftl

) 0 ---~gt- __L8s ~Zi diams ( T~ _middot_ ~~ ~

I AN ~~-~ j t bi 0

~ I

~ I L i

-_gt ji o 5 c 5 Tl middot 0 0 ~-i p__i=r 2=f I_ I 1 NZJSNA 1

1 8 2 4 km )

SCALE I 00 J_(1 CONTOURS REPRESENT cos f

1 0 I --- I - ))) 35

PACIFIC OCEAN

Figure 16 TRAJECTORY E~VELOPE FOR AIR ARRI1gtJG OVER REDL_)DS AT 1800 PDT JULY 23 l =i73

224

JULY 25 1973

LA DOWNTOWN

0sect040 a

~

~ 020 0 X z0 ~ LJ 0 ~ z

~5 040 330POMONA 0 ~ en~ 020 w z _J

w w 0 (9 z O----u-~~-__~_-~~~-------L-~-0--0-0~----- z

ltt~ 040 56 (I)z

0 0o _ RIVERSIDE _J0 20 t6 ~

0~ Qt---0-0--ltrO-ltgt-C~------~~~~ a

LL ~

Rate ~ IO mph___ (I) w

_J~ ~ ~

et~ lt(

3 040 PALM SPRINGS ~

j 020 ~

0------____-----L--___---------L---~--~

105

12 4 8 12 4 8 12 l~-s----am _ pm----1

HOUR OF DAY PST

Figure 17 Diurnal variation July 25 1973 of oxidant concentrations at air monitoring stations at Los Angeles Downtown Pomona Riverside and Palm Springs California Values are corrected data Los Angeles Downtown and Pomona x 11 and Riverside and Palm Springs X 08

CONO S t 1 fRESEIS7

~

~~ 0

ciffmiddotdK ~ ~v~~o

( ~s ~

bull ~r ~ bull 1--~~----Soootl ~ ~ ~ ~ lj i1 d t CJ ~ ampfrsmiddotflt- frac12 ~ middotL~Js _-- ~

_gtgt middot~ ~rroltf~-) ~ 0 s- r

middot-middot- r_~ ~~JtbO ~~bull~Jt ~~~ L r - bull _ ~ I= J 1 ~ ~ ~-~~bullJC ___ -_ middot ~ laquo -poundJ~ ~- middot1~ r-- - V--_1_ ~ I 1 S I

V ~ bullf-uv~ fi -~zumiddot -~middot~ LS gt -tmiddot-F Q~ ~-tv I_~ --- ONT p(_ s ~S ~~~-[ ( 0 c-_ --~ ~~~___d_) lt- ~ I -i-C - -

~----1-1 bull~~POMA ~V BN ) middot-~ f -- s - ~

~VA -middot- ~p AAL a 2~~ ~~middot01 r r ~ middot middot 0-- V

i LAX bull1

~ -~poundJ-i- ltllll _(__1-0~ ~t- degQ-0- ~~ _ _-__~~-qlK ( a_ II ~ ~p-~ ~J

N bull - - 0 r o_ _I ~ -~ ~middot ~ ~amp ~--= ~ ) s ~

- -~- - middotO _a - Tl --0- ov I lHOIO J I bull J -- ~ 6 ~ -__ 2 ~

(__ ~~ _- ~-~ middot8---fl~ -- ~ bull~-abullbull _~ ~-cgt ~ bull bull middot e bull bull l ~ 0

I 1A_ HZJ middoto~J

middot0 (~ ~ S TAA

- ~ - - - --0 () _-j J middotO=c==c-c==cc~~~ l ~~ ~ ~ bull-~---~ ~ bullbull -~ al1 ~ bull __ ~--middotmiddotmiddot

diams Skyforest _ Strawberry Mt Lookout

Figure 18 STRE ~[Ll)ES FOR 1600 PDT on 8 1673

~ ~--

vO 0

N N V1

au

91 V7

-1 ~ -=1 ~~ ~~~~l r=--~d- ---1 _J-_

~E1 ~L1-~f~

3100 ---------------------------------

2900r-----------------------------

T

e w 0

~ 5 Cl Ground Elevation

1560 m

T PARAMETER UNIT SnbullBOL

NOx N 01 02 03 04 05 03

ppm z co ppm C

10 15 20 25 30 35 40 --

45 50

170

I I I z

0 5

-5 - -0~ 5 10 15 20 25 30 35 40 45 TEMPERATURE oc T

0

0

10

I

20

2

30

3

40

4

50

5

60

6

70

7

80

8

90

9

100

o

RELATIVE HUMIDITY

bcot CN

TUR8ULENC~

110-4m-

cm-3 tobull 213 1 cm sec-

H

8 X E N

N OI

Figure 19 VER TI CAL PROFILE OVER ARROWHEAD u-RR_l A CG CST I 6 1973 939 PDT

3100----------------------------------

N2900r----------------------------- -i

N

2700i-------------------------------

2500

e 0 uJ 2300 gt ~ ct

2100

1900i---------------------+--------------

~le 1iation 1360 m) 17001 ~

- -PARA1jETER UNIT SYMBOL

T NOx N1500 o ppm01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50

TEWERATJRE oc T-5 middot --~o--- 5 10 15 20 25 30 35 40 45

IOO RELATIVE HUWIOIT Y H0 10 20 30 40 50 60 70 80 90 bcat 10-~- 1 8

CN cm- 3 104 X0 I 2 3 4 5 6 7 8 9 10 213 1 tURBliiENCE cm sec- E

Figure 20 VERTICAL PROFILE OVER ARROWHEA D -RR 1 --- -AUGlJST 16 I) 16--1S PDT

1-~i w--~i_f l-=--bullC- ---~-4

1600 bull t c- N 8 ff Tbull C[ 8 H 1 bull H z H T ~ C f N 1 H T bull C rn 1 C NE bull-~z Hi400 bull bull tf T bull N ~r --middot _P H -ybull EC N z__e H T i 8 z H Tbull C E HD Z H T POLLUTANTS REMAINING FROM bullt C Hbull L T PREVIOUS DAY1200 Et HO I II -middot-- bull Ct H 9 - H T

___ Hbull( E N 1 a tC N i--_ -1 H

C N Tbull Z HP poundIC C H z_ 1111 1

- bull C H Z l _H_ _J1000 )( cc H -z emiddot ksect bull C N ~ T

)( iz H 8 H TIAI -t XC z 7-- T0 bull pound N t H_8

t-gt

YCpound N 1800 l I-gtltbull - H (Jet

N i -r~Bltt t bull gt- t C X N H T

[ BUOYANT POINT SOURCE PLUMEH 1

N ~z-- -

C H

-bull SUPERIMPOSED ON POLLUTANTSC JZ X H T 600 -~ E c REMAINING FROM PREVIOUS OtY Cl JC t H H f bull cmiddot t HT -fl

C- X t fl _ REMNANT OF NOCTURNAL RADIATION INVERSION(I-----e-C f N K I T H

C Z [ T H x-8 400 _Zc r -H -K SURFACE MIXING LAYERz C II H K 8

C N T pound H M 8 _ I -t ff H E N -9 l

Ground Elevation 305 rn200

PARAMETER UNIT SYMBOL

_ I - I I I NOx N00 ppm01 02 03 04 05 03 z

co ppm C 0 5 IO 15 20 25 30 35 40 45 50

L middot1 TEMPERATURE oc T-5 0 5 IO 15 20 25 30 35 40 45

100 RELATIVE HUPAIDIT y H0 10 20 30 40 50 60 70 80 90 bscot o-4m- 1 B

CN cm-3 x 104 X0 2 3 4 5 6 7 8 9 10 TURBULENC~ cm213sec-1 E N

N co

Figure 21 VERTICAL PROFILE OVER BRACKETT (BRA) JULY 26 1973 0825 PDT SHOWING BUOYANT PLUME AND UNDERCUTTING BY RADIATION INVERSION

N N 01600

___bull C M C

C

1400~~~ t C [ middot H LAYER CAUSED BY

C C H C [ H UPSLOPE FLOWl

1200

1000 ] w

SURFACE MIXING LAYER 0 --= ~ -~~ 6 800~ er

C C

600t-i C C t C

I ~00

Ground Elevation 436 m 2001-------------------------------

PAIUWETU UNIT SYWBOL

NOx N ppm0 0 01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50 I I I I I I I I TEWPERAT1JftE degC T-o b 5 10 15 20 25 30 35 40 45

100 ~EIATIVE HUWIOITY H0 10 20 30 40 50 60 70 80 90 b1tt1 10-m- 8

CN enr3 110 X0 2 3 4 5 6 7 8 9 10 Tu RUL Erct cm23sec- E

Figt1re 22 VERTICAl PROFILE AT RIALTO (RIA) JlJL Y 19 1973 1738 PDT SHOWI=JG LAYER CAUSED BY UPSLOPE FLOW

~~-7 ~ ~- 1 ~iri ~~- ~~-~ ~t ~~ ~ =~middot-1

1200 I t 1 If J-

1000

I C ltTl a_ ~l- t

800

600

L gE __r H

H

400 j (~ c pound N C E I~

t EH -

1-1 M

H H

H M H H

H

H H

11 bull H M H

M H If

H H

H

- C t H ~ C poundmiddot H

I C E I(

200

1600--------------------------- t

T t t T l

l T t

T t_

t 1

l] w ) g f

Tt t

ltt ~ T

t J t T

t J

f 1

t

Klt

H M Cro1nd Elevation 250 m HT X

5Yl80LPAllAlETER ~

NOx N0 0 ppm01 02 03 04 05 03 z

co ppm C0 5 10 io 20 25 30 35 40 45 50

25~--- ---35~~-40 TEMPERATU~E oc T-5 0 5 lO 15 20 30 45

100 RELATIVE HUMIDITY H0 iO 20 30 40 50 60 70 80 90 bact 10--ltllm-1 B

CN cmmiddot3 11 04 X0 I 2 3 4 5 6 7 8 9 10 IURBULENCE cm2hioC-1 E

Figure 23 VERTICAL PROFILE OVER RIVERSIDE (RAL) N

JULY 26 1973 2239 PDT I)

middot==-=-=

0

bull

N w 1--

ii -s~~ l-obull

CJ ~

obull -obull obull

5 02~

bscat

Oa

4l o2J

-I 3 e I 0

--)(

~

Abullu 2

ll

ol

Traverse at 750 m msl 35 km Downwind (SW) of Arch - St Louis Mo 1117 - 1137 CDT

( Power Plant Plume -01 Ibull-[ ~ e

11 bull E I -)(I

I0bull I 1r~ l -

0

I I Io 1 u I

I r- l A bull I i I 1I

H1I I 4 t I II I I

11 I I

I I r I I I

I I qo 01 I I

I I bullJ~viI I middot ~

I

I I

~

Urban Plume

ood 0 10 20 30 40 50

kilometers

o~

02

01

s 1

P

0bull 01

00S~J1 I ti middotmiddot1 middotvmiddotmiddot~ J

Urban Plume

I y

oo 0 10 20 30 40 so

kilometers

Traverse at 750 m msl 46 km Downwind (SVV) of Arch - St Louis Mo 153 0 - J 549 CDT

---- bscat

o-

Power Plant Plume

1l~ 11I 1 t

ill~t fl Ibull I ii

I

lmiddotmiddotrI

I I I I t II

l vrI V

JV-f Jl bull

bull t I bull I

Figure 24

l

232 RELATIVE CONTRIBUTIONS OF STATIONARY ANDMOilILE

SOURCES TO OXIDANT FORMATION IN LOS ANGELES COUN1Y IMPLICATIONS FOR CONTROL STRATEGIES

by Robert G Lunche Air Pollution Control Officer

Los Angeles County Air Pollution Control District Los Angeles California

Introduction

The type of air pollution problem characteristic of the west coast of the

United States and particularly of Southern California has come to be known

as photochemical smog because it is the result of sunlight-energized atmospheric

reations involving oxides of nitrogen and reactive hydrocarbons Its manifesta-

tions- -eye irritation reduced visibility damage to vegetation and accumula-

tion of abnormally high concentrations of ozone or oxidant - -are by now well

known In fact the occurrence of high levels of oxidant which consists almost

entirely of ozone has become the primary indicator for the presence and relative

severity of photochemical smog

During the 25 years since photochemical smog in Los Angeles County was

first identified an extensive program has been underway for control of the responshy

sible contaminant emissions Initially during the 1950 s these programs concenshy

trated on controlling emissions of hydrocarbons from the stationary sources of this

contaminant In the early 60 s programs for the control of hydrocarbon emissions

from motor vehicles in California were begun An exhaust emission control proshy

gram for hydrocarbons and carbon monoxide from new vehicles was begun in 1966

C011trol of oxides of nitrogen emissions from motor vehicles began in 1971

As a result of the overall control program by 1974 emissions of reactive

hydrocarbons from stationary sources have been reduced 70fo from uncontrolled

levels and about the same percentage from mobile sources Oxides of nitrcgen emissions

233

from statjonary sources have been reduced about 53 while emissions from moshy

bile sources are still about 7 above uncontrolled levels due to the increase

in NOx from 1966-1970 models Additional controls already planned for the future

will by 1980 achieve reductions of reactive hydrocarbons from stationary sources

of about 87 from uncontrolled levels and from mobile sources about 93 By

1980 emissions of oxides of nitrogen from stationary sources will have been reshy

duced 53 and from mobile sources 63 from uncontrolled levels The past

present and projected emissions of these contaminants are shown in Figure 1

A I though compliance with the air quality standards has not yet been achieved-shy

and is not likely before 1980- -the results of these programs have been reflected rather

predictably in changes in certain of the manifestations of photochemical smog For

example eye irritation is less frequent and less severe and in some areas js

rarely felt at all any more and damage to vegetation has been markedly reduced

Ozone (or oxidant) concentrations have been decreasing in Southern California

coastal areas since _1964 in areas 10-15 miles from the coast since 1966 and in

inland areas 40-60 miles from the coast since 1970 or 1971 as shown on Figures

2 arrl 3- All of these positive effects have occurred despite the continuing growth

of the area indicating that themiddot control programs are gradually achieving their purpos

a return to clean air

This improvement is al~o refutation of the so-called Big Box -concept which

assumes that the total daily emissions in a given area are somehow uniformly disshy

tributed throughout that area--regardless of its size or of known facts about the

meteorology of the area or the spatial and temporal distribution of its emissions- -

234

and of control strategies based on that concept And since the improvement in

air quality refutes the control strategies based on reductions in total emissions

it thus confirms the value of more recent control strategies which emphasize conshy

trol of motor vehicle emissions and use of a source-effect area concept

Following is a brief listing of the evidence we intend to present as supporting

our views on just what control strategy is appropriate

Examination of relative contributions of HC and NOx from stationarybull and mobile sources demonstrates that motor vehicles are the overwhelming

f source of both contaminants~

I bull Observation of air monitoring data shows that the effects of photochem -

ical smog are not uniformly distributed t_hroughout the county

bull Study of the meteorology of LA County shows consistent paths of trans -

port for various air parcels and consistent relationships between the

areas most seriously affected by photochemical smog and high oxidant

concentrations and certain other areas

bull The upwind areas are found to be source areas--the downwind areas-shy

effect areas

bull Central L A is found to be the predominant source area for the effectI area in which the highest oxidant levels in the SCAB consistently occur

bull The predominant source of emissions in this source area is found to

be motor vehicles

bull Central LA has the highest traffic density I

ij bull Both pr~mary and secondary contaminant concentrations reflect the effects

of the new motor vehicle control program in a predictable fashion 11 I

A strategy based upon these findings is gradually being verified by atmosshybull pheric oxidant data~

235

The Evidence that Motor Vehicle Emissions Are the Principal Source of Oxidant

As seen from Figure 1 at the present time the total daily emissions of I-IC

and_ NOx from all sources in Los Angeles middotcounty are primarily due to the motor

vehicle The problem now is to find the spatial and temporal representation of

emissions which when examined in the light of the known meteorology and geogra -

phy of the Los Angeles region best describes the source of emissions responsible

for the highest observed oxidant readings

In the rollback models used by EPA and others the basin is treated as a

big box with uniformly distributed emissions and peak oxidant is considered to

be proportional to total basinwide hydrocarbon emissions

The fact is that the middotemitted contaminants from which the smog is formed

and the effects which characterize that smog are not evenly distributed throughout

the Los Angeles Basin in other words the basin area under the inversion is not one

large box filled to all corners with homogeneously distributed air contaminants and

photochemical smog

Refutation of Big Box Myth

Examination of atmospheric contaminant concentrations refutes the big box

concept It is found for example that concentrations of djrectly emitted contam -

inants measured at a particular sampling site reflect the emissions within a rather

limited area around that site For this reason contaminant concentration levels

vary from one location to another and each has a characteristic daily pattern which

reflects the daily pattern of emissions in that area

middot 236

The big box concept is further refuted by the fact that peak concentrations

of carbon monoxide and oxides of nitrogen in areas of high traffic density were

fairly static prior to 1966 Thus they did not reflect the 45-50 per cent growth

in motor vehicle registrations and gasoline consumption which occurred in Los

Angeles County between 1955 and 1965 and which caused comparable increases in

total daily emissions of such vehicle-related contaminants This demonstrates

that growth was outward rather than upward so that a larger area of the County

began to be affected by photochemical smog but no area experienced smog ofJ

greater severity than that originally affected by smog formed from the vehicular

emissions which accumulated each weekday in central Los Angeles and were trans-

1 I

ported later that day to the San Gabriel Valley

1 Meteorological Evidence

To verify the geographical dependence of emissions and resulting atmospheric

concentrations let us examine the meteorology of these large areas of Southern

California Both the County and the Basin have many meteorological sub-regions

in which the patterns of wind speed and direction may be similar but within

which the patterns of air transport are parallel with those of adjacent sub-regions

and the respective air parcels do not ever meet or join

The characteristic patterns of inversion height and wind speed and direction

in these sub-regions and their patterns of vehicular emissions together have

created a network of source areas- -those in which the reactant contaminants accu -1T

i ~ mulate in the morning and begin to react--and related receptor areas--those to which

~ the products and associated effects of the photochemical reactions of the contamshy)

inants originally emitted in the source areas are carried by the late morning and

237 middot

afternoon winds ( sea breeze)

Wind-flow patterns show that characteristic patterns of transport for related

source area-effect area combinations are separate and parallel not mixing or

joining Each source area has its own reactor pipeline to its own effect area

or areas

To illustrate this source area-effect area relationship the typical flow of

polluted air from downtown Los Angeles to Pasadena was selected as a worst

case situation for in-depth examination Figure 4 shows that the air in downtown

Los Angeles on the morning of smoggy days moves directly from the central area

to Pasadena

Vehicular traffic is the predominant emission source in both downtown Los

Angeles and Pasadena Thus the air in each locality should contain CO Also

since oxidant would form in the air parcel moving from Los Angeles to Pasadena

oxidant levels would be expected to be higher in Pasadena than in downtown Los

Angeles

Figure 5 shows these relationships for the period 1960-1972 The atmosshy

pheric CO level is similar for the two areas while oxidant levels were higher in

Pasadena than in Los Angeles throughout this time period This demonstrates

that a significant amount of oxidant formed in the air as it moved to Pasadena

containing both the unreactive CO and the photochemical reactants for producing

oxidant Both CO and oxidant show a marked downward trend in each locality since

1965 which emphasizes the effect of vehicle exhaust controls and the correlation

between the localities

238

On a day which is favorable to the formation and accumulation of photoshy

chemical smog a contaminated air parcel normally originates during the

6-9 a m period on a weekday from an area of dense traffic centered just

south and west of Downtown Los Angeles It is oxidant generated within that air

parcel which usually affects Central Los Angeles and the West San Gabriel

middotK IJ l J

Valley area around Pasadena

The traffic area in which this smog had its origin is about the most dense

in Los Angeles County and has been so for the past 25-30 years No area

has a higher effective density thampn-this Using carbon monoxide which

1

is almost entirely attributable to motor vehicles as an indicator of such emis-

sions it is found that the concentrations of emitted vehicular contaminants

middotr i

measured in Central Los Angeles during the past 15 years confirms both this lack

of change in effective density and the absence of any area of any greater effective

density when local differences in inversion are acknowledged

This area the Central Source Area is depicted in Figure 4 The size

and shape of the Central Source Area was ch~sen to be large enough to reduce to

an insignificant level any diffusion or transport into this area from any externally

l generated reactants This conclusion is based in part on the trajectory studies

previously referenced as well as an analysis of the diffusion and transport parashy

meters for the area

239

The Central Source Area has been identified as that geographical region

which contributes essentially all of the primary contaminant emissions giving

rise to the highatmospheric oxidant levels in the West San Gabriel Valley

The proportion of emissions in the CSA due to motor vehicles and that due to

stationary sources is shown in Table 1 For the County as a whole about 80 per

cent of _(6-9) AM reactive hydrocarbons are due to motor vehicle emissions and this

figure rises to 90 per cent for the CSA The same conclusion a pp lies to NOx

emissions The Central Source Area contains the greatest density of vehicle traffic

in the County and thus the greatest density of source emissions Thus it appears

that the source area with the highest density of emissions during the critical (6-9)

AM period is responsible for the highest afternoon oxidant levels observed in Los

A i1geles County and in the South Coast Air Basin These highest oxidant levels

are consistently observed to occur in the San Gabriel Valley This is true whether

the LAAPCD or the ARB oxidant calibration procedure is used

Further the atmospheric concentrations of the primary pollutants can be

identified as originating primarily from the motor vehicle and they reflect the

effects of the motor vehicle emission control program A vehtcular source area

can be identified by its atmospheric levels of CO and NOx Figure 6 compares

measured atmospheric levels with calculated atmospheric levels for CO NOx

and the CONOx ratio in the downtown area

TABLE 1 240

REACTIVE HYDROCARBON EMISSIONS

(6-9) AM

1970

LOS ANGELES COUN1Y middot CENTRAL SOURCE AREA middot SOURCE TONS PER CENT TONS PER CENT

Mobile 1260 81 3 135 91 2

Stationary 290 187 1 3 88

Total 1s~o 1000 148 1000

By 7 -Mode Gallonage

241

The calculated values shown in Figure 6 were derived from a baseline

survey of 1100 vehicles and continued surveillance tests both using the Calishy

fornia 7-Mode test cycle The baseline survey showed that motor vehicles withshy

out exhaust control systems had average exhaust emissions concentrations of 3 4

per cent CO and 1000 parts per million of NOx Baseline emissions data apply

to 1965 and earlier model vehicleg and surveillance data to 1966 and later modelsmiddot

Since it can be concluded from calculations and observations that the dilushy

tion of auto exhaust emissions in the atmosphere on a smoggy day in Los Angeles

is approximately 1000 to 1 the calculated values for CO and NOx prior to 1965 are

34 ppm CO and 1 ppm NOxo After 1965 the changing effect of controlled vehicles

in the total vehicle population is reflected in the calculated values

CO and NOx values measured in the atmosphere are also shown in Figure

6 and confirm the values calculated entirely as diluted vehicular emissions NOx

concentrations measured in the atmosphere tend to be consistently a little lower

than the calculated values probably because photochemical reactions remove some

NOx from the system

The data for CO and NOx calculated and measured show that emissions in

downtown Los Angeles originate almost exclusively from motor vehicles and that

atmospheric concentrations there reflect the average emissions from a representashy

tive vehicle population

The ARB has recently published a report entitled A Trend Study of Two

Indicator Hydrocarbons in the South Coast Air Basin Acetylene was used as a

242

specific indicator of automobile exhaust emissions and it was found to have de-

clined in concentration in the Los Angeles atmosphere at an annual rate of 12 5

per cent since 1970 To quote from this report The California implementation

plan requires an annual average reduction in these emissions (reactive organic

compounds) of 166 tons per day or 11 1 of the 1970 tonnage per year The per cent

reductions in the_ acetylene levels at Los Angeles and Azusa are greater than reshy

quired by the implementation plan Since acetylene is almost entirely associated

J with auto exhaust this demonstrates that the motor vehicle emission control

program is achieving its purpose

To summarize at this point it has been deomonstrated that high oxidant values

are due to motor vehicular emissions of NOx and HC because

NOx and HC are the principal reactants in the oxidant formation process

and they originate primarily from motor vehicle emissions and

The highest oxidant values are recorded in_ effect areas that receive air

from source areas where motor vehicles are clearly identified as the

dominant source of NOx and HC

243

Future Control Strategy

The APCD strategy for achieving and maintaining the oxidant air quality

standard is based upon the fact that high oxidant values are due to motor ve-

hicle emissions of hydrocarlxms arrl nitrogen oxides This strategy is as follows

1 Both Hydrocarbon and Nitrogen Oxides Emissions Must Be Considered To Achieve the Federal Oxidant Standard

There is wide agreement that NOx and HC are the principal reactants in

the oxidant formation process and that vehicular emissions are a major source

of NOx HC and CO

2 Effective Regulation of Atmospheric Concentrations of Both HC and NOx and of the Ratio Between Them is necessary for Attainment of the Federal Air Quality Standard for Oxidant

Basmiddoted on the abundance middotof available experimental evidence it is our firm

position that the most rational approach to solving the photochemical oxidant smog

problem in the South Coast Air Basin (SCAB) is to control the quantities of emissions

from motor vehicles of both smog precursors--Hcmiddot and NOx--their resulting atmosshy

pheric concentrations and the ratios between both contaminants which will result

from these controls

We arc also convinced that the oxidant and nitrogen dioxide air quality stanshy

dards can and will be met not by 1975 or 1977 but by the early 1980 s if the emisshy

sion control program as originally outlined by Ca~ifornia or a slight modification

of it proposed by the District is followed and enforced This should also provide

for continued compliance with these air quality standards at least through 1990

244

It will also allow time for a reappraisal in about 1978 of the whole situation relative

to the ultimate emission standards required and the best approach to their impleshy

mentation

Calculation of the degree of control necessary to attain the air quality

~ standards for oxidant and nitrogen dioxide involves indirect complex methods 1

aimed at determ_ining the degree of control of the primary contaminants directly

emitted by automobiles

The following evidence supports our proposed solution to the problem in

terms of both the atmospheric concentrations of the oxidant precursors NOx

and HC the ratio between them as reflected in their exhaust emission standards

and the resulting atmospheric concentrations of oxidant which comply with the air

quality standards

Chamber Results and Projections to the Atmosphere

The importance of environmental chamberwork cannot be minimized the

j need for and direction of the whole emission control program was based initially

j on the results of chamber experiments In order to understand the importance to

air quality of achieving both the correct low quantities of emissions and the right

ratio we can present several graphic portrayals of analyses of experimental labshy

oratory work together with their relationship to past present and future air quality

in terms of both morning primary reactant concentrations during the morning

traffic peak and the equivalent emissions which would produce them

245

Figure 7 shows maximum ozone levels that were obtained by irradiating

varying amounts of auto exhaust hydrocarbons and oxides of nitrogen in an environshy

mental chamber The corresponding ozone levels then can be found for any comshy

bination of BC and NOx concentrations Thus high ozone is produced with high

emissions of both hydrocarbons and oxides of nitrogen and low oxidant is formed with

low emissions However either low NOx or low HC emissions11 can also produce

low oxidant--graphic and clear evidence of the importance of the NOxHC ratio in

ozone formation Furthermore each and every possible combination of values for

NOx and HC has then a corresponding characteristic maximum chamber ozone

concentration

Using this graph we can estimate what ozone levels would result if certain

atmospheric mixtures of NOx and HC could be injected into the chamber and

irradiated Such estimates were made for 1960 and 1965 using atmospheric data

rlThe points labeles 1960 and 65 show the location of the highest levels of both

HC and NOx found in the air in those years in Downtown Los Angeles (OOLA) area

during the 6-9 AM traffic peak

It has been demonstrated by use of CO and NOx data and CONOx ratios

hnw well the characteristics of vehicle emissions are reflected in the atmosphere

We know what emissions from the average vehicle were then in 1960-1965 both

for HC and NOx so that we can mathematically relate emissions to atmospheric

concentrations for those years and so for future years also knowing or calculating

only what the characteristic emissions will be from the average vehicle

246

The NOx concentrations stayed about the same from 1960 through 1965 because

average vehicle emissions of that contaminant did not change during that time

Mobile source emissions can be shown to have contributed essentially all of this obshy

served result However blow by controls did reduce emissions of HC and the

concentrations dropped accordingly In 1965 the last year before exhaust controls

the point 65 indicates where we were then in terms of maximum ozone formation

to be expected in a chamber with the highest HC and NO concentrations found in the X

air that year Levels of ozone actually measured in the atmosphere however

are higher than those shown on the graph for high NOx and I-IC concentrations for

those years up to the present

The strategy to meet the oxidant standard is obvious--get atmospheric NOx

and HC concentrations out of the area on the chart that produces high ozone levels

and put them in tie areas with the lowest levels This can only be done by implementshy

ing appropriate emission standards

As can be seen that did not happen between 1965 and 1970 because manufacshy

turers used controls on new cars in California which while causing a decrease in

BC (and CO) allowed a large increase in NOx emissions Thus the path line of

the atmosphere on the chart goes up from 65 and diagonally to the left passing

through an area of higher ozone levels The atmospheric concentrations of oxidant

predictably increased during the years 1967 and 1968 By 1970 they dropped to lower

levels - -back to about the same as in 1965- -exactly as predicted by the model The

app14oximate location of the point for 1970 (70) was both predicted on the basis of

247

the mathematical model and confirmed by atm-ospheric measurements of

[)owntown Los Angeles morning summertime NOx and calculated HC values

Again it should be pointed out that those points show the highest possible

concentrations of NOx and HC Years with less restrictive weather conditions

(for accumulating high primary contaminant levels) would cause lower measured

maximum NOx and HC levels but the calculations would still yield the points

shown Thus we are taking the most pessimistic view

Future Projections

In 1973 we were at about the point labeled 73 and ozone levels were beginshy

ning to drop as expected middot It should be emphasized that ozone values plotted on

thi$ graph are for the chamber only- -not the atmosphere The future path the

points 7 4 and on to 90 represents our estimate of future atmospheric levels of

NO and BC expected if the exhaust emission standards are just met While that X -

is optimistic it is all we really can do since performance of future vehicle models

is unknown We will achieve maximum ozone levels at or below the standard by

about 1980-1985 This will only be true however if cars in compliance with the

California interim standards for HC and NOx continue to be added to the vehicle

population at the normal rate These standards provide the optimum ratio of NO X

to HC necessary to provide the nitric oxide (NO) needed for the reaction that re-

moves from the air both oxidant formed photochemically and oxidant which occurs

as natural background which alone may cause the standard to be exceeded This

ratio is about 112 or 2 parts NOx to 1 part HC

248

The optimum NOxHC ratio is a key element in the APCD strategy but will

require a finite time for its attainment Replacement of older cars by newer ones

equipped to meet the most stringent standards is the only reasonable mechanism

which can change it VMT reduction proposed as a prime strategy by EPA cannot

change this crl(ical ratio which is a basic characteristic of the population at any

given time

Validation of the Districts Control Strategy

Figure 8 compares (1) future chamber oxidant levels based upon the

future maximum concentrations of HC and NOx we expect each year with the

California control program (2) calculated atmospheric concentrations using ~ I

our chamber-to-atmasphere empirical translation and (3) actual measured atmos-f 1l pheric oxidant maxima This clearly sets forth the relationship among these three

factors

The chamber concentrations (lower curve) middotare the lowest values shown

The actual atmospheric data (points connected by heavy dotted and solid lines)

vary considerably from year to year partly because of the vagaries of the weather

In all cases the atmospheric oxidant values are higher than the chamber values

because of the addition of vehicle emissions as the air parcel travels from source

to receptor areas The calculated atmospheric data (thin dashed and solid curves)

are shown to be the highest generally exceeding or equalling the actual measured

data and of course always exceeding the chamber data Thus the model paints

the most pessimistic picture possible It can be seen that by about 19801 1985 atmos -

pheric levels should be at or below the Federal air quality standard of 0 08 ppm oxidant

249

3 Motor Vehicle Exhaust Control is the Only Requirement for Achieving the Oxidant Standard by 1980

We can show that the existing motor vehicle control program has resulted

in a significant reduction of oxidant concentrations in the air

The foregoing material explained the relationship between vehicula~ emis -

sions in source areas and the high oxidant levels measured in effect areas This

relationship is exemplified by the downward trend of oxidant levels in the atmosshy

phere and by the similar year-by-year trends of NO and HC emissions from the X

average motor vehicle A projection of these vehicle emissions factors shows that

the associated maximum oxidant level in the atmosphere will meet the oxidant standard

by about 1980-1985

Figure 9 compares by year the number of days that the oxidant air quality

standard was exceeded in three separate areas with the average NO and HC emissions X

per vehicle mile To comply with the air quality regulations the number of days that

this standard is exceeded must be reduced to one per year

The lines plotted on Figure 9 show that a definite relationship exists between

the emissions from the average motor vehicle and the number of days each year that

the oxidant concentration in the air exceeds the clean air standard

The oxidant trendlines for downtown Los Angeles Pasadena arrl Azusa are

all downward and the slopes are about the same This similarity is logical because

the process that results in the suppression of oxidant accumulation simply has been

displaced from one area to another This was a unique one time situation because

of the increase in NOx between 1966 and 1971 After 1971 all areas are down Thus

l

250

the same conclusion is reached that the oxidantstandard will be met in the 1980s

I whether air quality data or vehicle emissions trends are projected middot~ Ul-

This outlook is based on the APCD s belief that future growth in both the

Los Angeles area and SCAB will not create any locality with a traffic density greater

than any traffic density in the area to date For the past 25 years the area around

downtown Los Angeles has been the area of maximum traffic density and therefore

the emissions source area responsible for the maximum effect area measurements

It is assumed that the traffic density in any future source area will be no

greater than the traffic density in downtown Los Angeles Thus since the

vehicular emissions control program will achieve and maintain the air quality

standards in areas affected by vehicular emissions from downtown Los Angeles it

will also achieve and maintain them for any area of SCAB

Summary Conclusions and Recommendations

In conclusion we have shown that a source and effect area analysis of emisshy

sions and resulting oxidant is a more reasonable and accurate representation of

the Los Angeles area for air quality analysis than gross integration metho9s such

as the big box technique It has been shown that motor vehicles are the major and

almost sole contributor to the primary HC and NOx emissions in the downtown source

area which results in the high oxidant levels in the San Gabriel Valley in fact the

highest in SCAB An air quality model and vehicle emissions control strategy has

been suggested to meet the oxidant standard by mid-1980 s

251

We have shown that

bull Only by adjusting the ratio of NOxHC in the motor vehicle emissions to

permit accumulation of sufficient atmospheric NO to sea venge the normal

atmospheric background oxidant can the standard be attained

bull The APCD strategy which provides for implementation of the present

California interim emissions standards for NOx HC and CO for new

motor vehicles in California beginning with the 1975 model vehicles will

result in compliance with the CO N02 and oxidant air quality standards

by the mid 1980 s and will maintain this compliance until 1990 and

possibly longer

bull The effectiveness of the present California motor vehicle control program

is easily demonstrable using air quality data from several areas in Los

Angeles County 1960-1973

bull To assure achievement and maintenance of the air quality goals as now preshy

dicted there must be periodic assessments of the effectiveness of the

motor vehicle control program followed by corrective actions if necessary

What has been accomplished thus far is significant but much more remains

to be done so that the best possible representation of emissions and resulting air

quality may be available for use in this air basin A much better emission inventory

defining the spatial and temporal distribution of both mobile and stationary sources

is needed Better statbnary source information is needed to evaluate the local

effects of these emissions Further detailed studies are needed to establish the

252

true relationship between emissions data from vehicle test cycles and the actual

operation of vehicles neither the 7-mode nor the CVS procedure provides a true

representation of actual vehicle operation Further tracer studies to assess the

transport and dilution of mobile and stationary source emissions from selected

source areas are also needed

253

1111

IUD

a CC I w gt-

1111

1UO

IUD

I 990

IDJO

1180

1111

IUO

FIGURE I

HYDROCARBONS

STATIONARY SOURCES MOTOR VEHICLES

- --

8 12 II 20 742 2l IS 12 I 4

HUNDREDS

HYDROCARBON EMISSIONS STATIONARY SOURCES IN

OXIDES OF

0

OF TONSDAY

FROM MOTOO VEHICLES AND LOS ANGELES COUNTY

NITROGEN

STATIONARY SOURCES

MOTOR VEHICLES

011111111111111111110111bull1111111

IIIIIIHIIIIIIIIIHIUII

llillL Its rd

l1uu~111111u1111111

2 I O 1 J 3

HUND REDS OF TONSDAY

OXIDES OF NITROGEN EMISSIONS FROM MOTOR VEHICLES ANO STATIONARY SOURCES IN LOS ANGELES COUNTY

illl~ -~--~ i~-=i _J~l ~--~ bull_~L- I ~~~-~~--Z ~

6

6S-66 ox

ICS ~A~1 M

i ssmuwmmgt

bullI

e COROyent_

64 ~ IDB RIVERS~

ORAJfD

-

t t 10 miles

bullmiddotsame Avg Cone Both Years

Pigare 2

YEAR OP HIGHEST OXlDANI CONCENTRATIONS

Highest Average of Daily -Maiimum One-Hour Concentrations

During July August amp September 1963-1972

bullLj

I

64

70 s11 3RlU)U0

70

--__ 69bull

N V +=

middot Source Air Resources Board

-200o

t t 10 adlea

tDS ampIJtsect

-1~

-1611ASampXllmiddot bull - bull -z----~------

I ldmmprwJ

IIVERSIDI

~ - 70

OampY -1 U 70 bull L

I

N V1 V

middot-i___

-----------------------------------------------------------i----------------------------

Figure 3

CHANGE OP OXIDANT CONCENTRATIONS

Percent Change from the Highest Three-Year Average to the 1970-72 Average

Of Daily Maximum One-Hour Con~entrationa for JulY August amp September

Source Air Resources Board

256

FIGURE 4 TYPICAL FLOW OF POLLUTED Am PARCEIS CIUGINATING AT DIFFERENT LOCATIONS IN THE LOS ARE~S BASIN - STARTIOO 0900 PST

l I

OAT

TRAJECTORY SUWMATIOl4

----- SMOG ~AVS

I

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullNONbullSlfOG DAYS

ISTARTING Tl~ cgxpsy

~ HAW

(CA

257

FiGURE 5 ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AND OXIDANT IN DOWlflC1N LOS AIDELES (SOURCE AREA) AND PASADENA (EFFECT AREA) 1

1960-1972

LO CARBON MONOXIDE

30

Pasadena

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullbullbullbullbull Downtown Los Angeles

20

10

o_______________________________

OXIDANT

)

2 Down~ Los Angeles

1

o________________________ 1960 1962 196L 1966 1968 1970 1972

YEAR

bullbullbullbullbull

bullbullbullbullbullbullbull

258

FIGURE 6 COMPARISON 01 CALCULATED AND MEASURED ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AN1) OXIDES OF NITROOEN IN DCMNTOWN IDS AIJELES

196o-1972

CARBON MONOXIDE

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ~ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot _-- ---_ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ----middotmiddot-bullw-_~ ---bullbullbull

10

o_______________1111111_____

OXIDES OF NITROGEN25

20

15 bullbullbullbullbullmiddotmiddotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~

1-i 10 middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ---

oS o_______________________

RATIO CONOx

40

50

0 +raquo Cd

p 30

~ 20

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot bullbullbullbullbull middotmiddotmiddotmiddotmiddot-shybullbullbullbullbull 0 u

bullbullbullbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot 10

0 j

ilI 196o 1964 1968 1970 1972 I

YEAR

Measured~D-owntown Los Angeles (90th percentile ofmiddot daily] instantaneous maxima)

Calculated - Aver~ge vehicle emissions - Present control program

259

FIGURE 7

25

t i5

flJ

~ on ~ ~ Q) bO 100 Jo

+gt on z

o5

EFFECT OF CALIFORNIA 1 s AUTO EXHAUST CONTROL ffiOORA M ON MAXIMUM CHAMBER OZONE CONCENTRATION

- PPM

357bullbull

r 76 bull

11 l

30

20

CHAMBER OZONE MAXIMUM

50

10

o___________111111111111______111111111111_____________

0 05 10 15 20 25

Hydrocarbons m-2 (LB-15) - PPM (as Hexane)middot

--

bull bull bull

r--=--~1 ~a==-~ - _~l ~ y--===-- ~~--~-- ~ r---~~

o

o8

~ I

~ 0 H 8 o6 I

c~ ~ 0 z 0 0

8

~ o+ A H gtlto-

02

middoto

Figure 8 Calculated t1ax1mum Levels Instantaneous and Hourly Average

of Atmospheric Oxidant Compared to Measured Los Angeles County Maxima-with Projections to 1990

(California Standards)

~ -Calculated Inst ax ~

f Calculate Max Hr Avg 03

_ bullbull _ _ - i bull

0 bullbull -l bullbull a0Ieasured Inst Lax o3 bull middotmiddotmiddot~bull 0bull _ ____ V ~ ea~ured ~ Hr Avr o3

~~ r---

~ ~ NB r~ima for 197 4 amiddots of 121074--- -_ Chamber Ozone F ~_ _~

- 1L_

~ Federal Primarfo Air ~uality Standard ~6- -UaximumT- our Avera~elr~ppm-------------- --~ ------- -~- -~-- ~

I I I I I I I I I I I I I I I I I N1 O

1960 6i 64 66 ~i middot-o 72 74 76 79 middotso middot92 84 bullg s9 9o

TBAR (end)

0

261 FIGURE -OMPARISON OF ATMOSPHERIC OXIDANT TRENDS WITH AVERAGE NCJx AND

HC EMISSIONS (Grams per Mile from Average Vehicle)

JOO Number of days state oxidant standara wds equalled or exceeded

--- Azusa __ Pasadena ________ Downtown Los Angeles

20

15 u

___ Hydroc_arbons Oxides of Nitrogenbullmiddotmiddotmiddotmiddotmiddotbullbullmiddot 1975 and later-assume middotcalifornia ARB standards

o_ ___________________________11111____

1965 1970 1975middot 198omiddot 198S 1990

140

There is a great uniformity in the deBigns which the U S manufacturshy

ers have selected for the 1975 California vehicles For those of you who

do not live in California about 80 of thl~ vehicles in the rest of the

country will be catalyst equipped General Motors is going with 100

catalysts apparently to realize the fuel economy benefit of their system

which more than pays for the cost of the catalyst system We have the very

interesting situation that the more stringent 1975 emission standards have

not only reduced the emissions of the 1975 vheicles with respect to the

1973-1974 vehicles but have also reduced the cost of operating the car

and have improved fuel economy The idea that emissions control and fuel

economy and economical operation are always one at odds with the other is

simply not true Compared to the previous years vehicles the more

stringent emissions standards of 1975 have brought improvements to fuel

economy because they forced the introduction of more advanced technology

The fuel savings which have been realized produce a net decrease in operashy

tional costs over the lifetime of the car This is not to say that pollution

control doesnt cost something If you were to compare the 1975 vehicle

with a completely uncontrolled vehicle tht~re would indeed be an incremental

cost associated with the 1975 vehicle

The foreign manufacturers have demonstrated a greater variety of

approaches in meeting the 1975 California standards but again they are

producing mostly catalyst equipped vehicles There is a widespread use of

fuel injection by the foreign manufacturers especially the Europeans

apparently because this is the easiest appmiddotroach for them and they realize

that only a fraction of their production comes to the United States

Volkswagen for example apparently has gone to 100 fuel injection on its

air cooled engines to be sold in California Mazda will continue to sell

141

rotary engine vehicles and thereby be the only rotary engine vehicle

manufacturer and marketer in the United States General Motorsgt elimination

of therotary engine stated for reasons of emissions is probably more

influenced by problems with fml economy although the two are a bit

difficult to separate Mazda is meeting the 1975 emissions standards and

in fact can meet the 1977 emission standards It has not solved its fuel

economy difficulties on the 1975 cars they will do better in 1976 All

evidence points to a fuel economy penalty for the rotary engine Nonetheshy

less we do have this option available because of the Japanese Also the

foreign manufacturers are providing us with a small number of diesel

engine cars These are of great interest because of definite fuel economy

advantages The diesel engine vehicles also meet the 1977 emissions

standards right now Also in J975 well 3ee the CVCC engine marketed by

Honda

The costs of the 1975 vehicles over tae lifetime of the vehicle are

definitely lower than the costs of the 197~ vehicles The National Academy

of Sciences estimate averaged over all vehicles is that in comparison to

the 1970 vehicles the lifetime cost of emission control system including

maintenance and fuel economy costs is aboJt $250 per vehicle greater in

1975 than 1970 Since the 1974 vehicles w2re about $500 more expensive

there has been a net saving in going from 1974 to 1975 I think the

conclusion we should draw for 1975 is that the auto industry has done a

pretty good job in meeting these standards This is something which they

said they couldnt do a few years ago something which they said that if

they could do it would be much more expewdve than it has turned out to

be

The same technology can be applied to 1977 models with no technological

difficulty and only slight refinements of the systems The fuel economy

142

penalties as estimated by the National Academy of Sciences are small 3

or less in going to the 1977 standards This estimate does assume further

advancements by the auto industry to improve fuel economy--primarily

improved exhaust gas recirculation systems It is unfortunate that this

issue of fuel economy has become so mixed up with the air pollution question

because the two are only slightly related If one is really concerned about

fuel economy and there isnt too much evidence that the auto industry or

the American public really is too concerned right now there is only one

way to have a drastic effect on fuel economy and that is to decrease the

vehicle weight Until that is done with gains on the order of 50 or

more to worry about 3 or 5 differences in fuel economy related to emission

control systems is simply to focus upon the wrong issue

Now what are the problem areas What remains to be done The

problems certainly arent over with the introduction of the 1975 vehicles

Problem Area Number One Field performance What is going to happen

to these vehicles when they get into actual service Past experience with

the 1971 through 1973 vehicles has been rather poor in that EPA and

California surveillance data show that these vehicles are not meeting the

standards Many of them did not meet the standards when they were new

The situation in general is getting worse at least for CO and hydrocarbons

that is with time the emission levels of CO and hydrocarbons for the 1971 I through 1973 vehicles is degrading There is no in-service experience of

this sort with the 1975 vehicles yet The certification data look quite I promising but the test procedures especially for durability are not ithe same as what occurs in actual use It is generally stated that the

1actual use situation for the catalysts will be more severe than the EPA

test procedure A larger number of cold starts are involved in actual use

than in the EPA test procedure and thermal cycling will probably have an

143

adverse effect on the lifetime of the cata]_yst This is not so obvious

It is also likely that the higher temperature duty cycle in actual use will

improve the performance of the catalyst in that it will help to regenerate

the catalyst through the removal of contaminants as long as one does not

get into an overheat situation The National Academy of Sciences estimate

was that the number of catalyst failures tn the first 50000 miles would

be on the order of about 7 Thats a very difficult number to estimate in

the absence of any real data A 7 failure still leaves a net gain in

emissions control even if nothing is done about this failure This points

to the problem of what happens after 50000 miles The EPA certification

procedure and control program only addresses the first 50000 miles The

second 50000 miles or slightly less for the average car is the responsishy

bility of the states Unfortunately then~ seems to be very little progress

in the area of mandatory inspection and ma-Lntenance--very little thought

being given to whether the replacement ofthe catalyst at 50000 miles

if it has failed is going to be required and how that is going to be

brought about The area of field performance remains a major problem

area one which obviously needs to be monitored as the California Air

Resources Board has been doing in the past but probably even more carefully

because the unknowns are higher with the catalyst systems

Problem Area Number Two Evaporative hydrocarbons from automobiles

It was identified at least 18 months ago that the evaporative emission

control systems are not working that the evaporative emissions are on the

order of 10 times greater than generally thought In the Los Angeles

area cars which are supposed to be under good evaporative emissions

controls are emitting approximately 19 grams per mile of hydrocarbons

through evaporation This apparently has to do with the test procedure used

144

The EPA is pursuing this The California Air Resources Board does have some

consideration going on for this but it appears that the level of activity

in resolving this problem is simply not adequate If we are to go ahead

to 04 of a gram per mile exhaust emissions standards for hydrocarbons

then it just doesnt make sense to let 19 grams per mile equivalent escape

through evaporative sources

Problem Area Number Three What about the secondary effects of the

catalyst control systems Specifically this is the sulfate emissions

problem and I really do not know the answer to that Our appraisal is

that it is not going to be an immediate problem so we can find out what

the problem is in time to solve it The way to solve it now since the

automobile industry is committed to catalysts and it is unreasonable

to expect that they will reverse that technology in any short period of

time is take the sulfur out of the gasoline The cost of removing sulfur

from gasoline is apparently less than one cent per gallon Therefore if

it becomes necessary to be concerned with sulfate emissions the way to

meet the problem is to take the sulfur out of gasoline Obviously sulfate

emissions need to be monitored very carefully to see what happens The

final appraisal is certainly not now available Another secondary effect

of the catalysts is the introduction of significant quantities of platinum

into an environment where it hasnt existed before Not only through

exhaust emissions which appear to be small but also through the disposal

problem of the catalytic reactors Since the quantity of platinum involved

is quite small the argument is sometimes used that platinum does not

represent much of a problem The fact that the amount of platinum in the

catalyst is so small may also mean that its not economical to recover it

This is probably unfortunate because then the disposal of these catalysts

l Jj

145

I becomes important I will not speak to the medical issues because

am not qualified The evidence is that theuro~ platinum will be emitted in a

form which does not enter into biological cycles--but this is no assurance

that it couldnt later be transformed in such a form What is obviously

needed is a very careful monitoring program which hopefully was started

before the catalysts were put into service If it wasnt then it should

be started today

Problem Area Number Four NO control The big problem with NO X X

control is that nobody seems to know or to be willing to establish what

the emission control level should be It is essential that this be tied

down rapidly and that it be fixed for a reiatively long period of time

because the NO level is going to have a VE~ry important ef feet upon the X

development of advanced engine technology The 20 gm level has been

attained in California with some loss of fuel economy through the use of

EGR and it is not unreasonable in our estimation to go to 15 grams per

mile with very little loss in fuel economy To go to 04 gram per mile

with present technology requires the use of one of two catalytic systems

either the reduction catalyst in tandem with the oxidation catalyst or what

is known as the three-way catalyst Both of these systems require technoshy

logical gains The state of development appears to be roughly that of the

oxidation catalyst two years ago The auto industry will probably say

that it is not quite that advanced but that if it were required to go to

04 gram per mile in 1978 that it could be done With the catalyst systems

the fuel economy penalties would not be great in fact the improvement to

the engine which would be required to make the system work would again

probably even allow a slight improvement in fuel economy What the 04

gram per mile NO catalyst system would appear to do however is to X

146

eliminate the possibility of the introduction of stratified charge engines

both the CVCC and the direction injection system and also diesel engines

It is in the context of the advantages of these advanced engines to meet

emission standards with improved fuel economy that one should be very

cautious about the 04 grammile oxides of nitrogen standards for automoshy

biles My own personal opinion is that the number should not be that

stringent that a number of 1 or 15 gm is appropriate Such a level

would require advancements but would not incur great penalties

Other items which I view as problem areas are less technically

involved and therefore require fewer comments

bull Nonregulated pollutants--again thls is a matter of keeping track

of particulates aldehydes hydrocarbon composition to make

certain that important pollutants ire not being overlooked or

that emission control systems are not increasing the output of

some of these pollutants

bull Fuel economy The pressures of fuel economy are going to be used

as arguments against going ahead wlth emissions control Mostly

these two can be resolved simultaneously We should simply ask

the automobile industry to work harder at this

bull Final problem area New fuels Again it does not appear that

the introduction of new fuels will come about as an emissions

control approach but that they may be introduced because of the

changing fuel availability patterns and the energy crisis These

fuels should be watched carefully for their impact upon emissions

This does middotappear to be an area in which a great deal of study is

going on at the present time It is one problem area perhaps in

which the amount of wprk being done is adequate to the problem

which is involved

147

In sunnnary then the appraisal of the 1975 systems is that they are

a big advancement they will be a lot better than most of us thought and

that we should give the automobile industry credit for the job theyve

done in coming up with their emissions control systems

With that boost for the auto industry which Im very unaccustomed

to Ill entertain your questions

-------=-~ ~~~ U- ~a1

~_~a--~-~ -J~ ~ -~r- _ --=~-- -___ja--~ __1~~ ~-~----=

AIR

1-4 FUEL----1

I I ENGINE

I II

_________ EXHAUST SYSTEM I bull EXHAUST

I I I

+ MIXTURE CONTROL COMBUSTION MODIFICATION EXHAUST TREATMENT

FuelAir Metering Ignition Air Jnjection FuelAir Mixing Chamber Geometry Thermal Reactor Fuel Vaporization Spark Timing Oxidation Catalyst Mixture Distribution Staged Combustion Reduction Catalyst Fuel Characteristics Ex tern almiddot Combustion Three Way Catalyst Exhaust Gas Redrculation Particulate Trap

FIGURE 1 Approaches to the Control of Engine Emissions

~ i 00

149

TABLE I

Average Emissions of 1975 Certification Vehicles (As Corrected Using the 50000-Mile Deterioration Factor)

Emissions in gmi Fraction of Standard HC CO NO HC CO NO

Federal 1975 X X

AMC 065 67 25 043 045 080

Chrysler 074 77 25 049 051 082

Ford 081 92 24 054 061 078

GM 083 80 23 055 053 074

Weighted Average 080 82 24 053 055 076

California 1975

AMC 042 49 17 047 054 087

Chrysler 048 61 16 053 067 082

Ford 052 56 13 058 062 067

GM 065 55 16 0 72 061 082

Weighted Average 058 56 16 064 062 078

kWeighted average assumes the following market shares AMC 3 Chrysler 16 Ford 27 and GM 54

150

TABLE II

Total Number of Vehicles Certified for California 1975 Standard and the Number (and percentage) of These Able to Meet

Certain More Stringent Standards

Calif 1975 Federal 1977 Hypothesized Hypothes ized 099020 04J420 049020 093420

i ~

Manufacturer no () no () no () no ()

AMC 16 (100) 1 ( 6) ti ( 38) 3 (19)

Chrysler 21 (100) 2 ( 9) ( 33) 0 ( O)

Ford 26 (100) 4 (15) -middot ( 15) 5 (19)

l GM 46 (100) 1 ( 2) -1 ( 9) 5 (11)

Foreign 62 (100) 21 (34) 3H (61) 28 (45)

1J

f

-l

151

CURRENT STATUS OF ALTERNATIVE AUTOM)BIIE ENGINE TECHNOLCXY

by

Henry K Newhall Project Leader Fuels Division

Chevron Research CanpanyRicbmmd California

I

iH1middot

10 1ntroduction and General Background

I

11 General

The term stratified ct1arge englne has been used for many

years in connection with a variety of unconventional engine

combustion systems Common to nearly all such systems is

the combustion of fuel-air mixtures havlng a significant

gradation or stratification in fuel- concentration within the

engine combustion chamber Henee the term nstratifled charge

Historically the objective of stratified charge engine designs

has been to permit spark ignition engine operation with average

or overall fuel-air ratios lean beyond the ignition limits of

conventional combustion systems The advantages of this type

of operation will be enumerated shortly Attempts at achieving

this objective date back to the first or second decade of this

century 1

More recently the stratified charge engine has been recognized

as a potential means for control of vehicle pollutant emissions

with minimum loss of fuel economy As a consequence the

various stratified charge concepts have been the focus of

renewed interest

152

12 Advantages and Disadvantages of Lean Mixture Operation

Fuel-lean combustion as achieved in a number of the stratified

charge engine designs receiving current attention has both

advantages and disadvantages wnen considered from the comshy

bined standpoints of emissionsmiddot control vehicle performance

and fuel economy

Advantages of lean mixture operation include the following

Excess oxygen contained in lean mixture combustion

gases helps to promote complete oxidation of hydroshy

carbons (HG) and carbon monoxide (CO) both in the

engine cylinder and in the exhaust system

Lean mixture combustion results in reduced peak

engine cycle temperatures and can therefore yield

lowered nitrogen oxide (NOx) emissions

Thermodynamic properties of lean mixture combustion

products are favorable from the standpoint of engine

cycle thermal efficiency (reduced extent cf dissociashy

tion and higher effective specific heats ratio)

Lean mixture operation caG reduce or eliminate the

need for air throttling as a means of engine load

control The consequent reduction in pumping losses

can result in significantly improved part load fuel

economy

153

Disadvantages of lean mixture operation include the following

Relatively low combustion gas temperatures during

the engine cycle expansion and exhaust processes

are inherent i~ lean mixture operation As a conseshy

quence hydrocarbon oxidation reactions are retarded

and unburned hydrocarbon exhaust emissions can be

excessive

Engine modifications aimed at raising exhaust temperashy

i tures for improved HC emissions control (retarded middot~

ignition timing lowered compression ratlo protrtacted combustion) necessarily impair engine fuel economy1 I

1j bull If lean mixture operation is to be maintained over ~

the entire engine load range maximum power output t l and hence vehicle performance are significantly

impaired

Lean mixture exhaust gases are not amenable to treatshy

ment by existing reducing catalysts for NOx emissions

control

Lean mixture combustion if not carefully controlled

can result in formation of undesirable odorant

materials that appear ln significant concentrations

in the engine exhaust Diesel exhaust odor is typical

of this problem and is thought to derive from lean mixshy

ture regions of the combustion chamber

154

Measures required for control of NOx emissions

to low levels (as example EGR) can accentuate

the above HC and odorant emissions problems

Successful developmentmiddotor the several stratified charge

engine designs now receiving serious attention will depend

very much on the balance that can be achieved among the

foregoing favorable and unfavorable features of lean comshy

bustion This balance will of course depend ultimately on

the standards or goals that are set for emissions control

fuel economy vehicle performance and cost Of particular

importance are the relationships between three factors -

UBHC emissions NOx emissions and fuel economy

13 Stratified Charge Engine Concepts

Charge stratification permitting lean mixture operation has

been achieved in a number of ways using differing concepts

and design configurations

Irrespective of the means used for achieving charge stratifishy

cation two distinct types of combustion process can be idenshy

tified One approach involves ignition of a small and

localized quantity of flammable mixture which in turn serves

to ignite a much larger quantity of adjoining or sur~rounding

fuel-lean mixture - too lean for ignition under normal cirshy

cumstances Requisite m1xture stratification has been achieved

155

in several different ways rangiDg from use of fuel injection

djrectly into open combustion chambers to use of dual

combustion chambers divided physically into rich and lean

mixture regions Under most operating conditions the

overall or average fuel-air ratio is fuel-lean and the

advantages enumerated above for lean operation can be realized

A second approach involves timed staging of the combustion

process An initial rich mj_xture stage in which major comshy

bustion reactions are completed is followed by rapid mixing

of rich mixture combustion products with an excess of air

Mixing and the resultant temperature reduction can in

principle occur so rapidly that minimum opportunity for NO

formation exists and as a consequence NOx emissions are

low Sufficient excess air is made available to encourage

complete oxidation of hydrocarbons and CO in the engine

cylinder and exhaust system The staged combustion concept

has been specifically exploited 1n so-called divided-chamber

or large volume prechamber engine designs But lt will be

seen that staging is also inherent to some degree in other

types of stratified charge engines

The foregoing would indicate that stratified charge engines

can be categorized either as lean burn engines or staged

combustion engines In reality the division between conshy

cepts is not so clear cut Many engines encompass features

of both concepts

156

14 Scope of This Report

During the past several years a large number of engine designs

falling into the broad category of stratified charge engines

have been proposed Many of these have been evaluated by comshy

petent organizations and have been found lacking in one or a

number of important areas A much smaller number of stratified

charge engine designs have shown promise for improved emissions

control and fuel economy with acceptable performance durashy

bility and production feasibility These are currently

receiving intensive research andor development efforts by

major organizations - both domestic and foreign

The purpose of this report is not to enumerate and describe the

many variations of stratified charge engine design that have

been proposed in recent years Rather it is intended to focus

on those engines that are receiving serious development efforts

and for which a reasonably Jarge and sound body of experimental

data has evolved It is hoped that this approach will lead to

a reliable appraisal of the potential for stratified charge

engine systems

20 Open-Chamber Stratified Charge Engines

21 General

From the standpoint of mechanical design stratified charge

engines can be conveniently divided into two types open-chamber

and dual-chamber The open-chamber stratjfied charge engine

has a long history of research lnterest Those crigines

157

reaching the most advanced stages of development are probably

the Ford-programmed c~mbustion process (PROC0) 2 3 and Texacos

controlled combustion process (TCCS) 4 5 Both engines employ a

combination of inlet aar swirl and direct timed combustion

chamber fuel injection to achieve a local fuel-rich ignitable

mixture near the point of ignition _For both engines the overshy

all mixture ratio under most operating conditions is fuel lean

Aside from these general design features that are common to

the two engiries details of their respective engine_cycle proshy

cesses are quite different and these differences reflect

strongly in comparisons of engine performance and emissions

characteristics

22 The Ford PROCO Engin~

221 Description

The Ford PROCO engine is an outgrowth of a stratified charge

development program initiated by Ford in the late 1950s The

development objective at that time was an engine having dieselshy

like fuel economy but with performance noise levels and

driveability comparable to those of conventional engines In

the 1960s objectives were broadened to include exhaust

emissions control

A recent developmental version of the PROCO engine is shown in

Figure 2-1 Fuel is injected directly into the combustion chamber

during the compression stroke resulting in vaporjzation and

formation of a rich mixture cloud or kernel in the immediate

158

vicinity of the spark plug(s) A flame initiated in this rich

mixture region propagates outwardly to the increasingly fuelshy

lean regions of the chamber At the same time high air swirl

velocities resulting from special orientation of the air inlet

system help to promote rapid mixing of fuel-rich combustion

products with excess air contained in the lean region Air

swirl is augmented by the squ1sh action of the piston as it

approaches the combustion chamber roof at the end of the comshy

pression stroke The effect of rapid mixing can be viewed as

promoting a second stage of cori1bustion in which rlch mixture

zone products mix with air contained in lean regions Charge

stratification permits operation with very lean fuel-air mixshy

tures with attendent fuel economy and emissj_ons advantages In

addition charge stratification and direct fuel injection pershy

mit use of high compression ratios with gasolines of moderate

octane quality - again giving a substantial fuel economy

advantage

Present engine operation includes enrichment under maximum

power demand conditions to mixture ratios richer than

stoichiometric Performance therefore closely matches

that of conventionally powered vehicles

Nearly all PROCO development plans at the present time include

use of oxidizing catalysts for HC emissions control For a

given HC emissions standard oxidizing catalyts permit use

of leaner air-fuel ratios (lower exhaust temperatures)

1

l

159

together with fuel injection and ignition timing charactershy

istics optimized for improved fuel economy

222 Emissions and Fuel Economy

Figure 2-2 is a plot of PROCO vehicle fuel economy versus NOx

emissions based or1 the Federal CVS-CH test procedure Also

included are corresponding HC and CO emissions levels Only

the most recent test data have been plotted since these are

most representative of current program directions and also

reflect most accurately current emphasis on improved vehicle

fuel economy 6 7 For comparison purposes average fuel

economies for 1974 production vehicles weighing 4500 pounds

and 5000 pounds have been plotted~ (The CVS-C values

reported in Reference 8 have been adjusted by 5 to obtain

estimated CVS-CH values)

Data points to the left on Figure 2-2 at the o4 gmile

NOx level represent efforts to achieve statutory 1977

emissions levels 6 While the NOx target of o4 gmile was

met the requisite use of exhaust gas recirculation (EGR)

resulted in HC emissions above the statutory level

A redefined NOx target of 2 gn1ile has resulted in the recent

data points appearing in the upper right hand region of

Figure 2-2 7 The HC and CO emissions values listed are

without exhaust oxidation catalysts Assuming catalyst middotl

conversion efficiencies of 50-60 at the end of 50000 miles

of operation HC and CO levels will approach but not meet

160

statutory levels It is clear that excellent fuel economies

have been obtained at the indlcated levels of emissions

control - some 40 to 45 improved re1at1ve to 1974 produc-

tj_on vehicle averages for the same weight class

The cross-hatched horizontal band appearing across the upper

part of Figure 2-2 represents the reductions in NOx emissions

achieveble with use of EGR if HC emissions are unrestricted

The statutory 04 gmile level can apparently be achieved

with this engine with little or no loss of fuel economy but

with significant increases in HC emissions The HC increase

is ascribed to the quenching effect of EGR in lean-middotmixture

regions of the combustion chamber

223 Fuel Requirements

Current PROCO engines operated v1ith 11 1 compression ratio

yield a significant fuel economy advantage over conventional

production engines at current compression ratios According

to Ford engineers the PROCO engine at this compression

ratio j_s satisfied by typical fu1J-boi1ing commercial gasoshy

lines of 91 RON rating Conventional engines are limited to

compression ratios of about 81 and possibly less for

operation on similar fuels

Results of preliminary experiments indicate that the PROCO

engine may be less sensitive to fuel volatility than convenshy

tional engines - m1 important ff1ctor in flextb1 llty from the

standpoint of the fuel supplier

161

224 Present Status

Present development objectives are two-fold

Develop calibrations for alternate emissions target

levels carefully defining the fueleconofuy pbtenshy

tial associated with each level of emissions control

Convert engine and auxiliary systems to designs

feasible for high volume production

23 The Texaco TCCS Stratified Charge Engine

231 General Description

Like the Ford PROCO engine Texacos TCCS system involves_

coordinated air swirl and direct combustion chamber fuel

injection to achieve charge stratification Inlet portshy

induced cylinder air swirl rates typically approach ten times

the rotational engine speed A sectional view of the TCCS

combustion chamber is shown in Figure 2-3

Unlike the PROCO engine fuel injection in the TCCS engine

begins very late in the compression stroke - just before th~

desired time of ignition As shown in Figure 2-4 the first

portion of fuel injected is immediately swept by the swirling

air into the spark plug region where ignition occurs and a

flame front is established The continuing stream of injected

fuel mixes with swirling air and is swept into the flame

region In many respects the Texaco process resembles the

162

spray burning typical of dj_esel combustion ~r1th the difshy

ference that ignition is achieved by energy from an elec-

tric spark rather than by high compression temperatures

The Texaco engine like the diesel engine does not have a

significant fuel octane requirement Further use of positive

spark ignition obviates fuel I

cetane requirements character-

istic of diesel engines The resultant flexibility of the

TCCS engine regarding fuel requirements is a si~1ificant

attribute

In contrast to the TCCS system Fords PROCO system employs

relatively early injection vaporization and mixing of fuel

with air The combustion process more closely resembles the

premixed flame propagation typical of conventional gasoline

engines The PROCO engine therefore has a definite fuel

octane requirement and cannot be considered a multifuel

system

The TCCS engine operates with hi__gh compression ratios and

with little or no inlet air throttling except at idle conshy

ditions As a consequence fuel economy is excellent--both

at full load and under part load operating conditions

232 Exhaust Emissions and Fuel Economv

Low exhaust temperatures characteristlc of the TCCS system

have necessitated use of exhaust oxidation catalysts for

control of HC emissions to low lf~Vels A11 recent development

163

programs have therefore included use of exhaust oxidation

catalysts and most of the data reported here r~present tests

with catalysts installed or with engines tuned for use with

catalysts

Figures 2-5 and 2-6 present fuel economy data at several

exhaust emissions levels for two vehicles--a US Army M-151

vehicle with naturally aspirated 4-cylinder TCCS conversion

and a Plymouth Cricket with turbocharged 4-cylinder TCCS

engine 9 10 1urbocharging has been used to advantage to

increase maximum power output Also plotted in these figures

I are average fuel economies for 1974 production vehicles of

similar weight 8

I When optimized for maximum fuel economy the rrccs vehicles

can meet NOx levels of about 2 gmile It should be noted

that these are relatively lightueight vehicles and that

increasing vehicle weight to the 4000-5000 pound level could

result in significantly increased NOx emissions Figur~s 2-5

and 2-6 both show that engine modifications for reduced NOx

levels including retarded combustion timing EGR and increased

exhaust back pressure result in substantial fuel economy

penalties

For the naturally aspirated engine reducing NOx emissions

from the 2 gmile level to O l~ gmile incurred a fuel

economy penalty of 20 Reducing NOx from the tllrbocharged

164

engine from 15 gmile to 04 gmile gave a 25 fuel economy

penalty Fuel economies for both engines appear to decrease

uniformly as NOx emissions are lowered

For the current TCCS systems most of the fuel economy penalty

associated with emissions control can be ascribed to control

of NOx emissions although several of the measures used for

NOx control (retarded cornbusticn timing and increased exhaust

back pressure) also help to reduce HG emissions HC and CO

emissions ari effectively controlled with oxidation catalysts

resulting in relatively minor reductions in engine efficiency

233 TCCS Fuel Reauirements

The TCCS engine is unique among current stratified charge

systems in its multifuel capability Successful operation

with a nuraber of fuels ranging from gasoline to No 2 diesel

Table 2-I

Emissions and Fuel Economy of Turbocharged TCCS Engine-Powered Vehicle 1

Fuel

Emissions gMile 2 Fuel Economy

mng 2HC co NOx

Gasoline

JP-4

100-600

No 2 Diesel

033

026

014

027

104

109

072

J bull l ~

-

061

050

059

060

197

202

213

230

1M-151 vehicle 8 degrees coffibustion retard 16 light load EGR tw0 catalysts (Ref 10)

2 CVS-CH 2750 pounds tnert1a welght

165

l

has been demonstrated Table ~-I lists emissions levels and

fuel economies obtained with a turbocharged TCCS-powered

M-151 vehicle when operated on each of four different fuels 10

These fuels encompass wide ranges in gravity volatjlity

octane number and cetane leve 1 as middotshown in Table 2-II

Table 2-II

Fuel Specifications for TCCS Emissions Tests (Reference 10)

Gravity 0 API Sulfur

OFDistillation~

Gasolj_ne 100-600 JP-4 No 2

Diesel

88 -

86 124 233 342 388

0024 912

-

486 012

110 170 358 544 615

0002 57 356

541 0020

136 230 314 459 505

-middot --

369 0065

390 435 508 562 594

--

lta 9

IBP 10 50 90 EP

TEL gGal Research Octane Cetane No

Generally the emissions levels were little affected by the

wide variations in fuel properties Vehicle fuel economy

varied in proportion to fuel energy content

As stated above the TCCS engine is unique in its multifuel

capability The results of Tables 2-I and 2-II demonshy

strate that the engine has neither 8ign1ficant fuel octane

nor cetane requirements and further that it can tolerate

166

wide variations j_n fuel volati1tty rhe flexibility offered

by this type of system could be of major importance in

future years

234 Durability Performance Production Readiness

Emissions control system durability has been demonstrated by

mileage accumulation tests Ignltion system service is more

severe than for conventional engines due to heterogeneity of

the fuel-air mixture and also to the high compression ratios

involved The ignition system has been the subject of

intensive development and significant progress in system

reliability has been made

A preproduction prototype engine employing the TCCS process is

now being developed by the Hercules Division of White Motors

Corporation under contract to the US Army Tank Automotive

Command Southwest Research Inr)titute will conduct reliability

tests on the White-developed enGines when installed in Military

vehlcles

30 Small Volume Prechambcr Eng1nes (3-Valve Prechamber Engines Jet Ignition Engines Torch Ignition Engines)

31 General

A number of designs achieve charge stratification through

division of the combustion region into two adjacent chambers

The emissions reduction potentiampl for two types of dualshy

chamber engines has been demonstrated F1 rst ~ j n B desJgn

trad1t1on~JJy caJJld the nrreebrnber engine a 2m211 auxil1ary

167

or ignition chamber equipped w1th a spark plug communicates

with the much larger main combustion chamber located in the

space above the piston (Figure 3-1) The prechamber which

typically contains 5-15 of the total combustion volume

is supplied with a small quantity of fuel-rich ignitable

fuel-air mixture while a large quantity of very lean and

normally unignitable mixture is applied to the main chamber

above the piston Expansion of high temperature flame

products from the prechamber leads to ignition and burning

of the lean maj_n chamber fuel-a_r charge Ignitionmiddot and

combustion in the lean main chamber region are promoted both

by the high temperatures of prechamber gases and bythe

mixing that accompanies the jet-like motion of prechamber

products into the main chamber

I jl

I i j

I

Operation with lean overall mixtures tends to limit peak comshy

bustion temperatures thus minimizing the formation of nitric

oxide Further lean mixture combustion products contain

sufficient oxygen for complete oxidation of HC and CO in the

engine cylinder and exhaust system

It should be reemphasized here that a iraditional problem

with lean mixture engines has been low exhaust temperatures

which tend to quench HC oxidation reactions leading to

excessive emissions

Control of HC emissions to low levels requires a retarded or

slowly developing combustion process The consequent extenshy

sion of heat release j nto 1ate porttt)ns of the engtne cycle

168

tends to raise exhaust gas temperatures thus promoting

complete oxidation of hydrocarbons and carbon monoxide

32 Historical Background and Current Status

321 Early Developm9nt Objectives and Engine Def igns

The prechamber stratified charge engine has existed in various

forms for many years Early work by Ricardo 1 indicated that

the engine could perform very efficiently within a limited

range of carefully controlled operating conditions Both

fuel-injected and carbureted prechambcr engines have been

built A fuel-injected design Lnittally conceived by

Brodersen 11 was the subject of extensive study at the

University of Rochester for nearly a decade 12 13 Unforshy

tunately the University of Rochester work was undertaken prior

to widespread recognition of the automobile emissions problem

and as a consequence emission characteristics of the

Brodersen engine were not determined Another prechamber

engine receiving attention in the early 1960s is that conshy

ceived by R M Heintz 14 bull The objectives of this design

were reduced HC emissions incr0ased fuel economy and more

flexible fuel requirements

Experiments with a prechamber engine design called the torch

ignition enginen were reported n the USSR by Nilov 15

and later by Kerimov and Mekhtier 16 This designation

refers to the torchlike jet of hot comhust1on gases issuing

169

from the precombustion chamber upon j_gnj_ tion In a recent

publication 17 Varshaoski et al have presented emissions

data obtained with a torch ignition engine These data show

significant pollutant reductions relative to conventional

engines however their interpretation in terms of requireshy

ments based on the Federal emissions test procedure is not

clear

l

3 2 2 Current DeveloJ)ments

A carbureted middotthree-valve prechamber engine the Honda CVCC

system has received considerable recent attention as a

potential low emissions power plant 18 This system is

illustrated in Figure 3-2 Hondas current design employs a

conventional engine block and piston assembly Only_ the

cylinder head and fuel inlet system differ from current

automotive practice Each cylinder is equipped with a small

precombustion chamber communicating by means of an orifice

with the main combustion chambe situated above the piston lj

ij_ A small inlet valve is located in each precharnber Larger

inlet and exhaust valves typical of conventlonal automotive

practice are located in the main combustion chamber Proper

proportioning of fuel-air mixture between prechamber and

main chamber is achieved by a combination of throttle conshy

trol and appropriate inlet valve timing A relatively slow

and uniform burning process gjvjng rise to elevated combusshy

tion temperatures late in the expansion stroke and during

the exhaust procezs is achieved H1 gh tewperaturr--s in thin

part of the engine cycle ar-e necessary to promote complete

170

oxidation of HC and CO It si1ould be no~ed that these

elevated exhaust temperatures are necessarily obtained at

the expense of a fuel economy penalty

To reduce HC and CO emissions to required levels it has been

necessary for Honda to employ specially designed inlet and

exhaust systems Supply of extremely rich fuel-air mixtures

to the precombustion chambers requires extensive inlet manifold

heating to provide adequate fuel vaporization This is accomshy

plished with a heat exchange system between inlet and exhaust

streams

To promote maximum oxidation of HC and CO in the lean mixture

CVCC engine exhaust gases it has been necessary to conserve

as much exhaust heat as possible and also to increase exhaust

manifold residence time This has been done by using a relashy

tively large exhaust manifold fitted with an internal heat

shield or liner to minimize heat losses In additj_on the

exhaust ports are equipped with thin metallic liners to

minimize loss of heat from exhaust gases to the cylinder

head casting

Engines similar in concept to the Honda CVCC system are under

development by other companies including Ttyota and Nissan

in Japan and General Motors and Fo~d in the United States

Honda presently markets a CVCC-powered vehicle tn tTapan and

plans US introduction in 1975 Othe~ manufactur~rs

includlnr General Motors and Forgtd 1n thr U S havf~ stated

171

that CVCC-type engines could be manufactured for use in limited

numbers of vehicles by as early as 1977 or 1978

33 Emissions and Fuel Economywith CVCC-Type Engines

331 Recent Emissions Test Results

Results of emissions tests with the Honda engine have been very

promising The emissions levels shown in Table 3-I are typical

and demonstate that the Honda engine can meet statutory 1975-1976

HC and CO stindards and can approach the statutory 1976 NOx

standard 19 Of particular importance durability of this

system appears excellent as evidenced by the high mileage

emissions levels reported in Table 3-I Any deterioration of

l emissions after 50000 miles of engine operation was slight

and apparently insignificant

I Table 3-I

Honda Compound Vortex-Controlled Combustion-Powered Vehicle 1 Emissions

Fuel Economy

Emissions 2 mpg gMile 1972

HC 1975 FTP FTPco NOv

210 50000-Mile Car+ No 2034 Low Mileage Car 3 No 3652 018 212 221089

024 065 198 1976 Standards

213175 20o41 34 - -04o411977 Standards 34 - -

1Honda Civic vehicles 2 1975 CVS C-H procedure with 2000-lb inertia weight3Average of five tests aAverage of four tests

172

Recently the EPA has tested a larger vehicle conve~ted to the

Honda system 20 This vehicle a 1973 Chevrolet Impala with

a 350-CID V-8 engine was equipped with cylinder heads and

induction system built by Honda The vehicle met the present

1976 interim Federal emissions standards though NOx levels

were substantially higher than for the much lighter weight

Honda Civic vehicles

Results of development tests conducted by General Motors are

shown in Table 3-II 21 These tests involved a 5000-pound

Chevrolet Impala with stratified charge engine conversion

HC and CO emissions were below 1977 statutory limits while

NOx emissions ranged from 15 to 2 gmile Average CVS-CH

fuel ec9nomy was 112 miles per gallon

Table 3-II

Emissions and Fuel Economy for Chevrolet Impala Strmiddotatified

Charge Engine Conversion (Ref 21)

Test

Exhaust Emlssions

gMile 1 Fuel

Economy mpgHC co NOx

1 2 3 4 5

Average

020 026 020 029 0 18

023

25 29 31 32 28

29

17 15 19 1 6 19

17

108 117 114 109 111

112

1cvs-CH 5000-lb inertia weight

173

I

332 HC Control Has a Significant Impact on Fuel Economy

In Figure 3-3 fuel economy data for several levels of hydroshy

carbon emissions from QVCC-type stratified charge engines

are plotted 22 23 ~ 24 At the 1 gmile HC level stratified

charge engine fuel economy appears better than the average

fuel economy for 1973-74 production vehicles of equivalent

weight Reduction of HC emissions below the 1-gram level

necessitates lowered compression ratios andor retarded

ignition timing with a consequent loss of efficiencymiddot For

the light-weight (2000-pound) vehicles the O~ gmile IIC

emissions standard can be met with a fuel economy of 25 mpg

a level approximately equal to the average of 1973 producshy

tion vehicles in this weight class 8 For heavier cars the

HC emissions versus fuel economy trade-off appears less

favorable A fuel economy penalty of 10 relative to 1974

production vehicles in the 2750-pound weight class is

required to meet the statutory 04 gmile HC level

333 Effect of NOx Emissions Control on Fuel Economy

Data showing the effect of NOx emissions control appear in

Figure 3-~ 22 These data are based on modifications of a Honda

CVCC-powered Civic vehicle (2000-pound test weight) to meet

increasingly stringent NOx standards ranging from 12 gmile

to as low as 03 gmile For all tests HC and CO emissions

are within the statutory 1977 standards

NOx control as shown in Figure 3-4 has been effected by use

of exhaust gas recirculation 1n comb1nation w1th retarded

174

ignj_tion timing It is clear that control of rmx emissions

to levels below l to 1 5 gmile results in stgnificant fuel

economy penalties The penalty increases uniformly as NOx

emissions are reduced ~nd appears to be 25 or more as the

04 gmile NOx level is approached

It should be emphasized that the data of Fisure 3-4 apply

specifically to a 2000-pound vehicle With increased vehicle

weight NOx emissions control becomes more difficult and the

fuel economy penalty more severe The effect of vehicle

weight on NOx emissions is apparent when comparing the data

of Table 3-I for 2000-pound vehicles with that of Table 3-II

for a 5000-pound vehicle While HC and CO emissio~s for the

two vehicles are roughly comparable there is over a factor

of two difference in average NOx emissions

34 Fuel Requirements

To meet present and future US emissions control standards

compression ratio and maximum ignltion advance are limited

by HC emissions control rather than by the octane quality of

existing gasolines CVCC engines tuned to meet 1975 California

emissions standards appear to be easily satisfied with

presently available 91 RON commercial unleaded gasolines

CVCC engines are lead tolerant and have completed emissions

certification test programs using leaded gasolines However

with the low octane requirement of the CVCC engine as noted

above the economic benefits of lead antlknock compoundt ar-euromiddot

not realized

175

It is possible that fuel volatLLity characteristlcs may be of

importance in relation to vaporization within the high

temperature fuel-rich regions of the prechamber cup inlet

port and prechamber iQlet manifold However experimental

data on this question aomiddot not appear to be available at

present

~O Divided-Chamber Staged Combustion Engines (Large-Volume Prechamber Engines Fuel-Injected Blind Prechamber Engines)

41 General

Dual-chamber engines of a type often called divided-chamber

or large-volume prechamber engines employ a two-stage comshy

bustion process Here initial r~ich mixture combustion and

heat release (first stage of combustion) are followed by rapid

dilution of combustion products with relatively low temperature

air (second stage of combustion) The object of this engine

design is to effect the transitjon from overall rich combustion

products to overall lean products with sufficient speed that

time is not available for formation of significant quantities

of NO During the second low temperature lean stage of

combustion oxidation of HC and CO goes to completion

An experimental divided-chamber engine design that has been

built and tested is represented schematically in Figure ~-1 25 26

A dividing orifice (3) separates the primary combustion

chamber (1) from the secondary combustion chamber (2) which

includes the cylinder volume above the piston top A fuel

injector (4) supplies fuel to the primary chamber only

176

Injection timing is arranged such that fuel continuously

mixes with air entering the primary chamber during the

compression stroke At the end of compression as the

piston nears its top center position the primary chamber

contains an ignitable fuel-air mixture while the secondary

chamber adjacent to the piston top contains only air

Following ignition of the primary chamber mixture by a spark

plug (6) located near the dividing orifice high temperature

rich mixture combustion products expand rapidly into and mix

with the relatively cool air contained in the secondary

chamber The resulting dilution of combustion products with

attendant temperature reduction rapidly suppresses formation

of NO At the same time the presence of excess air in the

secondary chamber tends to promote complete oxidation of HC

and CO

42 Exhaust Emissions and Fuel Economy

Results of limited research conducted both by university and

industrial laboratories indicat~ that NOx reductions of as

much as 80-95 relative to conventional engines are possible

with the divided-chamber staged combustion process Typical

experimentally determined NOx emissions levels are presented

in Figure 4-2 27 Here NOx emissions for two different

divided-chamber configurations 8re compared with typical

emissions levels for conventional uncontrolled automobile

engines The volume ratio 8 appearing as a parameter in

Figure 4-2 represents the fraction of total combustion volume

contained in the primary chamber For a values approaching

I

i J_

177

1

05 or lower NOx emissions reach extremely low levels Howshy

ever maximum power output capability for a given engine size

decreases with decreasing 6 values Optimum primary chamber

volume must ultimately_represent a compromise between low

emissions levels and desired maximum power output

HC and particularly CO emissions from the divided-chamber

engine are substantially lower than eonventional engine

levels However further detailed work with combustion

chamber geometries and fuel injection systems will be necesshy

sary to fully evaluate the potential for reduction of these

emissions

i Recent tests by Ford Motor Company show that the large volume

prechamber engine may be capable of better HC emissions conshy

trol and fuel economy than their PROCO engine This is shown

by the laboratory engine test comparison of Table 4-I 19

Table 4-I

Single-Cylinder Low Emissions middot11 ~ _____En____g__~ne __middot _e_s_-_s_____

Engine

NO--X Reduction

Method

Em1ssions g1 hp-Hr

Fuel Economy

Lb1 hp-HrNOv HC- co

PROCO

Divided Chamber

PROCO

Divided Chamber

EGR

None

EGR

None

10 30

10 04

05 ~o

o J_o 75

130

25

l 1i bull 0

33

0377

0378

0383

0377

178

Fuel injection spray characteristics are critical to control

of HC emissions from this type of engine and Fords success

in this regard is probably due in part to use of the already

highly developed PROCO-gasoline injection system Figure 4-3

is a cutaway view of Fords adaptation of a 400-CID V-8 engine

to the divided-chamber system 2 e

Volkswagen (VW) has recently published results of a program

aimed at development of a large volume precharnber engine 29

In the Volkswagen adaptation the primary chamber which comshy

prises about 30 of the total clearance volume is fueled by a

direct timed injection system and auxiliary fuel for high

power output conditions is supplied to the cylinder region by

a carburetor

Table 4-II presents emissions data for both air-cooled and

water-cooled versions of VW s dtvided-middotchamber engine 3 0

Emissions levels while quite low do not meet the ultimate

1978 statutory US standards

179

Table 4-II

Volkswagen Jarge Volume _Jrechamber Er[ Lne Emissions

Exhaust Emissions

_ _gMile 1

___E_n_gi_n_e__t--H_C___c_o__N_O_x____E_ng__i_n_e_S_p_e_c_i_f_i_c_a_tmiddot_1_middoto_n_s__

20 50 09 841 compression ratio Air-Cooled 16-Liter

prechamber volume 28 of total clearance volume conventional exhaust manishyfold direct prechamber fuel injection

20-Liter 10 40 10 91 compression ratio Water-Cooled prechamber volume 28 of

total clearance volume simple exhaust manifold reactor direct prechamber fuel injection

1cvs c-H

Toyota also has experimented wlth ___a large volume prechamber

engine using direct prechamber fuel injection and has

reported emissions levels comparable to those of Table 4-II 31

43 Problem Areas

A number of major problems inherent in the large volume

prechamber engine remain to be 3olved I~ These problems include the following II

Fuel injection spray characteristics are critically

important to achieving acceptable HC emissions

The feasibility of producing asatisfactory injecshy

tion system hasnot been estab1ished

180

Combustion noise due to high turbulence levels and

hence high rates of heat release and pres[-ure rise

in the prechamber can be excessive It has been

shown that the-noise level can be modified through

careful chamber design and combustion event timing

If the engine is operated with prechamber fuel

injection as the sole fuel source maximum engine

power output is limited This might be overcome

by a~xiliary carburetion of the air inlet for maximum

power demand or possibly by turbocharging Either

approach adds to system complexity

The engine is charmiddotaeter1zed by low exhaust temperatures

typical of most lean mixture engines

References

1 Ricardo H R Recent Research Work on the Internal Combustion Engine 11 SAE Journal Vol 10 p 305-336 (1922)

2 Bishop I N and Simko A Society of Automotive Engineers Paper 680041 (1968)

3 Simko A Choma M A and Repco L L Society of Automotive Engineers Paper 720052 (1972)

4 Mitchell E Cobb JM and Frost R A Society of Automotive Engineers Paper 680042 (1968)

5 Mitchell E Alperstein M and Cobb JM Society of Automotive Engineers Paper 720051 (1972)

6 1975-77 Emission Control Program Status Report submitted to EPA by Ford Motor Company November 26 1973

181

if

7 consultant Report on Emissions Control of Engine Systems National Academy of Sciences Committee on Motor Vehicle Emissions Washington DC September 1974

8 Austin T C and Hellman K H Society of Automotive Engineers Paper 730790 (1973)

9 See Ref 7

10 Alperstein M Schafer G H and Villforth F J Iiil SAE Paper 740563 (1974)

11 US Patent No 2615437 and No 2690741 Method of Operating Internal Combustion Engines Neil O Broderson Rochester New York

12 Conta L~ D and Pandeli American Society of Mechanical Engineers Paper 59-SA-25 (1959)

13 Canta L D and Pandeli American Society of Mechanical Engineers Paper 60-WA-314 (1960)

14 US Patent No 2884913 0 Internal Combustion Engine R Mi Heintz i

15 Nilov N A Automobilnaya Promyshlennost No 8 (1958)

l 16 Kerimov N A and Metehtiev R I Automobilnoya Promyshlennost No 1 p8-11 (1967)

17 Varshaoski I L Konev B F and Klatskin V B Automobilnaya Promyshlennost No 4 (1970)

18 An Evaluation of Three Honda Compound Vortex Controlled Combustion (CVCC) Powered Vehicles Report B-11 issued by Test and Evaluation Branch Environmental Protection Agency December 1972

19 Automotive Spark Ignition Engine Emission Control Systems to Meet Requirements of the 1970 Clean Air Amendments report of the Emissions Control Systems Panel to the Committee on Motor Vehicle Emissions National Academy of Sciences May 1973

20 An Evaluation of a 300-CID Compound Vortex Controlled Combustion (CVCC) Powered Chevrolet Impala Report 74-13 DWP issued by Test and Evaluation Branch Environmental Protection Agency October 1973

21 See Ref 7

22 See Ref 7

23 See Ref 7

24 See Ref 7

182

25 Newhall H K and El-Messiri I A Combustion and Flame 14 p 155-158 (1970)

26 Newhall H K and El-Messiri I A Society of Automotive Engineers Transaction Ford 78 Paper 700491 (1970)

27 El-Messiri I A and Newhall H K Proc Intersociety Energy Conversion Engineering Conference p 63 (1971)

28 See Ref 7

29 Decker G and Brandstetter W MTZ Motortechnische Zeitschrift Vol 34 No 10 p 317-322 (1973)

30 See Ref 7

31 See Ref 7

183

Fig 2-1 FORD PROCO ENGINE

l

Ford Proco Engine Fuel Economy and Emissions _ 15 _ f--1

00 +

I ~ x X gt( X _ x A 7- ~ X x~ ~c - l4catalyst Feed u NOx vs ruel Econ with 1 C0-71 CJ) 14 x x Ynn H( RP c tr ir-t irm vltgtZ G I HC - C0-127 _ A txcessve c

13 Approx W EG R

~ C~~r 351 CID 5000 Lb Inertia Weight

Q 21 A L 0 u w II _j

LJ =gt LL

10

35i CD 4500 Lb Inertia Weight

~ 1974 Production Average Fuel Economy

4 soo _b r-r-r-----z~lt_~~---7--_~--r--1r-7-r1--~-rz7-w~~

150 0 0 Lb PU221ufrac122-1 I

LO 20 30

NOx EMISSIONS-GMSMILE (CVS-CH) Revised216174

0

HKN 71074

Fig 2-2

l

~___-~ ~--=---~ ~=---__---~1 f-=-----1__middot-_~J ~-----------1 ~bull-=-=- (-~-~ LJii-ZJj ~ ~~-~ ~~ -__c~~ 1--~~ ~----~--1 ---------s___-c--1 ~~~-~~~bull r~~-~--middot1 ____c__ J~ p- ~

Texaco TCCS Engine

Shrouded Intake Valve

~ Intakemiddot r~ )p__-- Fuel Nozzle Fuel Nozzte Port ~ -- -yen -_~

X f -J J ( ~1 I --- ~ f middotmiddotj_Ja 1(~-~_ frff 1-Cylinderv~ v_ r--L~ I (~~)J ~- Intake 1 - ------L- middotmiddot - middotmiddot -1 H0 ad middot --- - -- 1 Po rt I 1 I ~~ ) ~ ~ ~~~ -A- I ------

- I _ ---_ ~ P1ston-mgt-lt_ffrac12 T_77~~~--1 i- r_-~J N

- ~- i~-L - _ _ - IExhaust - - I ~ - 1-_ r- bullsect ~ ----lt_ ~ I PortJ~bJ lt 7A--7~ ~1 ~j --~ ~ yl ind er

-__~lli- klmiddot ~ro v_t_gt11J1bull Bti Or K__ - middot ~

I t--tL pgt-- Ultmiddot middot- - Spark Plugr- -1 --U2middot- ~-~

LHorizont al Projections of Nozzle and Spark Plug Centerlines

Fig 2-3 i--1 00 U1

---~---~-~ -------c- --~--- 7middot-r---c-- ~- -~~~==---~~~~~- srsr RZIIEF7 11t111-~-----==-----=-~--~-~~---c=rmiddot=

OPEN CHAMBER TYPE STRATI Fl ED CHARGE ENGINE i-shyCj

DIRECTIONAl~Fsw7 Q

NOZZLE P

I

~J~treg lt-_(__(lt-(11

c_-- _7- -

SPARK PLUG_ l 1__- -_ - l --_ ~ ----__ lt_ lt_ -- --

ltlt_I_--- _

~ gt - _____- -- --~ ~-l_- 1_~ -~- ~ ------

~~~ r_I FUEL SPRAY 2 FUEL-AIR MIXING ZONE ~- _ -------

FLAME FRONT AREA 4 COMBUSTION PRODUCTS

TCCS COMBUSTION SYSTEM

Fig 2-4

3

----==-----~ l~~----bulli r-~ ~-----=-- 1 ~~ ~ -~ ~~ ___-_=gt---l p--- --=-=-_-__71-~-~~ 1-0-- --=---=-- 4 L--_-_-~ P--- ~

25

-c u

f

Cl) 24 gt u _

tgt 23a ~

I

gt-~ 220 2 0 u w 21 _J

lJJ gt LL

2

Texaco TCCS Powered Cricket Vehicle

Max Econ Setting gt A L07 HC

141 CID JQf CR 084 CO 2500 Lb Inertia Wgt

50-so Retard_ 0_73 HC

12 co 051 HC ~ 061 HC

085COA 064CO Retard+ ESPRetard+

EGR

036 HC ~ 115 co Retard +ESP+ EGR

04 06 08 10 12 14 16 18 20 NOx EMISSIONS-GMSMILE (CVS-CH) HtltN1110114

I- 00 -JFig 2-5

-~ ~=- ~ - -i______c_J ~-====c= wr=- ~-~ p--w~~~ rr w -

25

-c u

I

(f)

gt u-lt a_

2

gt-I 20

~ 0 z 0 u LLI

_J

w tJ_

15

I- CJ) CJ)

Turbocharged Texaco TCCS Ml51 Vehicle

Max Econ Adjustment_ HC-3J catalyst Feed C0-70

141 CID 10~1 CR 2750 Inertia Weight 8deg Retard ~

~bull HC-3middot2 catalyst Feed ~~ _ C0-64

_ 5deg Retard HC-0 30 8degRetard LowEGV bullco-11 ~bull HC-3middot6 catalyst Feed WIW21

Med EGR C0-67 1974 Production 33 Average Fuel Economy ~

COmiddoti05 (2750Lb)

I

bull HC-035 co- 141 13deg Retard High EGR

04 10 20 NOx EMISSIONS -GMSMILE (CVS-CH) ~~ts~b~~~74

Fig 2-6

189

Fig 3-1

PRECHAMBER TYPE STRATIFIED CHARGE ENGINE

r Inlet

(Fuel-lean Mixture )

I 0 I

Spark -Prechamber (Fuel-rich mixture)

-Main Chamber

1] HON DA CVCC ENGINE CONCEPT

190

Fig 3-2 Honda CVCC Engine

28 -l u

1

UJ 26 -gt u-(9 CL 24 2-

f

gtshy0gt

22 z ~ _)

u w

20 _J

w ~ LL

18

J= ---- 4 --~~-_----a ~~ _-_bull --~~ 1~~1 ltiil~I ~ ~-r~ ~ -~ ~-~ ~J~-iii-1 ~~1 s _-_ __-

Fuel Economy vs HC Emissions for 3-Valve Prechamber Engines

e NOx-14 15 Liter

bull Honda CVCC 2000 LbsNOx - 12 A Datsun NVCCbull15 Liter

bull ~JOx -09 A 2500 Lbs J LL 1ter NOv -15

2750 Lbs -NOx -17

- I AiJOx -12

0 02 04 06 08 LO 0HYDROCARBON EMiSSlmiddotONS - Glv1 I MILE (CVS-CH) I-

Fig 3-3

J--1

1--Fuel Economy vs NOx Emissions IO N

-- for Honda CVCC Powered Vehiclesr 26 u

l VHc-023 U1 gt umiddot 24_-__

(_IJ o_

~ 22 l

gt-5~-0 z 20 C0-200 u A HC-033w I co -3o_j

_A HC-029w 18 J I C0-27 LL

_ HC-025

HC-017 co -2-3

C0-22

0 -- 02 04 06middot 08 10 12 NOx Ef11SSIONS -GlviS MILE (CVS-CH)

Fig 3-4 middot

I

I

i93

J J

Fig 4-1 Divided Chamber Engine

middot(4) Fuel Injector

1

f J

f ff

f

~ Ii

I f

i

I f ] [

~~

0 0 0 0

i ~ I

1jl

194

E Cl 0

C QJ

CJl 0 _

-1-

z

0

Vl (lJ

-0

X 0

-t-J

V1 ro c X

LLI

Fig ~-2

COMPARISON OF CONVENTIONAL AND DIVIDED COMBUSTION CHAMBER NOx EMISSIONS

5000 MBT Ignition Timing Wide Open Ttl rattle

4000 Conventional Charnber

3000

J = fraction of Total Combustion 2000 Volume in Primary Ct1arnber

Divided Chamber 13 = 0 85

1000

Divided Chamber fo = 0 52

05 06 0 7 08 09 10 11

O~erall Fuel-Air Equivalence Ratio

195

196

AIRBORNE SURVEYS IN URBAN AIR BASINS IMPLICATIONS FOR MODEL DEVELOPMENT

by

Donald L Blumenthal Manager of Program Development

Meteorology Research Inc Altadena California 91001

middotI would like to make several points today First ozonemiddotis basically

a regional long-range problem There is a lot of long range ozone transshy

port and this transport is a normal occurrence The second point is that

ozone is stable in the absence of scavengers Junge mentions in his book

that the residence time of ozone in the troposphere is on the order of a

month Third vertical variations in concentration and ventilation rate are i very important in modeling atmospheres such as Los Angeles Layers aloft

are ventilated down to the surface on occasion and surface pollutants are

ventilated up mountain slopes as Jim Edinger has pointed out before and

often ventilated out of the basin in upper winds Fourth the day to day

carry over of pollutants from one day to the next is a very important considshy

eration in the Los Angeles Basin Finally there is a definite background

level of ozone The geophysical literature says its about O 02 to O 03 ppm (

in various parts of the world Weve seen data varying from 003 to 005 ppm

The difference may be due to calibration differences In any case numbers

like 005 are pretty substantial background levels for ozone

I am going to illustrate the points listed above with some data from

Los Angeles Basin The data were collected during a two-year study funded

by the Air Resources Board some of the analyses were funded by EPA The

study examined the three dimensional distribution of pollutants in the Los

Angeles Basin using airborne sampling systems Coinvestigators on the

project were Dr Ted Smith and Warren White of Meteorology Research Inc (MRI)

197

The first slide shows one of the aircraft we used Its a Cessna 205

which had sampling inlets on the side of the aircraft Figure 2 shows the

instrument system on the inside of the aircraft We were measuring nitrogen

oxides ozone scattering coefficient with a nephelometer condensation nuclei

carbon monoxide and meteorological parameters such as temperature humidity

turbulance Altitude and position were also measured

Figure 4 shows that the typical sampling pattern was a series of spirals

from the top of the mixing layer over an airport virtually to ground level

then we would climb up to the next point on the route and spiral down again

We had three routes (A B C Figure 3) that we would fly We had two airshy

craft and we would fly two of these three routes three times a day any

given day that we could The day I will be talking about September 25~ 1973

we flew what was called the Riverside route (C) and the Los Angeles route

(A) The 25th of July 1973 you might remember was the day before the

federal office buildings were closed in the area here because of smog

Figure 5 shows the surface streamlines at 0300 Pacific Standard Time

about 4 oclock in the morning daylight time on July 25 This streamline

analysis points out the morning stagnation conditions which are a very normal

occurrence in the Los Angeles Basin You start out with very light winds

quite variable maybe a slight off shore flow early in the morning On this

particular day this kind of situation extended well into midday The sea

breeze did not really pick up until up around noon When you have this kind

of a situation and a low radiation inversion at night you have a

long period of accumulation of pollutants all over the Basin espt~cialJy

in the prime source area the southwest portion of the Basin

198

I

Figure 6 shows the streamline pattern at 1600--400 cclock in the

afternoon same day sea breezes develop and with them a transport pattern

that carries pollutants up to the northeast and out toward the eastern por-

tion of the Basin This is a very regular pattern which we see day after l middot

day On July 25 1973 it was a little bit exaggerated The sea breeze was

held off for awhile started a bit late and so there was a very long period

of accumulation in the southwest area and then transport across the Basin

Figure 7 is an average streamline pattern at 1600 PacHic Daylight Time

on low inversion days for August 1970 It is included to show that the pattern

shown before is very typical Flow starts in the western portion of the

Basin and goes right across to the eastern portion This is using surface

data There is a very high average wind velocity in Ontario about 13 m iles

per hour and 23 mph in Riverside This is the average for the whole month

of August at 1600 PDT on low inversion days There is a considerable amount

of transport across the Basin starting relatively slowly in the morning and

accelerating in the afternoon

Figure 8 shows a verticle cross section of the scattering coefficient

The darker areas indicate higher levels of particulates Scattering coefficshy

ient is inversely proportional to visibility In the crosshatched area

visibility is less than about 3 miles In plotting altitude versus distance

inland from the coast you have Santa Monica (SMO) on the coast El Monte (EMT)

Pomona (BRA) Rialto (RIA) Redlands (RED) The lower broken line is surface

ground level The heavy dashed line is the base of the subsidence inversion

that occurred on the two days during this episode The middle line is the

base of the marine inversion There is a large area over in the western

portion of the Basin where emissions accumulate for much of the day At

199

midday the sea breeze has just started ventilating the Santa Monica area

The layer between the inversions is a layer aloft which is fairly well separshy

ated from the surface layer Ozone concentrations for instance in the

layer aloft were on the order of 04 05 ppm using the ARB calibration

method Down in the surface layer they were quite a bit lower in the mornshy

ing due to scavenging

Figure 9 shows that by afternoon the sea breeze starts and you get

kind of a clean air front Sea breeze starts ventilating the whole Basin

the stuff that was over in the west is transported eastward and at approxishy

mately Brackett (BRA) at 1700 PDT there is a clean air front The high conshy

centrations that were over Los Angeles earlier are now centered near Upland

(CAB) The numbers shown over CAB are data taken from a vertical profile

spiral over Upland at about 1600 That turns out to be the time when there

was the worst ozone concentration of the day in the Basin and it did occur

at Upland It could well be a result of the very polluted mass from the

western Basin being transported over the Upland area The layer aloft has

been a bit undercut by the sea breeze and some of the polluted mass has been

around possibly as long as the night before There has been very little

transport in the area aloft ozone concentrations are still very high

Figure 10 shows a trajectory analysis of the air arriving at Upland at

1600 since that was the worst time of the day at Upland We developed a

trajectory envelope using surface wind data and winds aloft so the air

arriving at Upland at 1600 started out somewhere back within this envelope

for example at 1130 PDT We did not go earlier than 1130 because the winds

were pretty much light and variable before that The air that arrives at

Upland at 1600 has been over the western portion of the Basin for much of

200

the morning and q~ite a bit of the evening before Thus there is

a very long period of accumulation and then a transport a pulsing effect

where you have pollutants moved across the Basin

Figure 11 is an isopleth map of surface ozone concentrations Again all

data are corrected to agree with the ARB calibration method Again you can

see that for the hours between 1600 and 1700 using surface data the Upland

area has the highest surface ozone concentrations about 063 ppm The western

area has been well ventilated by the sea breezes and it is cleaned out

The transport is actually pretty much perpendicular to the isopleth line

just about like that

Figure 12 is a vertical profile taken over Upland Cable Airportat

roughly the time of maximum ozone concentration 1636 PDT We are plotting

pollutant concentration on the x-axis versus altitude in meters (since it was

done for an EPA report) Surface leveJ at Upland is a little over 400 meters

the Z line is ozone Ozone concentration within the surface mixing layer

is pegged on the instrument at somewhat above 05 ppm Above the surface

mixing layer it drops off considerably and eventually get down to background

The T line is temperature and you ean see the subsidence inversion

on this day is very nicely documented here and provides a very strong trap

in that area The B line is the scattering coefficient inversely proporshy

tional to visibility Within the surface mixing layer visibility is on the

order of 3 miles or less while up above the surface mixing layer just a few

hundred feet difference visibilities get up to 60 or 80 miles The X is

condensation nuclei the measure of the very fine particles below about 010

micron It is a measure of quite fresh emissions If you have a high condenshy

sation nuclei count there are very fresh combustion emissions If you have

I

201

an aged air mass the condensation nuclei coagulate and the count decreases

considerably You can see that there are still some fresh emissions within

this surface layer as well But up above the surface mixing layer all the

pollutant indicators decrease considerably

Figure 13 is the same type of vertical profile taken over El Monte

which is on the western side of the sea breeze front The sea breeze front

has passed El Monte at this time almost 1700 PDT and again there are

distinct differences between the mass below the mixing layer within the sea

breeze front (below 400 meters) the marine inversion (400 to 800 meters) and

the subsidence inversion The subsidence inversion occurs at about 800 meters

and there is an old layer of very polluted stuff aloft The surface concenshy

trations are lower because of the ventilation by the sea breeze Condensashy

tion nuclei count (X line) within the surface layer is quite high There

are still fresh emissions in the El Monte area The 11 Z line is ozone

about 02 ppm within the surface layer (200 m) but it is 05 ppm up above

the surface mixing layer The scattering coefficient (B line) is very

similar it is lower at the surface and increases to a visibility equivalent

of less than 3 miles above the surface mixing layer The condensation nuclei

count is high in the lower portion of this (eg at 600 m) hut decreases conshy

siderably above This portion of the upper layer (600 m) has been around

at least all morning and condensation nuclei have been scattered from the

area The portion of the upper layer below 600 m has probably just recently

been undercut by the sea breeze and there are still some condensation nuclei

left in it

Figure 14 illustrates a different method of looking at the flushing

problems in the Basin We have tried to develop an objective criteria based

on ground level ozone to show the cleansing of the basin using the time of

202

arrival of clean air We determine the time when the ozone concentrations

drop by a factor of two at any given point The 1600 line means that between

1500 and 1700 the ozone concentration at that point dropped a factor of two

This sort of isopleth chart of when the clean air arrives agrees quite well

with the trajectory analyses although the numbers are a little bit behind

the trajectory analyses for the polluted air Figure 14 again shows the

transport process that takes place across the Basin which is ventilated from

west to east At 1900 some of the fresh ocean air finally gets out to

Redlands

In Figure 15 in order to put this whole flux problem into some perspecshy

tive we looked at the numbers the actual amount of ozone flux across the

basin We calculated the mean trajectory from Torrance towards Redlands

using the surface and upper air data We looked at the flux from the western

basin to the eastern basin basically from Los Angeles and Orange Counties to

Riverside and San Bernardino Counties This is a calculation made at 1700 PDT

We used the winds aloft from Chino as well as the vertical profiles taken at

Pomona and Corona Averaging the ozone concentration throughout the mixing

layer and multiplying by an average wind speed we arrive at a number of 185

metric tons per hour being transported directly from one side of the Basin

to the other If you look at this in terms of actual concentration in the

eastern Basin and assume that the flow was constant for about an hour it

is eno_ugh to fill up the box shown in Figure 15 to 025 ppm ozone which

exceeds the air quality standard by a factor of three (using the ARB calibrashy

tion method) Thus there is a very significant transport of ozone or ozone

precursors from one portion of the Basin to the other side of the Basin One

thing to mention though is that the concentration would not be kept up on a

203

steady state basis because the transport is a result of the pulsing effect

I Illentioned earlier There is a lot of accumulati6n in the western Basin

and these accumulated pollutants are then transported across the Basin This

kind of transport did take place in a couple hours because we also have

measurements from 1500 PDT which give us similar flux numbers

Figure 16 is a trajectory envelope similar to Figure 10 calculated for

Upland at 1600 for the air arriving at Redlands about 600 oclock in the

afternoon I wanted to include this trajectory envelope to show that the

problem is not really simple You cannot say that the air at Redlands came

from Long Beach per se The air at Redlands if you look at the whole

envelope of possible trajectories using upper air data as well as surface

data could have come from anywhere between Downtown Los Angeles and over

the Pacific Ocean south of Long Beach

Another thing to recognize is that the wind actually changes direction

slightly as you go up and down through the mixing layer and the mixing layer

is exactly what it implies There is mixing within the mixing layer so if

you begin with a parcel of air near the surface this parcel may move to the

top of the mixing layer and go one direction for awhile it then may go back

down to the bottom of the mixing layer and move in another direction for

awhile The ratio of the length scales indicata3mixing layer depths of 1500

or 2000 ft and distances on the order of 70 miles This makes it very

difficult for tetroons to follow an air trajectory because they do not go

up and down They stay at one altitude and in one wind regime and yet the

wind regimes are different at different altitudes and the air is continually

mixed up and down through this layer You can often see this on time lapse

photographs

204

The question is where does the pollutant mass go after Redlands Figure

17 is a repeat of Jim Pitts slide from yesterday and it is data for the

same day that we did our analysis It shows the ozone peaks starting at

Pomona and Riverside and on July 25 1973 eventually getting out to Palm

Springs so there is quite a bit of long-range transport The ozone is

stable at 8 00 or 9 00 oclock at night There still are ozone concenshy

trations of 02 ppm it hasnt dissipated even at the surface Ozone does

dilute as the mass moves Other calculations we did were integrations

through the mixing layer of various pollutants such as ozone and CO along

with trajectories that we measured Th~se integrations show just what the

ground data show in Figure 17 The concentrations increase through the western

portion of the Basin and then show a decrease through the eastern portion

of the Basin CO tends to decrease faster than the ozone indicating a

continued production of ozone further east

Figure 18 is a streamline chart on a larger area map for the 16th of

August 1973 It shows the typical streamline patterns that occur for

ventilation from the Basin By mid-afternoon there is flow out through the

major passes to the north and towards Palm Springs (PSP) On this particushy

lar day we had data from Arrowhead showing that the air mass from the Basin

does indeed get up there

Figure 19 shows a vertical profile over Arrowhead early in the morning

16 August 1973 at a time when there was a north wind Ozone level was

about 005 ppm the scattering coefficient was quite low on the order of

probably 60 miles visibility or so Figure 20 is a vertical profile again

over Arrowhead late that afternoon when the winds had switched There is a

flow from the Los Angeles Basin into the Arrowhead area thus one sees a

205

vertical profile that shows a distinct increase near the surface in both the

ozone and the scattering coefficient and in the condensation nuclei Ahove

that you have fairly clean air The top of the polluted level is just about

the top of the mixing level over the Basin

I want to leave the transport now and discuss the complicated vertical

structure that can occur If you want to try to model something try this

one for instance Figure 21 is a vertical profile over Brackett Airport

Pomona about 830 in the morning on 26 July 1973 which is the day after

the episode shown earlier A bit of interpretation shows how complicated

th is can be If one looks at the temperature profile it would be very

difficult to pick out a mixing layer theres a little inversion here another

inversion there several more up here After looking at hundreds of these

profiles though you can start interpreting them What is happening is that

there is a surface mixing layer at about 500 m In this layer there is a

high condensation nuclei (X line) count due to morning traffic The San

Bernardino freeway is quite close to Brackett there is a relatively high

nitrogen oxide count about 02 ppm and the b-scat is fairly high Ozone (Z)

within the surface layer however at this time is quite low The layer beshy

tween 500 m and 700 rn turns out to be the Fontana complex plume Note the

very high b-scat level it is below 3 miles visibility the plume is very

visible especially at this time of the morning when it is fairly stab]e

There is a high nitrogen oxide level (800 m) a high condensation nuclei

level and again a deficit of ozone Above this layer (800 m) you have stuff

that has been left all night very low condensation nuclei indicating a very

aged air mass ozone concentrations about 016 ppm b-scat of about 04 It

has been around all night and not yet had a chance to mix down within the

206

surface layer In fact one good way of determining the surface mixing layer

early in the morning and at night is to look for the ozone deficit Another

thing to mention is that wind reversals occurred for each of these three

layers The winds were fairly light and westerly at the surface slightly

easterly in the 500 m 700 m layer and westerly above 800 m There is a

complicated situation early in the morning but the main problem is that by

the middle of the day there is good surface heating and the pollutants have

all been entrained and mixed down to the ground so in order to modeI what

happens on the second or third day of an episode you must be able to look

at both old pollutants as well as fresh emissions And you need to account

r for ozone that is actually transported down to the surface from layers aloft l

The next slide is a photograph (not included) which is another e xample

of some layers aloft This is due to upslope flow as explained by Jim Edinger

in his publications The mountains are heated during the day in turn heating

the air and making it buoyant there is upslope flow to a point where the

heating cannot overcome the subsidence inversion and the stuff comes right

out from the mountains and spreads out over the Basin The pollutants can

stay up there if the winds aloft are very light and on the subsequent day

will he re-entrained to the surface On the other hand if there are winds

aloft different from those in the surface mixing layer or the wind velocity

aloft is high there can be a very substantial ventilation process for the

Basin Pollutants can be ventilated up the slope and blown away in the upper

winds In the case of the entire July 25th episode winds aloft were quite

light and these upper layers remained

Figure 22 is a vertical profile of one of those upslope flow conditions

in the same location shown in the photograph but on a different day Again

207

there is a relatively high surface concentration of about 03 ppm of ozone

(Z line) a layer of clean air between 900 to 1100 m and then high concenshy

trations of ozone again above 1100 m It has gone up the slopes of the

mountains and then come back out Concentrations in the 1100 to 1300 m area

are just slightly lower than they were at 600 to 800 m area Notice however

that the condensation nuclei count (X line) is quite a bit lower mainly

because the stuff is much more aged above the 1000 m level than it is down

below 900 m

Figure 23 shows the stability of ozone the fact that it can stay around

all night long This is a vertical profile taken over Riverside about 2200

PDT 1000 oclock at night Above the surface mixing layer (600 m) there

are ozone concentrations of about 0 15 ppm (Z line) Within the surface

mixing layer (below 500 m) ozone is completely scavenged decreasing to

zero The nitrogen oxides within this surface layer are being contained and

are around 01 ppm from fresh emissions that occurred during the evening

Condensation nuclei near the surface are very high The temperature profile

is very stable You have a surface based radiation inversion which is a

little strange looking for a radiation inversion~ nevertheless it is quite

stable There is a definite restriction of the mixing--a very difficult

time getting air from below 500 m to above 500 m The ozone that exists in

the 700 m range is in air where the reactions have virtually gone to compleshy

tion and is very stable All the profiles on this night changed very little

the ozone peak stays there High concentrations stay around

Figure 24 is a cross section across theurban plume of the City of St

Louis I wanted to show that this occurrence is not limited to Los Angeles

We have seen ozone formation and transport in other urban plumes These data

l

208

were taken during a project sponsored by EPA in conjunction with R Husar of

Washington University and William Wilson of EPA The dark line on this is

the ozone concentration across the urban plume perpendicular to plume The

dashed line is the scattering coefficient The power plant plume is parallel

to the urban plume The data on the left were taken 35 kilometers down wind

about 1100 oclock in the morning The ozone concentration increases slightly

to 005 ppm in the urban plume there is a deficit of o in the power plant plume3

In the same urban plume same conditions 1500 CDT two hours later further

downwind there has been substantial increase in the ozone in the urban plume

itself The b-scat is very similar to what it was before but the ozone is

now increased quite substantially except in the power plant plume where

there is a strong deficit of ozone due to scavenging by nitrogen oxides So

the formation and transport of ozone and ozone precursors in urban plumes is

a regular occurrence that happens in more places than Los Angeles and as Bob

Neligan showed this morning it can happen over quite a bit longer distances

than we are showing here

To summarize the conclusions as they affect model development first

once ozone is formed in the absence of scavengers ozone is a very stable

compound It remains for long periods of time It can he transported for

very long distances Ozone is a regional problem which cannot be controlled

on a local basis To have effective ozone control middotone must have a regional

control strategy and probably regional type air pollution districts

A second conclusion is that the vertical distribution of pollutants can

be highly complex and models have to include more than just a simple wellshy

mixed surface layer

209

A third conclusion is that layers aloft can persist over night and can

be re-entrained within the surface mixing layer on subsequent days models

should be able to account for old pollution as well as fresh emissions Also

pollutant accumulation and transport can have distinct diurnal patterns that

are strongly dependent on the meteorology Models should be time dependent

and should start at the beginning of the accumulation period In other words

models ought to be able to run for 24 or 48 hours if they have to In this

case in Los Angeles there is often an accumulation of pollutants which starts

in one portion of the Basin at midnight and continues through the next mornshy

ing even before it starts to be transported

As far as recommendations go in many areas a lot of ambient data has

been collected and in some cases the data are actually ahead of some of the

models so I think a research program is needed in developing models that

will account for this vertical structure and the day to day carry over and

the models need to be extended to cover longer distances In addition more

smog chamber work is going to be needed in looking at the effects of carry

over and mixing old pollutants with fresh emissions How people go about

this I leave to the modelers and the smog chamber people They know more

about that than I do

I

210

I

~ INVERTER

AUDIO TAPE

MONIT0R

MONITOR OBSERVER SEAT

MON ITOR

NEPHELOMETFR FLfCTRONICS

j DIGITAL DATA LOGGER

CONDENSATION

VOR DME NEPHELOMETER TUBE

JUNCTION middoteox ASSORTED POWER

AIRBORNE

TEMPERATURE TURBULENCE

middot HUMIDITY

ALTITUDE BOX

__

middotE=-middot RECORDER ----r----------

NUCLEI KJNITOR

CONVERTER

SUPPLIES

INSTRUMENT PACKAGE (

lCO

03

Ndeg

-

-----NEPHELOMETER

BLOWER

Figure 2 Instrumentation Layout for Cessna 205

211

bullubullbullbullbull

Figure 3 Airborne Sampling Routes in the Los Angeles Basin

Figure 4 Vertie al Profile Flight Path

~-~ r~i ~~1 -- ~ ~ ~2-1~ LJ-----~ r~~ ~~ t~~--l

~ ALM l

0 RIA

ec 8v

M

~ Afo

-o

M 0

~IV

ltgt

IN J--1 N

SCALE II fi M I j_ ES 0 3 4 5 =-JSEJ--J~ _middot ~middot- - =- =

I

~

M

N~J

Figure 5 SURFACE STREAMLINE ANALYSIS - 0300 PST 25 July 1973

~~~ ~~-- cp1FJ=D -~~

~ 1

~ ~ 8c

8v

~25

PACIFIC OCEAN

diams Tt

0

9 I 4 5 10 I- m p H - -middotmiddot u 4H__8 middott_

D i6 J4 k W~D SPED llaquotl SNA NJ ~1

SCALE m ICtt84bullmh R v1s1a1L1n (mil 6 ~ CONTOURS REPRESENT

-- 10ml 16km (~() bull ~ ) ~ - 000 ft 3C5

Figure 6 S_cJRFACE WIND STREAMLINES - l 600 PDT JULY 2 S I 8 7 3

l - ~---i ~-=-___-----c---it~~-~~ r----=------1 ~-~~--cpc---_t__A --~ ---llil

~_ - ~-l-cL

34bull vi~-dff

bullbullbullbull bull ~ bull -1 bullbull - -_- L bull-J bull ~bull-bull-ii------~ bullmiddot r_ -~- ~ bullI ~_ bull bull bullbull bull I bull _ - bull -~-~ middotbullbullbull ~ ~ --middot -~- bullbullmiddot ~v ) ~ - -__rl v middotmiddot - 1- ~ -- middot middotmiddot - 1 91 frac12 - ~- lt( middot K i - middot bull - middot - bullmiddot~~-~lJ) obullmiddot~ ~-f- _J_~---Smiddot~middot-~----~~~---gt_middotfY-_middot-~middot --middot-~-~----fJ_middot- middotmiddotbullmiddot u-- bullmiddot ~ ~ -middot L~ bullbull

~bullbullbullbull bullbull l_bull bull bullbullbull EW bullbullbullbull-- ~ __bull f f - middotbull - J middot f bull S bull I ~ -r --

_ bullbull bull- _ bullbull-bull ~ ~ bull bull bull bull I bull bull bull bull bull bull gt - bull middotbulliJ -bull I bull bull _1 bullJ C-- ~-middot _ bull bullbull bullbull bull _____ ~ ~ l _ middot q bull 1 -middot middot ~~middot middot middotbull_ J ~gt - J bull-bullbullbullbull ) _ -middotmiddotbullmiddot J ~middotmiddotmiddot -bullmiddotbull fmiddot 7middot _middotmiddotmiddot bullmiddot(middot Ii~ middotmiddot~_--~middot 1middot__middotmiddotmiddotmiddot middot- gt_ -~ -~-- Imiddotbullmiddotbullbull_ -

- ()_I (w--_ bullbull__(i- bullOmiddotbull bull middotbull -bull-_jlJ middot bull lt 1(middot t gt bull - ~ rbull I bull middot middot- bull41-bull l~r v-middot~- middot middot middot bull_ - middotmiddot ~Jtj (middot~ ~middoti middot middot middot middot middot ~- ~ -tmiddot~ I - middot middot_- ~ - -~ middot_ _- ~bull - _ ~) i bull bullbull bull- middot_ bull middotbull __ ( bull 11bull bull ~ampmiddot ~ l bull bullQ bull - -1 bull JY1 bullbull ~ or bullbullbullbullbull bullbull-bullbull _ ~ - bull bull-bullbullbull middotimiddot middot 91 bull t bull - - tfaw lJ--r- bull bull _ bull middot- - l

f ~~middot--~ middotmiddott ~ltrgtmiddotmiddotJmiddot_bull - ~ - __ middot- LOS ANGELES BASIN - LOW LEVEL -__ jmiddot l-gt bull - bull J iI bullbull bull bull bull _ bullbull _ Jmiddot middotL~_1 middot middot bullbullmiddot ( C middot INVERSION MEAN WIND FLOW _ J

lmiddot - f bullbullbull~ - f 1bullbullbull _ ~)- bull middot- _---_- 7f-~bull~ REGIME _F_~ AUG_UST_~ ~600 P~--- l

-__L-~bull --ncmiddotbull~~-j--bullmiddot~bullmiddot_-bull _fJibullmiddot Imiddotmiddotmiddot-bullmiddot- bullbull ~ bullbullbullbullmiddotmiddotmiddot~middotbull ___ bullJ_ _middot~0))deg bullt t1yensmiddotmiddot ( middot middotmiddot middot middot ~ middot lbullbull1 t_c0 bull -middot---l lt ~middot~- deg bullbull --= bull bull bull I bull bull bull bull bull bull bull bull bullbull _~bull b ---) bullbull-bull ) bulll middotbull middot1middot ) bullT --f bull I bullr ~bullbullbull bullbullbull( - -bull-- ( -o-----_i bull-~-l- i l l J l~-- c middotmiddot _--1 ---I middotmiddot ---- ~bull-bull bulli_ ALT Elmiddot_ bullbullbullbull _- ~~middot bull middot bullbull _ bull middotbull bull~ ~bull middot bull -middot bull--ua_-- bullbull bull

-- 01--- middot_ -middotmiddot hmiddotmiddot __1 ~-- ~ fi~~- ___ - ____ _ -middotmiddotmiddotmiddot~ ) -~-J bull bullbull bull bull 0 uc- -l ~- ~ IT ~~ll ~ bull -middot -middotmiddotmiddotmiddotbullCCAmiddotmiddotmiddot-middot middot bullbullbullbullbull

) i- 5 ~-==-- __ __ - bullbullbull _ bull~ bullbull _ bull bull l T[h4 ------ - 0

i17- o~-lt -(i-_~ 11t~bull-omiddot ~- -- 13 0l~~~bull bull Jbullbull~bull ~ ~bullbullbull bull bull x- middot~---=-~~ -=aJlll8 bull Ibull bull ~~ middotbull rbull~---bull1-~middot-middot _ middotmiddotmiddot-middot 1 0 ~vrbullmiddot ~middot ~ (J~-middot _-_~) ) ~ bull middot

l middot _ POMA_ middot =~~~----ti~ jmiddotmiddotmiddot - middot bull [j

~A ii J0 Vfli middot bullHud __=bt_ bull

CImiddot ~-- ~- middot)middot PACIFIC OCEAN I middot ---- middotmiddot ~

__ middot__ ~ - _ 23~1 middotbull 8 4 1 middot middot ~ middot middot gt ~~- l ~ u middot

bull - bull- I ~------ --1~ i middotmiddotmiddot - n _c-118 1130

~ n r -t ~~gt25) cmiddotbullmiddot

~--lt- ~~- 1-~__( i - t ~ _ middot 0 igt(_J

11bull bull11 ~~ -~[ ~i~gt----gtmiddotmiddotmiddotmiddot--~l_ ~~ ELEVATION

IN FEET bullbull (_- middot bullbullbull -middot middotbull middot ~~ middotmiddot bulltbullbull _ffmiddotmiddot-middot v I )tylt~ -~bullbull1bullbullrbullbull ~-lt -~ ( I~

600~ A0 Cv(A (1829 m AND OVER) deg )_ rJ__~7 middot middot ~--middot L==1 _J bullbullbull - bull -middot~-- rgt ~ middot(Zmiddot- middotbullmiddot middot

Z~C)-tGOO (762 middot 1829 m) 9-N4 __J (r -- lf _ bull bullgt-~~~ ~ _ w _ _ I (1 bullmiddot( middot1 middot -----~~~- middot L-bullmiddotbullW bullbullbull3 STA r I0-4 lODEL

100i -2soo (305~762m) -- Ow - -~1_- i ~~--- bull v~rvt ~~ -middot )) ~--

II gt J (-_bullmiddot middot~ l bull bull tr 1 )~ gt ) bullbull-_bullI-middot -middot bull~0 3 Mor nuq1ENr Wlbull~O JIAtCTIO-bull bull - lbull C---gt bullbull )t bullbull -( I bullf I - 20-00 (61 bull 305 ml J( Jloa xxE- -bullbull00 - -- middot1

0-200 (0middot61m) Wl)7 AVBt~gpound ) bullmiddot-iiNL~ middotntmiddot_ 1 iJJlt( _1J- ~ VAq IA9 IL ITY 0 ~ 10 15 ltS lHPtl

~--_ bull bull I bullbullbullbull 1 ~) J)J ~ bull Is bullmiddot bullbullbullbullbull ~ 3 V IS A VAqlABLE OIR~CTIO- 0 8 16 2-4 km

(SPEEDS SHOWN IN mph 10 mphbull 16 h1llr) -- middot ktr~~~ lt~ ) -middot-SCALE

Figure 7 LOS ANGELES BASIN MEAN WIND FLOW FOR DAYS WITH LOW LEVEL INVERSIONS DURING AUGUST I 970 AT 1600 PDT

-~~~~-=======~middot~-~======~middot--=-==-===gt=---==____________=== ~--=-J~==-- -=-ee----=-------

500

N f-- V

- - - SUBSIDENCE INVERSION

----MARINE INVERSION

bullbull-bull-bullbullGROUND LEVEL

x WINOS ALOFT (kmht)

WESTERN middoteASIN EASTERN BASIN

LAX WINOS EMT IHOS I I

CNO WIHOS

s_ 04 13 1500- 05 02 08

I 06 069 middot

11-1--

04 04 i ~4

06 ~ 4--

I 2

1000 n1 1005 -_E

lll --1 lJ -----------~----

~11

--=i-+- c -- 9 _____ - ~ C

lt I

I 6 4 _r 31

I 6 5 ~~ ~_ bull ---middot- 64 ~li- - middot- bullc - middot-----------

10

SMO (1347 PDT)

EMT (1246 PDT)

BRA CAB (1459 PDT) (1335 PDT

RIA (1349 PDT)

RED (1406PDT)

Figure 8 VERTICAL CROSS-SECTION OF bscat FOR lvflDDAY

T t 10-4 -1)(l n1 s are m

JULY 25 1973

- c - -~

~--~ JC_-_1- ~1pi~ oamp----~JilliiiM~f~-U~ -~--- --~~~ ~~~

-=--~

-E-- O

_ lt

1500 05

06 15

09 __~

1000 --

~- ~---middotmiddot 29

500

oJ11

__a

07

I 07 I

I I

I

09

I

I

I

I 7 ---

11 -----

~ ----- 6

---------------lt- -~middot4 --------

20

29

-

10 10

11 07 08 08

10

08

~8 _____ Y-

N

- - bull SUBSIDENCE INVERSION

----MARINE INVERSION

-bull-bull-bull GROUND LEVEL

WES TERN BASIN EASTERN BASIN x WINOS ALOFT (kmhr)

t t

CNO WINOSILA WllltOS poundMT WINOS

SMO LA EMT BRA CAB RIA RED O (1736 PDT) (1655 PDT) (1707 PDT) (163 PDT) (1823PDT) 1805 PDT)

Figure 9 VERTICAL CROSS-SECTION OF b FOR AFTERlOON OF JULY 25 1973 scat

T bull 1o- 4 - l )(units are m

__~~---iii~~- ~- ~~______ ~~- --~~J---=-~ ~

N ~ -J

PACIFiC OCEAN

0 5 10 15 1111

E 8 4 I 0 8 6 2 ~ bull

SCALE

dh Mes

CONTOURS REPRESENT - 000 ft 305 m

0 SNA

c8s

ec 8v

amp R~b

Figure 10 TRAJECTORY ENVELOPE FOR AIR ARRI1G AT CABLE AIRPORT (CPLAD) 1600 PDT JULY 25 1973

~-~

q_- ~ ------1 H~~~ -~~--~ ___---___--i- __r-=-1--===12---1 ~ ___r~ _==---_ - ~- f~~ ~-- - -5plusmn-at -~middot~

ll~~r1 ri

40

ec 8v

-1 I

amp

0 HQ_

7 0

CAP LAAR) O

VER

PACIFIC OCEAN ~ 0

RLA

4

WHqR d

diams

H ~I

I l

0 COMA

3

L~

LAH

Fa_ f ~~

S ~ LA APCD VALUES ADJUSTED TO AGREE ~

lt

0

5 10 15 mi0 WITH ARB CALIBRATIONE-j I I CONTOURS REPRESENT NZJ ~ 0 a SCALE 6 24 km - 1000 ft 305m COS v~J

______ J 10 ro ( igtf t-i

coFigure 11 SURFACE OZONE CONCENTRATIONS (pphm) I 600- I 700 PDT JULY 25 1973 ~

~~~~~C-~ ------=--~-__-~--~~~=--- ----=--~

N

-E

D1600----------------------------- 1--

14001-------------------------------

1200

I Ground Elevation

1000 middot 445 m ] lampJ

sect ~~ 7 ) SURFACE i6~ 800 MIXED LAYER

~

~ [ J ~ ~ I OZONE CONCENTRATIONS~ 600 E E GREATER THAN

( 50 pohm

400 I C H T Z GROUND LEVEL

200

I PUUloCETER UNIT SnbullBOL

NOc N0 0 ppm01 02 03 04 05 03 z

40 --~45~~ 50 co pm C0 5 10 15 20 25 30 35 I I I I I I I I I I TEIIPERATURE oc T-5 b 5 10 15 20 25 30 35 40 45

I-- 100 RELATIVE HUlillOITY H0 10 20 30 40 50 60 70 60 90 b1eot IOmiddotm- 1 8

CN cmmiddot3 1 IO X0 I 2 3 4 ~ 6 7 8 9 10 URBJLENC-C cm213ue- E

Figure 12 VERTICAL PROFILE OVER CABLE (CAB) J CLY 2 5 l C)7 3 l 63 6 PDT

~ _~ ~--- -

--

1400 I bull bull

1200

1000-5 LampJ 0 ~ I- 800 ~ c(

sooLl

-1-=-1-~--t j --=~c-o-----i-bull 1-~~~ ilt~~ -~-1 lta-abull--~ -c-~---=---r F--- ---- I n_--middot- =~~ ai~IHJ

(~-It

1600 ___________________________________

C r 11 s Ground Elevation t~C E H I~lcc

- ~ 1 90 m

4001 bullc C H

C UNDrnCUTTNG svC ~ Ic- H

SEA BREEZEC II 200

C C

[C -PARAMETER ---UNIT SYMBOL

NOx N0 0 ppm01 02 03 04 05 03 z co ppm C0 5 10 15 20 25 30 35 40 45 50

-5 middot- -~20~----25 TEMPERATURE oc T0 5 10 15 30 35 40 45

100 RELATIVE HUIOITY H0 JO 20 30 40 50 60 70 80 90 bcot 10-4m-1 8

CN crrr3 10 0 I 2 3 4 5 6 7 8 9 10 X TURBULENCE cmZ-13 sec-1 E

N N

_-----=-G--~---

Figure 13 VER TICAL PROFILE AT EL MONTE (EMT) JULY 25 1971 1656 PDT SHOWING UNDERCUTTING BY THE SEA BREEZE

0

middot~_lt ~middotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotbullbull

-~

LACA

0 - )

i r=

-v2v

~

_middot~middot)( I bullbull

bullJ

K~Ji~middot

~~ 61iAS 0

EMT J~J---6~-11 ~orr

PACIFIC OCEAN

WEST 0

SMC

0RLA

14

L~8

R~A

~BL

16 ~ ~

0 5s Pcfrac14A c1i ~ )

wFJfo~J_) ltI~~~

_ff-Clf1ito J )

HILL~

~J U

~ _~~~

~

I o middot

1 1$ ~ 11yen ~middot ~I N

I

N I- I

t

0 --pomiddotmiddot bullmiddot i- 1LO middot Joomiddotmiddotmiddot -- middot middotmiddot -middotmiddot

_middotmiddot 0 middot middotbull MWS r

L4 ( 1 T bull bull __-- -A bullbullbullbull middot

0 i __ bullbull

17 t-J~ N7 a S I ~r ~ 1 rtd ~lt A-~ v- middot ~ - cXa 0

RIA 19

CLO

ltJ~

bull ~ 0

(

--

1

_ _

-2Wl

~s~o -- _)~J0JgtJ~ ___ Q

15 l1JI

0 15 r(A0

CAP

CLARR)~R 1900 1-shyPDT

II (_-L~X L2X I 0~ R[V

0 CCtwA

I

I18=00 POT~ l4 r1

fj

-11J - ----- 11=oomiddotmiddotpor

l~i middotmiddot- o

i

5 10 5 Tl o~1 middot--middotmiddotmiddot middotmiddot

_q it==i--__F-3 9 I I CONTOURS REPRESENT SNA NZJ ~1 o

_- I 0 8 16 24 km I - 1000 ft 305 m middot ~

7 14~CALE --- 2500 ft o2m V lr1 ) middot I i0 _ il o5

16QQ pol(middot v( ____________ _L

I i

Figure 14 APPROXIMATE TIME (PDT) OF ARRIVAL OF SEA BREEZE Jl-LY 25 1973 (Ogt_iective criterion based on ground level ozone concentrations)

~ -___~==~ ~~ - ~ =-~ f7r=~1 _j~-~ --c_~~

u-middot - middot middotmiddotmiddotmiddotmiddot

~- middotmiddot~ ~1 WESTERN BASIN r Joa_middotmiddotmiddotmiddot_ NOxEMISSION RATE ~- 95 METRIC TONShr

-----bull_ ~ ~middot~ I -OUR -----middot )omiddotmiddotmiddot - middot~ l21 (fTI

~ AT middot ~ middotbullmiddot- ~- ~ middot 4bull-middot

I EASTERN BASIN NOx EMISSION RATE 10 METRIC TONS hr

ri r bullbull

t10 Joa

) __ 8v -a_ -- -bull-I O ~AGA -_ ~S ___ _ middotmiddotmiddot -

~ ~v ai- omiddot-middot~-- - ) r -middotmiddotmiddot f middot( ---~ -l A ~ _ (- bull ___

it~ ~~~ middot-middot -- ~-~ ~~~ 0 0 AZU~

AVERAGE CONCEN7RCTi)N iN BOX (IF STEADY STATE)

IS 25 pphm

1 r f--Ji 7 ~Sv PAS ou )V~(~- ~ t i -~ Li_) 03 FLUX THROUGH f~

~ ~JI_~ - amp_ JiM O SHADED BOUNOA~middot~-~ ~~-s-- EMT 185 t 60 METRI~ bull ~ ~ TONShr 0 (m)

c~~~ 1t~CS A~JFP

1000 _29

-i32

_~o tUA

_

1

O~ ~

0 -__rJ( (r- J PACIFIC OCEAN LAX _ C-middotJbull _

l o M R No _

550m

r

A frac14

HAR O HJ LAH

_ o camptA REDLANDS 18QO POT ~ r

I bull ~

RB MEAN TRAJECT~~~y

0

TOA L~S

0 AN

I - ~ 8 OUNOARY ~ ~middotltdeg ~ ~ BETWEEN middot __ WES~ERN ANO- middot middot - ~

I gt I lt bullmiddot bull (EASTERN ~ i middotmiddot middot - - ~

S ~ ~~ ~ - middot-

rt1~1_--t------l

middot1-- BASIN ~-~

1-)~~--middot ~ ~l

~~ ~-bull bull J --

-is-eo -_

0 5 10

j=i r-i C

0 8 ltl

SCALE

5 mi

2~ un

CONTOURS REPRESENT - 1000 ft 3gt5 m

--middotmiddot 2500 ft 1 762 m

~

0SNA

cos 0

_ --~ ----- --- ( bullmiddotmiddotgt

- middotlt- ltgtmiddot t__ Q ~

1 1 rmiddot bullbullbullbullmiddot ~9

NZJ ~ middotmiddot - middot- Alr ---middotmiddot- middot middot( middotmiddotmiddotmiddotv ~ bullbullbullw bullbullbull bullmiddot 1 bullbullr~ ~-- -middot ~--v ~- - I -~

ESTIMATED OZONE FLUX FROM VESTER~ TO EASTER-J BASIN JULY 25 1973 I 700 PDT

C ~IV

N N N

I

l ~

-~~

I

iI

i I

I t

t

~ ---~ --

Figure 15

~Qa llfJD fl(~middot ~ 11f ~I I

l

Lfb ec~s0 CPK v2v 0

ALT 8v Ld~_----1

I

HO-

0 CA

middotLARRv O VE~

1330

ol(Di

A~U

0ENT

~lt

s~e ~ 1530

F8f 1730

~

rbull-~

oc (WljT) -_-~(~~c lt-rw---_

~~ ~-_i~cB~~~

2-~) - ~ ~ l~w-~~ p~- pound)_

0 ojI middot tl-1CfUp I ~ ) 1 ~ J~I i bull middotbull middot~-Li 1)- ) I

DiI ~- 0

i ) 0 l I I

t

A RALc~o JI

C

-~

0 r-iR

~IV 1230 1~

RE PO ~- I - Ftl

) 0 ---~gt- __L8s ~Zi diams ( T~ _middot_ ~~ ~

I AN ~~-~ j t bi 0

~ I

~ I L i

-_gt ji o 5 c 5 Tl middot 0 0 ~-i p__i=r 2=f I_ I 1 NZJSNA 1

1 8 2 4 km )

SCALE I 00 J_(1 CONTOURS REPRESENT cos f

1 0 I --- I - ))) 35

PACIFIC OCEAN

Figure 16 TRAJECTORY E~VELOPE FOR AIR ARRI1gtJG OVER REDL_)DS AT 1800 PDT JULY 23 l =i73

224

JULY 25 1973

LA DOWNTOWN

0sect040 a

~

~ 020 0 X z0 ~ LJ 0 ~ z

~5 040 330POMONA 0 ~ en~ 020 w z _J

w w 0 (9 z O----u-~~-__~_-~~~-------L-~-0--0-0~----- z

ltt~ 040 56 (I)z

0 0o _ RIVERSIDE _J0 20 t6 ~

0~ Qt---0-0--ltrO-ltgt-C~------~~~~ a

LL ~

Rate ~ IO mph___ (I) w

_J~ ~ ~

et~ lt(

3 040 PALM SPRINGS ~

j 020 ~

0------____-----L--___---------L---~--~

105

12 4 8 12 4 8 12 l~-s----am _ pm----1

HOUR OF DAY PST

Figure 17 Diurnal variation July 25 1973 of oxidant concentrations at air monitoring stations at Los Angeles Downtown Pomona Riverside and Palm Springs California Values are corrected data Los Angeles Downtown and Pomona x 11 and Riverside and Palm Springs X 08

CONO S t 1 fRESEIS7

~

~~ 0

ciffmiddotdK ~ ~v~~o

( ~s ~

bull ~r ~ bull 1--~~----Soootl ~ ~ ~ ~ lj i1 d t CJ ~ ampfrsmiddotflt- frac12 ~ middotL~Js _-- ~

_gtgt middot~ ~rroltf~-) ~ 0 s- r

middot-middot- r_~ ~~JtbO ~~bull~Jt ~~~ L r - bull _ ~ I= J 1 ~ ~ ~-~~bullJC ___ -_ middot ~ laquo -poundJ~ ~- middot1~ r-- - V--_1_ ~ I 1 S I

V ~ bullf-uv~ fi -~zumiddot -~middot~ LS gt -tmiddot-F Q~ ~-tv I_~ --- ONT p(_ s ~S ~~~-[ ( 0 c-_ --~ ~~~___d_) lt- ~ I -i-C - -

~----1-1 bull~~POMA ~V BN ) middot-~ f -- s - ~

~VA -middot- ~p AAL a 2~~ ~~middot01 r r ~ middot middot 0-- V

i LAX bull1

~ -~poundJ-i- ltllll _(__1-0~ ~t- degQ-0- ~~ _ _-__~~-qlK ( a_ II ~ ~p-~ ~J

N bull - - 0 r o_ _I ~ -~ ~middot ~ ~amp ~--= ~ ) s ~

- -~- - middotO _a - Tl --0- ov I lHOIO J I bull J -- ~ 6 ~ -__ 2 ~

(__ ~~ _- ~-~ middot8---fl~ -- ~ bull~-abullbull _~ ~-cgt ~ bull bull middot e bull bull l ~ 0

I 1A_ HZJ middoto~J

middot0 (~ ~ S TAA

- ~ - - - --0 () _-j J middotO=c==c-c==cc~~~ l ~~ ~ ~ bull-~---~ ~ bullbull -~ al1 ~ bull __ ~--middotmiddotmiddot

diams Skyforest _ Strawberry Mt Lookout

Figure 18 STRE ~[Ll)ES FOR 1600 PDT on 8 1673

~ ~--

vO 0

N N V1

au

91 V7

-1 ~ -=1 ~~ ~~~~l r=--~d- ---1 _J-_

~E1 ~L1-~f~

3100 ---------------------------------

2900r-----------------------------

T

e w 0

~ 5 Cl Ground Elevation

1560 m

T PARAMETER UNIT SnbullBOL

NOx N 01 02 03 04 05 03

ppm z co ppm C

10 15 20 25 30 35 40 --

45 50

170

I I I z

0 5

-5 - -0~ 5 10 15 20 25 30 35 40 45 TEMPERATURE oc T

0

0

10

I

20

2

30

3

40

4

50

5

60

6

70

7

80

8

90

9

100

o

RELATIVE HUMIDITY

bcot CN

TUR8ULENC~

110-4m-

cm-3 tobull 213 1 cm sec-

H

8 X E N

N OI

Figure 19 VER TI CAL PROFILE OVER ARROWHEAD u-RR_l A CG CST I 6 1973 939 PDT

3100----------------------------------

N2900r----------------------------- -i

N

2700i-------------------------------

2500

e 0 uJ 2300 gt ~ ct

2100

1900i---------------------+--------------

~le 1iation 1360 m) 17001 ~

- -PARA1jETER UNIT SYMBOL

T NOx N1500 o ppm01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50

TEWERATJRE oc T-5 middot --~o--- 5 10 15 20 25 30 35 40 45

IOO RELATIVE HUWIOIT Y H0 10 20 30 40 50 60 70 80 90 bcat 10-~- 1 8

CN cm- 3 104 X0 I 2 3 4 5 6 7 8 9 10 213 1 tURBliiENCE cm sec- E

Figure 20 VERTICAL PROFILE OVER ARROWHEA D -RR 1 --- -AUGlJST 16 I) 16--1S PDT

1-~i w--~i_f l-=--bullC- ---~-4

1600 bull t c- N 8 ff Tbull C[ 8 H 1 bull H z H T ~ C f N 1 H T bull C rn 1 C NE bull-~z Hi400 bull bull tf T bull N ~r --middot _P H -ybull EC N z__e H T i 8 z H Tbull C E HD Z H T POLLUTANTS REMAINING FROM bullt C Hbull L T PREVIOUS DAY1200 Et HO I II -middot-- bull Ct H 9 - H T

___ Hbull( E N 1 a tC N i--_ -1 H

C N Tbull Z HP poundIC C H z_ 1111 1

- bull C H Z l _H_ _J1000 )( cc H -z emiddot ksect bull C N ~ T

)( iz H 8 H TIAI -t XC z 7-- T0 bull pound N t H_8

t-gt

YCpound N 1800 l I-gtltbull - H (Jet

N i -r~Bltt t bull gt- t C X N H T

[ BUOYANT POINT SOURCE PLUMEH 1

N ~z-- -

C H

-bull SUPERIMPOSED ON POLLUTANTSC JZ X H T 600 -~ E c REMAINING FROM PREVIOUS OtY Cl JC t H H f bull cmiddot t HT -fl

C- X t fl _ REMNANT OF NOCTURNAL RADIATION INVERSION(I-----e-C f N K I T H

C Z [ T H x-8 400 _Zc r -H -K SURFACE MIXING LAYERz C II H K 8

C N T pound H M 8 _ I -t ff H E N -9 l

Ground Elevation 305 rn200

PARAMETER UNIT SYMBOL

_ I - I I I NOx N00 ppm01 02 03 04 05 03 z

co ppm C 0 5 IO 15 20 25 30 35 40 45 50

L middot1 TEMPERATURE oc T-5 0 5 IO 15 20 25 30 35 40 45

100 RELATIVE HUPAIDIT y H0 10 20 30 40 50 60 70 80 90 bscot o-4m- 1 B

CN cm-3 x 104 X0 2 3 4 5 6 7 8 9 10 TURBULENC~ cm213sec-1 E N

N co

Figure 21 VERTICAL PROFILE OVER BRACKETT (BRA) JULY 26 1973 0825 PDT SHOWING BUOYANT PLUME AND UNDERCUTTING BY RADIATION INVERSION

N N 01600

___bull C M C

C

1400~~~ t C [ middot H LAYER CAUSED BY

C C H C [ H UPSLOPE FLOWl

1200

1000 ] w

SURFACE MIXING LAYER 0 --= ~ -~~ 6 800~ er

C C

600t-i C C t C

I ~00

Ground Elevation 436 m 2001-------------------------------

PAIUWETU UNIT SYWBOL

NOx N ppm0 0 01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50 I I I I I I I I TEWPERAT1JftE degC T-o b 5 10 15 20 25 30 35 40 45

100 ~EIATIVE HUWIOITY H0 10 20 30 40 50 60 70 80 90 b1tt1 10-m- 8

CN enr3 110 X0 2 3 4 5 6 7 8 9 10 Tu RUL Erct cm23sec- E

Figt1re 22 VERTICAl PROFILE AT RIALTO (RIA) JlJL Y 19 1973 1738 PDT SHOWI=JG LAYER CAUSED BY UPSLOPE FLOW

~~-7 ~ ~- 1 ~iri ~~- ~~-~ ~t ~~ ~ =~middot-1

1200 I t 1 If J-

1000

I C ltTl a_ ~l- t

800

600

L gE __r H

H

400 j (~ c pound N C E I~

t EH -

1-1 M

H H

H M H H

H

H H

11 bull H M H

M H If

H H

H

- C t H ~ C poundmiddot H

I C E I(

200

1600--------------------------- t

T t t T l

l T t

T t_

t 1

l] w ) g f

Tt t

ltt ~ T

t J t T

t J

f 1

t

Klt

H M Cro1nd Elevation 250 m HT X

5Yl80LPAllAlETER ~

NOx N0 0 ppm01 02 03 04 05 03 z

co ppm C0 5 10 io 20 25 30 35 40 45 50

25~--- ---35~~-40 TEMPERATU~E oc T-5 0 5 lO 15 20 30 45

100 RELATIVE HUMIDITY H0 iO 20 30 40 50 60 70 80 90 bact 10--ltllm-1 B

CN cmmiddot3 11 04 X0 I 2 3 4 5 6 7 8 9 10 IURBULENCE cm2hioC-1 E

Figure 23 VERTICAL PROFILE OVER RIVERSIDE (RAL) N

JULY 26 1973 2239 PDT I)

middot==-=-=

0

bull

N w 1--

ii -s~~ l-obull

CJ ~

obull -obull obull

5 02~

bscat

Oa

4l o2J

-I 3 e I 0

--)(

~

Abullu 2

ll

ol

Traverse at 750 m msl 35 km Downwind (SW) of Arch - St Louis Mo 1117 - 1137 CDT

( Power Plant Plume -01 Ibull-[ ~ e

11 bull E I -)(I

I0bull I 1r~ l -

0

I I Io 1 u I

I r- l A bull I i I 1I

H1I I 4 t I II I I

11 I I

I I r I I I

I I qo 01 I I

I I bullJ~viI I middot ~

I

I I

~

Urban Plume

ood 0 10 20 30 40 50

kilometers

o~

02

01

s 1

P

0bull 01

00S~J1 I ti middotmiddot1 middotvmiddotmiddot~ J

Urban Plume

I y

oo 0 10 20 30 40 so

kilometers

Traverse at 750 m msl 46 km Downwind (SVV) of Arch - St Louis Mo 153 0 - J 549 CDT

---- bscat

o-

Power Plant Plume

1l~ 11I 1 t

ill~t fl Ibull I ii

I

lmiddotmiddotrI

I I I I t II

l vrI V

JV-f Jl bull

bull t I bull I

Figure 24

l

232 RELATIVE CONTRIBUTIONS OF STATIONARY ANDMOilILE

SOURCES TO OXIDANT FORMATION IN LOS ANGELES COUN1Y IMPLICATIONS FOR CONTROL STRATEGIES

by Robert G Lunche Air Pollution Control Officer

Los Angeles County Air Pollution Control District Los Angeles California

Introduction

The type of air pollution problem characteristic of the west coast of the

United States and particularly of Southern California has come to be known

as photochemical smog because it is the result of sunlight-energized atmospheric

reations involving oxides of nitrogen and reactive hydrocarbons Its manifesta-

tions- -eye irritation reduced visibility damage to vegetation and accumula-

tion of abnormally high concentrations of ozone or oxidant - -are by now well

known In fact the occurrence of high levels of oxidant which consists almost

entirely of ozone has become the primary indicator for the presence and relative

severity of photochemical smog

During the 25 years since photochemical smog in Los Angeles County was

first identified an extensive program has been underway for control of the responshy

sible contaminant emissions Initially during the 1950 s these programs concenshy

trated on controlling emissions of hydrocarbons from the stationary sources of this

contaminant In the early 60 s programs for the control of hydrocarbon emissions

from motor vehicles in California were begun An exhaust emission control proshy

gram for hydrocarbons and carbon monoxide from new vehicles was begun in 1966

C011trol of oxides of nitrogen emissions from motor vehicles began in 1971

As a result of the overall control program by 1974 emissions of reactive

hydrocarbons from stationary sources have been reduced 70fo from uncontrolled

levels and about the same percentage from mobile sources Oxides of nitrcgen emissions

233

from statjonary sources have been reduced about 53 while emissions from moshy

bile sources are still about 7 above uncontrolled levels due to the increase

in NOx from 1966-1970 models Additional controls already planned for the future

will by 1980 achieve reductions of reactive hydrocarbons from stationary sources

of about 87 from uncontrolled levels and from mobile sources about 93 By

1980 emissions of oxides of nitrogen from stationary sources will have been reshy

duced 53 and from mobile sources 63 from uncontrolled levels The past

present and projected emissions of these contaminants are shown in Figure 1

A I though compliance with the air quality standards has not yet been achieved-shy

and is not likely before 1980- -the results of these programs have been reflected rather

predictably in changes in certain of the manifestations of photochemical smog For

example eye irritation is less frequent and less severe and in some areas js

rarely felt at all any more and damage to vegetation has been markedly reduced

Ozone (or oxidant) concentrations have been decreasing in Southern California

coastal areas since _1964 in areas 10-15 miles from the coast since 1966 and in

inland areas 40-60 miles from the coast since 1970 or 1971 as shown on Figures

2 arrl 3- All of these positive effects have occurred despite the continuing growth

of the area indicating that themiddot control programs are gradually achieving their purpos

a return to clean air

This improvement is al~o refutation of the so-called Big Box -concept which

assumes that the total daily emissions in a given area are somehow uniformly disshy

tributed throughout that area--regardless of its size or of known facts about the

meteorology of the area or the spatial and temporal distribution of its emissions- -

234

and of control strategies based on that concept And since the improvement in

air quality refutes the control strategies based on reductions in total emissions

it thus confirms the value of more recent control strategies which emphasize conshy

trol of motor vehicle emissions and use of a source-effect area concept

Following is a brief listing of the evidence we intend to present as supporting

our views on just what control strategy is appropriate

Examination of relative contributions of HC and NOx from stationarybull and mobile sources demonstrates that motor vehicles are the overwhelming

f source of both contaminants~

I bull Observation of air monitoring data shows that the effects of photochem -

ical smog are not uniformly distributed t_hroughout the county

bull Study of the meteorology of LA County shows consistent paths of trans -

port for various air parcels and consistent relationships between the

areas most seriously affected by photochemical smog and high oxidant

concentrations and certain other areas

bull The upwind areas are found to be source areas--the downwind areas-shy

effect areas

bull Central L A is found to be the predominant source area for the effectI area in which the highest oxidant levels in the SCAB consistently occur

bull The predominant source of emissions in this source area is found to

be motor vehicles

bull Central LA has the highest traffic density I

ij bull Both pr~mary and secondary contaminant concentrations reflect the effects

of the new motor vehicle control program in a predictable fashion 11 I

A strategy based upon these findings is gradually being verified by atmosshybull pheric oxidant data~

235

The Evidence that Motor Vehicle Emissions Are the Principal Source of Oxidant

As seen from Figure 1 at the present time the total daily emissions of I-IC

and_ NOx from all sources in Los Angeles middotcounty are primarily due to the motor

vehicle The problem now is to find the spatial and temporal representation of

emissions which when examined in the light of the known meteorology and geogra -

phy of the Los Angeles region best describes the source of emissions responsible

for the highest observed oxidant readings

In the rollback models used by EPA and others the basin is treated as a

big box with uniformly distributed emissions and peak oxidant is considered to

be proportional to total basinwide hydrocarbon emissions

The fact is that the middotemitted contaminants from which the smog is formed

and the effects which characterize that smog are not evenly distributed throughout

the Los Angeles Basin in other words the basin area under the inversion is not one

large box filled to all corners with homogeneously distributed air contaminants and

photochemical smog

Refutation of Big Box Myth

Examination of atmospheric contaminant concentrations refutes the big box

concept It is found for example that concentrations of djrectly emitted contam -

inants measured at a particular sampling site reflect the emissions within a rather

limited area around that site For this reason contaminant concentration levels

vary from one location to another and each has a characteristic daily pattern which

reflects the daily pattern of emissions in that area

middot 236

The big box concept is further refuted by the fact that peak concentrations

of carbon monoxide and oxides of nitrogen in areas of high traffic density were

fairly static prior to 1966 Thus they did not reflect the 45-50 per cent growth

in motor vehicle registrations and gasoline consumption which occurred in Los

Angeles County between 1955 and 1965 and which caused comparable increases in

total daily emissions of such vehicle-related contaminants This demonstrates

that growth was outward rather than upward so that a larger area of the County

began to be affected by photochemical smog but no area experienced smog ofJ

greater severity than that originally affected by smog formed from the vehicular

emissions which accumulated each weekday in central Los Angeles and were trans-

1 I

ported later that day to the San Gabriel Valley

1 Meteorological Evidence

To verify the geographical dependence of emissions and resulting atmospheric

concentrations let us examine the meteorology of these large areas of Southern

California Both the County and the Basin have many meteorological sub-regions

in which the patterns of wind speed and direction may be similar but within

which the patterns of air transport are parallel with those of adjacent sub-regions

and the respective air parcels do not ever meet or join

The characteristic patterns of inversion height and wind speed and direction

in these sub-regions and their patterns of vehicular emissions together have

created a network of source areas- -those in which the reactant contaminants accu -1T

i ~ mulate in the morning and begin to react--and related receptor areas--those to which

~ the products and associated effects of the photochemical reactions of the contamshy)

inants originally emitted in the source areas are carried by the late morning and

237 middot

afternoon winds ( sea breeze)

Wind-flow patterns show that characteristic patterns of transport for related

source area-effect area combinations are separate and parallel not mixing or

joining Each source area has its own reactor pipeline to its own effect area

or areas

To illustrate this source area-effect area relationship the typical flow of

polluted air from downtown Los Angeles to Pasadena was selected as a worst

case situation for in-depth examination Figure 4 shows that the air in downtown

Los Angeles on the morning of smoggy days moves directly from the central area

to Pasadena

Vehicular traffic is the predominant emission source in both downtown Los

Angeles and Pasadena Thus the air in each locality should contain CO Also

since oxidant would form in the air parcel moving from Los Angeles to Pasadena

oxidant levels would be expected to be higher in Pasadena than in downtown Los

Angeles

Figure 5 shows these relationships for the period 1960-1972 The atmosshy

pheric CO level is similar for the two areas while oxidant levels were higher in

Pasadena than in Los Angeles throughout this time period This demonstrates

that a significant amount of oxidant formed in the air as it moved to Pasadena

containing both the unreactive CO and the photochemical reactants for producing

oxidant Both CO and oxidant show a marked downward trend in each locality since

1965 which emphasizes the effect of vehicle exhaust controls and the correlation

between the localities

238

On a day which is favorable to the formation and accumulation of photoshy

chemical smog a contaminated air parcel normally originates during the

6-9 a m period on a weekday from an area of dense traffic centered just

south and west of Downtown Los Angeles It is oxidant generated within that air

parcel which usually affects Central Los Angeles and the West San Gabriel

middotK IJ l J

Valley area around Pasadena

The traffic area in which this smog had its origin is about the most dense

in Los Angeles County and has been so for the past 25-30 years No area

has a higher effective density thampn-this Using carbon monoxide which

1

is almost entirely attributable to motor vehicles as an indicator of such emis-

sions it is found that the concentrations of emitted vehicular contaminants

middotr i

measured in Central Los Angeles during the past 15 years confirms both this lack

of change in effective density and the absence of any area of any greater effective

density when local differences in inversion are acknowledged

This area the Central Source Area is depicted in Figure 4 The size

and shape of the Central Source Area was ch~sen to be large enough to reduce to

an insignificant level any diffusion or transport into this area from any externally

l generated reactants This conclusion is based in part on the trajectory studies

previously referenced as well as an analysis of the diffusion and transport parashy

meters for the area

239

The Central Source Area has been identified as that geographical region

which contributes essentially all of the primary contaminant emissions giving

rise to the highatmospheric oxidant levels in the West San Gabriel Valley

The proportion of emissions in the CSA due to motor vehicles and that due to

stationary sources is shown in Table 1 For the County as a whole about 80 per

cent of _(6-9) AM reactive hydrocarbons are due to motor vehicle emissions and this

figure rises to 90 per cent for the CSA The same conclusion a pp lies to NOx

emissions The Central Source Area contains the greatest density of vehicle traffic

in the County and thus the greatest density of source emissions Thus it appears

that the source area with the highest density of emissions during the critical (6-9)

AM period is responsible for the highest afternoon oxidant levels observed in Los

A i1geles County and in the South Coast Air Basin These highest oxidant levels

are consistently observed to occur in the San Gabriel Valley This is true whether

the LAAPCD or the ARB oxidant calibration procedure is used

Further the atmospheric concentrations of the primary pollutants can be

identified as originating primarily from the motor vehicle and they reflect the

effects of the motor vehicle emission control program A vehtcular source area

can be identified by its atmospheric levels of CO and NOx Figure 6 compares

measured atmospheric levels with calculated atmospheric levels for CO NOx

and the CONOx ratio in the downtown area

TABLE 1 240

REACTIVE HYDROCARBON EMISSIONS

(6-9) AM

1970

LOS ANGELES COUN1Y middot CENTRAL SOURCE AREA middot SOURCE TONS PER CENT TONS PER CENT

Mobile 1260 81 3 135 91 2

Stationary 290 187 1 3 88

Total 1s~o 1000 148 1000

By 7 -Mode Gallonage

241

The calculated values shown in Figure 6 were derived from a baseline

survey of 1100 vehicles and continued surveillance tests both using the Calishy

fornia 7-Mode test cycle The baseline survey showed that motor vehicles withshy

out exhaust control systems had average exhaust emissions concentrations of 3 4

per cent CO and 1000 parts per million of NOx Baseline emissions data apply

to 1965 and earlier model vehicleg and surveillance data to 1966 and later modelsmiddot

Since it can be concluded from calculations and observations that the dilushy

tion of auto exhaust emissions in the atmosphere on a smoggy day in Los Angeles

is approximately 1000 to 1 the calculated values for CO and NOx prior to 1965 are

34 ppm CO and 1 ppm NOxo After 1965 the changing effect of controlled vehicles

in the total vehicle population is reflected in the calculated values

CO and NOx values measured in the atmosphere are also shown in Figure

6 and confirm the values calculated entirely as diluted vehicular emissions NOx

concentrations measured in the atmosphere tend to be consistently a little lower

than the calculated values probably because photochemical reactions remove some

NOx from the system

The data for CO and NOx calculated and measured show that emissions in

downtown Los Angeles originate almost exclusively from motor vehicles and that

atmospheric concentrations there reflect the average emissions from a representashy

tive vehicle population

The ARB has recently published a report entitled A Trend Study of Two

Indicator Hydrocarbons in the South Coast Air Basin Acetylene was used as a

242

specific indicator of automobile exhaust emissions and it was found to have de-

clined in concentration in the Los Angeles atmosphere at an annual rate of 12 5

per cent since 1970 To quote from this report The California implementation

plan requires an annual average reduction in these emissions (reactive organic

compounds) of 166 tons per day or 11 1 of the 1970 tonnage per year The per cent

reductions in the_ acetylene levels at Los Angeles and Azusa are greater than reshy

quired by the implementation plan Since acetylene is almost entirely associated

J with auto exhaust this demonstrates that the motor vehicle emission control

program is achieving its purpose

To summarize at this point it has been deomonstrated that high oxidant values

are due to motor vehicular emissions of NOx and HC because

NOx and HC are the principal reactants in the oxidant formation process

and they originate primarily from motor vehicle emissions and

The highest oxidant values are recorded in_ effect areas that receive air

from source areas where motor vehicles are clearly identified as the

dominant source of NOx and HC

243

Future Control Strategy

The APCD strategy for achieving and maintaining the oxidant air quality

standard is based upon the fact that high oxidant values are due to motor ve-

hicle emissions of hydrocarlxms arrl nitrogen oxides This strategy is as follows

1 Both Hydrocarbon and Nitrogen Oxides Emissions Must Be Considered To Achieve the Federal Oxidant Standard

There is wide agreement that NOx and HC are the principal reactants in

the oxidant formation process and that vehicular emissions are a major source

of NOx HC and CO

2 Effective Regulation of Atmospheric Concentrations of Both HC and NOx and of the Ratio Between Them is necessary for Attainment of the Federal Air Quality Standard for Oxidant

Basmiddoted on the abundance middotof available experimental evidence it is our firm

position that the most rational approach to solving the photochemical oxidant smog

problem in the South Coast Air Basin (SCAB) is to control the quantities of emissions

from motor vehicles of both smog precursors--Hcmiddot and NOx--their resulting atmosshy

pheric concentrations and the ratios between both contaminants which will result

from these controls

We arc also convinced that the oxidant and nitrogen dioxide air quality stanshy

dards can and will be met not by 1975 or 1977 but by the early 1980 s if the emisshy

sion control program as originally outlined by Ca~ifornia or a slight modification

of it proposed by the District is followed and enforced This should also provide

for continued compliance with these air quality standards at least through 1990

244

It will also allow time for a reappraisal in about 1978 of the whole situation relative

to the ultimate emission standards required and the best approach to their impleshy

mentation

Calculation of the degree of control necessary to attain the air quality

~ standards for oxidant and nitrogen dioxide involves indirect complex methods 1

aimed at determ_ining the degree of control of the primary contaminants directly

emitted by automobiles

The following evidence supports our proposed solution to the problem in

terms of both the atmospheric concentrations of the oxidant precursors NOx

and HC the ratio between them as reflected in their exhaust emission standards

and the resulting atmospheric concentrations of oxidant which comply with the air

quality standards

Chamber Results and Projections to the Atmosphere

The importance of environmental chamberwork cannot be minimized the

j need for and direction of the whole emission control program was based initially

j on the results of chamber experiments In order to understand the importance to

air quality of achieving both the correct low quantities of emissions and the right

ratio we can present several graphic portrayals of analyses of experimental labshy

oratory work together with their relationship to past present and future air quality

in terms of both morning primary reactant concentrations during the morning

traffic peak and the equivalent emissions which would produce them

245

Figure 7 shows maximum ozone levels that were obtained by irradiating

varying amounts of auto exhaust hydrocarbons and oxides of nitrogen in an environshy

mental chamber The corresponding ozone levels then can be found for any comshy

bination of BC and NOx concentrations Thus high ozone is produced with high

emissions of both hydrocarbons and oxides of nitrogen and low oxidant is formed with

low emissions However either low NOx or low HC emissions11 can also produce

low oxidant--graphic and clear evidence of the importance of the NOxHC ratio in

ozone formation Furthermore each and every possible combination of values for

NOx and HC has then a corresponding characteristic maximum chamber ozone

concentration

Using this graph we can estimate what ozone levels would result if certain

atmospheric mixtures of NOx and HC could be injected into the chamber and

irradiated Such estimates were made for 1960 and 1965 using atmospheric data

rlThe points labeles 1960 and 65 show the location of the highest levels of both

HC and NOx found in the air in those years in Downtown Los Angeles (OOLA) area

during the 6-9 AM traffic peak

It has been demonstrated by use of CO and NOx data and CONOx ratios

hnw well the characteristics of vehicle emissions are reflected in the atmosphere

We know what emissions from the average vehicle were then in 1960-1965 both

for HC and NOx so that we can mathematically relate emissions to atmospheric

concentrations for those years and so for future years also knowing or calculating

only what the characteristic emissions will be from the average vehicle

246

The NOx concentrations stayed about the same from 1960 through 1965 because

average vehicle emissions of that contaminant did not change during that time

Mobile source emissions can be shown to have contributed essentially all of this obshy

served result However blow by controls did reduce emissions of HC and the

concentrations dropped accordingly In 1965 the last year before exhaust controls

the point 65 indicates where we were then in terms of maximum ozone formation

to be expected in a chamber with the highest HC and NO concentrations found in the X

air that year Levels of ozone actually measured in the atmosphere however

are higher than those shown on the graph for high NOx and I-IC concentrations for

those years up to the present

The strategy to meet the oxidant standard is obvious--get atmospheric NOx

and HC concentrations out of the area on the chart that produces high ozone levels

and put them in tie areas with the lowest levels This can only be done by implementshy

ing appropriate emission standards

As can be seen that did not happen between 1965 and 1970 because manufacshy

turers used controls on new cars in California which while causing a decrease in

BC (and CO) allowed a large increase in NOx emissions Thus the path line of

the atmosphere on the chart goes up from 65 and diagonally to the left passing

through an area of higher ozone levels The atmospheric concentrations of oxidant

predictably increased during the years 1967 and 1968 By 1970 they dropped to lower

levels - -back to about the same as in 1965- -exactly as predicted by the model The

app14oximate location of the point for 1970 (70) was both predicted on the basis of

247

the mathematical model and confirmed by atm-ospheric measurements of

[)owntown Los Angeles morning summertime NOx and calculated HC values

Again it should be pointed out that those points show the highest possible

concentrations of NOx and HC Years with less restrictive weather conditions

(for accumulating high primary contaminant levels) would cause lower measured

maximum NOx and HC levels but the calculations would still yield the points

shown Thus we are taking the most pessimistic view

Future Projections

In 1973 we were at about the point labeled 73 and ozone levels were beginshy

ning to drop as expected middot It should be emphasized that ozone values plotted on

thi$ graph are for the chamber only- -not the atmosphere The future path the

points 7 4 and on to 90 represents our estimate of future atmospheric levels of

NO and BC expected if the exhaust emission standards are just met While that X -

is optimistic it is all we really can do since performance of future vehicle models

is unknown We will achieve maximum ozone levels at or below the standard by

about 1980-1985 This will only be true however if cars in compliance with the

California interim standards for HC and NOx continue to be added to the vehicle

population at the normal rate These standards provide the optimum ratio of NO X

to HC necessary to provide the nitric oxide (NO) needed for the reaction that re-

moves from the air both oxidant formed photochemically and oxidant which occurs

as natural background which alone may cause the standard to be exceeded This

ratio is about 112 or 2 parts NOx to 1 part HC

248

The optimum NOxHC ratio is a key element in the APCD strategy but will

require a finite time for its attainment Replacement of older cars by newer ones

equipped to meet the most stringent standards is the only reasonable mechanism

which can change it VMT reduction proposed as a prime strategy by EPA cannot

change this crl(ical ratio which is a basic characteristic of the population at any

given time

Validation of the Districts Control Strategy

Figure 8 compares (1) future chamber oxidant levels based upon the

future maximum concentrations of HC and NOx we expect each year with the

California control program (2) calculated atmospheric concentrations using ~ I

our chamber-to-atmasphere empirical translation and (3) actual measured atmos-f 1l pheric oxidant maxima This clearly sets forth the relationship among these three

factors

The chamber concentrations (lower curve) middotare the lowest values shown

The actual atmospheric data (points connected by heavy dotted and solid lines)

vary considerably from year to year partly because of the vagaries of the weather

In all cases the atmospheric oxidant values are higher than the chamber values

because of the addition of vehicle emissions as the air parcel travels from source

to receptor areas The calculated atmospheric data (thin dashed and solid curves)

are shown to be the highest generally exceeding or equalling the actual measured

data and of course always exceeding the chamber data Thus the model paints

the most pessimistic picture possible It can be seen that by about 19801 1985 atmos -

pheric levels should be at or below the Federal air quality standard of 0 08 ppm oxidant

249

3 Motor Vehicle Exhaust Control is the Only Requirement for Achieving the Oxidant Standard by 1980

We can show that the existing motor vehicle control program has resulted

in a significant reduction of oxidant concentrations in the air

The foregoing material explained the relationship between vehicula~ emis -

sions in source areas and the high oxidant levels measured in effect areas This

relationship is exemplified by the downward trend of oxidant levels in the atmosshy

phere and by the similar year-by-year trends of NO and HC emissions from the X

average motor vehicle A projection of these vehicle emissions factors shows that

the associated maximum oxidant level in the atmosphere will meet the oxidant standard

by about 1980-1985

Figure 9 compares by year the number of days that the oxidant air quality

standard was exceeded in three separate areas with the average NO and HC emissions X

per vehicle mile To comply with the air quality regulations the number of days that

this standard is exceeded must be reduced to one per year

The lines plotted on Figure 9 show that a definite relationship exists between

the emissions from the average motor vehicle and the number of days each year that

the oxidant concentration in the air exceeds the clean air standard

The oxidant trendlines for downtown Los Angeles Pasadena arrl Azusa are

all downward and the slopes are about the same This similarity is logical because

the process that results in the suppression of oxidant accumulation simply has been

displaced from one area to another This was a unique one time situation because

of the increase in NOx between 1966 and 1971 After 1971 all areas are down Thus

l

250

the same conclusion is reached that the oxidantstandard will be met in the 1980s

I whether air quality data or vehicle emissions trends are projected middot~ Ul-

This outlook is based on the APCD s belief that future growth in both the

Los Angeles area and SCAB will not create any locality with a traffic density greater

than any traffic density in the area to date For the past 25 years the area around

downtown Los Angeles has been the area of maximum traffic density and therefore

the emissions source area responsible for the maximum effect area measurements

It is assumed that the traffic density in any future source area will be no

greater than the traffic density in downtown Los Angeles Thus since the

vehicular emissions control program will achieve and maintain the air quality

standards in areas affected by vehicular emissions from downtown Los Angeles it

will also achieve and maintain them for any area of SCAB

Summary Conclusions and Recommendations

In conclusion we have shown that a source and effect area analysis of emisshy

sions and resulting oxidant is a more reasonable and accurate representation of

the Los Angeles area for air quality analysis than gross integration metho9s such

as the big box technique It has been shown that motor vehicles are the major and

almost sole contributor to the primary HC and NOx emissions in the downtown source

area which results in the high oxidant levels in the San Gabriel Valley in fact the

highest in SCAB An air quality model and vehicle emissions control strategy has

been suggested to meet the oxidant standard by mid-1980 s

251

We have shown that

bull Only by adjusting the ratio of NOxHC in the motor vehicle emissions to

permit accumulation of sufficient atmospheric NO to sea venge the normal

atmospheric background oxidant can the standard be attained

bull The APCD strategy which provides for implementation of the present

California interim emissions standards for NOx HC and CO for new

motor vehicles in California beginning with the 1975 model vehicles will

result in compliance with the CO N02 and oxidant air quality standards

by the mid 1980 s and will maintain this compliance until 1990 and

possibly longer

bull The effectiveness of the present California motor vehicle control program

is easily demonstrable using air quality data from several areas in Los

Angeles County 1960-1973

bull To assure achievement and maintenance of the air quality goals as now preshy

dicted there must be periodic assessments of the effectiveness of the

motor vehicle control program followed by corrective actions if necessary

What has been accomplished thus far is significant but much more remains

to be done so that the best possible representation of emissions and resulting air

quality may be available for use in this air basin A much better emission inventory

defining the spatial and temporal distribution of both mobile and stationary sources

is needed Better statbnary source information is needed to evaluate the local

effects of these emissions Further detailed studies are needed to establish the

252

true relationship between emissions data from vehicle test cycles and the actual

operation of vehicles neither the 7-mode nor the CVS procedure provides a true

representation of actual vehicle operation Further tracer studies to assess the

transport and dilution of mobile and stationary source emissions from selected

source areas are also needed

253

1111

IUD

a CC I w gt-

1111

1UO

IUD

I 990

IDJO

1180

1111

IUO

FIGURE I

HYDROCARBONS

STATIONARY SOURCES MOTOR VEHICLES

- --

8 12 II 20 742 2l IS 12 I 4

HUNDREDS

HYDROCARBON EMISSIONS STATIONARY SOURCES IN

OXIDES OF

0

OF TONSDAY

FROM MOTOO VEHICLES AND LOS ANGELES COUNTY

NITROGEN

STATIONARY SOURCES

MOTOR VEHICLES

011111111111111111110111bull1111111

IIIIIIHIIIIIIIIIHIUII

llillL Its rd

l1uu~111111u1111111

2 I O 1 J 3

HUND REDS OF TONSDAY

OXIDES OF NITROGEN EMISSIONS FROM MOTOR VEHICLES ANO STATIONARY SOURCES IN LOS ANGELES COUNTY

illl~ -~--~ i~-=i _J~l ~--~ bull_~L- I ~~~-~~--Z ~

6

6S-66 ox

ICS ~A~1 M

i ssmuwmmgt

bullI

e COROyent_

64 ~ IDB RIVERS~

ORAJfD

-

t t 10 miles

bullmiddotsame Avg Cone Both Years

Pigare 2

YEAR OP HIGHEST OXlDANI CONCENTRATIONS

Highest Average of Daily -Maiimum One-Hour Concentrations

During July August amp September 1963-1972

bullLj

I

64

70 s11 3RlU)U0

70

--__ 69bull

N V +=

middot Source Air Resources Board

-200o

t t 10 adlea

tDS ampIJtsect

-1~

-1611ASampXllmiddot bull - bull -z----~------

I ldmmprwJ

IIVERSIDI

~ - 70

OampY -1 U 70 bull L

I

N V1 V

middot-i___

-----------------------------------------------------------i----------------------------

Figure 3

CHANGE OP OXIDANT CONCENTRATIONS

Percent Change from the Highest Three-Year Average to the 1970-72 Average

Of Daily Maximum One-Hour Con~entrationa for JulY August amp September

Source Air Resources Board

256

FIGURE 4 TYPICAL FLOW OF POLLUTED Am PARCEIS CIUGINATING AT DIFFERENT LOCATIONS IN THE LOS ARE~S BASIN - STARTIOO 0900 PST

l I

OAT

TRAJECTORY SUWMATIOl4

----- SMOG ~AVS

I

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullNONbullSlfOG DAYS

ISTARTING Tl~ cgxpsy

~ HAW

(CA

257

FiGURE 5 ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AND OXIDANT IN DOWlflC1N LOS AIDELES (SOURCE AREA) AND PASADENA (EFFECT AREA) 1

1960-1972

LO CARBON MONOXIDE

30

Pasadena

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullbullbullbullbull Downtown Los Angeles

20

10

o_______________________________

OXIDANT

)

2 Down~ Los Angeles

1

o________________________ 1960 1962 196L 1966 1968 1970 1972

YEAR

bullbullbullbullbull

bullbullbullbullbullbullbull

258

FIGURE 6 COMPARISON 01 CALCULATED AND MEASURED ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AN1) OXIDES OF NITROOEN IN DCMNTOWN IDS AIJELES

196o-1972

CARBON MONOXIDE

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ~ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot _-- ---_ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ----middotmiddot-bullw-_~ ---bullbullbull

10

o_______________1111111_____

OXIDES OF NITROGEN25

20

15 bullbullbullbullbullmiddotmiddotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~

1-i 10 middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ---

oS o_______________________

RATIO CONOx

40

50

0 +raquo Cd

p 30

~ 20

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot bullbullbullbullbull middotmiddotmiddotmiddotmiddot-shybullbullbullbullbull 0 u

bullbullbullbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot 10

0 j

ilI 196o 1964 1968 1970 1972 I

YEAR

Measured~D-owntown Los Angeles (90th percentile ofmiddot daily] instantaneous maxima)

Calculated - Aver~ge vehicle emissions - Present control program

259

FIGURE 7

25

t i5

flJ

~ on ~ ~ Q) bO 100 Jo

+gt on z

o5

EFFECT OF CALIFORNIA 1 s AUTO EXHAUST CONTROL ffiOORA M ON MAXIMUM CHAMBER OZONE CONCENTRATION

- PPM

357bullbull

r 76 bull

11 l

30

20

CHAMBER OZONE MAXIMUM

50

10

o___________111111111111______111111111111_____________

0 05 10 15 20 25

Hydrocarbons m-2 (LB-15) - PPM (as Hexane)middot

--

bull bull bull

r--=--~1 ~a==-~ - _~l ~ y--===-- ~~--~-- ~ r---~~

o

o8

~ I

~ 0 H 8 o6 I

c~ ~ 0 z 0 0

8

~ o+ A H gtlto-

02

middoto

Figure 8 Calculated t1ax1mum Levels Instantaneous and Hourly Average

of Atmospheric Oxidant Compared to Measured Los Angeles County Maxima-with Projections to 1990

(California Standards)

~ -Calculated Inst ax ~

f Calculate Max Hr Avg 03

_ bullbull _ _ - i bull

0 bullbull -l bullbull a0Ieasured Inst Lax o3 bull middotmiddotmiddot~bull 0bull _ ____ V ~ ea~ured ~ Hr Avr o3

~~ r---

~ ~ NB r~ima for 197 4 amiddots of 121074--- -_ Chamber Ozone F ~_ _~

- 1L_

~ Federal Primarfo Air ~uality Standard ~6- -UaximumT- our Avera~elr~ppm-------------- --~ ------- -~- -~-- ~

I I I I I I I I I I I I I I I I I N1 O

1960 6i 64 66 ~i middot-o 72 74 76 79 middotso middot92 84 bullg s9 9o

TBAR (end)

0

261 FIGURE -OMPARISON OF ATMOSPHERIC OXIDANT TRENDS WITH AVERAGE NCJx AND

HC EMISSIONS (Grams per Mile from Average Vehicle)

JOO Number of days state oxidant standara wds equalled or exceeded

--- Azusa __ Pasadena ________ Downtown Los Angeles

20

15 u

___ Hydroc_arbons Oxides of Nitrogenbullmiddotmiddotmiddotmiddotmiddotbullbullmiddot 1975 and later-assume middotcalifornia ARB standards

o_ ___________________________11111____

1965 1970 1975middot 198omiddot 198S 1990

141

rotary engine vehicles and thereby be the only rotary engine vehicle

manufacturer and marketer in the United States General Motorsgt elimination

of therotary engine stated for reasons of emissions is probably more

influenced by problems with fml economy although the two are a bit

difficult to separate Mazda is meeting the 1975 emissions standards and

in fact can meet the 1977 emission standards It has not solved its fuel

economy difficulties on the 1975 cars they will do better in 1976 All

evidence points to a fuel economy penalty for the rotary engine Nonetheshy

less we do have this option available because of the Japanese Also the

foreign manufacturers are providing us with a small number of diesel

engine cars These are of great interest because of definite fuel economy

advantages The diesel engine vehicles also meet the 1977 emissions

standards right now Also in J975 well 3ee the CVCC engine marketed by

Honda

The costs of the 1975 vehicles over tae lifetime of the vehicle are

definitely lower than the costs of the 197~ vehicles The National Academy

of Sciences estimate averaged over all vehicles is that in comparison to

the 1970 vehicles the lifetime cost of emission control system including

maintenance and fuel economy costs is aboJt $250 per vehicle greater in

1975 than 1970 Since the 1974 vehicles w2re about $500 more expensive

there has been a net saving in going from 1974 to 1975 I think the

conclusion we should draw for 1975 is that the auto industry has done a

pretty good job in meeting these standards This is something which they

said they couldnt do a few years ago something which they said that if

they could do it would be much more expewdve than it has turned out to

be

The same technology can be applied to 1977 models with no technological

difficulty and only slight refinements of the systems The fuel economy

142

penalties as estimated by the National Academy of Sciences are small 3

or less in going to the 1977 standards This estimate does assume further

advancements by the auto industry to improve fuel economy--primarily

improved exhaust gas recirculation systems It is unfortunate that this

issue of fuel economy has become so mixed up with the air pollution question

because the two are only slightly related If one is really concerned about

fuel economy and there isnt too much evidence that the auto industry or

the American public really is too concerned right now there is only one

way to have a drastic effect on fuel economy and that is to decrease the

vehicle weight Until that is done with gains on the order of 50 or

more to worry about 3 or 5 differences in fuel economy related to emission

control systems is simply to focus upon the wrong issue

Now what are the problem areas What remains to be done The

problems certainly arent over with the introduction of the 1975 vehicles

Problem Area Number One Field performance What is going to happen

to these vehicles when they get into actual service Past experience with

the 1971 through 1973 vehicles has been rather poor in that EPA and

California surveillance data show that these vehicles are not meeting the

standards Many of them did not meet the standards when they were new

The situation in general is getting worse at least for CO and hydrocarbons

that is with time the emission levels of CO and hydrocarbons for the 1971 I through 1973 vehicles is degrading There is no in-service experience of

this sort with the 1975 vehicles yet The certification data look quite I promising but the test procedures especially for durability are not ithe same as what occurs in actual use It is generally stated that the

1actual use situation for the catalysts will be more severe than the EPA

test procedure A larger number of cold starts are involved in actual use

than in the EPA test procedure and thermal cycling will probably have an

143

adverse effect on the lifetime of the cata]_yst This is not so obvious

It is also likely that the higher temperature duty cycle in actual use will

improve the performance of the catalyst in that it will help to regenerate

the catalyst through the removal of contaminants as long as one does not

get into an overheat situation The National Academy of Sciences estimate

was that the number of catalyst failures tn the first 50000 miles would

be on the order of about 7 Thats a very difficult number to estimate in

the absence of any real data A 7 failure still leaves a net gain in

emissions control even if nothing is done about this failure This points

to the problem of what happens after 50000 miles The EPA certification

procedure and control program only addresses the first 50000 miles The

second 50000 miles or slightly less for the average car is the responsishy

bility of the states Unfortunately then~ seems to be very little progress

in the area of mandatory inspection and ma-Lntenance--very little thought

being given to whether the replacement ofthe catalyst at 50000 miles

if it has failed is going to be required and how that is going to be

brought about The area of field performance remains a major problem

area one which obviously needs to be monitored as the California Air

Resources Board has been doing in the past but probably even more carefully

because the unknowns are higher with the catalyst systems

Problem Area Number Two Evaporative hydrocarbons from automobiles

It was identified at least 18 months ago that the evaporative emission

control systems are not working that the evaporative emissions are on the

order of 10 times greater than generally thought In the Los Angeles

area cars which are supposed to be under good evaporative emissions

controls are emitting approximately 19 grams per mile of hydrocarbons

through evaporation This apparently has to do with the test procedure used

144

The EPA is pursuing this The California Air Resources Board does have some

consideration going on for this but it appears that the level of activity

in resolving this problem is simply not adequate If we are to go ahead

to 04 of a gram per mile exhaust emissions standards for hydrocarbons

then it just doesnt make sense to let 19 grams per mile equivalent escape

through evaporative sources

Problem Area Number Three What about the secondary effects of the

catalyst control systems Specifically this is the sulfate emissions

problem and I really do not know the answer to that Our appraisal is

that it is not going to be an immediate problem so we can find out what

the problem is in time to solve it The way to solve it now since the

automobile industry is committed to catalysts and it is unreasonable

to expect that they will reverse that technology in any short period of

time is take the sulfur out of the gasoline The cost of removing sulfur

from gasoline is apparently less than one cent per gallon Therefore if

it becomes necessary to be concerned with sulfate emissions the way to

meet the problem is to take the sulfur out of gasoline Obviously sulfate

emissions need to be monitored very carefully to see what happens The

final appraisal is certainly not now available Another secondary effect

of the catalysts is the introduction of significant quantities of platinum

into an environment where it hasnt existed before Not only through

exhaust emissions which appear to be small but also through the disposal

problem of the catalytic reactors Since the quantity of platinum involved

is quite small the argument is sometimes used that platinum does not

represent much of a problem The fact that the amount of platinum in the

catalyst is so small may also mean that its not economical to recover it

This is probably unfortunate because then the disposal of these catalysts

l Jj

145

I becomes important I will not speak to the medical issues because

am not qualified The evidence is that theuro~ platinum will be emitted in a

form which does not enter into biological cycles--but this is no assurance

that it couldnt later be transformed in such a form What is obviously

needed is a very careful monitoring program which hopefully was started

before the catalysts were put into service If it wasnt then it should

be started today

Problem Area Number Four NO control The big problem with NO X X

control is that nobody seems to know or to be willing to establish what

the emission control level should be It is essential that this be tied

down rapidly and that it be fixed for a reiatively long period of time

because the NO level is going to have a VE~ry important ef feet upon the X

development of advanced engine technology The 20 gm level has been

attained in California with some loss of fuel economy through the use of

EGR and it is not unreasonable in our estimation to go to 15 grams per

mile with very little loss in fuel economy To go to 04 gram per mile

with present technology requires the use of one of two catalytic systems

either the reduction catalyst in tandem with the oxidation catalyst or what

is known as the three-way catalyst Both of these systems require technoshy

logical gains The state of development appears to be roughly that of the

oxidation catalyst two years ago The auto industry will probably say

that it is not quite that advanced but that if it were required to go to

04 gram per mile in 1978 that it could be done With the catalyst systems

the fuel economy penalties would not be great in fact the improvement to

the engine which would be required to make the system work would again

probably even allow a slight improvement in fuel economy What the 04

gram per mile NO catalyst system would appear to do however is to X

146

eliminate the possibility of the introduction of stratified charge engines

both the CVCC and the direction injection system and also diesel engines

It is in the context of the advantages of these advanced engines to meet

emission standards with improved fuel economy that one should be very

cautious about the 04 grammile oxides of nitrogen standards for automoshy

biles My own personal opinion is that the number should not be that

stringent that a number of 1 or 15 gm is appropriate Such a level

would require advancements but would not incur great penalties

Other items which I view as problem areas are less technically

involved and therefore require fewer comments

bull Nonregulated pollutants--again thls is a matter of keeping track

of particulates aldehydes hydrocarbon composition to make

certain that important pollutants ire not being overlooked or

that emission control systems are not increasing the output of

some of these pollutants

bull Fuel economy The pressures of fuel economy are going to be used

as arguments against going ahead wlth emissions control Mostly

these two can be resolved simultaneously We should simply ask

the automobile industry to work harder at this

bull Final problem area New fuels Again it does not appear that

the introduction of new fuels will come about as an emissions

control approach but that they may be introduced because of the

changing fuel availability patterns and the energy crisis These

fuels should be watched carefully for their impact upon emissions

This does middotappear to be an area in which a great deal of study is

going on at the present time It is one problem area perhaps in

which the amount of wprk being done is adequate to the problem

which is involved

147

In sunnnary then the appraisal of the 1975 systems is that they are

a big advancement they will be a lot better than most of us thought and

that we should give the automobile industry credit for the job theyve

done in coming up with their emissions control systems

With that boost for the auto industry which Im very unaccustomed

to Ill entertain your questions

-------=-~ ~~~ U- ~a1

~_~a--~-~ -J~ ~ -~r- _ --=~-- -___ja--~ __1~~ ~-~----=

AIR

1-4 FUEL----1

I I ENGINE

I II

_________ EXHAUST SYSTEM I bull EXHAUST

I I I

+ MIXTURE CONTROL COMBUSTION MODIFICATION EXHAUST TREATMENT

FuelAir Metering Ignition Air Jnjection FuelAir Mixing Chamber Geometry Thermal Reactor Fuel Vaporization Spark Timing Oxidation Catalyst Mixture Distribution Staged Combustion Reduction Catalyst Fuel Characteristics Ex tern almiddot Combustion Three Way Catalyst Exhaust Gas Redrculation Particulate Trap

FIGURE 1 Approaches to the Control of Engine Emissions

~ i 00

149

TABLE I

Average Emissions of 1975 Certification Vehicles (As Corrected Using the 50000-Mile Deterioration Factor)

Emissions in gmi Fraction of Standard HC CO NO HC CO NO

Federal 1975 X X

AMC 065 67 25 043 045 080

Chrysler 074 77 25 049 051 082

Ford 081 92 24 054 061 078

GM 083 80 23 055 053 074

Weighted Average 080 82 24 053 055 076

California 1975

AMC 042 49 17 047 054 087

Chrysler 048 61 16 053 067 082

Ford 052 56 13 058 062 067

GM 065 55 16 0 72 061 082

Weighted Average 058 56 16 064 062 078

kWeighted average assumes the following market shares AMC 3 Chrysler 16 Ford 27 and GM 54

150

TABLE II

Total Number of Vehicles Certified for California 1975 Standard and the Number (and percentage) of These Able to Meet

Certain More Stringent Standards

Calif 1975 Federal 1977 Hypothesized Hypothes ized 099020 04J420 049020 093420

i ~

Manufacturer no () no () no () no ()

AMC 16 (100) 1 ( 6) ti ( 38) 3 (19)

Chrysler 21 (100) 2 ( 9) ( 33) 0 ( O)

Ford 26 (100) 4 (15) -middot ( 15) 5 (19)

l GM 46 (100) 1 ( 2) -1 ( 9) 5 (11)

Foreign 62 (100) 21 (34) 3H (61) 28 (45)

1J

f

-l

151

CURRENT STATUS OF ALTERNATIVE AUTOM)BIIE ENGINE TECHNOLCXY

by

Henry K Newhall Project Leader Fuels Division

Chevron Research CanpanyRicbmmd California

I

iH1middot

10 1ntroduction and General Background

I

11 General

The term stratified ct1arge englne has been used for many

years in connection with a variety of unconventional engine

combustion systems Common to nearly all such systems is

the combustion of fuel-air mixtures havlng a significant

gradation or stratification in fuel- concentration within the

engine combustion chamber Henee the term nstratifled charge

Historically the objective of stratified charge engine designs

has been to permit spark ignition engine operation with average

or overall fuel-air ratios lean beyond the ignition limits of

conventional combustion systems The advantages of this type

of operation will be enumerated shortly Attempts at achieving

this objective date back to the first or second decade of this

century 1

More recently the stratified charge engine has been recognized

as a potential means for control of vehicle pollutant emissions

with minimum loss of fuel economy As a consequence the

various stratified charge concepts have been the focus of

renewed interest

152

12 Advantages and Disadvantages of Lean Mixture Operation

Fuel-lean combustion as achieved in a number of the stratified

charge engine designs receiving current attention has both

advantages and disadvantages wnen considered from the comshy

bined standpoints of emissionsmiddot control vehicle performance

and fuel economy

Advantages of lean mixture operation include the following

Excess oxygen contained in lean mixture combustion

gases helps to promote complete oxidation of hydroshy

carbons (HG) and carbon monoxide (CO) both in the

engine cylinder and in the exhaust system

Lean mixture combustion results in reduced peak

engine cycle temperatures and can therefore yield

lowered nitrogen oxide (NOx) emissions

Thermodynamic properties of lean mixture combustion

products are favorable from the standpoint of engine

cycle thermal efficiency (reduced extent cf dissociashy

tion and higher effective specific heats ratio)

Lean mixture operation caG reduce or eliminate the

need for air throttling as a means of engine load

control The consequent reduction in pumping losses

can result in significantly improved part load fuel

economy

153

Disadvantages of lean mixture operation include the following

Relatively low combustion gas temperatures during

the engine cycle expansion and exhaust processes

are inherent i~ lean mixture operation As a conseshy

quence hydrocarbon oxidation reactions are retarded

and unburned hydrocarbon exhaust emissions can be

excessive

Engine modifications aimed at raising exhaust temperashy

i tures for improved HC emissions control (retarded middot~

ignition timing lowered compression ratlo protrtacted combustion) necessarily impair engine fuel economy1 I

1j bull If lean mixture operation is to be maintained over ~

the entire engine load range maximum power output t l and hence vehicle performance are significantly

impaired

Lean mixture exhaust gases are not amenable to treatshy

ment by existing reducing catalysts for NOx emissions

control

Lean mixture combustion if not carefully controlled

can result in formation of undesirable odorant

materials that appear ln significant concentrations

in the engine exhaust Diesel exhaust odor is typical

of this problem and is thought to derive from lean mixshy

ture regions of the combustion chamber

154

Measures required for control of NOx emissions

to low levels (as example EGR) can accentuate

the above HC and odorant emissions problems

Successful developmentmiddotor the several stratified charge

engine designs now receiving serious attention will depend

very much on the balance that can be achieved among the

foregoing favorable and unfavorable features of lean comshy

bustion This balance will of course depend ultimately on

the standards or goals that are set for emissions control

fuel economy vehicle performance and cost Of particular

importance are the relationships between three factors -

UBHC emissions NOx emissions and fuel economy

13 Stratified Charge Engine Concepts

Charge stratification permitting lean mixture operation has

been achieved in a number of ways using differing concepts

and design configurations

Irrespective of the means used for achieving charge stratifishy

cation two distinct types of combustion process can be idenshy

tified One approach involves ignition of a small and

localized quantity of flammable mixture which in turn serves

to ignite a much larger quantity of adjoining or sur~rounding

fuel-lean mixture - too lean for ignition under normal cirshy

cumstances Requisite m1xture stratification has been achieved

155

in several different ways rangiDg from use of fuel injection

djrectly into open combustion chambers to use of dual

combustion chambers divided physically into rich and lean

mixture regions Under most operating conditions the

overall or average fuel-air ratio is fuel-lean and the

advantages enumerated above for lean operation can be realized

A second approach involves timed staging of the combustion

process An initial rich mj_xture stage in which major comshy

bustion reactions are completed is followed by rapid mixing

of rich mixture combustion products with an excess of air

Mixing and the resultant temperature reduction can in

principle occur so rapidly that minimum opportunity for NO

formation exists and as a consequence NOx emissions are

low Sufficient excess air is made available to encourage

complete oxidation of hydrocarbons and CO in the engine

cylinder and exhaust system The staged combustion concept

has been specifically exploited 1n so-called divided-chamber

or large volume prechamber engine designs But lt will be

seen that staging is also inherent to some degree in other

types of stratified charge engines

The foregoing would indicate that stratified charge engines

can be categorized either as lean burn engines or staged

combustion engines In reality the division between conshy

cepts is not so clear cut Many engines encompass features

of both concepts

156

14 Scope of This Report

During the past several years a large number of engine designs

falling into the broad category of stratified charge engines

have been proposed Many of these have been evaluated by comshy

petent organizations and have been found lacking in one or a

number of important areas A much smaller number of stratified

charge engine designs have shown promise for improved emissions

control and fuel economy with acceptable performance durashy

bility and production feasibility These are currently

receiving intensive research andor development efforts by

major organizations - both domestic and foreign

The purpose of this report is not to enumerate and describe the

many variations of stratified charge engine design that have

been proposed in recent years Rather it is intended to focus

on those engines that are receiving serious development efforts

and for which a reasonably Jarge and sound body of experimental

data has evolved It is hoped that this approach will lead to

a reliable appraisal of the potential for stratified charge

engine systems

20 Open-Chamber Stratified Charge Engines

21 General

From the standpoint of mechanical design stratified charge

engines can be conveniently divided into two types open-chamber

and dual-chamber The open-chamber stratjfied charge engine

has a long history of research lnterest Those crigines

157

reaching the most advanced stages of development are probably

the Ford-programmed c~mbustion process (PROC0) 2 3 and Texacos

controlled combustion process (TCCS) 4 5 Both engines employ a

combination of inlet aar swirl and direct timed combustion

chamber fuel injection to achieve a local fuel-rich ignitable

mixture near the point of ignition _For both engines the overshy

all mixture ratio under most operating conditions is fuel lean

Aside from these general design features that are common to

the two engiries details of their respective engine_cycle proshy

cesses are quite different and these differences reflect

strongly in comparisons of engine performance and emissions

characteristics

22 The Ford PROCO Engin~

221 Description

The Ford PROCO engine is an outgrowth of a stratified charge

development program initiated by Ford in the late 1950s The

development objective at that time was an engine having dieselshy

like fuel economy but with performance noise levels and

driveability comparable to those of conventional engines In

the 1960s objectives were broadened to include exhaust

emissions control

A recent developmental version of the PROCO engine is shown in

Figure 2-1 Fuel is injected directly into the combustion chamber

during the compression stroke resulting in vaporjzation and

formation of a rich mixture cloud or kernel in the immediate

158

vicinity of the spark plug(s) A flame initiated in this rich

mixture region propagates outwardly to the increasingly fuelshy

lean regions of the chamber At the same time high air swirl

velocities resulting from special orientation of the air inlet

system help to promote rapid mixing of fuel-rich combustion

products with excess air contained in the lean region Air

swirl is augmented by the squ1sh action of the piston as it

approaches the combustion chamber roof at the end of the comshy

pression stroke The effect of rapid mixing can be viewed as

promoting a second stage of cori1bustion in which rlch mixture

zone products mix with air contained in lean regions Charge

stratification permits operation with very lean fuel-air mixshy

tures with attendent fuel economy and emissj_ons advantages In

addition charge stratification and direct fuel injection pershy

mit use of high compression ratios with gasolines of moderate

octane quality - again giving a substantial fuel economy

advantage

Present engine operation includes enrichment under maximum

power demand conditions to mixture ratios richer than

stoichiometric Performance therefore closely matches

that of conventionally powered vehicles

Nearly all PROCO development plans at the present time include

use of oxidizing catalysts for HC emissions control For a

given HC emissions standard oxidizing catalyts permit use

of leaner air-fuel ratios (lower exhaust temperatures)

1

l

159

together with fuel injection and ignition timing charactershy

istics optimized for improved fuel economy

222 Emissions and Fuel Economy

Figure 2-2 is a plot of PROCO vehicle fuel economy versus NOx

emissions based or1 the Federal CVS-CH test procedure Also

included are corresponding HC and CO emissions levels Only

the most recent test data have been plotted since these are

most representative of current program directions and also

reflect most accurately current emphasis on improved vehicle

fuel economy 6 7 For comparison purposes average fuel

economies for 1974 production vehicles weighing 4500 pounds

and 5000 pounds have been plotted~ (The CVS-C values

reported in Reference 8 have been adjusted by 5 to obtain

estimated CVS-CH values)

Data points to the left on Figure 2-2 at the o4 gmile

NOx level represent efforts to achieve statutory 1977

emissions levels 6 While the NOx target of o4 gmile was

met the requisite use of exhaust gas recirculation (EGR)

resulted in HC emissions above the statutory level

A redefined NOx target of 2 gn1ile has resulted in the recent

data points appearing in the upper right hand region of

Figure 2-2 7 The HC and CO emissions values listed are

without exhaust oxidation catalysts Assuming catalyst middotl

conversion efficiencies of 50-60 at the end of 50000 miles

of operation HC and CO levels will approach but not meet

160

statutory levels It is clear that excellent fuel economies

have been obtained at the indlcated levels of emissions

control - some 40 to 45 improved re1at1ve to 1974 produc-

tj_on vehicle averages for the same weight class

The cross-hatched horizontal band appearing across the upper

part of Figure 2-2 represents the reductions in NOx emissions

achieveble with use of EGR if HC emissions are unrestricted

The statutory 04 gmile level can apparently be achieved

with this engine with little or no loss of fuel economy but

with significant increases in HC emissions The HC increase

is ascribed to the quenching effect of EGR in lean-middotmixture

regions of the combustion chamber

223 Fuel Requirements

Current PROCO engines operated v1ith 11 1 compression ratio

yield a significant fuel economy advantage over conventional

production engines at current compression ratios According

to Ford engineers the PROCO engine at this compression

ratio j_s satisfied by typical fu1J-boi1ing commercial gasoshy

lines of 91 RON rating Conventional engines are limited to

compression ratios of about 81 and possibly less for

operation on similar fuels

Results of preliminary experiments indicate that the PROCO

engine may be less sensitive to fuel volatility than convenshy

tional engines - m1 important ff1ctor in flextb1 llty from the

standpoint of the fuel supplier

161

224 Present Status

Present development objectives are two-fold

Develop calibrations for alternate emissions target

levels carefully defining the fueleconofuy pbtenshy

tial associated with each level of emissions control

Convert engine and auxiliary systems to designs

feasible for high volume production

23 The Texaco TCCS Stratified Charge Engine

231 General Description

Like the Ford PROCO engine Texacos TCCS system involves_

coordinated air swirl and direct combustion chamber fuel

injection to achieve charge stratification Inlet portshy

induced cylinder air swirl rates typically approach ten times

the rotational engine speed A sectional view of the TCCS

combustion chamber is shown in Figure 2-3

Unlike the PROCO engine fuel injection in the TCCS engine

begins very late in the compression stroke - just before th~

desired time of ignition As shown in Figure 2-4 the first

portion of fuel injected is immediately swept by the swirling

air into the spark plug region where ignition occurs and a

flame front is established The continuing stream of injected

fuel mixes with swirling air and is swept into the flame

region In many respects the Texaco process resembles the

162

spray burning typical of dj_esel combustion ~r1th the difshy

ference that ignition is achieved by energy from an elec-

tric spark rather than by high compression temperatures

The Texaco engine like the diesel engine does not have a

significant fuel octane requirement Further use of positive

spark ignition obviates fuel I

cetane requirements character-

istic of diesel engines The resultant flexibility of the

TCCS engine regarding fuel requirements is a si~1ificant

attribute

In contrast to the TCCS system Fords PROCO system employs

relatively early injection vaporization and mixing of fuel

with air The combustion process more closely resembles the

premixed flame propagation typical of conventional gasoline

engines The PROCO engine therefore has a definite fuel

octane requirement and cannot be considered a multifuel

system

The TCCS engine operates with hi__gh compression ratios and

with little or no inlet air throttling except at idle conshy

ditions As a consequence fuel economy is excellent--both

at full load and under part load operating conditions

232 Exhaust Emissions and Fuel Economv

Low exhaust temperatures characteristlc of the TCCS system

have necessitated use of exhaust oxidation catalysts for

control of HC emissions to low lf~Vels A11 recent development

163

programs have therefore included use of exhaust oxidation

catalysts and most of the data reported here r~present tests

with catalysts installed or with engines tuned for use with

catalysts

Figures 2-5 and 2-6 present fuel economy data at several

exhaust emissions levels for two vehicles--a US Army M-151

vehicle with naturally aspirated 4-cylinder TCCS conversion

and a Plymouth Cricket with turbocharged 4-cylinder TCCS

engine 9 10 1urbocharging has been used to advantage to

increase maximum power output Also plotted in these figures

I are average fuel economies for 1974 production vehicles of

similar weight 8

I When optimized for maximum fuel economy the rrccs vehicles

can meet NOx levels of about 2 gmile It should be noted

that these are relatively lightueight vehicles and that

increasing vehicle weight to the 4000-5000 pound level could

result in significantly increased NOx emissions Figur~s 2-5

and 2-6 both show that engine modifications for reduced NOx

levels including retarded combustion timing EGR and increased

exhaust back pressure result in substantial fuel economy

penalties

For the naturally aspirated engine reducing NOx emissions

from the 2 gmile level to O l~ gmile incurred a fuel

economy penalty of 20 Reducing NOx from the tllrbocharged

164

engine from 15 gmile to 04 gmile gave a 25 fuel economy

penalty Fuel economies for both engines appear to decrease

uniformly as NOx emissions are lowered

For the current TCCS systems most of the fuel economy penalty

associated with emissions control can be ascribed to control

of NOx emissions although several of the measures used for

NOx control (retarded cornbusticn timing and increased exhaust

back pressure) also help to reduce HG emissions HC and CO

emissions ari effectively controlled with oxidation catalysts

resulting in relatively minor reductions in engine efficiency

233 TCCS Fuel Reauirements

The TCCS engine is unique among current stratified charge

systems in its multifuel capability Successful operation

with a nuraber of fuels ranging from gasoline to No 2 diesel

Table 2-I

Emissions and Fuel Economy of Turbocharged TCCS Engine-Powered Vehicle 1

Fuel

Emissions gMile 2 Fuel Economy

mng 2HC co NOx

Gasoline

JP-4

100-600

No 2 Diesel

033

026

014

027

104

109

072

J bull l ~

-

061

050

059

060

197

202

213

230

1M-151 vehicle 8 degrees coffibustion retard 16 light load EGR tw0 catalysts (Ref 10)

2 CVS-CH 2750 pounds tnert1a welght

165

l

has been demonstrated Table ~-I lists emissions levels and

fuel economies obtained with a turbocharged TCCS-powered

M-151 vehicle when operated on each of four different fuels 10

These fuels encompass wide ranges in gravity volatjlity

octane number and cetane leve 1 as middotshown in Table 2-II

Table 2-II

Fuel Specifications for TCCS Emissions Tests (Reference 10)

Gravity 0 API Sulfur

OFDistillation~

Gasolj_ne 100-600 JP-4 No 2

Diesel

88 -

86 124 233 342 388

0024 912

-

486 012

110 170 358 544 615

0002 57 356

541 0020

136 230 314 459 505

-middot --

369 0065

390 435 508 562 594

--

lta 9

IBP 10 50 90 EP

TEL gGal Research Octane Cetane No

Generally the emissions levels were little affected by the

wide variations in fuel properties Vehicle fuel economy

varied in proportion to fuel energy content

As stated above the TCCS engine is unique in its multifuel

capability The results of Tables 2-I and 2-II demonshy

strate that the engine has neither 8ign1ficant fuel octane

nor cetane requirements and further that it can tolerate

166

wide variations j_n fuel volati1tty rhe flexibility offered

by this type of system could be of major importance in

future years

234 Durability Performance Production Readiness

Emissions control system durability has been demonstrated by

mileage accumulation tests Ignltion system service is more

severe than for conventional engines due to heterogeneity of

the fuel-air mixture and also to the high compression ratios

involved The ignition system has been the subject of

intensive development and significant progress in system

reliability has been made

A preproduction prototype engine employing the TCCS process is

now being developed by the Hercules Division of White Motors

Corporation under contract to the US Army Tank Automotive

Command Southwest Research Inr)titute will conduct reliability

tests on the White-developed enGines when installed in Military

vehlcles

30 Small Volume Prechambcr Eng1nes (3-Valve Prechamber Engines Jet Ignition Engines Torch Ignition Engines)

31 General

A number of designs achieve charge stratification through

division of the combustion region into two adjacent chambers

The emissions reduction potentiampl for two types of dualshy

chamber engines has been demonstrated F1 rst ~ j n B desJgn

trad1t1on~JJy caJJld the nrreebrnber engine a 2m211 auxil1ary

167

or ignition chamber equipped w1th a spark plug communicates

with the much larger main combustion chamber located in the

space above the piston (Figure 3-1) The prechamber which

typically contains 5-15 of the total combustion volume

is supplied with a small quantity of fuel-rich ignitable

fuel-air mixture while a large quantity of very lean and

normally unignitable mixture is applied to the main chamber

above the piston Expansion of high temperature flame

products from the prechamber leads to ignition and burning

of the lean maj_n chamber fuel-a_r charge Ignitionmiddot and

combustion in the lean main chamber region are promoted both

by the high temperatures of prechamber gases and bythe

mixing that accompanies the jet-like motion of prechamber

products into the main chamber

I jl

I i j

I

Operation with lean overall mixtures tends to limit peak comshy

bustion temperatures thus minimizing the formation of nitric

oxide Further lean mixture combustion products contain

sufficient oxygen for complete oxidation of HC and CO in the

engine cylinder and exhaust system

It should be reemphasized here that a iraditional problem

with lean mixture engines has been low exhaust temperatures

which tend to quench HC oxidation reactions leading to

excessive emissions

Control of HC emissions to low levels requires a retarded or

slowly developing combustion process The consequent extenshy

sion of heat release j nto 1ate porttt)ns of the engtne cycle

168

tends to raise exhaust gas temperatures thus promoting

complete oxidation of hydrocarbons and carbon monoxide

32 Historical Background and Current Status

321 Early Developm9nt Objectives and Engine Def igns

The prechamber stratified charge engine has existed in various

forms for many years Early work by Ricardo 1 indicated that

the engine could perform very efficiently within a limited

range of carefully controlled operating conditions Both

fuel-injected and carbureted prechambcr engines have been

built A fuel-injected design Lnittally conceived by

Brodersen 11 was the subject of extensive study at the

University of Rochester for nearly a decade 12 13 Unforshy

tunately the University of Rochester work was undertaken prior

to widespread recognition of the automobile emissions problem

and as a consequence emission characteristics of the

Brodersen engine were not determined Another prechamber

engine receiving attention in the early 1960s is that conshy

ceived by R M Heintz 14 bull The objectives of this design

were reduced HC emissions incr0ased fuel economy and more

flexible fuel requirements

Experiments with a prechamber engine design called the torch

ignition enginen were reported n the USSR by Nilov 15

and later by Kerimov and Mekhtier 16 This designation

refers to the torchlike jet of hot comhust1on gases issuing

169

from the precombustion chamber upon j_gnj_ tion In a recent

publication 17 Varshaoski et al have presented emissions

data obtained with a torch ignition engine These data show

significant pollutant reductions relative to conventional

engines however their interpretation in terms of requireshy

ments based on the Federal emissions test procedure is not

clear

l

3 2 2 Current DeveloJ)ments

A carbureted middotthree-valve prechamber engine the Honda CVCC

system has received considerable recent attention as a

potential low emissions power plant 18 This system is

illustrated in Figure 3-2 Hondas current design employs a

conventional engine block and piston assembly Only_ the

cylinder head and fuel inlet system differ from current

automotive practice Each cylinder is equipped with a small

precombustion chamber communicating by means of an orifice

with the main combustion chambe situated above the piston lj

ij_ A small inlet valve is located in each precharnber Larger

inlet and exhaust valves typical of conventlonal automotive

practice are located in the main combustion chamber Proper

proportioning of fuel-air mixture between prechamber and

main chamber is achieved by a combination of throttle conshy

trol and appropriate inlet valve timing A relatively slow

and uniform burning process gjvjng rise to elevated combusshy

tion temperatures late in the expansion stroke and during

the exhaust procezs is achieved H1 gh tewperaturr--s in thin

part of the engine cycle ar-e necessary to promote complete

170

oxidation of HC and CO It si1ould be no~ed that these

elevated exhaust temperatures are necessarily obtained at

the expense of a fuel economy penalty

To reduce HC and CO emissions to required levels it has been

necessary for Honda to employ specially designed inlet and

exhaust systems Supply of extremely rich fuel-air mixtures

to the precombustion chambers requires extensive inlet manifold

heating to provide adequate fuel vaporization This is accomshy

plished with a heat exchange system between inlet and exhaust

streams

To promote maximum oxidation of HC and CO in the lean mixture

CVCC engine exhaust gases it has been necessary to conserve

as much exhaust heat as possible and also to increase exhaust

manifold residence time This has been done by using a relashy

tively large exhaust manifold fitted with an internal heat

shield or liner to minimize heat losses In additj_on the

exhaust ports are equipped with thin metallic liners to

minimize loss of heat from exhaust gases to the cylinder

head casting

Engines similar in concept to the Honda CVCC system are under

development by other companies including Ttyota and Nissan

in Japan and General Motors and Fo~d in the United States

Honda presently markets a CVCC-powered vehicle tn tTapan and

plans US introduction in 1975 Othe~ manufactur~rs

includlnr General Motors and Forgtd 1n thr U S havf~ stated

171

that CVCC-type engines could be manufactured for use in limited

numbers of vehicles by as early as 1977 or 1978

33 Emissions and Fuel Economywith CVCC-Type Engines

331 Recent Emissions Test Results

Results of emissions tests with the Honda engine have been very

promising The emissions levels shown in Table 3-I are typical

and demonstate that the Honda engine can meet statutory 1975-1976

HC and CO stindards and can approach the statutory 1976 NOx

standard 19 Of particular importance durability of this

system appears excellent as evidenced by the high mileage

emissions levels reported in Table 3-I Any deterioration of

l emissions after 50000 miles of engine operation was slight

and apparently insignificant

I Table 3-I

Honda Compound Vortex-Controlled Combustion-Powered Vehicle 1 Emissions

Fuel Economy

Emissions 2 mpg gMile 1972

HC 1975 FTP FTPco NOv

210 50000-Mile Car+ No 2034 Low Mileage Car 3 No 3652 018 212 221089

024 065 198 1976 Standards

213175 20o41 34 - -04o411977 Standards 34 - -

1Honda Civic vehicles 2 1975 CVS C-H procedure with 2000-lb inertia weight3Average of five tests aAverage of four tests

172

Recently the EPA has tested a larger vehicle conve~ted to the

Honda system 20 This vehicle a 1973 Chevrolet Impala with

a 350-CID V-8 engine was equipped with cylinder heads and

induction system built by Honda The vehicle met the present

1976 interim Federal emissions standards though NOx levels

were substantially higher than for the much lighter weight

Honda Civic vehicles

Results of development tests conducted by General Motors are

shown in Table 3-II 21 These tests involved a 5000-pound

Chevrolet Impala with stratified charge engine conversion

HC and CO emissions were below 1977 statutory limits while

NOx emissions ranged from 15 to 2 gmile Average CVS-CH

fuel ec9nomy was 112 miles per gallon

Table 3-II

Emissions and Fuel Economy for Chevrolet Impala Strmiddotatified

Charge Engine Conversion (Ref 21)

Test

Exhaust Emlssions

gMile 1 Fuel

Economy mpgHC co NOx

1 2 3 4 5

Average

020 026 020 029 0 18

023

25 29 31 32 28

29

17 15 19 1 6 19

17

108 117 114 109 111

112

1cvs-CH 5000-lb inertia weight

173

I

332 HC Control Has a Significant Impact on Fuel Economy

In Figure 3-3 fuel economy data for several levels of hydroshy

carbon emissions from QVCC-type stratified charge engines

are plotted 22 23 ~ 24 At the 1 gmile HC level stratified

charge engine fuel economy appears better than the average

fuel economy for 1973-74 production vehicles of equivalent

weight Reduction of HC emissions below the 1-gram level

necessitates lowered compression ratios andor retarded

ignition timing with a consequent loss of efficiencymiddot For

the light-weight (2000-pound) vehicles the O~ gmile IIC

emissions standard can be met with a fuel economy of 25 mpg

a level approximately equal to the average of 1973 producshy

tion vehicles in this weight class 8 For heavier cars the

HC emissions versus fuel economy trade-off appears less

favorable A fuel economy penalty of 10 relative to 1974

production vehicles in the 2750-pound weight class is

required to meet the statutory 04 gmile HC level

333 Effect of NOx Emissions Control on Fuel Economy

Data showing the effect of NOx emissions control appear in

Figure 3-~ 22 These data are based on modifications of a Honda

CVCC-powered Civic vehicle (2000-pound test weight) to meet

increasingly stringent NOx standards ranging from 12 gmile

to as low as 03 gmile For all tests HC and CO emissions

are within the statutory 1977 standards

NOx control as shown in Figure 3-4 has been effected by use

of exhaust gas recirculation 1n comb1nation w1th retarded

174

ignj_tion timing It is clear that control of rmx emissions

to levels below l to 1 5 gmile results in stgnificant fuel

economy penalties The penalty increases uniformly as NOx

emissions are reduced ~nd appears to be 25 or more as the

04 gmile NOx level is approached

It should be emphasized that the data of Fisure 3-4 apply

specifically to a 2000-pound vehicle With increased vehicle

weight NOx emissions control becomes more difficult and the

fuel economy penalty more severe The effect of vehicle

weight on NOx emissions is apparent when comparing the data

of Table 3-I for 2000-pound vehicles with that of Table 3-II

for a 5000-pound vehicle While HC and CO emissio~s for the

two vehicles are roughly comparable there is over a factor

of two difference in average NOx emissions

34 Fuel Requirements

To meet present and future US emissions control standards

compression ratio and maximum ignltion advance are limited

by HC emissions control rather than by the octane quality of

existing gasolines CVCC engines tuned to meet 1975 California

emissions standards appear to be easily satisfied with

presently available 91 RON commercial unleaded gasolines

CVCC engines are lead tolerant and have completed emissions

certification test programs using leaded gasolines However

with the low octane requirement of the CVCC engine as noted

above the economic benefits of lead antlknock compoundt ar-euromiddot

not realized

175

It is possible that fuel volatLLity characteristlcs may be of

importance in relation to vaporization within the high

temperature fuel-rich regions of the prechamber cup inlet

port and prechamber iQlet manifold However experimental

data on this question aomiddot not appear to be available at

present

~O Divided-Chamber Staged Combustion Engines (Large-Volume Prechamber Engines Fuel-Injected Blind Prechamber Engines)

41 General

Dual-chamber engines of a type often called divided-chamber

or large-volume prechamber engines employ a two-stage comshy

bustion process Here initial r~ich mixture combustion and

heat release (first stage of combustion) are followed by rapid

dilution of combustion products with relatively low temperature

air (second stage of combustion) The object of this engine

design is to effect the transitjon from overall rich combustion

products to overall lean products with sufficient speed that

time is not available for formation of significant quantities

of NO During the second low temperature lean stage of

combustion oxidation of HC and CO goes to completion

An experimental divided-chamber engine design that has been

built and tested is represented schematically in Figure ~-1 25 26

A dividing orifice (3) separates the primary combustion

chamber (1) from the secondary combustion chamber (2) which

includes the cylinder volume above the piston top A fuel

injector (4) supplies fuel to the primary chamber only

176

Injection timing is arranged such that fuel continuously

mixes with air entering the primary chamber during the

compression stroke At the end of compression as the

piston nears its top center position the primary chamber

contains an ignitable fuel-air mixture while the secondary

chamber adjacent to the piston top contains only air

Following ignition of the primary chamber mixture by a spark

plug (6) located near the dividing orifice high temperature

rich mixture combustion products expand rapidly into and mix

with the relatively cool air contained in the secondary

chamber The resulting dilution of combustion products with

attendant temperature reduction rapidly suppresses formation

of NO At the same time the presence of excess air in the

secondary chamber tends to promote complete oxidation of HC

and CO

42 Exhaust Emissions and Fuel Economy

Results of limited research conducted both by university and

industrial laboratories indicat~ that NOx reductions of as

much as 80-95 relative to conventional engines are possible

with the divided-chamber staged combustion process Typical

experimentally determined NOx emissions levels are presented

in Figure 4-2 27 Here NOx emissions for two different

divided-chamber configurations 8re compared with typical

emissions levels for conventional uncontrolled automobile

engines The volume ratio 8 appearing as a parameter in

Figure 4-2 represents the fraction of total combustion volume

contained in the primary chamber For a values approaching

I

i J_

177

1

05 or lower NOx emissions reach extremely low levels Howshy

ever maximum power output capability for a given engine size

decreases with decreasing 6 values Optimum primary chamber

volume must ultimately_represent a compromise between low

emissions levels and desired maximum power output

HC and particularly CO emissions from the divided-chamber

engine are substantially lower than eonventional engine

levels However further detailed work with combustion

chamber geometries and fuel injection systems will be necesshy

sary to fully evaluate the potential for reduction of these

emissions

i Recent tests by Ford Motor Company show that the large volume

prechamber engine may be capable of better HC emissions conshy

trol and fuel economy than their PROCO engine This is shown

by the laboratory engine test comparison of Table 4-I 19

Table 4-I

Single-Cylinder Low Emissions middot11 ~ _____En____g__~ne __middot _e_s_-_s_____

Engine

NO--X Reduction

Method

Em1ssions g1 hp-Hr

Fuel Economy

Lb1 hp-HrNOv HC- co

PROCO

Divided Chamber

PROCO

Divided Chamber

EGR

None

EGR

None

10 30

10 04

05 ~o

o J_o 75

130

25

l 1i bull 0

33

0377

0378

0383

0377

178

Fuel injection spray characteristics are critical to control

of HC emissions from this type of engine and Fords success

in this regard is probably due in part to use of the already

highly developed PROCO-gasoline injection system Figure 4-3

is a cutaway view of Fords adaptation of a 400-CID V-8 engine

to the divided-chamber system 2 e

Volkswagen (VW) has recently published results of a program

aimed at development of a large volume precharnber engine 29

In the Volkswagen adaptation the primary chamber which comshy

prises about 30 of the total clearance volume is fueled by a

direct timed injection system and auxiliary fuel for high

power output conditions is supplied to the cylinder region by

a carburetor

Table 4-II presents emissions data for both air-cooled and

water-cooled versions of VW s dtvided-middotchamber engine 3 0

Emissions levels while quite low do not meet the ultimate

1978 statutory US standards

179

Table 4-II

Volkswagen Jarge Volume _Jrechamber Er[ Lne Emissions

Exhaust Emissions

_ _gMile 1

___E_n_gi_n_e__t--H_C___c_o__N_O_x____E_ng__i_n_e_S_p_e_c_i_f_i_c_a_tmiddot_1_middoto_n_s__

20 50 09 841 compression ratio Air-Cooled 16-Liter

prechamber volume 28 of total clearance volume conventional exhaust manishyfold direct prechamber fuel injection

20-Liter 10 40 10 91 compression ratio Water-Cooled prechamber volume 28 of

total clearance volume simple exhaust manifold reactor direct prechamber fuel injection

1cvs c-H

Toyota also has experimented wlth ___a large volume prechamber

engine using direct prechamber fuel injection and has

reported emissions levels comparable to those of Table 4-II 31

43 Problem Areas

A number of major problems inherent in the large volume

prechamber engine remain to be 3olved I~ These problems include the following II

Fuel injection spray characteristics are critically

important to achieving acceptable HC emissions

The feasibility of producing asatisfactory injecshy

tion system hasnot been estab1ished

180

Combustion noise due to high turbulence levels and

hence high rates of heat release and pres[-ure rise

in the prechamber can be excessive It has been

shown that the-noise level can be modified through

careful chamber design and combustion event timing

If the engine is operated with prechamber fuel

injection as the sole fuel source maximum engine

power output is limited This might be overcome

by a~xiliary carburetion of the air inlet for maximum

power demand or possibly by turbocharging Either

approach adds to system complexity

The engine is charmiddotaeter1zed by low exhaust temperatures

typical of most lean mixture engines

References

1 Ricardo H R Recent Research Work on the Internal Combustion Engine 11 SAE Journal Vol 10 p 305-336 (1922)

2 Bishop I N and Simko A Society of Automotive Engineers Paper 680041 (1968)

3 Simko A Choma M A and Repco L L Society of Automotive Engineers Paper 720052 (1972)

4 Mitchell E Cobb JM and Frost R A Society of Automotive Engineers Paper 680042 (1968)

5 Mitchell E Alperstein M and Cobb JM Society of Automotive Engineers Paper 720051 (1972)

6 1975-77 Emission Control Program Status Report submitted to EPA by Ford Motor Company November 26 1973

181

if

7 consultant Report on Emissions Control of Engine Systems National Academy of Sciences Committee on Motor Vehicle Emissions Washington DC September 1974

8 Austin T C and Hellman K H Society of Automotive Engineers Paper 730790 (1973)

9 See Ref 7

10 Alperstein M Schafer G H and Villforth F J Iiil SAE Paper 740563 (1974)

11 US Patent No 2615437 and No 2690741 Method of Operating Internal Combustion Engines Neil O Broderson Rochester New York

12 Conta L~ D and Pandeli American Society of Mechanical Engineers Paper 59-SA-25 (1959)

13 Canta L D and Pandeli American Society of Mechanical Engineers Paper 60-WA-314 (1960)

14 US Patent No 2884913 0 Internal Combustion Engine R Mi Heintz i

15 Nilov N A Automobilnaya Promyshlennost No 8 (1958)

l 16 Kerimov N A and Metehtiev R I Automobilnoya Promyshlennost No 1 p8-11 (1967)

17 Varshaoski I L Konev B F and Klatskin V B Automobilnaya Promyshlennost No 4 (1970)

18 An Evaluation of Three Honda Compound Vortex Controlled Combustion (CVCC) Powered Vehicles Report B-11 issued by Test and Evaluation Branch Environmental Protection Agency December 1972

19 Automotive Spark Ignition Engine Emission Control Systems to Meet Requirements of the 1970 Clean Air Amendments report of the Emissions Control Systems Panel to the Committee on Motor Vehicle Emissions National Academy of Sciences May 1973

20 An Evaluation of a 300-CID Compound Vortex Controlled Combustion (CVCC) Powered Chevrolet Impala Report 74-13 DWP issued by Test and Evaluation Branch Environmental Protection Agency October 1973

21 See Ref 7

22 See Ref 7

23 See Ref 7

24 See Ref 7

182

25 Newhall H K and El-Messiri I A Combustion and Flame 14 p 155-158 (1970)

26 Newhall H K and El-Messiri I A Society of Automotive Engineers Transaction Ford 78 Paper 700491 (1970)

27 El-Messiri I A and Newhall H K Proc Intersociety Energy Conversion Engineering Conference p 63 (1971)

28 See Ref 7

29 Decker G and Brandstetter W MTZ Motortechnische Zeitschrift Vol 34 No 10 p 317-322 (1973)

30 See Ref 7

31 See Ref 7

183

Fig 2-1 FORD PROCO ENGINE

l

Ford Proco Engine Fuel Economy and Emissions _ 15 _ f--1

00 +

I ~ x X gt( X _ x A 7- ~ X x~ ~c - l4catalyst Feed u NOx vs ruel Econ with 1 C0-71 CJ) 14 x x Ynn H( RP c tr ir-t irm vltgtZ G I HC - C0-127 _ A txcessve c

13 Approx W EG R

~ C~~r 351 CID 5000 Lb Inertia Weight

Q 21 A L 0 u w II _j

LJ =gt LL

10

35i CD 4500 Lb Inertia Weight

~ 1974 Production Average Fuel Economy

4 soo _b r-r-r-----z~lt_~~---7--_~--r--1r-7-r1--~-rz7-w~~

150 0 0 Lb PU221ufrac122-1 I

LO 20 30

NOx EMISSIONS-GMSMILE (CVS-CH) Revised216174

0

HKN 71074

Fig 2-2

l

~___-~ ~--=---~ ~=---__---~1 f-=-----1__middot-_~J ~-----------1 ~bull-=-=- (-~-~ LJii-ZJj ~ ~~-~ ~~ -__c~~ 1--~~ ~----~--1 ---------s___-c--1 ~~~-~~~bull r~~-~--middot1 ____c__ J~ p- ~

Texaco TCCS Engine

Shrouded Intake Valve

~ Intakemiddot r~ )p__-- Fuel Nozzle Fuel Nozzte Port ~ -- -yen -_~

X f -J J ( ~1 I --- ~ f middotmiddotj_Ja 1(~-~_ frff 1-Cylinderv~ v_ r--L~ I (~~)J ~- Intake 1 - ------L- middotmiddot - middotmiddot -1 H0 ad middot --- - -- 1 Po rt I 1 I ~~ ) ~ ~ ~~~ -A- I ------

- I _ ---_ ~ P1ston-mgt-lt_ffrac12 T_77~~~--1 i- r_-~J N

- ~- i~-L - _ _ - IExhaust - - I ~ - 1-_ r- bullsect ~ ----lt_ ~ I PortJ~bJ lt 7A--7~ ~1 ~j --~ ~ yl ind er

-__~lli- klmiddot ~ro v_t_gt11J1bull Bti Or K__ - middot ~

I t--tL pgt-- Ultmiddot middot- - Spark Plugr- -1 --U2middot- ~-~

LHorizont al Projections of Nozzle and Spark Plug Centerlines

Fig 2-3 i--1 00 U1

---~---~-~ -------c- --~--- 7middot-r---c-- ~- -~~~==---~~~~~- srsr RZIIEF7 11t111-~-----==-----=-~--~-~~---c=rmiddot=

OPEN CHAMBER TYPE STRATI Fl ED CHARGE ENGINE i-shyCj

DIRECTIONAl~Fsw7 Q

NOZZLE P

I

~J~treg lt-_(__(lt-(11

c_-- _7- -

SPARK PLUG_ l 1__- -_ - l --_ ~ ----__ lt_ lt_ -- --

ltlt_I_--- _

~ gt - _____- -- --~ ~-l_- 1_~ -~- ~ ------

~~~ r_I FUEL SPRAY 2 FUEL-AIR MIXING ZONE ~- _ -------

FLAME FRONT AREA 4 COMBUSTION PRODUCTS

TCCS COMBUSTION SYSTEM

Fig 2-4

3

----==-----~ l~~----bulli r-~ ~-----=-- 1 ~~ ~ -~ ~~ ___-_=gt---l p--- --=-=-_-__71-~-~~ 1-0-- --=---=-- 4 L--_-_-~ P--- ~

25

-c u

f

Cl) 24 gt u _

tgt 23a ~

I

gt-~ 220 2 0 u w 21 _J

lJJ gt LL

2

Texaco TCCS Powered Cricket Vehicle

Max Econ Setting gt A L07 HC

141 CID JQf CR 084 CO 2500 Lb Inertia Wgt

50-so Retard_ 0_73 HC

12 co 051 HC ~ 061 HC

085COA 064CO Retard+ ESPRetard+

EGR

036 HC ~ 115 co Retard +ESP+ EGR

04 06 08 10 12 14 16 18 20 NOx EMISSIONS-GMSMILE (CVS-CH) HtltN1110114

I- 00 -JFig 2-5

-~ ~=- ~ - -i______c_J ~-====c= wr=- ~-~ p--w~~~ rr w -

25

-c u

I

(f)

gt u-lt a_

2

gt-I 20

~ 0 z 0 u LLI

_J

w tJ_

15

I- CJ) CJ)

Turbocharged Texaco TCCS Ml51 Vehicle

Max Econ Adjustment_ HC-3J catalyst Feed C0-70

141 CID 10~1 CR 2750 Inertia Weight 8deg Retard ~

~bull HC-3middot2 catalyst Feed ~~ _ C0-64

_ 5deg Retard HC-0 30 8degRetard LowEGV bullco-11 ~bull HC-3middot6 catalyst Feed WIW21

Med EGR C0-67 1974 Production 33 Average Fuel Economy ~

COmiddoti05 (2750Lb)

I

bull HC-035 co- 141 13deg Retard High EGR

04 10 20 NOx EMISSIONS -GMSMILE (CVS-CH) ~~ts~b~~~74

Fig 2-6

189

Fig 3-1

PRECHAMBER TYPE STRATIFIED CHARGE ENGINE

r Inlet

(Fuel-lean Mixture )

I 0 I

Spark -Prechamber (Fuel-rich mixture)

-Main Chamber

1] HON DA CVCC ENGINE CONCEPT

190

Fig 3-2 Honda CVCC Engine

28 -l u

1

UJ 26 -gt u-(9 CL 24 2-

f

gtshy0gt

22 z ~ _)

u w

20 _J

w ~ LL

18

J= ---- 4 --~~-_----a ~~ _-_bull --~~ 1~~1 ltiil~I ~ ~-r~ ~ -~ ~-~ ~J~-iii-1 ~~1 s _-_ __-

Fuel Economy vs HC Emissions for 3-Valve Prechamber Engines

e NOx-14 15 Liter

bull Honda CVCC 2000 LbsNOx - 12 A Datsun NVCCbull15 Liter

bull ~JOx -09 A 2500 Lbs J LL 1ter NOv -15

2750 Lbs -NOx -17

- I AiJOx -12

0 02 04 06 08 LO 0HYDROCARBON EMiSSlmiddotONS - Glv1 I MILE (CVS-CH) I-

Fig 3-3

J--1

1--Fuel Economy vs NOx Emissions IO N

-- for Honda CVCC Powered Vehiclesr 26 u

l VHc-023 U1 gt umiddot 24_-__

(_IJ o_

~ 22 l

gt-5~-0 z 20 C0-200 u A HC-033w I co -3o_j

_A HC-029w 18 J I C0-27 LL

_ HC-025

HC-017 co -2-3

C0-22

0 -- 02 04 06middot 08 10 12 NOx Ef11SSIONS -GlviS MILE (CVS-CH)

Fig 3-4 middot

I

I

i93

J J

Fig 4-1 Divided Chamber Engine

middot(4) Fuel Injector

1

f J

f ff

f

~ Ii

I f

i

I f ] [

~~

0 0 0 0

i ~ I

1jl

194

E Cl 0

C QJ

CJl 0 _

-1-

z

0

Vl (lJ

-0

X 0

-t-J

V1 ro c X

LLI

Fig ~-2

COMPARISON OF CONVENTIONAL AND DIVIDED COMBUSTION CHAMBER NOx EMISSIONS

5000 MBT Ignition Timing Wide Open Ttl rattle

4000 Conventional Charnber

3000

J = fraction of Total Combustion 2000 Volume in Primary Ct1arnber

Divided Chamber 13 = 0 85

1000

Divided Chamber fo = 0 52

05 06 0 7 08 09 10 11

O~erall Fuel-Air Equivalence Ratio

195

196

AIRBORNE SURVEYS IN URBAN AIR BASINS IMPLICATIONS FOR MODEL DEVELOPMENT

by

Donald L Blumenthal Manager of Program Development

Meteorology Research Inc Altadena California 91001

middotI would like to make several points today First ozonemiddotis basically

a regional long-range problem There is a lot of long range ozone transshy

port and this transport is a normal occurrence The second point is that

ozone is stable in the absence of scavengers Junge mentions in his book

that the residence time of ozone in the troposphere is on the order of a

month Third vertical variations in concentration and ventilation rate are i very important in modeling atmospheres such as Los Angeles Layers aloft

are ventilated down to the surface on occasion and surface pollutants are

ventilated up mountain slopes as Jim Edinger has pointed out before and

often ventilated out of the basin in upper winds Fourth the day to day

carry over of pollutants from one day to the next is a very important considshy

eration in the Los Angeles Basin Finally there is a definite background

level of ozone The geophysical literature says its about O 02 to O 03 ppm (

in various parts of the world Weve seen data varying from 003 to 005 ppm

The difference may be due to calibration differences In any case numbers

like 005 are pretty substantial background levels for ozone

I am going to illustrate the points listed above with some data from

Los Angeles Basin The data were collected during a two-year study funded

by the Air Resources Board some of the analyses were funded by EPA The

study examined the three dimensional distribution of pollutants in the Los

Angeles Basin using airborne sampling systems Coinvestigators on the

project were Dr Ted Smith and Warren White of Meteorology Research Inc (MRI)

197

The first slide shows one of the aircraft we used Its a Cessna 205

which had sampling inlets on the side of the aircraft Figure 2 shows the

instrument system on the inside of the aircraft We were measuring nitrogen

oxides ozone scattering coefficient with a nephelometer condensation nuclei

carbon monoxide and meteorological parameters such as temperature humidity

turbulance Altitude and position were also measured

Figure 4 shows that the typical sampling pattern was a series of spirals

from the top of the mixing layer over an airport virtually to ground level

then we would climb up to the next point on the route and spiral down again

We had three routes (A B C Figure 3) that we would fly We had two airshy

craft and we would fly two of these three routes three times a day any

given day that we could The day I will be talking about September 25~ 1973

we flew what was called the Riverside route (C) and the Los Angeles route

(A) The 25th of July 1973 you might remember was the day before the

federal office buildings were closed in the area here because of smog

Figure 5 shows the surface streamlines at 0300 Pacific Standard Time

about 4 oclock in the morning daylight time on July 25 This streamline

analysis points out the morning stagnation conditions which are a very normal

occurrence in the Los Angeles Basin You start out with very light winds

quite variable maybe a slight off shore flow early in the morning On this

particular day this kind of situation extended well into midday The sea

breeze did not really pick up until up around noon When you have this kind

of a situation and a low radiation inversion at night you have a

long period of accumulation of pollutants all over the Basin espt~cialJy

in the prime source area the southwest portion of the Basin

198

I

Figure 6 shows the streamline pattern at 1600--400 cclock in the

afternoon same day sea breezes develop and with them a transport pattern

that carries pollutants up to the northeast and out toward the eastern por-

tion of the Basin This is a very regular pattern which we see day after l middot

day On July 25 1973 it was a little bit exaggerated The sea breeze was

held off for awhile started a bit late and so there was a very long period

of accumulation in the southwest area and then transport across the Basin

Figure 7 is an average streamline pattern at 1600 PacHic Daylight Time

on low inversion days for August 1970 It is included to show that the pattern

shown before is very typical Flow starts in the western portion of the

Basin and goes right across to the eastern portion This is using surface

data There is a very high average wind velocity in Ontario about 13 m iles

per hour and 23 mph in Riverside This is the average for the whole month

of August at 1600 PDT on low inversion days There is a considerable amount

of transport across the Basin starting relatively slowly in the morning and

accelerating in the afternoon

Figure 8 shows a verticle cross section of the scattering coefficient

The darker areas indicate higher levels of particulates Scattering coefficshy

ient is inversely proportional to visibility In the crosshatched area

visibility is less than about 3 miles In plotting altitude versus distance

inland from the coast you have Santa Monica (SMO) on the coast El Monte (EMT)

Pomona (BRA) Rialto (RIA) Redlands (RED) The lower broken line is surface

ground level The heavy dashed line is the base of the subsidence inversion

that occurred on the two days during this episode The middle line is the

base of the marine inversion There is a large area over in the western

portion of the Basin where emissions accumulate for much of the day At

199

midday the sea breeze has just started ventilating the Santa Monica area

The layer between the inversions is a layer aloft which is fairly well separshy

ated from the surface layer Ozone concentrations for instance in the

layer aloft were on the order of 04 05 ppm using the ARB calibration

method Down in the surface layer they were quite a bit lower in the mornshy

ing due to scavenging

Figure 9 shows that by afternoon the sea breeze starts and you get

kind of a clean air front Sea breeze starts ventilating the whole Basin

the stuff that was over in the west is transported eastward and at approxishy

mately Brackett (BRA) at 1700 PDT there is a clean air front The high conshy

centrations that were over Los Angeles earlier are now centered near Upland

(CAB) The numbers shown over CAB are data taken from a vertical profile

spiral over Upland at about 1600 That turns out to be the time when there

was the worst ozone concentration of the day in the Basin and it did occur

at Upland It could well be a result of the very polluted mass from the

western Basin being transported over the Upland area The layer aloft has

been a bit undercut by the sea breeze and some of the polluted mass has been

around possibly as long as the night before There has been very little

transport in the area aloft ozone concentrations are still very high

Figure 10 shows a trajectory analysis of the air arriving at Upland at

1600 since that was the worst time of the day at Upland We developed a

trajectory envelope using surface wind data and winds aloft so the air

arriving at Upland at 1600 started out somewhere back within this envelope

for example at 1130 PDT We did not go earlier than 1130 because the winds

were pretty much light and variable before that The air that arrives at

Upland at 1600 has been over the western portion of the Basin for much of

200

the morning and q~ite a bit of the evening before Thus there is

a very long period of accumulation and then a transport a pulsing effect

where you have pollutants moved across the Basin

Figure 11 is an isopleth map of surface ozone concentrations Again all

data are corrected to agree with the ARB calibration method Again you can

see that for the hours between 1600 and 1700 using surface data the Upland

area has the highest surface ozone concentrations about 063 ppm The western

area has been well ventilated by the sea breezes and it is cleaned out

The transport is actually pretty much perpendicular to the isopleth line

just about like that

Figure 12 is a vertical profile taken over Upland Cable Airportat

roughly the time of maximum ozone concentration 1636 PDT We are plotting

pollutant concentration on the x-axis versus altitude in meters (since it was

done for an EPA report) Surface leveJ at Upland is a little over 400 meters

the Z line is ozone Ozone concentration within the surface mixing layer

is pegged on the instrument at somewhat above 05 ppm Above the surface

mixing layer it drops off considerably and eventually get down to background

The T line is temperature and you ean see the subsidence inversion

on this day is very nicely documented here and provides a very strong trap

in that area The B line is the scattering coefficient inversely proporshy

tional to visibility Within the surface mixing layer visibility is on the

order of 3 miles or less while up above the surface mixing layer just a few

hundred feet difference visibilities get up to 60 or 80 miles The X is

condensation nuclei the measure of the very fine particles below about 010

micron It is a measure of quite fresh emissions If you have a high condenshy

sation nuclei count there are very fresh combustion emissions If you have

I

201

an aged air mass the condensation nuclei coagulate and the count decreases

considerably You can see that there are still some fresh emissions within

this surface layer as well But up above the surface mixing layer all the

pollutant indicators decrease considerably

Figure 13 is the same type of vertical profile taken over El Monte

which is on the western side of the sea breeze front The sea breeze front

has passed El Monte at this time almost 1700 PDT and again there are

distinct differences between the mass below the mixing layer within the sea

breeze front (below 400 meters) the marine inversion (400 to 800 meters) and

the subsidence inversion The subsidence inversion occurs at about 800 meters

and there is an old layer of very polluted stuff aloft The surface concenshy

trations are lower because of the ventilation by the sea breeze Condensashy

tion nuclei count (X line) within the surface layer is quite high There

are still fresh emissions in the El Monte area The 11 Z line is ozone

about 02 ppm within the surface layer (200 m) but it is 05 ppm up above

the surface mixing layer The scattering coefficient (B line) is very

similar it is lower at the surface and increases to a visibility equivalent

of less than 3 miles above the surface mixing layer The condensation nuclei

count is high in the lower portion of this (eg at 600 m) hut decreases conshy

siderably above This portion of the upper layer (600 m) has been around

at least all morning and condensation nuclei have been scattered from the

area The portion of the upper layer below 600 m has probably just recently

been undercut by the sea breeze and there are still some condensation nuclei

left in it

Figure 14 illustrates a different method of looking at the flushing

problems in the Basin We have tried to develop an objective criteria based

on ground level ozone to show the cleansing of the basin using the time of

202

arrival of clean air We determine the time when the ozone concentrations

drop by a factor of two at any given point The 1600 line means that between

1500 and 1700 the ozone concentration at that point dropped a factor of two

This sort of isopleth chart of when the clean air arrives agrees quite well

with the trajectory analyses although the numbers are a little bit behind

the trajectory analyses for the polluted air Figure 14 again shows the

transport process that takes place across the Basin which is ventilated from

west to east At 1900 some of the fresh ocean air finally gets out to

Redlands

In Figure 15 in order to put this whole flux problem into some perspecshy

tive we looked at the numbers the actual amount of ozone flux across the

basin We calculated the mean trajectory from Torrance towards Redlands

using the surface and upper air data We looked at the flux from the western

basin to the eastern basin basically from Los Angeles and Orange Counties to

Riverside and San Bernardino Counties This is a calculation made at 1700 PDT

We used the winds aloft from Chino as well as the vertical profiles taken at

Pomona and Corona Averaging the ozone concentration throughout the mixing

layer and multiplying by an average wind speed we arrive at a number of 185

metric tons per hour being transported directly from one side of the Basin

to the other If you look at this in terms of actual concentration in the

eastern Basin and assume that the flow was constant for about an hour it

is eno_ugh to fill up the box shown in Figure 15 to 025 ppm ozone which

exceeds the air quality standard by a factor of three (using the ARB calibrashy

tion method) Thus there is a very significant transport of ozone or ozone

precursors from one portion of the Basin to the other side of the Basin One

thing to mention though is that the concentration would not be kept up on a

203

steady state basis because the transport is a result of the pulsing effect

I Illentioned earlier There is a lot of accumulati6n in the western Basin

and these accumulated pollutants are then transported across the Basin This

kind of transport did take place in a couple hours because we also have

measurements from 1500 PDT which give us similar flux numbers

Figure 16 is a trajectory envelope similar to Figure 10 calculated for

Upland at 1600 for the air arriving at Redlands about 600 oclock in the

afternoon I wanted to include this trajectory envelope to show that the

problem is not really simple You cannot say that the air at Redlands came

from Long Beach per se The air at Redlands if you look at the whole

envelope of possible trajectories using upper air data as well as surface

data could have come from anywhere between Downtown Los Angeles and over

the Pacific Ocean south of Long Beach

Another thing to recognize is that the wind actually changes direction

slightly as you go up and down through the mixing layer and the mixing layer

is exactly what it implies There is mixing within the mixing layer so if

you begin with a parcel of air near the surface this parcel may move to the

top of the mixing layer and go one direction for awhile it then may go back

down to the bottom of the mixing layer and move in another direction for

awhile The ratio of the length scales indicata3mixing layer depths of 1500

or 2000 ft and distances on the order of 70 miles This makes it very

difficult for tetroons to follow an air trajectory because they do not go

up and down They stay at one altitude and in one wind regime and yet the

wind regimes are different at different altitudes and the air is continually

mixed up and down through this layer You can often see this on time lapse

photographs

204

The question is where does the pollutant mass go after Redlands Figure

17 is a repeat of Jim Pitts slide from yesterday and it is data for the

same day that we did our analysis It shows the ozone peaks starting at

Pomona and Riverside and on July 25 1973 eventually getting out to Palm

Springs so there is quite a bit of long-range transport The ozone is

stable at 8 00 or 9 00 oclock at night There still are ozone concenshy

trations of 02 ppm it hasnt dissipated even at the surface Ozone does

dilute as the mass moves Other calculations we did were integrations

through the mixing layer of various pollutants such as ozone and CO along

with trajectories that we measured Th~se integrations show just what the

ground data show in Figure 17 The concentrations increase through the western

portion of the Basin and then show a decrease through the eastern portion

of the Basin CO tends to decrease faster than the ozone indicating a

continued production of ozone further east

Figure 18 is a streamline chart on a larger area map for the 16th of

August 1973 It shows the typical streamline patterns that occur for

ventilation from the Basin By mid-afternoon there is flow out through the

major passes to the north and towards Palm Springs (PSP) On this particushy

lar day we had data from Arrowhead showing that the air mass from the Basin

does indeed get up there

Figure 19 shows a vertical profile over Arrowhead early in the morning

16 August 1973 at a time when there was a north wind Ozone level was

about 005 ppm the scattering coefficient was quite low on the order of

probably 60 miles visibility or so Figure 20 is a vertical profile again

over Arrowhead late that afternoon when the winds had switched There is a

flow from the Los Angeles Basin into the Arrowhead area thus one sees a

205

vertical profile that shows a distinct increase near the surface in both the

ozone and the scattering coefficient and in the condensation nuclei Ahove

that you have fairly clean air The top of the polluted level is just about

the top of the mixing level over the Basin

I want to leave the transport now and discuss the complicated vertical

structure that can occur If you want to try to model something try this

one for instance Figure 21 is a vertical profile over Brackett Airport

Pomona about 830 in the morning on 26 July 1973 which is the day after

the episode shown earlier A bit of interpretation shows how complicated

th is can be If one looks at the temperature profile it would be very

difficult to pick out a mixing layer theres a little inversion here another

inversion there several more up here After looking at hundreds of these

profiles though you can start interpreting them What is happening is that

there is a surface mixing layer at about 500 m In this layer there is a

high condensation nuclei (X line) count due to morning traffic The San

Bernardino freeway is quite close to Brackett there is a relatively high

nitrogen oxide count about 02 ppm and the b-scat is fairly high Ozone (Z)

within the surface layer however at this time is quite low The layer beshy

tween 500 m and 700 rn turns out to be the Fontana complex plume Note the

very high b-scat level it is below 3 miles visibility the plume is very

visible especially at this time of the morning when it is fairly stab]e

There is a high nitrogen oxide level (800 m) a high condensation nuclei

level and again a deficit of ozone Above this layer (800 m) you have stuff

that has been left all night very low condensation nuclei indicating a very

aged air mass ozone concentrations about 016 ppm b-scat of about 04 It

has been around all night and not yet had a chance to mix down within the

206

surface layer In fact one good way of determining the surface mixing layer

early in the morning and at night is to look for the ozone deficit Another

thing to mention is that wind reversals occurred for each of these three

layers The winds were fairly light and westerly at the surface slightly

easterly in the 500 m 700 m layer and westerly above 800 m There is a

complicated situation early in the morning but the main problem is that by

the middle of the day there is good surface heating and the pollutants have

all been entrained and mixed down to the ground so in order to modeI what

happens on the second or third day of an episode you must be able to look

at both old pollutants as well as fresh emissions And you need to account

r for ozone that is actually transported down to the surface from layers aloft l

The next slide is a photograph (not included) which is another e xample

of some layers aloft This is due to upslope flow as explained by Jim Edinger

in his publications The mountains are heated during the day in turn heating

the air and making it buoyant there is upslope flow to a point where the

heating cannot overcome the subsidence inversion and the stuff comes right

out from the mountains and spreads out over the Basin The pollutants can

stay up there if the winds aloft are very light and on the subsequent day

will he re-entrained to the surface On the other hand if there are winds

aloft different from those in the surface mixing layer or the wind velocity

aloft is high there can be a very substantial ventilation process for the

Basin Pollutants can be ventilated up the slope and blown away in the upper

winds In the case of the entire July 25th episode winds aloft were quite

light and these upper layers remained

Figure 22 is a vertical profile of one of those upslope flow conditions

in the same location shown in the photograph but on a different day Again

207

there is a relatively high surface concentration of about 03 ppm of ozone

(Z line) a layer of clean air between 900 to 1100 m and then high concenshy

trations of ozone again above 1100 m It has gone up the slopes of the

mountains and then come back out Concentrations in the 1100 to 1300 m area

are just slightly lower than they were at 600 to 800 m area Notice however

that the condensation nuclei count (X line) is quite a bit lower mainly

because the stuff is much more aged above the 1000 m level than it is down

below 900 m

Figure 23 shows the stability of ozone the fact that it can stay around

all night long This is a vertical profile taken over Riverside about 2200

PDT 1000 oclock at night Above the surface mixing layer (600 m) there

are ozone concentrations of about 0 15 ppm (Z line) Within the surface

mixing layer (below 500 m) ozone is completely scavenged decreasing to

zero The nitrogen oxides within this surface layer are being contained and

are around 01 ppm from fresh emissions that occurred during the evening

Condensation nuclei near the surface are very high The temperature profile

is very stable You have a surface based radiation inversion which is a

little strange looking for a radiation inversion~ nevertheless it is quite

stable There is a definite restriction of the mixing--a very difficult

time getting air from below 500 m to above 500 m The ozone that exists in

the 700 m range is in air where the reactions have virtually gone to compleshy

tion and is very stable All the profiles on this night changed very little

the ozone peak stays there High concentrations stay around

Figure 24 is a cross section across theurban plume of the City of St

Louis I wanted to show that this occurrence is not limited to Los Angeles

We have seen ozone formation and transport in other urban plumes These data

l

208

were taken during a project sponsored by EPA in conjunction with R Husar of

Washington University and William Wilson of EPA The dark line on this is

the ozone concentration across the urban plume perpendicular to plume The

dashed line is the scattering coefficient The power plant plume is parallel

to the urban plume The data on the left were taken 35 kilometers down wind

about 1100 oclock in the morning The ozone concentration increases slightly

to 005 ppm in the urban plume there is a deficit of o in the power plant plume3

In the same urban plume same conditions 1500 CDT two hours later further

downwind there has been substantial increase in the ozone in the urban plume

itself The b-scat is very similar to what it was before but the ozone is

now increased quite substantially except in the power plant plume where

there is a strong deficit of ozone due to scavenging by nitrogen oxides So

the formation and transport of ozone and ozone precursors in urban plumes is

a regular occurrence that happens in more places than Los Angeles and as Bob

Neligan showed this morning it can happen over quite a bit longer distances

than we are showing here

To summarize the conclusions as they affect model development first

once ozone is formed in the absence of scavengers ozone is a very stable

compound It remains for long periods of time It can he transported for

very long distances Ozone is a regional problem which cannot be controlled

on a local basis To have effective ozone control middotone must have a regional

control strategy and probably regional type air pollution districts

A second conclusion is that the vertical distribution of pollutants can

be highly complex and models have to include more than just a simple wellshy

mixed surface layer

209

A third conclusion is that layers aloft can persist over night and can

be re-entrained within the surface mixing layer on subsequent days models

should be able to account for old pollution as well as fresh emissions Also

pollutant accumulation and transport can have distinct diurnal patterns that

are strongly dependent on the meteorology Models should be time dependent

and should start at the beginning of the accumulation period In other words

models ought to be able to run for 24 or 48 hours if they have to In this

case in Los Angeles there is often an accumulation of pollutants which starts

in one portion of the Basin at midnight and continues through the next mornshy

ing even before it starts to be transported

As far as recommendations go in many areas a lot of ambient data has

been collected and in some cases the data are actually ahead of some of the

models so I think a research program is needed in developing models that

will account for this vertical structure and the day to day carry over and

the models need to be extended to cover longer distances In addition more

smog chamber work is going to be needed in looking at the effects of carry

over and mixing old pollutants with fresh emissions How people go about

this I leave to the modelers and the smog chamber people They know more

about that than I do

I

210

I

~ INVERTER

AUDIO TAPE

MONIT0R

MONITOR OBSERVER SEAT

MON ITOR

NEPHELOMETFR FLfCTRONICS

j DIGITAL DATA LOGGER

CONDENSATION

VOR DME NEPHELOMETER TUBE

JUNCTION middoteox ASSORTED POWER

AIRBORNE

TEMPERATURE TURBULENCE

middot HUMIDITY

ALTITUDE BOX

__

middotE=-middot RECORDER ----r----------

NUCLEI KJNITOR

CONVERTER

SUPPLIES

INSTRUMENT PACKAGE (

lCO

03

Ndeg

-

-----NEPHELOMETER

BLOWER

Figure 2 Instrumentation Layout for Cessna 205

211

bullubullbullbullbull

Figure 3 Airborne Sampling Routes in the Los Angeles Basin

Figure 4 Vertie al Profile Flight Path

~-~ r~i ~~1 -- ~ ~ ~2-1~ LJ-----~ r~~ ~~ t~~--l

~ ALM l

0 RIA

ec 8v

M

~ Afo

-o

M 0

~IV

ltgt

IN J--1 N

SCALE II fi M I j_ ES 0 3 4 5 =-JSEJ--J~ _middot ~middot- - =- =

I

~

M

N~J

Figure 5 SURFACE STREAMLINE ANALYSIS - 0300 PST 25 July 1973

~~~ ~~-- cp1FJ=D -~~

~ 1

~ ~ 8c

8v

~25

PACIFIC OCEAN

diams Tt

0

9 I 4 5 10 I- m p H - -middotmiddot u 4H__8 middott_

D i6 J4 k W~D SPED llaquotl SNA NJ ~1

SCALE m ICtt84bullmh R v1s1a1L1n (mil 6 ~ CONTOURS REPRESENT

-- 10ml 16km (~() bull ~ ) ~ - 000 ft 3C5

Figure 6 S_cJRFACE WIND STREAMLINES - l 600 PDT JULY 2 S I 8 7 3

l - ~---i ~-=-___-----c---it~~-~~ r----=------1 ~-~~--cpc---_t__A --~ ---llil

~_ - ~-l-cL

34bull vi~-dff

bullbullbullbull bull ~ bull -1 bullbull - -_- L bull-J bull ~bull-bull-ii------~ bullmiddot r_ -~- ~ bullI ~_ bull bull bullbull bull I bull _ - bull -~-~ middotbullbullbull ~ ~ --middot -~- bullbullmiddot ~v ) ~ - -__rl v middotmiddot - 1- ~ -- middot middotmiddot - 1 91 frac12 - ~- lt( middot K i - middot bull - middot - bullmiddot~~-~lJ) obullmiddot~ ~-f- _J_~---Smiddot~middot-~----~~~---gt_middotfY-_middot-~middot --middot-~-~----fJ_middot- middotmiddotbullmiddot u-- bullmiddot ~ ~ -middot L~ bullbull

~bullbullbullbull bullbull l_bull bull bullbullbull EW bullbullbullbull-- ~ __bull f f - middotbull - J middot f bull S bull I ~ -r --

_ bullbull bull- _ bullbull-bull ~ ~ bull bull bull bull I bull bull bull bull bull bull gt - bull middotbulliJ -bull I bull bull _1 bullJ C-- ~-middot _ bull bullbull bullbull bull _____ ~ ~ l _ middot q bull 1 -middot middot ~~middot middot middotbull_ J ~gt - J bull-bullbullbullbull ) _ -middotmiddotbullmiddot J ~middotmiddotmiddot -bullmiddotbull fmiddot 7middot _middotmiddotmiddot bullmiddot(middot Ii~ middotmiddot~_--~middot 1middot__middotmiddotmiddotmiddot middot- gt_ -~ -~-- Imiddotbullmiddotbullbull_ -

- ()_I (w--_ bullbull__(i- bullOmiddotbull bull middotbull -bull-_jlJ middot bull lt 1(middot t gt bull - ~ rbull I bull middot middot- bull41-bull l~r v-middot~- middot middot middot bull_ - middotmiddot ~Jtj (middot~ ~middoti middot middot middot middot middot ~- ~ -tmiddot~ I - middot middot_- ~ - -~ middot_ _- ~bull - _ ~) i bull bullbull bull- middot_ bull middotbull __ ( bull 11bull bull ~ampmiddot ~ l bull bullQ bull - -1 bull JY1 bullbull ~ or bullbullbullbullbull bullbull-bullbull _ ~ - bull bull-bullbullbull middotimiddot middot 91 bull t bull - - tfaw lJ--r- bull bull _ bull middot- - l

f ~~middot--~ middotmiddott ~ltrgtmiddotmiddotJmiddot_bull - ~ - __ middot- LOS ANGELES BASIN - LOW LEVEL -__ jmiddot l-gt bull - bull J iI bullbull bull bull bull _ bullbull _ Jmiddot middotL~_1 middot middot bullbullmiddot ( C middot INVERSION MEAN WIND FLOW _ J

lmiddot - f bullbullbull~ - f 1bullbullbull _ ~)- bull middot- _---_- 7f-~bull~ REGIME _F_~ AUG_UST_~ ~600 P~--- l

-__L-~bull --ncmiddotbull~~-j--bullmiddot~bullmiddot_-bull _fJibullmiddot Imiddotmiddotmiddot-bullmiddot- bullbull ~ bullbullbullbullmiddotmiddotmiddot~middotbull ___ bullJ_ _middot~0))deg bullt t1yensmiddotmiddot ( middot middotmiddot middot middot ~ middot lbullbull1 t_c0 bull -middot---l lt ~middot~- deg bullbull --= bull bull bull I bull bull bull bull bull bull bull bull bullbull _~bull b ---) bullbull-bull ) bulll middotbull middot1middot ) bullT --f bull I bullr ~bullbullbull bullbullbull( - -bull-- ( -o-----_i bull-~-l- i l l J l~-- c middotmiddot _--1 ---I middotmiddot ---- ~bull-bull bulli_ ALT Elmiddot_ bullbullbullbull _- ~~middot bull middot bullbull _ bull middotbull bull~ ~bull middot bull -middot bull--ua_-- bullbull bull

-- 01--- middot_ -middotmiddot hmiddotmiddot __1 ~-- ~ fi~~- ___ - ____ _ -middotmiddotmiddotmiddot~ ) -~-J bull bullbull bull bull 0 uc- -l ~- ~ IT ~~ll ~ bull -middot -middotmiddotmiddotmiddotbullCCAmiddotmiddotmiddot-middot middot bullbullbullbullbull

) i- 5 ~-==-- __ __ - bullbullbull _ bull~ bullbull _ bull bull l T[h4 ------ - 0

i17- o~-lt -(i-_~ 11t~bull-omiddot ~- -- 13 0l~~~bull bull Jbullbull~bull ~ ~bullbullbull bull bull x- middot~---=-~~ -=aJlll8 bull Ibull bull ~~ middotbull rbull~---bull1-~middot-middot _ middotmiddotmiddot-middot 1 0 ~vrbullmiddot ~middot ~ (J~-middot _-_~) ) ~ bull middot

l middot _ POMA_ middot =~~~----ti~ jmiddotmiddotmiddot - middot bull [j

~A ii J0 Vfli middot bullHud __=bt_ bull

CImiddot ~-- ~- middot)middot PACIFIC OCEAN I middot ---- middotmiddot ~

__ middot__ ~ - _ 23~1 middotbull 8 4 1 middot middot ~ middot middot gt ~~- l ~ u middot

bull - bull- I ~------ --1~ i middotmiddotmiddot - n _c-118 1130

~ n r -t ~~gt25) cmiddotbullmiddot

~--lt- ~~- 1-~__( i - t ~ _ middot 0 igt(_J

11bull bull11 ~~ -~[ ~i~gt----gtmiddotmiddotmiddotmiddot--~l_ ~~ ELEVATION

IN FEET bullbull (_- middot bullbullbull -middot middotbull middot ~~ middotmiddot bulltbullbull _ffmiddotmiddot-middot v I )tylt~ -~bullbull1bullbullrbullbull ~-lt -~ ( I~

600~ A0 Cv(A (1829 m AND OVER) deg )_ rJ__~7 middot middot ~--middot L==1 _J bullbullbull - bull -middot~-- rgt ~ middot(Zmiddot- middotbullmiddot middot

Z~C)-tGOO (762 middot 1829 m) 9-N4 __J (r -- lf _ bull bullgt-~~~ ~ _ w _ _ I (1 bullmiddot( middot1 middot -----~~~- middot L-bullmiddotbullW bullbullbull3 STA r I0-4 lODEL

100i -2soo (305~762m) -- Ow - -~1_- i ~~--- bull v~rvt ~~ -middot )) ~--

II gt J (-_bullmiddot middot~ l bull bull tr 1 )~ gt ) bullbull-_bullI-middot -middot bull~0 3 Mor nuq1ENr Wlbull~O JIAtCTIO-bull bull - lbull C---gt bullbull )t bullbull -( I bullf I - 20-00 (61 bull 305 ml J( Jloa xxE- -bullbull00 - -- middot1

0-200 (0middot61m) Wl)7 AVBt~gpound ) bullmiddot-iiNL~ middotntmiddot_ 1 iJJlt( _1J- ~ VAq IA9 IL ITY 0 ~ 10 15 ltS lHPtl

~--_ bull bull I bullbullbullbull 1 ~) J)J ~ bull Is bullmiddot bullbullbullbullbull ~ 3 V IS A VAqlABLE OIR~CTIO- 0 8 16 2-4 km

(SPEEDS SHOWN IN mph 10 mphbull 16 h1llr) -- middot ktr~~~ lt~ ) -middot-SCALE

Figure 7 LOS ANGELES BASIN MEAN WIND FLOW FOR DAYS WITH LOW LEVEL INVERSIONS DURING AUGUST I 970 AT 1600 PDT

-~~~~-=======~middot~-~======~middot--=-==-===gt=---==____________=== ~--=-J~==-- -=-ee----=-------

500

N f-- V

- - - SUBSIDENCE INVERSION

----MARINE INVERSION

bullbull-bull-bullbullGROUND LEVEL

x WINOS ALOFT (kmht)

WESTERN middoteASIN EASTERN BASIN

LAX WINOS EMT IHOS I I

CNO WIHOS

s_ 04 13 1500- 05 02 08

I 06 069 middot

11-1--

04 04 i ~4

06 ~ 4--

I 2

1000 n1 1005 -_E

lll --1 lJ -----------~----

~11

--=i-+- c -- 9 _____ - ~ C

lt I

I 6 4 _r 31

I 6 5 ~~ ~_ bull ---middot- 64 ~li- - middot- bullc - middot-----------

10

SMO (1347 PDT)

EMT (1246 PDT)

BRA CAB (1459 PDT) (1335 PDT

RIA (1349 PDT)

RED (1406PDT)

Figure 8 VERTICAL CROSS-SECTION OF bscat FOR lvflDDAY

T t 10-4 -1)(l n1 s are m

JULY 25 1973

- c - -~

~--~ JC_-_1- ~1pi~ oamp----~JilliiiM~f~-U~ -~--- --~~~ ~~~

-=--~

-E-- O

_ lt

1500 05

06 15

09 __~

1000 --

~- ~---middotmiddot 29

500

oJ11

__a

07

I 07 I

I I

I

09

I

I

I

I 7 ---

11 -----

~ ----- 6

---------------lt- -~middot4 --------

20

29

-

10 10

11 07 08 08

10

08

~8 _____ Y-

N

- - bull SUBSIDENCE INVERSION

----MARINE INVERSION

-bull-bull-bull GROUND LEVEL

WES TERN BASIN EASTERN BASIN x WINOS ALOFT (kmhr)

t t

CNO WINOSILA WllltOS poundMT WINOS

SMO LA EMT BRA CAB RIA RED O (1736 PDT) (1655 PDT) (1707 PDT) (163 PDT) (1823PDT) 1805 PDT)

Figure 9 VERTICAL CROSS-SECTION OF b FOR AFTERlOON OF JULY 25 1973 scat

T bull 1o- 4 - l )(units are m

__~~---iii~~- ~- ~~______ ~~- --~~J---=-~ ~

N ~ -J

PACIFiC OCEAN

0 5 10 15 1111

E 8 4 I 0 8 6 2 ~ bull

SCALE

dh Mes

CONTOURS REPRESENT - 000 ft 305 m

0 SNA

c8s

ec 8v

amp R~b

Figure 10 TRAJECTORY ENVELOPE FOR AIR ARRI1G AT CABLE AIRPORT (CPLAD) 1600 PDT JULY 25 1973

~-~

q_- ~ ------1 H~~~ -~~--~ ___---___--i- __r-=-1--===12---1 ~ ___r~ _==---_ - ~- f~~ ~-- - -5plusmn-at -~middot~

ll~~r1 ri

40

ec 8v

-1 I

amp

0 HQ_

7 0

CAP LAAR) O

VER

PACIFIC OCEAN ~ 0

RLA

4

WHqR d

diams

H ~I

I l

0 COMA

3

L~

LAH

Fa_ f ~~

S ~ LA APCD VALUES ADJUSTED TO AGREE ~

lt

0

5 10 15 mi0 WITH ARB CALIBRATIONE-j I I CONTOURS REPRESENT NZJ ~ 0 a SCALE 6 24 km - 1000 ft 305m COS v~J

______ J 10 ro ( igtf t-i

coFigure 11 SURFACE OZONE CONCENTRATIONS (pphm) I 600- I 700 PDT JULY 25 1973 ~

~~~~~C-~ ------=--~-__-~--~~~=--- ----=--~

N

-E

D1600----------------------------- 1--

14001-------------------------------

1200

I Ground Elevation

1000 middot 445 m ] lampJ

sect ~~ 7 ) SURFACE i6~ 800 MIXED LAYER

~

~ [ J ~ ~ I OZONE CONCENTRATIONS~ 600 E E GREATER THAN

( 50 pohm

400 I C H T Z GROUND LEVEL

200

I PUUloCETER UNIT SnbullBOL

NOc N0 0 ppm01 02 03 04 05 03 z

40 --~45~~ 50 co pm C0 5 10 15 20 25 30 35 I I I I I I I I I I TEIIPERATURE oc T-5 b 5 10 15 20 25 30 35 40 45

I-- 100 RELATIVE HUlillOITY H0 10 20 30 40 50 60 70 60 90 b1eot IOmiddotm- 1 8

CN cmmiddot3 1 IO X0 I 2 3 4 ~ 6 7 8 9 10 URBJLENC-C cm213ue- E

Figure 12 VERTICAL PROFILE OVER CABLE (CAB) J CLY 2 5 l C)7 3 l 63 6 PDT

~ _~ ~--- -

--

1400 I bull bull

1200

1000-5 LampJ 0 ~ I- 800 ~ c(

sooLl

-1-=-1-~--t j --=~c-o-----i-bull 1-~~~ ilt~~ -~-1 lta-abull--~ -c-~---=---r F--- ---- I n_--middot- =~~ ai~IHJ

(~-It

1600 ___________________________________

C r 11 s Ground Elevation t~C E H I~lcc

- ~ 1 90 m

4001 bullc C H

C UNDrnCUTTNG svC ~ Ic- H

SEA BREEZEC II 200

C C

[C -PARAMETER ---UNIT SYMBOL

NOx N0 0 ppm01 02 03 04 05 03 z co ppm C0 5 10 15 20 25 30 35 40 45 50

-5 middot- -~20~----25 TEMPERATURE oc T0 5 10 15 30 35 40 45

100 RELATIVE HUIOITY H0 JO 20 30 40 50 60 70 80 90 bcot 10-4m-1 8

CN crrr3 10 0 I 2 3 4 5 6 7 8 9 10 X TURBULENCE cmZ-13 sec-1 E

N N

_-----=-G--~---

Figure 13 VER TICAL PROFILE AT EL MONTE (EMT) JULY 25 1971 1656 PDT SHOWING UNDERCUTTING BY THE SEA BREEZE

0

middot~_lt ~middotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotbullbull

-~

LACA

0 - )

i r=

-v2v

~

_middot~middot)( I bullbull

bullJ

K~Ji~middot

~~ 61iAS 0

EMT J~J---6~-11 ~orr

PACIFIC OCEAN

WEST 0

SMC

0RLA

14

L~8

R~A

~BL

16 ~ ~

0 5s Pcfrac14A c1i ~ )

wFJfo~J_) ltI~~~

_ff-Clf1ito J )

HILL~

~J U

~ _~~~

~

I o middot

1 1$ ~ 11yen ~middot ~I N

I

N I- I

t

0 --pomiddotmiddot bullmiddot i- 1LO middot Joomiddotmiddotmiddot -- middot middotmiddot -middotmiddot

_middotmiddot 0 middot middotbull MWS r

L4 ( 1 T bull bull __-- -A bullbullbullbull middot

0 i __ bullbull

17 t-J~ N7 a S I ~r ~ 1 rtd ~lt A-~ v- middot ~ - cXa 0

RIA 19

CLO

ltJ~

bull ~ 0

(

--

1

_ _

-2Wl

~s~o -- _)~J0JgtJ~ ___ Q

15 l1JI

0 15 r(A0

CAP

CLARR)~R 1900 1-shyPDT

II (_-L~X L2X I 0~ R[V

0 CCtwA

I

I18=00 POT~ l4 r1

fj

-11J - ----- 11=oomiddotmiddotpor

l~i middotmiddot- o

i

5 10 5 Tl o~1 middot--middotmiddotmiddot middotmiddot

_q it==i--__F-3 9 I I CONTOURS REPRESENT SNA NZJ ~1 o

_- I 0 8 16 24 km I - 1000 ft 305 m middot ~

7 14~CALE --- 2500 ft o2m V lr1 ) middot I i0 _ il o5

16QQ pol(middot v( ____________ _L

I i

Figure 14 APPROXIMATE TIME (PDT) OF ARRIVAL OF SEA BREEZE Jl-LY 25 1973 (Ogt_iective criterion based on ground level ozone concentrations)

~ -___~==~ ~~ - ~ =-~ f7r=~1 _j~-~ --c_~~

u-middot - middot middotmiddotmiddotmiddotmiddot

~- middotmiddot~ ~1 WESTERN BASIN r Joa_middotmiddotmiddotmiddot_ NOxEMISSION RATE ~- 95 METRIC TONShr

-----bull_ ~ ~middot~ I -OUR -----middot )omiddotmiddotmiddot - middot~ l21 (fTI

~ AT middot ~ middotbullmiddot- ~- ~ middot 4bull-middot

I EASTERN BASIN NOx EMISSION RATE 10 METRIC TONS hr

ri r bullbull

t10 Joa

) __ 8v -a_ -- -bull-I O ~AGA -_ ~S ___ _ middotmiddotmiddot -

~ ~v ai- omiddot-middot~-- - ) r -middotmiddotmiddot f middot( ---~ -l A ~ _ (- bull ___

it~ ~~~ middot-middot -- ~-~ ~~~ 0 0 AZU~

AVERAGE CONCEN7RCTi)N iN BOX (IF STEADY STATE)

IS 25 pphm

1 r f--Ji 7 ~Sv PAS ou )V~(~- ~ t i -~ Li_) 03 FLUX THROUGH f~

~ ~JI_~ - amp_ JiM O SHADED BOUNOA~middot~-~ ~~-s-- EMT 185 t 60 METRI~ bull ~ ~ TONShr 0 (m)

c~~~ 1t~CS A~JFP

1000 _29

-i32

_~o tUA

_

1

O~ ~

0 -__rJ( (r- J PACIFIC OCEAN LAX _ C-middotJbull _

l o M R No _

550m

r

A frac14

HAR O HJ LAH

_ o camptA REDLANDS 18QO POT ~ r

I bull ~

RB MEAN TRAJECT~~~y

0

TOA L~S

0 AN

I - ~ 8 OUNOARY ~ ~middotltdeg ~ ~ BETWEEN middot __ WES~ERN ANO- middot middot - ~

I gt I lt bullmiddot bull (EASTERN ~ i middotmiddot middot - - ~

S ~ ~~ ~ - middot-

rt1~1_--t------l

middot1-- BASIN ~-~

1-)~~--middot ~ ~l

~~ ~-bull bull J --

-is-eo -_

0 5 10

j=i r-i C

0 8 ltl

SCALE

5 mi

2~ un

CONTOURS REPRESENT - 1000 ft 3gt5 m

--middotmiddot 2500 ft 1 762 m

~

0SNA

cos 0

_ --~ ----- --- ( bullmiddotmiddotgt

- middotlt- ltgtmiddot t__ Q ~

1 1 rmiddot bullbullbullbullmiddot ~9

NZJ ~ middotmiddot - middot- Alr ---middotmiddot- middot middot( middotmiddotmiddotmiddotv ~ bullbullbullw bullbullbull bullmiddot 1 bullbullr~ ~-- -middot ~--v ~- - I -~

ESTIMATED OZONE FLUX FROM VESTER~ TO EASTER-J BASIN JULY 25 1973 I 700 PDT

C ~IV

N N N

I

l ~

-~~

I

iI

i I

I t

t

~ ---~ --

Figure 15

~Qa llfJD fl(~middot ~ 11f ~I I

l

Lfb ec~s0 CPK v2v 0

ALT 8v Ld~_----1

I

HO-

0 CA

middotLARRv O VE~

1330

ol(Di

A~U

0ENT

~lt

s~e ~ 1530

F8f 1730

~

rbull-~

oc (WljT) -_-~(~~c lt-rw---_

~~ ~-_i~cB~~~

2-~) - ~ ~ l~w-~~ p~- pound)_

0 ojI middot tl-1CfUp I ~ ) 1 ~ J~I i bull middotbull middot~-Li 1)- ) I

DiI ~- 0

i ) 0 l I I

t

A RALc~o JI

C

-~

0 r-iR

~IV 1230 1~

RE PO ~- I - Ftl

) 0 ---~gt- __L8s ~Zi diams ( T~ _middot_ ~~ ~

I AN ~~-~ j t bi 0

~ I

~ I L i

-_gt ji o 5 c 5 Tl middot 0 0 ~-i p__i=r 2=f I_ I 1 NZJSNA 1

1 8 2 4 km )

SCALE I 00 J_(1 CONTOURS REPRESENT cos f

1 0 I --- I - ))) 35

PACIFIC OCEAN

Figure 16 TRAJECTORY E~VELOPE FOR AIR ARRI1gtJG OVER REDL_)DS AT 1800 PDT JULY 23 l =i73

224

JULY 25 1973

LA DOWNTOWN

0sect040 a

~

~ 020 0 X z0 ~ LJ 0 ~ z

~5 040 330POMONA 0 ~ en~ 020 w z _J

w w 0 (9 z O----u-~~-__~_-~~~-------L-~-0--0-0~----- z

ltt~ 040 56 (I)z

0 0o _ RIVERSIDE _J0 20 t6 ~

0~ Qt---0-0--ltrO-ltgt-C~------~~~~ a

LL ~

Rate ~ IO mph___ (I) w

_J~ ~ ~

et~ lt(

3 040 PALM SPRINGS ~

j 020 ~

0------____-----L--___---------L---~--~

105

12 4 8 12 4 8 12 l~-s----am _ pm----1

HOUR OF DAY PST

Figure 17 Diurnal variation July 25 1973 of oxidant concentrations at air monitoring stations at Los Angeles Downtown Pomona Riverside and Palm Springs California Values are corrected data Los Angeles Downtown and Pomona x 11 and Riverside and Palm Springs X 08

CONO S t 1 fRESEIS7

~

~~ 0

ciffmiddotdK ~ ~v~~o

( ~s ~

bull ~r ~ bull 1--~~----Soootl ~ ~ ~ ~ lj i1 d t CJ ~ ampfrsmiddotflt- frac12 ~ middotL~Js _-- ~

_gtgt middot~ ~rroltf~-) ~ 0 s- r

middot-middot- r_~ ~~JtbO ~~bull~Jt ~~~ L r - bull _ ~ I= J 1 ~ ~ ~-~~bullJC ___ -_ middot ~ laquo -poundJ~ ~- middot1~ r-- - V--_1_ ~ I 1 S I

V ~ bullf-uv~ fi -~zumiddot -~middot~ LS gt -tmiddot-F Q~ ~-tv I_~ --- ONT p(_ s ~S ~~~-[ ( 0 c-_ --~ ~~~___d_) lt- ~ I -i-C - -

~----1-1 bull~~POMA ~V BN ) middot-~ f -- s - ~

~VA -middot- ~p AAL a 2~~ ~~middot01 r r ~ middot middot 0-- V

i LAX bull1

~ -~poundJ-i- ltllll _(__1-0~ ~t- degQ-0- ~~ _ _-__~~-qlK ( a_ II ~ ~p-~ ~J

N bull - - 0 r o_ _I ~ -~ ~middot ~ ~amp ~--= ~ ) s ~

- -~- - middotO _a - Tl --0- ov I lHOIO J I bull J -- ~ 6 ~ -__ 2 ~

(__ ~~ _- ~-~ middot8---fl~ -- ~ bull~-abullbull _~ ~-cgt ~ bull bull middot e bull bull l ~ 0

I 1A_ HZJ middoto~J

middot0 (~ ~ S TAA

- ~ - - - --0 () _-j J middotO=c==c-c==cc~~~ l ~~ ~ ~ bull-~---~ ~ bullbull -~ al1 ~ bull __ ~--middotmiddotmiddot

diams Skyforest _ Strawberry Mt Lookout

Figure 18 STRE ~[Ll)ES FOR 1600 PDT on 8 1673

~ ~--

vO 0

N N V1

au

91 V7

-1 ~ -=1 ~~ ~~~~l r=--~d- ---1 _J-_

~E1 ~L1-~f~

3100 ---------------------------------

2900r-----------------------------

T

e w 0

~ 5 Cl Ground Elevation

1560 m

T PARAMETER UNIT SnbullBOL

NOx N 01 02 03 04 05 03

ppm z co ppm C

10 15 20 25 30 35 40 --

45 50

170

I I I z

0 5

-5 - -0~ 5 10 15 20 25 30 35 40 45 TEMPERATURE oc T

0

0

10

I

20

2

30

3

40

4

50

5

60

6

70

7

80

8

90

9

100

o

RELATIVE HUMIDITY

bcot CN

TUR8ULENC~

110-4m-

cm-3 tobull 213 1 cm sec-

H

8 X E N

N OI

Figure 19 VER TI CAL PROFILE OVER ARROWHEAD u-RR_l A CG CST I 6 1973 939 PDT

3100----------------------------------

N2900r----------------------------- -i

N

2700i-------------------------------

2500

e 0 uJ 2300 gt ~ ct

2100

1900i---------------------+--------------

~le 1iation 1360 m) 17001 ~

- -PARA1jETER UNIT SYMBOL

T NOx N1500 o ppm01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50

TEWERATJRE oc T-5 middot --~o--- 5 10 15 20 25 30 35 40 45

IOO RELATIVE HUWIOIT Y H0 10 20 30 40 50 60 70 80 90 bcat 10-~- 1 8

CN cm- 3 104 X0 I 2 3 4 5 6 7 8 9 10 213 1 tURBliiENCE cm sec- E

Figure 20 VERTICAL PROFILE OVER ARROWHEA D -RR 1 --- -AUGlJST 16 I) 16--1S PDT

1-~i w--~i_f l-=--bullC- ---~-4

1600 bull t c- N 8 ff Tbull C[ 8 H 1 bull H z H T ~ C f N 1 H T bull C rn 1 C NE bull-~z Hi400 bull bull tf T bull N ~r --middot _P H -ybull EC N z__e H T i 8 z H Tbull C E HD Z H T POLLUTANTS REMAINING FROM bullt C Hbull L T PREVIOUS DAY1200 Et HO I II -middot-- bull Ct H 9 - H T

___ Hbull( E N 1 a tC N i--_ -1 H

C N Tbull Z HP poundIC C H z_ 1111 1

- bull C H Z l _H_ _J1000 )( cc H -z emiddot ksect bull C N ~ T

)( iz H 8 H TIAI -t XC z 7-- T0 bull pound N t H_8

t-gt

YCpound N 1800 l I-gtltbull - H (Jet

N i -r~Bltt t bull gt- t C X N H T

[ BUOYANT POINT SOURCE PLUMEH 1

N ~z-- -

C H

-bull SUPERIMPOSED ON POLLUTANTSC JZ X H T 600 -~ E c REMAINING FROM PREVIOUS OtY Cl JC t H H f bull cmiddot t HT -fl

C- X t fl _ REMNANT OF NOCTURNAL RADIATION INVERSION(I-----e-C f N K I T H

C Z [ T H x-8 400 _Zc r -H -K SURFACE MIXING LAYERz C II H K 8

C N T pound H M 8 _ I -t ff H E N -9 l

Ground Elevation 305 rn200

PARAMETER UNIT SYMBOL

_ I - I I I NOx N00 ppm01 02 03 04 05 03 z

co ppm C 0 5 IO 15 20 25 30 35 40 45 50

L middot1 TEMPERATURE oc T-5 0 5 IO 15 20 25 30 35 40 45

100 RELATIVE HUPAIDIT y H0 10 20 30 40 50 60 70 80 90 bscot o-4m- 1 B

CN cm-3 x 104 X0 2 3 4 5 6 7 8 9 10 TURBULENC~ cm213sec-1 E N

N co

Figure 21 VERTICAL PROFILE OVER BRACKETT (BRA) JULY 26 1973 0825 PDT SHOWING BUOYANT PLUME AND UNDERCUTTING BY RADIATION INVERSION

N N 01600

___bull C M C

C

1400~~~ t C [ middot H LAYER CAUSED BY

C C H C [ H UPSLOPE FLOWl

1200

1000 ] w

SURFACE MIXING LAYER 0 --= ~ -~~ 6 800~ er

C C

600t-i C C t C

I ~00

Ground Elevation 436 m 2001-------------------------------

PAIUWETU UNIT SYWBOL

NOx N ppm0 0 01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50 I I I I I I I I TEWPERAT1JftE degC T-o b 5 10 15 20 25 30 35 40 45

100 ~EIATIVE HUWIOITY H0 10 20 30 40 50 60 70 80 90 b1tt1 10-m- 8

CN enr3 110 X0 2 3 4 5 6 7 8 9 10 Tu RUL Erct cm23sec- E

Figt1re 22 VERTICAl PROFILE AT RIALTO (RIA) JlJL Y 19 1973 1738 PDT SHOWI=JG LAYER CAUSED BY UPSLOPE FLOW

~~-7 ~ ~- 1 ~iri ~~- ~~-~ ~t ~~ ~ =~middot-1

1200 I t 1 If J-

1000

I C ltTl a_ ~l- t

800

600

L gE __r H

H

400 j (~ c pound N C E I~

t EH -

1-1 M

H H

H M H H

H

H H

11 bull H M H

M H If

H H

H

- C t H ~ C poundmiddot H

I C E I(

200

1600--------------------------- t

T t t T l

l T t

T t_

t 1

l] w ) g f

Tt t

ltt ~ T

t J t T

t J

f 1

t

Klt

H M Cro1nd Elevation 250 m HT X

5Yl80LPAllAlETER ~

NOx N0 0 ppm01 02 03 04 05 03 z

co ppm C0 5 10 io 20 25 30 35 40 45 50

25~--- ---35~~-40 TEMPERATU~E oc T-5 0 5 lO 15 20 30 45

100 RELATIVE HUMIDITY H0 iO 20 30 40 50 60 70 80 90 bact 10--ltllm-1 B

CN cmmiddot3 11 04 X0 I 2 3 4 5 6 7 8 9 10 IURBULENCE cm2hioC-1 E

Figure 23 VERTICAL PROFILE OVER RIVERSIDE (RAL) N

JULY 26 1973 2239 PDT I)

middot==-=-=

0

bull

N w 1--

ii -s~~ l-obull

CJ ~

obull -obull obull

5 02~

bscat

Oa

4l o2J

-I 3 e I 0

--)(

~

Abullu 2

ll

ol

Traverse at 750 m msl 35 km Downwind (SW) of Arch - St Louis Mo 1117 - 1137 CDT

( Power Plant Plume -01 Ibull-[ ~ e

11 bull E I -)(I

I0bull I 1r~ l -

0

I I Io 1 u I

I r- l A bull I i I 1I

H1I I 4 t I II I I

11 I I

I I r I I I

I I qo 01 I I

I I bullJ~viI I middot ~

I

I I

~

Urban Plume

ood 0 10 20 30 40 50

kilometers

o~

02

01

s 1

P

0bull 01

00S~J1 I ti middotmiddot1 middotvmiddotmiddot~ J

Urban Plume

I y

oo 0 10 20 30 40 so

kilometers

Traverse at 750 m msl 46 km Downwind (SVV) of Arch - St Louis Mo 153 0 - J 549 CDT

---- bscat

o-

Power Plant Plume

1l~ 11I 1 t

ill~t fl Ibull I ii

I

lmiddotmiddotrI

I I I I t II

l vrI V

JV-f Jl bull

bull t I bull I

Figure 24

l

232 RELATIVE CONTRIBUTIONS OF STATIONARY ANDMOilILE

SOURCES TO OXIDANT FORMATION IN LOS ANGELES COUN1Y IMPLICATIONS FOR CONTROL STRATEGIES

by Robert G Lunche Air Pollution Control Officer

Los Angeles County Air Pollution Control District Los Angeles California

Introduction

The type of air pollution problem characteristic of the west coast of the

United States and particularly of Southern California has come to be known

as photochemical smog because it is the result of sunlight-energized atmospheric

reations involving oxides of nitrogen and reactive hydrocarbons Its manifesta-

tions- -eye irritation reduced visibility damage to vegetation and accumula-

tion of abnormally high concentrations of ozone or oxidant - -are by now well

known In fact the occurrence of high levels of oxidant which consists almost

entirely of ozone has become the primary indicator for the presence and relative

severity of photochemical smog

During the 25 years since photochemical smog in Los Angeles County was

first identified an extensive program has been underway for control of the responshy

sible contaminant emissions Initially during the 1950 s these programs concenshy

trated on controlling emissions of hydrocarbons from the stationary sources of this

contaminant In the early 60 s programs for the control of hydrocarbon emissions

from motor vehicles in California were begun An exhaust emission control proshy

gram for hydrocarbons and carbon monoxide from new vehicles was begun in 1966

C011trol of oxides of nitrogen emissions from motor vehicles began in 1971

As a result of the overall control program by 1974 emissions of reactive

hydrocarbons from stationary sources have been reduced 70fo from uncontrolled

levels and about the same percentage from mobile sources Oxides of nitrcgen emissions

233

from statjonary sources have been reduced about 53 while emissions from moshy

bile sources are still about 7 above uncontrolled levels due to the increase

in NOx from 1966-1970 models Additional controls already planned for the future

will by 1980 achieve reductions of reactive hydrocarbons from stationary sources

of about 87 from uncontrolled levels and from mobile sources about 93 By

1980 emissions of oxides of nitrogen from stationary sources will have been reshy

duced 53 and from mobile sources 63 from uncontrolled levels The past

present and projected emissions of these contaminants are shown in Figure 1

A I though compliance with the air quality standards has not yet been achieved-shy

and is not likely before 1980- -the results of these programs have been reflected rather

predictably in changes in certain of the manifestations of photochemical smog For

example eye irritation is less frequent and less severe and in some areas js

rarely felt at all any more and damage to vegetation has been markedly reduced

Ozone (or oxidant) concentrations have been decreasing in Southern California

coastal areas since _1964 in areas 10-15 miles from the coast since 1966 and in

inland areas 40-60 miles from the coast since 1970 or 1971 as shown on Figures

2 arrl 3- All of these positive effects have occurred despite the continuing growth

of the area indicating that themiddot control programs are gradually achieving their purpos

a return to clean air

This improvement is al~o refutation of the so-called Big Box -concept which

assumes that the total daily emissions in a given area are somehow uniformly disshy

tributed throughout that area--regardless of its size or of known facts about the

meteorology of the area or the spatial and temporal distribution of its emissions- -

234

and of control strategies based on that concept And since the improvement in

air quality refutes the control strategies based on reductions in total emissions

it thus confirms the value of more recent control strategies which emphasize conshy

trol of motor vehicle emissions and use of a source-effect area concept

Following is a brief listing of the evidence we intend to present as supporting

our views on just what control strategy is appropriate

Examination of relative contributions of HC and NOx from stationarybull and mobile sources demonstrates that motor vehicles are the overwhelming

f source of both contaminants~

I bull Observation of air monitoring data shows that the effects of photochem -

ical smog are not uniformly distributed t_hroughout the county

bull Study of the meteorology of LA County shows consistent paths of trans -

port for various air parcels and consistent relationships between the

areas most seriously affected by photochemical smog and high oxidant

concentrations and certain other areas

bull The upwind areas are found to be source areas--the downwind areas-shy

effect areas

bull Central L A is found to be the predominant source area for the effectI area in which the highest oxidant levels in the SCAB consistently occur

bull The predominant source of emissions in this source area is found to

be motor vehicles

bull Central LA has the highest traffic density I

ij bull Both pr~mary and secondary contaminant concentrations reflect the effects

of the new motor vehicle control program in a predictable fashion 11 I

A strategy based upon these findings is gradually being verified by atmosshybull pheric oxidant data~

235

The Evidence that Motor Vehicle Emissions Are the Principal Source of Oxidant

As seen from Figure 1 at the present time the total daily emissions of I-IC

and_ NOx from all sources in Los Angeles middotcounty are primarily due to the motor

vehicle The problem now is to find the spatial and temporal representation of

emissions which when examined in the light of the known meteorology and geogra -

phy of the Los Angeles region best describes the source of emissions responsible

for the highest observed oxidant readings

In the rollback models used by EPA and others the basin is treated as a

big box with uniformly distributed emissions and peak oxidant is considered to

be proportional to total basinwide hydrocarbon emissions

The fact is that the middotemitted contaminants from which the smog is formed

and the effects which characterize that smog are not evenly distributed throughout

the Los Angeles Basin in other words the basin area under the inversion is not one

large box filled to all corners with homogeneously distributed air contaminants and

photochemical smog

Refutation of Big Box Myth

Examination of atmospheric contaminant concentrations refutes the big box

concept It is found for example that concentrations of djrectly emitted contam -

inants measured at a particular sampling site reflect the emissions within a rather

limited area around that site For this reason contaminant concentration levels

vary from one location to another and each has a characteristic daily pattern which

reflects the daily pattern of emissions in that area

middot 236

The big box concept is further refuted by the fact that peak concentrations

of carbon monoxide and oxides of nitrogen in areas of high traffic density were

fairly static prior to 1966 Thus they did not reflect the 45-50 per cent growth

in motor vehicle registrations and gasoline consumption which occurred in Los

Angeles County between 1955 and 1965 and which caused comparable increases in

total daily emissions of such vehicle-related contaminants This demonstrates

that growth was outward rather than upward so that a larger area of the County

began to be affected by photochemical smog but no area experienced smog ofJ

greater severity than that originally affected by smog formed from the vehicular

emissions which accumulated each weekday in central Los Angeles and were trans-

1 I

ported later that day to the San Gabriel Valley

1 Meteorological Evidence

To verify the geographical dependence of emissions and resulting atmospheric

concentrations let us examine the meteorology of these large areas of Southern

California Both the County and the Basin have many meteorological sub-regions

in which the patterns of wind speed and direction may be similar but within

which the patterns of air transport are parallel with those of adjacent sub-regions

and the respective air parcels do not ever meet or join

The characteristic patterns of inversion height and wind speed and direction

in these sub-regions and their patterns of vehicular emissions together have

created a network of source areas- -those in which the reactant contaminants accu -1T

i ~ mulate in the morning and begin to react--and related receptor areas--those to which

~ the products and associated effects of the photochemical reactions of the contamshy)

inants originally emitted in the source areas are carried by the late morning and

237 middot

afternoon winds ( sea breeze)

Wind-flow patterns show that characteristic patterns of transport for related

source area-effect area combinations are separate and parallel not mixing or

joining Each source area has its own reactor pipeline to its own effect area

or areas

To illustrate this source area-effect area relationship the typical flow of

polluted air from downtown Los Angeles to Pasadena was selected as a worst

case situation for in-depth examination Figure 4 shows that the air in downtown

Los Angeles on the morning of smoggy days moves directly from the central area

to Pasadena

Vehicular traffic is the predominant emission source in both downtown Los

Angeles and Pasadena Thus the air in each locality should contain CO Also

since oxidant would form in the air parcel moving from Los Angeles to Pasadena

oxidant levels would be expected to be higher in Pasadena than in downtown Los

Angeles

Figure 5 shows these relationships for the period 1960-1972 The atmosshy

pheric CO level is similar for the two areas while oxidant levels were higher in

Pasadena than in Los Angeles throughout this time period This demonstrates

that a significant amount of oxidant formed in the air as it moved to Pasadena

containing both the unreactive CO and the photochemical reactants for producing

oxidant Both CO and oxidant show a marked downward trend in each locality since

1965 which emphasizes the effect of vehicle exhaust controls and the correlation

between the localities

238

On a day which is favorable to the formation and accumulation of photoshy

chemical smog a contaminated air parcel normally originates during the

6-9 a m period on a weekday from an area of dense traffic centered just

south and west of Downtown Los Angeles It is oxidant generated within that air

parcel which usually affects Central Los Angeles and the West San Gabriel

middotK IJ l J

Valley area around Pasadena

The traffic area in which this smog had its origin is about the most dense

in Los Angeles County and has been so for the past 25-30 years No area

has a higher effective density thampn-this Using carbon monoxide which

1

is almost entirely attributable to motor vehicles as an indicator of such emis-

sions it is found that the concentrations of emitted vehicular contaminants

middotr i

measured in Central Los Angeles during the past 15 years confirms both this lack

of change in effective density and the absence of any area of any greater effective

density when local differences in inversion are acknowledged

This area the Central Source Area is depicted in Figure 4 The size

and shape of the Central Source Area was ch~sen to be large enough to reduce to

an insignificant level any diffusion or transport into this area from any externally

l generated reactants This conclusion is based in part on the trajectory studies

previously referenced as well as an analysis of the diffusion and transport parashy

meters for the area

239

The Central Source Area has been identified as that geographical region

which contributes essentially all of the primary contaminant emissions giving

rise to the highatmospheric oxidant levels in the West San Gabriel Valley

The proportion of emissions in the CSA due to motor vehicles and that due to

stationary sources is shown in Table 1 For the County as a whole about 80 per

cent of _(6-9) AM reactive hydrocarbons are due to motor vehicle emissions and this

figure rises to 90 per cent for the CSA The same conclusion a pp lies to NOx

emissions The Central Source Area contains the greatest density of vehicle traffic

in the County and thus the greatest density of source emissions Thus it appears

that the source area with the highest density of emissions during the critical (6-9)

AM period is responsible for the highest afternoon oxidant levels observed in Los

A i1geles County and in the South Coast Air Basin These highest oxidant levels

are consistently observed to occur in the San Gabriel Valley This is true whether

the LAAPCD or the ARB oxidant calibration procedure is used

Further the atmospheric concentrations of the primary pollutants can be

identified as originating primarily from the motor vehicle and they reflect the

effects of the motor vehicle emission control program A vehtcular source area

can be identified by its atmospheric levels of CO and NOx Figure 6 compares

measured atmospheric levels with calculated atmospheric levels for CO NOx

and the CONOx ratio in the downtown area

TABLE 1 240

REACTIVE HYDROCARBON EMISSIONS

(6-9) AM

1970

LOS ANGELES COUN1Y middot CENTRAL SOURCE AREA middot SOURCE TONS PER CENT TONS PER CENT

Mobile 1260 81 3 135 91 2

Stationary 290 187 1 3 88

Total 1s~o 1000 148 1000

By 7 -Mode Gallonage

241

The calculated values shown in Figure 6 were derived from a baseline

survey of 1100 vehicles and continued surveillance tests both using the Calishy

fornia 7-Mode test cycle The baseline survey showed that motor vehicles withshy

out exhaust control systems had average exhaust emissions concentrations of 3 4

per cent CO and 1000 parts per million of NOx Baseline emissions data apply

to 1965 and earlier model vehicleg and surveillance data to 1966 and later modelsmiddot

Since it can be concluded from calculations and observations that the dilushy

tion of auto exhaust emissions in the atmosphere on a smoggy day in Los Angeles

is approximately 1000 to 1 the calculated values for CO and NOx prior to 1965 are

34 ppm CO and 1 ppm NOxo After 1965 the changing effect of controlled vehicles

in the total vehicle population is reflected in the calculated values

CO and NOx values measured in the atmosphere are also shown in Figure

6 and confirm the values calculated entirely as diluted vehicular emissions NOx

concentrations measured in the atmosphere tend to be consistently a little lower

than the calculated values probably because photochemical reactions remove some

NOx from the system

The data for CO and NOx calculated and measured show that emissions in

downtown Los Angeles originate almost exclusively from motor vehicles and that

atmospheric concentrations there reflect the average emissions from a representashy

tive vehicle population

The ARB has recently published a report entitled A Trend Study of Two

Indicator Hydrocarbons in the South Coast Air Basin Acetylene was used as a

242

specific indicator of automobile exhaust emissions and it was found to have de-

clined in concentration in the Los Angeles atmosphere at an annual rate of 12 5

per cent since 1970 To quote from this report The California implementation

plan requires an annual average reduction in these emissions (reactive organic

compounds) of 166 tons per day or 11 1 of the 1970 tonnage per year The per cent

reductions in the_ acetylene levels at Los Angeles and Azusa are greater than reshy

quired by the implementation plan Since acetylene is almost entirely associated

J with auto exhaust this demonstrates that the motor vehicle emission control

program is achieving its purpose

To summarize at this point it has been deomonstrated that high oxidant values

are due to motor vehicular emissions of NOx and HC because

NOx and HC are the principal reactants in the oxidant formation process

and they originate primarily from motor vehicle emissions and

The highest oxidant values are recorded in_ effect areas that receive air

from source areas where motor vehicles are clearly identified as the

dominant source of NOx and HC

243

Future Control Strategy

The APCD strategy for achieving and maintaining the oxidant air quality

standard is based upon the fact that high oxidant values are due to motor ve-

hicle emissions of hydrocarlxms arrl nitrogen oxides This strategy is as follows

1 Both Hydrocarbon and Nitrogen Oxides Emissions Must Be Considered To Achieve the Federal Oxidant Standard

There is wide agreement that NOx and HC are the principal reactants in

the oxidant formation process and that vehicular emissions are a major source

of NOx HC and CO

2 Effective Regulation of Atmospheric Concentrations of Both HC and NOx and of the Ratio Between Them is necessary for Attainment of the Federal Air Quality Standard for Oxidant

Basmiddoted on the abundance middotof available experimental evidence it is our firm

position that the most rational approach to solving the photochemical oxidant smog

problem in the South Coast Air Basin (SCAB) is to control the quantities of emissions

from motor vehicles of both smog precursors--Hcmiddot and NOx--their resulting atmosshy

pheric concentrations and the ratios between both contaminants which will result

from these controls

We arc also convinced that the oxidant and nitrogen dioxide air quality stanshy

dards can and will be met not by 1975 or 1977 but by the early 1980 s if the emisshy

sion control program as originally outlined by Ca~ifornia or a slight modification

of it proposed by the District is followed and enforced This should also provide

for continued compliance with these air quality standards at least through 1990

244

It will also allow time for a reappraisal in about 1978 of the whole situation relative

to the ultimate emission standards required and the best approach to their impleshy

mentation

Calculation of the degree of control necessary to attain the air quality

~ standards for oxidant and nitrogen dioxide involves indirect complex methods 1

aimed at determ_ining the degree of control of the primary contaminants directly

emitted by automobiles

The following evidence supports our proposed solution to the problem in

terms of both the atmospheric concentrations of the oxidant precursors NOx

and HC the ratio between them as reflected in their exhaust emission standards

and the resulting atmospheric concentrations of oxidant which comply with the air

quality standards

Chamber Results and Projections to the Atmosphere

The importance of environmental chamberwork cannot be minimized the

j need for and direction of the whole emission control program was based initially

j on the results of chamber experiments In order to understand the importance to

air quality of achieving both the correct low quantities of emissions and the right

ratio we can present several graphic portrayals of analyses of experimental labshy

oratory work together with their relationship to past present and future air quality

in terms of both morning primary reactant concentrations during the morning

traffic peak and the equivalent emissions which would produce them

245

Figure 7 shows maximum ozone levels that were obtained by irradiating

varying amounts of auto exhaust hydrocarbons and oxides of nitrogen in an environshy

mental chamber The corresponding ozone levels then can be found for any comshy

bination of BC and NOx concentrations Thus high ozone is produced with high

emissions of both hydrocarbons and oxides of nitrogen and low oxidant is formed with

low emissions However either low NOx or low HC emissions11 can also produce

low oxidant--graphic and clear evidence of the importance of the NOxHC ratio in

ozone formation Furthermore each and every possible combination of values for

NOx and HC has then a corresponding characteristic maximum chamber ozone

concentration

Using this graph we can estimate what ozone levels would result if certain

atmospheric mixtures of NOx and HC could be injected into the chamber and

irradiated Such estimates were made for 1960 and 1965 using atmospheric data

rlThe points labeles 1960 and 65 show the location of the highest levels of both

HC and NOx found in the air in those years in Downtown Los Angeles (OOLA) area

during the 6-9 AM traffic peak

It has been demonstrated by use of CO and NOx data and CONOx ratios

hnw well the characteristics of vehicle emissions are reflected in the atmosphere

We know what emissions from the average vehicle were then in 1960-1965 both

for HC and NOx so that we can mathematically relate emissions to atmospheric

concentrations for those years and so for future years also knowing or calculating

only what the characteristic emissions will be from the average vehicle

246

The NOx concentrations stayed about the same from 1960 through 1965 because

average vehicle emissions of that contaminant did not change during that time

Mobile source emissions can be shown to have contributed essentially all of this obshy

served result However blow by controls did reduce emissions of HC and the

concentrations dropped accordingly In 1965 the last year before exhaust controls

the point 65 indicates where we were then in terms of maximum ozone formation

to be expected in a chamber with the highest HC and NO concentrations found in the X

air that year Levels of ozone actually measured in the atmosphere however

are higher than those shown on the graph for high NOx and I-IC concentrations for

those years up to the present

The strategy to meet the oxidant standard is obvious--get atmospheric NOx

and HC concentrations out of the area on the chart that produces high ozone levels

and put them in tie areas with the lowest levels This can only be done by implementshy

ing appropriate emission standards

As can be seen that did not happen between 1965 and 1970 because manufacshy

turers used controls on new cars in California which while causing a decrease in

BC (and CO) allowed a large increase in NOx emissions Thus the path line of

the atmosphere on the chart goes up from 65 and diagonally to the left passing

through an area of higher ozone levels The atmospheric concentrations of oxidant

predictably increased during the years 1967 and 1968 By 1970 they dropped to lower

levels - -back to about the same as in 1965- -exactly as predicted by the model The

app14oximate location of the point for 1970 (70) was both predicted on the basis of

247

the mathematical model and confirmed by atm-ospheric measurements of

[)owntown Los Angeles morning summertime NOx and calculated HC values

Again it should be pointed out that those points show the highest possible

concentrations of NOx and HC Years with less restrictive weather conditions

(for accumulating high primary contaminant levels) would cause lower measured

maximum NOx and HC levels but the calculations would still yield the points

shown Thus we are taking the most pessimistic view

Future Projections

In 1973 we were at about the point labeled 73 and ozone levels were beginshy

ning to drop as expected middot It should be emphasized that ozone values plotted on

thi$ graph are for the chamber only- -not the atmosphere The future path the

points 7 4 and on to 90 represents our estimate of future atmospheric levels of

NO and BC expected if the exhaust emission standards are just met While that X -

is optimistic it is all we really can do since performance of future vehicle models

is unknown We will achieve maximum ozone levels at or below the standard by

about 1980-1985 This will only be true however if cars in compliance with the

California interim standards for HC and NOx continue to be added to the vehicle

population at the normal rate These standards provide the optimum ratio of NO X

to HC necessary to provide the nitric oxide (NO) needed for the reaction that re-

moves from the air both oxidant formed photochemically and oxidant which occurs

as natural background which alone may cause the standard to be exceeded This

ratio is about 112 or 2 parts NOx to 1 part HC

248

The optimum NOxHC ratio is a key element in the APCD strategy but will

require a finite time for its attainment Replacement of older cars by newer ones

equipped to meet the most stringent standards is the only reasonable mechanism

which can change it VMT reduction proposed as a prime strategy by EPA cannot

change this crl(ical ratio which is a basic characteristic of the population at any

given time

Validation of the Districts Control Strategy

Figure 8 compares (1) future chamber oxidant levels based upon the

future maximum concentrations of HC and NOx we expect each year with the

California control program (2) calculated atmospheric concentrations using ~ I

our chamber-to-atmasphere empirical translation and (3) actual measured atmos-f 1l pheric oxidant maxima This clearly sets forth the relationship among these three

factors

The chamber concentrations (lower curve) middotare the lowest values shown

The actual atmospheric data (points connected by heavy dotted and solid lines)

vary considerably from year to year partly because of the vagaries of the weather

In all cases the atmospheric oxidant values are higher than the chamber values

because of the addition of vehicle emissions as the air parcel travels from source

to receptor areas The calculated atmospheric data (thin dashed and solid curves)

are shown to be the highest generally exceeding or equalling the actual measured

data and of course always exceeding the chamber data Thus the model paints

the most pessimistic picture possible It can be seen that by about 19801 1985 atmos -

pheric levels should be at or below the Federal air quality standard of 0 08 ppm oxidant

249

3 Motor Vehicle Exhaust Control is the Only Requirement for Achieving the Oxidant Standard by 1980

We can show that the existing motor vehicle control program has resulted

in a significant reduction of oxidant concentrations in the air

The foregoing material explained the relationship between vehicula~ emis -

sions in source areas and the high oxidant levels measured in effect areas This

relationship is exemplified by the downward trend of oxidant levels in the atmosshy

phere and by the similar year-by-year trends of NO and HC emissions from the X

average motor vehicle A projection of these vehicle emissions factors shows that

the associated maximum oxidant level in the atmosphere will meet the oxidant standard

by about 1980-1985

Figure 9 compares by year the number of days that the oxidant air quality

standard was exceeded in three separate areas with the average NO and HC emissions X

per vehicle mile To comply with the air quality regulations the number of days that

this standard is exceeded must be reduced to one per year

The lines plotted on Figure 9 show that a definite relationship exists between

the emissions from the average motor vehicle and the number of days each year that

the oxidant concentration in the air exceeds the clean air standard

The oxidant trendlines for downtown Los Angeles Pasadena arrl Azusa are

all downward and the slopes are about the same This similarity is logical because

the process that results in the suppression of oxidant accumulation simply has been

displaced from one area to another This was a unique one time situation because

of the increase in NOx between 1966 and 1971 After 1971 all areas are down Thus

l

250

the same conclusion is reached that the oxidantstandard will be met in the 1980s

I whether air quality data or vehicle emissions trends are projected middot~ Ul-

This outlook is based on the APCD s belief that future growth in both the

Los Angeles area and SCAB will not create any locality with a traffic density greater

than any traffic density in the area to date For the past 25 years the area around

downtown Los Angeles has been the area of maximum traffic density and therefore

the emissions source area responsible for the maximum effect area measurements

It is assumed that the traffic density in any future source area will be no

greater than the traffic density in downtown Los Angeles Thus since the

vehicular emissions control program will achieve and maintain the air quality

standards in areas affected by vehicular emissions from downtown Los Angeles it

will also achieve and maintain them for any area of SCAB

Summary Conclusions and Recommendations

In conclusion we have shown that a source and effect area analysis of emisshy

sions and resulting oxidant is a more reasonable and accurate representation of

the Los Angeles area for air quality analysis than gross integration metho9s such

as the big box technique It has been shown that motor vehicles are the major and

almost sole contributor to the primary HC and NOx emissions in the downtown source

area which results in the high oxidant levels in the San Gabriel Valley in fact the

highest in SCAB An air quality model and vehicle emissions control strategy has

been suggested to meet the oxidant standard by mid-1980 s

251

We have shown that

bull Only by adjusting the ratio of NOxHC in the motor vehicle emissions to

permit accumulation of sufficient atmospheric NO to sea venge the normal

atmospheric background oxidant can the standard be attained

bull The APCD strategy which provides for implementation of the present

California interim emissions standards for NOx HC and CO for new

motor vehicles in California beginning with the 1975 model vehicles will

result in compliance with the CO N02 and oxidant air quality standards

by the mid 1980 s and will maintain this compliance until 1990 and

possibly longer

bull The effectiveness of the present California motor vehicle control program

is easily demonstrable using air quality data from several areas in Los

Angeles County 1960-1973

bull To assure achievement and maintenance of the air quality goals as now preshy

dicted there must be periodic assessments of the effectiveness of the

motor vehicle control program followed by corrective actions if necessary

What has been accomplished thus far is significant but much more remains

to be done so that the best possible representation of emissions and resulting air

quality may be available for use in this air basin A much better emission inventory

defining the spatial and temporal distribution of both mobile and stationary sources

is needed Better statbnary source information is needed to evaluate the local

effects of these emissions Further detailed studies are needed to establish the

252

true relationship between emissions data from vehicle test cycles and the actual

operation of vehicles neither the 7-mode nor the CVS procedure provides a true

representation of actual vehicle operation Further tracer studies to assess the

transport and dilution of mobile and stationary source emissions from selected

source areas are also needed

253

1111

IUD

a CC I w gt-

1111

1UO

IUD

I 990

IDJO

1180

1111

IUO

FIGURE I

HYDROCARBONS

STATIONARY SOURCES MOTOR VEHICLES

- --

8 12 II 20 742 2l IS 12 I 4

HUNDREDS

HYDROCARBON EMISSIONS STATIONARY SOURCES IN

OXIDES OF

0

OF TONSDAY

FROM MOTOO VEHICLES AND LOS ANGELES COUNTY

NITROGEN

STATIONARY SOURCES

MOTOR VEHICLES

011111111111111111110111bull1111111

IIIIIIHIIIIIIIIIHIUII

llillL Its rd

l1uu~111111u1111111

2 I O 1 J 3

HUND REDS OF TONSDAY

OXIDES OF NITROGEN EMISSIONS FROM MOTOR VEHICLES ANO STATIONARY SOURCES IN LOS ANGELES COUNTY

illl~ -~--~ i~-=i _J~l ~--~ bull_~L- I ~~~-~~--Z ~

6

6S-66 ox

ICS ~A~1 M

i ssmuwmmgt

bullI

e COROyent_

64 ~ IDB RIVERS~

ORAJfD

-

t t 10 miles

bullmiddotsame Avg Cone Both Years

Pigare 2

YEAR OP HIGHEST OXlDANI CONCENTRATIONS

Highest Average of Daily -Maiimum One-Hour Concentrations

During July August amp September 1963-1972

bullLj

I

64

70 s11 3RlU)U0

70

--__ 69bull

N V +=

middot Source Air Resources Board

-200o

t t 10 adlea

tDS ampIJtsect

-1~

-1611ASampXllmiddot bull - bull -z----~------

I ldmmprwJ

IIVERSIDI

~ - 70

OampY -1 U 70 bull L

I

N V1 V

middot-i___

-----------------------------------------------------------i----------------------------

Figure 3

CHANGE OP OXIDANT CONCENTRATIONS

Percent Change from the Highest Three-Year Average to the 1970-72 Average

Of Daily Maximum One-Hour Con~entrationa for JulY August amp September

Source Air Resources Board

256

FIGURE 4 TYPICAL FLOW OF POLLUTED Am PARCEIS CIUGINATING AT DIFFERENT LOCATIONS IN THE LOS ARE~S BASIN - STARTIOO 0900 PST

l I

OAT

TRAJECTORY SUWMATIOl4

----- SMOG ~AVS

I

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullNONbullSlfOG DAYS

ISTARTING Tl~ cgxpsy

~ HAW

(CA

257

FiGURE 5 ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AND OXIDANT IN DOWlflC1N LOS AIDELES (SOURCE AREA) AND PASADENA (EFFECT AREA) 1

1960-1972

LO CARBON MONOXIDE

30

Pasadena

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullbullbullbullbull Downtown Los Angeles

20

10

o_______________________________

OXIDANT

)

2 Down~ Los Angeles

1

o________________________ 1960 1962 196L 1966 1968 1970 1972

YEAR

bullbullbullbullbull

bullbullbullbullbullbullbull

258

FIGURE 6 COMPARISON 01 CALCULATED AND MEASURED ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AN1) OXIDES OF NITROOEN IN DCMNTOWN IDS AIJELES

196o-1972

CARBON MONOXIDE

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ~ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot _-- ---_ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ----middotmiddot-bullw-_~ ---bullbullbull

10

o_______________1111111_____

OXIDES OF NITROGEN25

20

15 bullbullbullbullbullmiddotmiddotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~

1-i 10 middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ---

oS o_______________________

RATIO CONOx

40

50

0 +raquo Cd

p 30

~ 20

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot bullbullbullbullbull middotmiddotmiddotmiddotmiddot-shybullbullbullbullbull 0 u

bullbullbullbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot 10

0 j

ilI 196o 1964 1968 1970 1972 I

YEAR

Measured~D-owntown Los Angeles (90th percentile ofmiddot daily] instantaneous maxima)

Calculated - Aver~ge vehicle emissions - Present control program

259

FIGURE 7

25

t i5

flJ

~ on ~ ~ Q) bO 100 Jo

+gt on z

o5

EFFECT OF CALIFORNIA 1 s AUTO EXHAUST CONTROL ffiOORA M ON MAXIMUM CHAMBER OZONE CONCENTRATION

- PPM

357bullbull

r 76 bull

11 l

30

20

CHAMBER OZONE MAXIMUM

50

10

o___________111111111111______111111111111_____________

0 05 10 15 20 25

Hydrocarbons m-2 (LB-15) - PPM (as Hexane)middot

--

bull bull bull

r--=--~1 ~a==-~ - _~l ~ y--===-- ~~--~-- ~ r---~~

o

o8

~ I

~ 0 H 8 o6 I

c~ ~ 0 z 0 0

8

~ o+ A H gtlto-

02

middoto

Figure 8 Calculated t1ax1mum Levels Instantaneous and Hourly Average

of Atmospheric Oxidant Compared to Measured Los Angeles County Maxima-with Projections to 1990

(California Standards)

~ -Calculated Inst ax ~

f Calculate Max Hr Avg 03

_ bullbull _ _ - i bull

0 bullbull -l bullbull a0Ieasured Inst Lax o3 bull middotmiddotmiddot~bull 0bull _ ____ V ~ ea~ured ~ Hr Avr o3

~~ r---

~ ~ NB r~ima for 197 4 amiddots of 121074--- -_ Chamber Ozone F ~_ _~

- 1L_

~ Federal Primarfo Air ~uality Standard ~6- -UaximumT- our Avera~elr~ppm-------------- --~ ------- -~- -~-- ~

I I I I I I I I I I I I I I I I I N1 O

1960 6i 64 66 ~i middot-o 72 74 76 79 middotso middot92 84 bullg s9 9o

TBAR (end)

0

261 FIGURE -OMPARISON OF ATMOSPHERIC OXIDANT TRENDS WITH AVERAGE NCJx AND

HC EMISSIONS (Grams per Mile from Average Vehicle)

JOO Number of days state oxidant standara wds equalled or exceeded

--- Azusa __ Pasadena ________ Downtown Los Angeles

20

15 u

___ Hydroc_arbons Oxides of Nitrogenbullmiddotmiddotmiddotmiddotmiddotbullbullmiddot 1975 and later-assume middotcalifornia ARB standards

o_ ___________________________11111____

1965 1970 1975middot 198omiddot 198S 1990

142

penalties as estimated by the National Academy of Sciences are small 3

or less in going to the 1977 standards This estimate does assume further

advancements by the auto industry to improve fuel economy--primarily

improved exhaust gas recirculation systems It is unfortunate that this

issue of fuel economy has become so mixed up with the air pollution question

because the two are only slightly related If one is really concerned about

fuel economy and there isnt too much evidence that the auto industry or

the American public really is too concerned right now there is only one

way to have a drastic effect on fuel economy and that is to decrease the

vehicle weight Until that is done with gains on the order of 50 or

more to worry about 3 or 5 differences in fuel economy related to emission

control systems is simply to focus upon the wrong issue

Now what are the problem areas What remains to be done The

problems certainly arent over with the introduction of the 1975 vehicles

Problem Area Number One Field performance What is going to happen

to these vehicles when they get into actual service Past experience with

the 1971 through 1973 vehicles has been rather poor in that EPA and

California surveillance data show that these vehicles are not meeting the

standards Many of them did not meet the standards when they were new

The situation in general is getting worse at least for CO and hydrocarbons

that is with time the emission levels of CO and hydrocarbons for the 1971 I through 1973 vehicles is degrading There is no in-service experience of

this sort with the 1975 vehicles yet The certification data look quite I promising but the test procedures especially for durability are not ithe same as what occurs in actual use It is generally stated that the

1actual use situation for the catalysts will be more severe than the EPA

test procedure A larger number of cold starts are involved in actual use

than in the EPA test procedure and thermal cycling will probably have an

143

adverse effect on the lifetime of the cata]_yst This is not so obvious

It is also likely that the higher temperature duty cycle in actual use will

improve the performance of the catalyst in that it will help to regenerate

the catalyst through the removal of contaminants as long as one does not

get into an overheat situation The National Academy of Sciences estimate

was that the number of catalyst failures tn the first 50000 miles would

be on the order of about 7 Thats a very difficult number to estimate in

the absence of any real data A 7 failure still leaves a net gain in

emissions control even if nothing is done about this failure This points

to the problem of what happens after 50000 miles The EPA certification

procedure and control program only addresses the first 50000 miles The

second 50000 miles or slightly less for the average car is the responsishy

bility of the states Unfortunately then~ seems to be very little progress

in the area of mandatory inspection and ma-Lntenance--very little thought

being given to whether the replacement ofthe catalyst at 50000 miles

if it has failed is going to be required and how that is going to be

brought about The area of field performance remains a major problem

area one which obviously needs to be monitored as the California Air

Resources Board has been doing in the past but probably even more carefully

because the unknowns are higher with the catalyst systems

Problem Area Number Two Evaporative hydrocarbons from automobiles

It was identified at least 18 months ago that the evaporative emission

control systems are not working that the evaporative emissions are on the

order of 10 times greater than generally thought In the Los Angeles

area cars which are supposed to be under good evaporative emissions

controls are emitting approximately 19 grams per mile of hydrocarbons

through evaporation This apparently has to do with the test procedure used

144

The EPA is pursuing this The California Air Resources Board does have some

consideration going on for this but it appears that the level of activity

in resolving this problem is simply not adequate If we are to go ahead

to 04 of a gram per mile exhaust emissions standards for hydrocarbons

then it just doesnt make sense to let 19 grams per mile equivalent escape

through evaporative sources

Problem Area Number Three What about the secondary effects of the

catalyst control systems Specifically this is the sulfate emissions

problem and I really do not know the answer to that Our appraisal is

that it is not going to be an immediate problem so we can find out what

the problem is in time to solve it The way to solve it now since the

automobile industry is committed to catalysts and it is unreasonable

to expect that they will reverse that technology in any short period of

time is take the sulfur out of the gasoline The cost of removing sulfur

from gasoline is apparently less than one cent per gallon Therefore if

it becomes necessary to be concerned with sulfate emissions the way to

meet the problem is to take the sulfur out of gasoline Obviously sulfate

emissions need to be monitored very carefully to see what happens The

final appraisal is certainly not now available Another secondary effect

of the catalysts is the introduction of significant quantities of platinum

into an environment where it hasnt existed before Not only through

exhaust emissions which appear to be small but also through the disposal

problem of the catalytic reactors Since the quantity of platinum involved

is quite small the argument is sometimes used that platinum does not

represent much of a problem The fact that the amount of platinum in the

catalyst is so small may also mean that its not economical to recover it

This is probably unfortunate because then the disposal of these catalysts

l Jj

145

I becomes important I will not speak to the medical issues because

am not qualified The evidence is that theuro~ platinum will be emitted in a

form which does not enter into biological cycles--but this is no assurance

that it couldnt later be transformed in such a form What is obviously

needed is a very careful monitoring program which hopefully was started

before the catalysts were put into service If it wasnt then it should

be started today

Problem Area Number Four NO control The big problem with NO X X

control is that nobody seems to know or to be willing to establish what

the emission control level should be It is essential that this be tied

down rapidly and that it be fixed for a reiatively long period of time

because the NO level is going to have a VE~ry important ef feet upon the X

development of advanced engine technology The 20 gm level has been

attained in California with some loss of fuel economy through the use of

EGR and it is not unreasonable in our estimation to go to 15 grams per

mile with very little loss in fuel economy To go to 04 gram per mile

with present technology requires the use of one of two catalytic systems

either the reduction catalyst in tandem with the oxidation catalyst or what

is known as the three-way catalyst Both of these systems require technoshy

logical gains The state of development appears to be roughly that of the

oxidation catalyst two years ago The auto industry will probably say

that it is not quite that advanced but that if it were required to go to

04 gram per mile in 1978 that it could be done With the catalyst systems

the fuel economy penalties would not be great in fact the improvement to

the engine which would be required to make the system work would again

probably even allow a slight improvement in fuel economy What the 04

gram per mile NO catalyst system would appear to do however is to X

146

eliminate the possibility of the introduction of stratified charge engines

both the CVCC and the direction injection system and also diesel engines

It is in the context of the advantages of these advanced engines to meet

emission standards with improved fuel economy that one should be very

cautious about the 04 grammile oxides of nitrogen standards for automoshy

biles My own personal opinion is that the number should not be that

stringent that a number of 1 or 15 gm is appropriate Such a level

would require advancements but would not incur great penalties

Other items which I view as problem areas are less technically

involved and therefore require fewer comments

bull Nonregulated pollutants--again thls is a matter of keeping track

of particulates aldehydes hydrocarbon composition to make

certain that important pollutants ire not being overlooked or

that emission control systems are not increasing the output of

some of these pollutants

bull Fuel economy The pressures of fuel economy are going to be used

as arguments against going ahead wlth emissions control Mostly

these two can be resolved simultaneously We should simply ask

the automobile industry to work harder at this

bull Final problem area New fuels Again it does not appear that

the introduction of new fuels will come about as an emissions

control approach but that they may be introduced because of the

changing fuel availability patterns and the energy crisis These

fuels should be watched carefully for their impact upon emissions

This does middotappear to be an area in which a great deal of study is

going on at the present time It is one problem area perhaps in

which the amount of wprk being done is adequate to the problem

which is involved

147

In sunnnary then the appraisal of the 1975 systems is that they are

a big advancement they will be a lot better than most of us thought and

that we should give the automobile industry credit for the job theyve

done in coming up with their emissions control systems

With that boost for the auto industry which Im very unaccustomed

to Ill entertain your questions

-------=-~ ~~~ U- ~a1

~_~a--~-~ -J~ ~ -~r- _ --=~-- -___ja--~ __1~~ ~-~----=

AIR

1-4 FUEL----1

I I ENGINE

I II

_________ EXHAUST SYSTEM I bull EXHAUST

I I I

+ MIXTURE CONTROL COMBUSTION MODIFICATION EXHAUST TREATMENT

FuelAir Metering Ignition Air Jnjection FuelAir Mixing Chamber Geometry Thermal Reactor Fuel Vaporization Spark Timing Oxidation Catalyst Mixture Distribution Staged Combustion Reduction Catalyst Fuel Characteristics Ex tern almiddot Combustion Three Way Catalyst Exhaust Gas Redrculation Particulate Trap

FIGURE 1 Approaches to the Control of Engine Emissions

~ i 00

149

TABLE I

Average Emissions of 1975 Certification Vehicles (As Corrected Using the 50000-Mile Deterioration Factor)

Emissions in gmi Fraction of Standard HC CO NO HC CO NO

Federal 1975 X X

AMC 065 67 25 043 045 080

Chrysler 074 77 25 049 051 082

Ford 081 92 24 054 061 078

GM 083 80 23 055 053 074

Weighted Average 080 82 24 053 055 076

California 1975

AMC 042 49 17 047 054 087

Chrysler 048 61 16 053 067 082

Ford 052 56 13 058 062 067

GM 065 55 16 0 72 061 082

Weighted Average 058 56 16 064 062 078

kWeighted average assumes the following market shares AMC 3 Chrysler 16 Ford 27 and GM 54

150

TABLE II

Total Number of Vehicles Certified for California 1975 Standard and the Number (and percentage) of These Able to Meet

Certain More Stringent Standards

Calif 1975 Federal 1977 Hypothesized Hypothes ized 099020 04J420 049020 093420

i ~

Manufacturer no () no () no () no ()

AMC 16 (100) 1 ( 6) ti ( 38) 3 (19)

Chrysler 21 (100) 2 ( 9) ( 33) 0 ( O)

Ford 26 (100) 4 (15) -middot ( 15) 5 (19)

l GM 46 (100) 1 ( 2) -1 ( 9) 5 (11)

Foreign 62 (100) 21 (34) 3H (61) 28 (45)

1J

f

-l

151

CURRENT STATUS OF ALTERNATIVE AUTOM)BIIE ENGINE TECHNOLCXY

by

Henry K Newhall Project Leader Fuels Division

Chevron Research CanpanyRicbmmd California

I

iH1middot

10 1ntroduction and General Background

I

11 General

The term stratified ct1arge englne has been used for many

years in connection with a variety of unconventional engine

combustion systems Common to nearly all such systems is

the combustion of fuel-air mixtures havlng a significant

gradation or stratification in fuel- concentration within the

engine combustion chamber Henee the term nstratifled charge

Historically the objective of stratified charge engine designs

has been to permit spark ignition engine operation with average

or overall fuel-air ratios lean beyond the ignition limits of

conventional combustion systems The advantages of this type

of operation will be enumerated shortly Attempts at achieving

this objective date back to the first or second decade of this

century 1

More recently the stratified charge engine has been recognized

as a potential means for control of vehicle pollutant emissions

with minimum loss of fuel economy As a consequence the

various stratified charge concepts have been the focus of

renewed interest

152

12 Advantages and Disadvantages of Lean Mixture Operation

Fuel-lean combustion as achieved in a number of the stratified

charge engine designs receiving current attention has both

advantages and disadvantages wnen considered from the comshy

bined standpoints of emissionsmiddot control vehicle performance

and fuel economy

Advantages of lean mixture operation include the following

Excess oxygen contained in lean mixture combustion

gases helps to promote complete oxidation of hydroshy

carbons (HG) and carbon monoxide (CO) both in the

engine cylinder and in the exhaust system

Lean mixture combustion results in reduced peak

engine cycle temperatures and can therefore yield

lowered nitrogen oxide (NOx) emissions

Thermodynamic properties of lean mixture combustion

products are favorable from the standpoint of engine

cycle thermal efficiency (reduced extent cf dissociashy

tion and higher effective specific heats ratio)

Lean mixture operation caG reduce or eliminate the

need for air throttling as a means of engine load

control The consequent reduction in pumping losses

can result in significantly improved part load fuel

economy

153

Disadvantages of lean mixture operation include the following

Relatively low combustion gas temperatures during

the engine cycle expansion and exhaust processes

are inherent i~ lean mixture operation As a conseshy

quence hydrocarbon oxidation reactions are retarded

and unburned hydrocarbon exhaust emissions can be

excessive

Engine modifications aimed at raising exhaust temperashy

i tures for improved HC emissions control (retarded middot~

ignition timing lowered compression ratlo protrtacted combustion) necessarily impair engine fuel economy1 I

1j bull If lean mixture operation is to be maintained over ~

the entire engine load range maximum power output t l and hence vehicle performance are significantly

impaired

Lean mixture exhaust gases are not amenable to treatshy

ment by existing reducing catalysts for NOx emissions

control

Lean mixture combustion if not carefully controlled

can result in formation of undesirable odorant

materials that appear ln significant concentrations

in the engine exhaust Diesel exhaust odor is typical

of this problem and is thought to derive from lean mixshy

ture regions of the combustion chamber

154

Measures required for control of NOx emissions

to low levels (as example EGR) can accentuate

the above HC and odorant emissions problems

Successful developmentmiddotor the several stratified charge

engine designs now receiving serious attention will depend

very much on the balance that can be achieved among the

foregoing favorable and unfavorable features of lean comshy

bustion This balance will of course depend ultimately on

the standards or goals that are set for emissions control

fuel economy vehicle performance and cost Of particular

importance are the relationships between three factors -

UBHC emissions NOx emissions and fuel economy

13 Stratified Charge Engine Concepts

Charge stratification permitting lean mixture operation has

been achieved in a number of ways using differing concepts

and design configurations

Irrespective of the means used for achieving charge stratifishy

cation two distinct types of combustion process can be idenshy

tified One approach involves ignition of a small and

localized quantity of flammable mixture which in turn serves

to ignite a much larger quantity of adjoining or sur~rounding

fuel-lean mixture - too lean for ignition under normal cirshy

cumstances Requisite m1xture stratification has been achieved

155

in several different ways rangiDg from use of fuel injection

djrectly into open combustion chambers to use of dual

combustion chambers divided physically into rich and lean

mixture regions Under most operating conditions the

overall or average fuel-air ratio is fuel-lean and the

advantages enumerated above for lean operation can be realized

A second approach involves timed staging of the combustion

process An initial rich mj_xture stage in which major comshy

bustion reactions are completed is followed by rapid mixing

of rich mixture combustion products with an excess of air

Mixing and the resultant temperature reduction can in

principle occur so rapidly that minimum opportunity for NO

formation exists and as a consequence NOx emissions are

low Sufficient excess air is made available to encourage

complete oxidation of hydrocarbons and CO in the engine

cylinder and exhaust system The staged combustion concept

has been specifically exploited 1n so-called divided-chamber

or large volume prechamber engine designs But lt will be

seen that staging is also inherent to some degree in other

types of stratified charge engines

The foregoing would indicate that stratified charge engines

can be categorized either as lean burn engines or staged

combustion engines In reality the division between conshy

cepts is not so clear cut Many engines encompass features

of both concepts

156

14 Scope of This Report

During the past several years a large number of engine designs

falling into the broad category of stratified charge engines

have been proposed Many of these have been evaluated by comshy

petent organizations and have been found lacking in one or a

number of important areas A much smaller number of stratified

charge engine designs have shown promise for improved emissions

control and fuel economy with acceptable performance durashy

bility and production feasibility These are currently

receiving intensive research andor development efforts by

major organizations - both domestic and foreign

The purpose of this report is not to enumerate and describe the

many variations of stratified charge engine design that have

been proposed in recent years Rather it is intended to focus

on those engines that are receiving serious development efforts

and for which a reasonably Jarge and sound body of experimental

data has evolved It is hoped that this approach will lead to

a reliable appraisal of the potential for stratified charge

engine systems

20 Open-Chamber Stratified Charge Engines

21 General

From the standpoint of mechanical design stratified charge

engines can be conveniently divided into two types open-chamber

and dual-chamber The open-chamber stratjfied charge engine

has a long history of research lnterest Those crigines

157

reaching the most advanced stages of development are probably

the Ford-programmed c~mbustion process (PROC0) 2 3 and Texacos

controlled combustion process (TCCS) 4 5 Both engines employ a

combination of inlet aar swirl and direct timed combustion

chamber fuel injection to achieve a local fuel-rich ignitable

mixture near the point of ignition _For both engines the overshy

all mixture ratio under most operating conditions is fuel lean

Aside from these general design features that are common to

the two engiries details of their respective engine_cycle proshy

cesses are quite different and these differences reflect

strongly in comparisons of engine performance and emissions

characteristics

22 The Ford PROCO Engin~

221 Description

The Ford PROCO engine is an outgrowth of a stratified charge

development program initiated by Ford in the late 1950s The

development objective at that time was an engine having dieselshy

like fuel economy but with performance noise levels and

driveability comparable to those of conventional engines In

the 1960s objectives were broadened to include exhaust

emissions control

A recent developmental version of the PROCO engine is shown in

Figure 2-1 Fuel is injected directly into the combustion chamber

during the compression stroke resulting in vaporjzation and

formation of a rich mixture cloud or kernel in the immediate

158

vicinity of the spark plug(s) A flame initiated in this rich

mixture region propagates outwardly to the increasingly fuelshy

lean regions of the chamber At the same time high air swirl

velocities resulting from special orientation of the air inlet

system help to promote rapid mixing of fuel-rich combustion

products with excess air contained in the lean region Air

swirl is augmented by the squ1sh action of the piston as it

approaches the combustion chamber roof at the end of the comshy

pression stroke The effect of rapid mixing can be viewed as

promoting a second stage of cori1bustion in which rlch mixture

zone products mix with air contained in lean regions Charge

stratification permits operation with very lean fuel-air mixshy

tures with attendent fuel economy and emissj_ons advantages In

addition charge stratification and direct fuel injection pershy

mit use of high compression ratios with gasolines of moderate

octane quality - again giving a substantial fuel economy

advantage

Present engine operation includes enrichment under maximum

power demand conditions to mixture ratios richer than

stoichiometric Performance therefore closely matches

that of conventionally powered vehicles

Nearly all PROCO development plans at the present time include

use of oxidizing catalysts for HC emissions control For a

given HC emissions standard oxidizing catalyts permit use

of leaner air-fuel ratios (lower exhaust temperatures)

1

l

159

together with fuel injection and ignition timing charactershy

istics optimized for improved fuel economy

222 Emissions and Fuel Economy

Figure 2-2 is a plot of PROCO vehicle fuel economy versus NOx

emissions based or1 the Federal CVS-CH test procedure Also

included are corresponding HC and CO emissions levels Only

the most recent test data have been plotted since these are

most representative of current program directions and also

reflect most accurately current emphasis on improved vehicle

fuel economy 6 7 For comparison purposes average fuel

economies for 1974 production vehicles weighing 4500 pounds

and 5000 pounds have been plotted~ (The CVS-C values

reported in Reference 8 have been adjusted by 5 to obtain

estimated CVS-CH values)

Data points to the left on Figure 2-2 at the o4 gmile

NOx level represent efforts to achieve statutory 1977

emissions levels 6 While the NOx target of o4 gmile was

met the requisite use of exhaust gas recirculation (EGR)

resulted in HC emissions above the statutory level

A redefined NOx target of 2 gn1ile has resulted in the recent

data points appearing in the upper right hand region of

Figure 2-2 7 The HC and CO emissions values listed are

without exhaust oxidation catalysts Assuming catalyst middotl

conversion efficiencies of 50-60 at the end of 50000 miles

of operation HC and CO levels will approach but not meet

160

statutory levels It is clear that excellent fuel economies

have been obtained at the indlcated levels of emissions

control - some 40 to 45 improved re1at1ve to 1974 produc-

tj_on vehicle averages for the same weight class

The cross-hatched horizontal band appearing across the upper

part of Figure 2-2 represents the reductions in NOx emissions

achieveble with use of EGR if HC emissions are unrestricted

The statutory 04 gmile level can apparently be achieved

with this engine with little or no loss of fuel economy but

with significant increases in HC emissions The HC increase

is ascribed to the quenching effect of EGR in lean-middotmixture

regions of the combustion chamber

223 Fuel Requirements

Current PROCO engines operated v1ith 11 1 compression ratio

yield a significant fuel economy advantage over conventional

production engines at current compression ratios According

to Ford engineers the PROCO engine at this compression

ratio j_s satisfied by typical fu1J-boi1ing commercial gasoshy

lines of 91 RON rating Conventional engines are limited to

compression ratios of about 81 and possibly less for

operation on similar fuels

Results of preliminary experiments indicate that the PROCO

engine may be less sensitive to fuel volatility than convenshy

tional engines - m1 important ff1ctor in flextb1 llty from the

standpoint of the fuel supplier

161

224 Present Status

Present development objectives are two-fold

Develop calibrations for alternate emissions target

levels carefully defining the fueleconofuy pbtenshy

tial associated with each level of emissions control

Convert engine and auxiliary systems to designs

feasible for high volume production

23 The Texaco TCCS Stratified Charge Engine

231 General Description

Like the Ford PROCO engine Texacos TCCS system involves_

coordinated air swirl and direct combustion chamber fuel

injection to achieve charge stratification Inlet portshy

induced cylinder air swirl rates typically approach ten times

the rotational engine speed A sectional view of the TCCS

combustion chamber is shown in Figure 2-3

Unlike the PROCO engine fuel injection in the TCCS engine

begins very late in the compression stroke - just before th~

desired time of ignition As shown in Figure 2-4 the first

portion of fuel injected is immediately swept by the swirling

air into the spark plug region where ignition occurs and a

flame front is established The continuing stream of injected

fuel mixes with swirling air and is swept into the flame

region In many respects the Texaco process resembles the

162

spray burning typical of dj_esel combustion ~r1th the difshy

ference that ignition is achieved by energy from an elec-

tric spark rather than by high compression temperatures

The Texaco engine like the diesel engine does not have a

significant fuel octane requirement Further use of positive

spark ignition obviates fuel I

cetane requirements character-

istic of diesel engines The resultant flexibility of the

TCCS engine regarding fuel requirements is a si~1ificant

attribute

In contrast to the TCCS system Fords PROCO system employs

relatively early injection vaporization and mixing of fuel

with air The combustion process more closely resembles the

premixed flame propagation typical of conventional gasoline

engines The PROCO engine therefore has a definite fuel

octane requirement and cannot be considered a multifuel

system

The TCCS engine operates with hi__gh compression ratios and

with little or no inlet air throttling except at idle conshy

ditions As a consequence fuel economy is excellent--both

at full load and under part load operating conditions

232 Exhaust Emissions and Fuel Economv

Low exhaust temperatures characteristlc of the TCCS system

have necessitated use of exhaust oxidation catalysts for

control of HC emissions to low lf~Vels A11 recent development

163

programs have therefore included use of exhaust oxidation

catalysts and most of the data reported here r~present tests

with catalysts installed or with engines tuned for use with

catalysts

Figures 2-5 and 2-6 present fuel economy data at several

exhaust emissions levels for two vehicles--a US Army M-151

vehicle with naturally aspirated 4-cylinder TCCS conversion

and a Plymouth Cricket with turbocharged 4-cylinder TCCS

engine 9 10 1urbocharging has been used to advantage to

increase maximum power output Also plotted in these figures

I are average fuel economies for 1974 production vehicles of

similar weight 8

I When optimized for maximum fuel economy the rrccs vehicles

can meet NOx levels of about 2 gmile It should be noted

that these are relatively lightueight vehicles and that

increasing vehicle weight to the 4000-5000 pound level could

result in significantly increased NOx emissions Figur~s 2-5

and 2-6 both show that engine modifications for reduced NOx

levels including retarded combustion timing EGR and increased

exhaust back pressure result in substantial fuel economy

penalties

For the naturally aspirated engine reducing NOx emissions

from the 2 gmile level to O l~ gmile incurred a fuel

economy penalty of 20 Reducing NOx from the tllrbocharged

164

engine from 15 gmile to 04 gmile gave a 25 fuel economy

penalty Fuel economies for both engines appear to decrease

uniformly as NOx emissions are lowered

For the current TCCS systems most of the fuel economy penalty

associated with emissions control can be ascribed to control

of NOx emissions although several of the measures used for

NOx control (retarded cornbusticn timing and increased exhaust

back pressure) also help to reduce HG emissions HC and CO

emissions ari effectively controlled with oxidation catalysts

resulting in relatively minor reductions in engine efficiency

233 TCCS Fuel Reauirements

The TCCS engine is unique among current stratified charge

systems in its multifuel capability Successful operation

with a nuraber of fuels ranging from gasoline to No 2 diesel

Table 2-I

Emissions and Fuel Economy of Turbocharged TCCS Engine-Powered Vehicle 1

Fuel

Emissions gMile 2 Fuel Economy

mng 2HC co NOx

Gasoline

JP-4

100-600

No 2 Diesel

033

026

014

027

104

109

072

J bull l ~

-

061

050

059

060

197

202

213

230

1M-151 vehicle 8 degrees coffibustion retard 16 light load EGR tw0 catalysts (Ref 10)

2 CVS-CH 2750 pounds tnert1a welght

165

l

has been demonstrated Table ~-I lists emissions levels and

fuel economies obtained with a turbocharged TCCS-powered

M-151 vehicle when operated on each of four different fuels 10

These fuels encompass wide ranges in gravity volatjlity

octane number and cetane leve 1 as middotshown in Table 2-II

Table 2-II

Fuel Specifications for TCCS Emissions Tests (Reference 10)

Gravity 0 API Sulfur

OFDistillation~

Gasolj_ne 100-600 JP-4 No 2

Diesel

88 -

86 124 233 342 388

0024 912

-

486 012

110 170 358 544 615

0002 57 356

541 0020

136 230 314 459 505

-middot --

369 0065

390 435 508 562 594

--

lta 9

IBP 10 50 90 EP

TEL gGal Research Octane Cetane No

Generally the emissions levels were little affected by the

wide variations in fuel properties Vehicle fuel economy

varied in proportion to fuel energy content

As stated above the TCCS engine is unique in its multifuel

capability The results of Tables 2-I and 2-II demonshy

strate that the engine has neither 8ign1ficant fuel octane

nor cetane requirements and further that it can tolerate

166

wide variations j_n fuel volati1tty rhe flexibility offered

by this type of system could be of major importance in

future years

234 Durability Performance Production Readiness

Emissions control system durability has been demonstrated by

mileage accumulation tests Ignltion system service is more

severe than for conventional engines due to heterogeneity of

the fuel-air mixture and also to the high compression ratios

involved The ignition system has been the subject of

intensive development and significant progress in system

reliability has been made

A preproduction prototype engine employing the TCCS process is

now being developed by the Hercules Division of White Motors

Corporation under contract to the US Army Tank Automotive

Command Southwest Research Inr)titute will conduct reliability

tests on the White-developed enGines when installed in Military

vehlcles

30 Small Volume Prechambcr Eng1nes (3-Valve Prechamber Engines Jet Ignition Engines Torch Ignition Engines)

31 General

A number of designs achieve charge stratification through

division of the combustion region into two adjacent chambers

The emissions reduction potentiampl for two types of dualshy

chamber engines has been demonstrated F1 rst ~ j n B desJgn

trad1t1on~JJy caJJld the nrreebrnber engine a 2m211 auxil1ary

167

or ignition chamber equipped w1th a spark plug communicates

with the much larger main combustion chamber located in the

space above the piston (Figure 3-1) The prechamber which

typically contains 5-15 of the total combustion volume

is supplied with a small quantity of fuel-rich ignitable

fuel-air mixture while a large quantity of very lean and

normally unignitable mixture is applied to the main chamber

above the piston Expansion of high temperature flame

products from the prechamber leads to ignition and burning

of the lean maj_n chamber fuel-a_r charge Ignitionmiddot and

combustion in the lean main chamber region are promoted both

by the high temperatures of prechamber gases and bythe

mixing that accompanies the jet-like motion of prechamber

products into the main chamber

I jl

I i j

I

Operation with lean overall mixtures tends to limit peak comshy

bustion temperatures thus minimizing the formation of nitric

oxide Further lean mixture combustion products contain

sufficient oxygen for complete oxidation of HC and CO in the

engine cylinder and exhaust system

It should be reemphasized here that a iraditional problem

with lean mixture engines has been low exhaust temperatures

which tend to quench HC oxidation reactions leading to

excessive emissions

Control of HC emissions to low levels requires a retarded or

slowly developing combustion process The consequent extenshy

sion of heat release j nto 1ate porttt)ns of the engtne cycle

168

tends to raise exhaust gas temperatures thus promoting

complete oxidation of hydrocarbons and carbon monoxide

32 Historical Background and Current Status

321 Early Developm9nt Objectives and Engine Def igns

The prechamber stratified charge engine has existed in various

forms for many years Early work by Ricardo 1 indicated that

the engine could perform very efficiently within a limited

range of carefully controlled operating conditions Both

fuel-injected and carbureted prechambcr engines have been

built A fuel-injected design Lnittally conceived by

Brodersen 11 was the subject of extensive study at the

University of Rochester for nearly a decade 12 13 Unforshy

tunately the University of Rochester work was undertaken prior

to widespread recognition of the automobile emissions problem

and as a consequence emission characteristics of the

Brodersen engine were not determined Another prechamber

engine receiving attention in the early 1960s is that conshy

ceived by R M Heintz 14 bull The objectives of this design

were reduced HC emissions incr0ased fuel economy and more

flexible fuel requirements

Experiments with a prechamber engine design called the torch

ignition enginen were reported n the USSR by Nilov 15

and later by Kerimov and Mekhtier 16 This designation

refers to the torchlike jet of hot comhust1on gases issuing

169

from the precombustion chamber upon j_gnj_ tion In a recent

publication 17 Varshaoski et al have presented emissions

data obtained with a torch ignition engine These data show

significant pollutant reductions relative to conventional

engines however their interpretation in terms of requireshy

ments based on the Federal emissions test procedure is not

clear

l

3 2 2 Current DeveloJ)ments

A carbureted middotthree-valve prechamber engine the Honda CVCC

system has received considerable recent attention as a

potential low emissions power plant 18 This system is

illustrated in Figure 3-2 Hondas current design employs a

conventional engine block and piston assembly Only_ the

cylinder head and fuel inlet system differ from current

automotive practice Each cylinder is equipped with a small

precombustion chamber communicating by means of an orifice

with the main combustion chambe situated above the piston lj

ij_ A small inlet valve is located in each precharnber Larger

inlet and exhaust valves typical of conventlonal automotive

practice are located in the main combustion chamber Proper

proportioning of fuel-air mixture between prechamber and

main chamber is achieved by a combination of throttle conshy

trol and appropriate inlet valve timing A relatively slow

and uniform burning process gjvjng rise to elevated combusshy

tion temperatures late in the expansion stroke and during

the exhaust procezs is achieved H1 gh tewperaturr--s in thin

part of the engine cycle ar-e necessary to promote complete

170

oxidation of HC and CO It si1ould be no~ed that these

elevated exhaust temperatures are necessarily obtained at

the expense of a fuel economy penalty

To reduce HC and CO emissions to required levels it has been

necessary for Honda to employ specially designed inlet and

exhaust systems Supply of extremely rich fuel-air mixtures

to the precombustion chambers requires extensive inlet manifold

heating to provide adequate fuel vaporization This is accomshy

plished with a heat exchange system between inlet and exhaust

streams

To promote maximum oxidation of HC and CO in the lean mixture

CVCC engine exhaust gases it has been necessary to conserve

as much exhaust heat as possible and also to increase exhaust

manifold residence time This has been done by using a relashy

tively large exhaust manifold fitted with an internal heat

shield or liner to minimize heat losses In additj_on the

exhaust ports are equipped with thin metallic liners to

minimize loss of heat from exhaust gases to the cylinder

head casting

Engines similar in concept to the Honda CVCC system are under

development by other companies including Ttyota and Nissan

in Japan and General Motors and Fo~d in the United States

Honda presently markets a CVCC-powered vehicle tn tTapan and

plans US introduction in 1975 Othe~ manufactur~rs

includlnr General Motors and Forgtd 1n thr U S havf~ stated

171

that CVCC-type engines could be manufactured for use in limited

numbers of vehicles by as early as 1977 or 1978

33 Emissions and Fuel Economywith CVCC-Type Engines

331 Recent Emissions Test Results

Results of emissions tests with the Honda engine have been very

promising The emissions levels shown in Table 3-I are typical

and demonstate that the Honda engine can meet statutory 1975-1976

HC and CO stindards and can approach the statutory 1976 NOx

standard 19 Of particular importance durability of this

system appears excellent as evidenced by the high mileage

emissions levels reported in Table 3-I Any deterioration of

l emissions after 50000 miles of engine operation was slight

and apparently insignificant

I Table 3-I

Honda Compound Vortex-Controlled Combustion-Powered Vehicle 1 Emissions

Fuel Economy

Emissions 2 mpg gMile 1972

HC 1975 FTP FTPco NOv

210 50000-Mile Car+ No 2034 Low Mileage Car 3 No 3652 018 212 221089

024 065 198 1976 Standards

213175 20o41 34 - -04o411977 Standards 34 - -

1Honda Civic vehicles 2 1975 CVS C-H procedure with 2000-lb inertia weight3Average of five tests aAverage of four tests

172

Recently the EPA has tested a larger vehicle conve~ted to the

Honda system 20 This vehicle a 1973 Chevrolet Impala with

a 350-CID V-8 engine was equipped with cylinder heads and

induction system built by Honda The vehicle met the present

1976 interim Federal emissions standards though NOx levels

were substantially higher than for the much lighter weight

Honda Civic vehicles

Results of development tests conducted by General Motors are

shown in Table 3-II 21 These tests involved a 5000-pound

Chevrolet Impala with stratified charge engine conversion

HC and CO emissions were below 1977 statutory limits while

NOx emissions ranged from 15 to 2 gmile Average CVS-CH

fuel ec9nomy was 112 miles per gallon

Table 3-II

Emissions and Fuel Economy for Chevrolet Impala Strmiddotatified

Charge Engine Conversion (Ref 21)

Test

Exhaust Emlssions

gMile 1 Fuel

Economy mpgHC co NOx

1 2 3 4 5

Average

020 026 020 029 0 18

023

25 29 31 32 28

29

17 15 19 1 6 19

17

108 117 114 109 111

112

1cvs-CH 5000-lb inertia weight

173

I

332 HC Control Has a Significant Impact on Fuel Economy

In Figure 3-3 fuel economy data for several levels of hydroshy

carbon emissions from QVCC-type stratified charge engines

are plotted 22 23 ~ 24 At the 1 gmile HC level stratified

charge engine fuel economy appears better than the average

fuel economy for 1973-74 production vehicles of equivalent

weight Reduction of HC emissions below the 1-gram level

necessitates lowered compression ratios andor retarded

ignition timing with a consequent loss of efficiencymiddot For

the light-weight (2000-pound) vehicles the O~ gmile IIC

emissions standard can be met with a fuel economy of 25 mpg

a level approximately equal to the average of 1973 producshy

tion vehicles in this weight class 8 For heavier cars the

HC emissions versus fuel economy trade-off appears less

favorable A fuel economy penalty of 10 relative to 1974

production vehicles in the 2750-pound weight class is

required to meet the statutory 04 gmile HC level

333 Effect of NOx Emissions Control on Fuel Economy

Data showing the effect of NOx emissions control appear in

Figure 3-~ 22 These data are based on modifications of a Honda

CVCC-powered Civic vehicle (2000-pound test weight) to meet

increasingly stringent NOx standards ranging from 12 gmile

to as low as 03 gmile For all tests HC and CO emissions

are within the statutory 1977 standards

NOx control as shown in Figure 3-4 has been effected by use

of exhaust gas recirculation 1n comb1nation w1th retarded

174

ignj_tion timing It is clear that control of rmx emissions

to levels below l to 1 5 gmile results in stgnificant fuel

economy penalties The penalty increases uniformly as NOx

emissions are reduced ~nd appears to be 25 or more as the

04 gmile NOx level is approached

It should be emphasized that the data of Fisure 3-4 apply

specifically to a 2000-pound vehicle With increased vehicle

weight NOx emissions control becomes more difficult and the

fuel economy penalty more severe The effect of vehicle

weight on NOx emissions is apparent when comparing the data

of Table 3-I for 2000-pound vehicles with that of Table 3-II

for a 5000-pound vehicle While HC and CO emissio~s for the

two vehicles are roughly comparable there is over a factor

of two difference in average NOx emissions

34 Fuel Requirements

To meet present and future US emissions control standards

compression ratio and maximum ignltion advance are limited

by HC emissions control rather than by the octane quality of

existing gasolines CVCC engines tuned to meet 1975 California

emissions standards appear to be easily satisfied with

presently available 91 RON commercial unleaded gasolines

CVCC engines are lead tolerant and have completed emissions

certification test programs using leaded gasolines However

with the low octane requirement of the CVCC engine as noted

above the economic benefits of lead antlknock compoundt ar-euromiddot

not realized

175

It is possible that fuel volatLLity characteristlcs may be of

importance in relation to vaporization within the high

temperature fuel-rich regions of the prechamber cup inlet

port and prechamber iQlet manifold However experimental

data on this question aomiddot not appear to be available at

present

~O Divided-Chamber Staged Combustion Engines (Large-Volume Prechamber Engines Fuel-Injected Blind Prechamber Engines)

41 General

Dual-chamber engines of a type often called divided-chamber

or large-volume prechamber engines employ a two-stage comshy

bustion process Here initial r~ich mixture combustion and

heat release (first stage of combustion) are followed by rapid

dilution of combustion products with relatively low temperature

air (second stage of combustion) The object of this engine

design is to effect the transitjon from overall rich combustion

products to overall lean products with sufficient speed that

time is not available for formation of significant quantities

of NO During the second low temperature lean stage of

combustion oxidation of HC and CO goes to completion

An experimental divided-chamber engine design that has been

built and tested is represented schematically in Figure ~-1 25 26

A dividing orifice (3) separates the primary combustion

chamber (1) from the secondary combustion chamber (2) which

includes the cylinder volume above the piston top A fuel

injector (4) supplies fuel to the primary chamber only

176

Injection timing is arranged such that fuel continuously

mixes with air entering the primary chamber during the

compression stroke At the end of compression as the

piston nears its top center position the primary chamber

contains an ignitable fuel-air mixture while the secondary

chamber adjacent to the piston top contains only air

Following ignition of the primary chamber mixture by a spark

plug (6) located near the dividing orifice high temperature

rich mixture combustion products expand rapidly into and mix

with the relatively cool air contained in the secondary

chamber The resulting dilution of combustion products with

attendant temperature reduction rapidly suppresses formation

of NO At the same time the presence of excess air in the

secondary chamber tends to promote complete oxidation of HC

and CO

42 Exhaust Emissions and Fuel Economy

Results of limited research conducted both by university and

industrial laboratories indicat~ that NOx reductions of as

much as 80-95 relative to conventional engines are possible

with the divided-chamber staged combustion process Typical

experimentally determined NOx emissions levels are presented

in Figure 4-2 27 Here NOx emissions for two different

divided-chamber configurations 8re compared with typical

emissions levels for conventional uncontrolled automobile

engines The volume ratio 8 appearing as a parameter in

Figure 4-2 represents the fraction of total combustion volume

contained in the primary chamber For a values approaching

I

i J_

177

1

05 or lower NOx emissions reach extremely low levels Howshy

ever maximum power output capability for a given engine size

decreases with decreasing 6 values Optimum primary chamber

volume must ultimately_represent a compromise between low

emissions levels and desired maximum power output

HC and particularly CO emissions from the divided-chamber

engine are substantially lower than eonventional engine

levels However further detailed work with combustion

chamber geometries and fuel injection systems will be necesshy

sary to fully evaluate the potential for reduction of these

emissions

i Recent tests by Ford Motor Company show that the large volume

prechamber engine may be capable of better HC emissions conshy

trol and fuel economy than their PROCO engine This is shown

by the laboratory engine test comparison of Table 4-I 19

Table 4-I

Single-Cylinder Low Emissions middot11 ~ _____En____g__~ne __middot _e_s_-_s_____

Engine

NO--X Reduction

Method

Em1ssions g1 hp-Hr

Fuel Economy

Lb1 hp-HrNOv HC- co

PROCO

Divided Chamber

PROCO

Divided Chamber

EGR

None

EGR

None

10 30

10 04

05 ~o

o J_o 75

130

25

l 1i bull 0

33

0377

0378

0383

0377

178

Fuel injection spray characteristics are critical to control

of HC emissions from this type of engine and Fords success

in this regard is probably due in part to use of the already

highly developed PROCO-gasoline injection system Figure 4-3

is a cutaway view of Fords adaptation of a 400-CID V-8 engine

to the divided-chamber system 2 e

Volkswagen (VW) has recently published results of a program

aimed at development of a large volume precharnber engine 29

In the Volkswagen adaptation the primary chamber which comshy

prises about 30 of the total clearance volume is fueled by a

direct timed injection system and auxiliary fuel for high

power output conditions is supplied to the cylinder region by

a carburetor

Table 4-II presents emissions data for both air-cooled and

water-cooled versions of VW s dtvided-middotchamber engine 3 0

Emissions levels while quite low do not meet the ultimate

1978 statutory US standards

179

Table 4-II

Volkswagen Jarge Volume _Jrechamber Er[ Lne Emissions

Exhaust Emissions

_ _gMile 1

___E_n_gi_n_e__t--H_C___c_o__N_O_x____E_ng__i_n_e_S_p_e_c_i_f_i_c_a_tmiddot_1_middoto_n_s__

20 50 09 841 compression ratio Air-Cooled 16-Liter

prechamber volume 28 of total clearance volume conventional exhaust manishyfold direct prechamber fuel injection

20-Liter 10 40 10 91 compression ratio Water-Cooled prechamber volume 28 of

total clearance volume simple exhaust manifold reactor direct prechamber fuel injection

1cvs c-H

Toyota also has experimented wlth ___a large volume prechamber

engine using direct prechamber fuel injection and has

reported emissions levels comparable to those of Table 4-II 31

43 Problem Areas

A number of major problems inherent in the large volume

prechamber engine remain to be 3olved I~ These problems include the following II

Fuel injection spray characteristics are critically

important to achieving acceptable HC emissions

The feasibility of producing asatisfactory injecshy

tion system hasnot been estab1ished

180

Combustion noise due to high turbulence levels and

hence high rates of heat release and pres[-ure rise

in the prechamber can be excessive It has been

shown that the-noise level can be modified through

careful chamber design and combustion event timing

If the engine is operated with prechamber fuel

injection as the sole fuel source maximum engine

power output is limited This might be overcome

by a~xiliary carburetion of the air inlet for maximum

power demand or possibly by turbocharging Either

approach adds to system complexity

The engine is charmiddotaeter1zed by low exhaust temperatures

typical of most lean mixture engines

References

1 Ricardo H R Recent Research Work on the Internal Combustion Engine 11 SAE Journal Vol 10 p 305-336 (1922)

2 Bishop I N and Simko A Society of Automotive Engineers Paper 680041 (1968)

3 Simko A Choma M A and Repco L L Society of Automotive Engineers Paper 720052 (1972)

4 Mitchell E Cobb JM and Frost R A Society of Automotive Engineers Paper 680042 (1968)

5 Mitchell E Alperstein M and Cobb JM Society of Automotive Engineers Paper 720051 (1972)

6 1975-77 Emission Control Program Status Report submitted to EPA by Ford Motor Company November 26 1973

181

if

7 consultant Report on Emissions Control of Engine Systems National Academy of Sciences Committee on Motor Vehicle Emissions Washington DC September 1974

8 Austin T C and Hellman K H Society of Automotive Engineers Paper 730790 (1973)

9 See Ref 7

10 Alperstein M Schafer G H and Villforth F J Iiil SAE Paper 740563 (1974)

11 US Patent No 2615437 and No 2690741 Method of Operating Internal Combustion Engines Neil O Broderson Rochester New York

12 Conta L~ D and Pandeli American Society of Mechanical Engineers Paper 59-SA-25 (1959)

13 Canta L D and Pandeli American Society of Mechanical Engineers Paper 60-WA-314 (1960)

14 US Patent No 2884913 0 Internal Combustion Engine R Mi Heintz i

15 Nilov N A Automobilnaya Promyshlennost No 8 (1958)

l 16 Kerimov N A and Metehtiev R I Automobilnoya Promyshlennost No 1 p8-11 (1967)

17 Varshaoski I L Konev B F and Klatskin V B Automobilnaya Promyshlennost No 4 (1970)

18 An Evaluation of Three Honda Compound Vortex Controlled Combustion (CVCC) Powered Vehicles Report B-11 issued by Test and Evaluation Branch Environmental Protection Agency December 1972

19 Automotive Spark Ignition Engine Emission Control Systems to Meet Requirements of the 1970 Clean Air Amendments report of the Emissions Control Systems Panel to the Committee on Motor Vehicle Emissions National Academy of Sciences May 1973

20 An Evaluation of a 300-CID Compound Vortex Controlled Combustion (CVCC) Powered Chevrolet Impala Report 74-13 DWP issued by Test and Evaluation Branch Environmental Protection Agency October 1973

21 See Ref 7

22 See Ref 7

23 See Ref 7

24 See Ref 7

182

25 Newhall H K and El-Messiri I A Combustion and Flame 14 p 155-158 (1970)

26 Newhall H K and El-Messiri I A Society of Automotive Engineers Transaction Ford 78 Paper 700491 (1970)

27 El-Messiri I A and Newhall H K Proc Intersociety Energy Conversion Engineering Conference p 63 (1971)

28 See Ref 7

29 Decker G and Brandstetter W MTZ Motortechnische Zeitschrift Vol 34 No 10 p 317-322 (1973)

30 See Ref 7

31 See Ref 7

183

Fig 2-1 FORD PROCO ENGINE

l

Ford Proco Engine Fuel Economy and Emissions _ 15 _ f--1

00 +

I ~ x X gt( X _ x A 7- ~ X x~ ~c - l4catalyst Feed u NOx vs ruel Econ with 1 C0-71 CJ) 14 x x Ynn H( RP c tr ir-t irm vltgtZ G I HC - C0-127 _ A txcessve c

13 Approx W EG R

~ C~~r 351 CID 5000 Lb Inertia Weight

Q 21 A L 0 u w II _j

LJ =gt LL

10

35i CD 4500 Lb Inertia Weight

~ 1974 Production Average Fuel Economy

4 soo _b r-r-r-----z~lt_~~---7--_~--r--1r-7-r1--~-rz7-w~~

150 0 0 Lb PU221ufrac122-1 I

LO 20 30

NOx EMISSIONS-GMSMILE (CVS-CH) Revised216174

0

HKN 71074

Fig 2-2

l

~___-~ ~--=---~ ~=---__---~1 f-=-----1__middot-_~J ~-----------1 ~bull-=-=- (-~-~ LJii-ZJj ~ ~~-~ ~~ -__c~~ 1--~~ ~----~--1 ---------s___-c--1 ~~~-~~~bull r~~-~--middot1 ____c__ J~ p- ~

Texaco TCCS Engine

Shrouded Intake Valve

~ Intakemiddot r~ )p__-- Fuel Nozzle Fuel Nozzte Port ~ -- -yen -_~

X f -J J ( ~1 I --- ~ f middotmiddotj_Ja 1(~-~_ frff 1-Cylinderv~ v_ r--L~ I (~~)J ~- Intake 1 - ------L- middotmiddot - middotmiddot -1 H0 ad middot --- - -- 1 Po rt I 1 I ~~ ) ~ ~ ~~~ -A- I ------

- I _ ---_ ~ P1ston-mgt-lt_ffrac12 T_77~~~--1 i- r_-~J N

- ~- i~-L - _ _ - IExhaust - - I ~ - 1-_ r- bullsect ~ ----lt_ ~ I PortJ~bJ lt 7A--7~ ~1 ~j --~ ~ yl ind er

-__~lli- klmiddot ~ro v_t_gt11J1bull Bti Or K__ - middot ~

I t--tL pgt-- Ultmiddot middot- - Spark Plugr- -1 --U2middot- ~-~

LHorizont al Projections of Nozzle and Spark Plug Centerlines

Fig 2-3 i--1 00 U1

---~---~-~ -------c- --~--- 7middot-r---c-- ~- -~~~==---~~~~~- srsr RZIIEF7 11t111-~-----==-----=-~--~-~~---c=rmiddot=

OPEN CHAMBER TYPE STRATI Fl ED CHARGE ENGINE i-shyCj

DIRECTIONAl~Fsw7 Q

NOZZLE P

I

~J~treg lt-_(__(lt-(11

c_-- _7- -

SPARK PLUG_ l 1__- -_ - l --_ ~ ----__ lt_ lt_ -- --

ltlt_I_--- _

~ gt - _____- -- --~ ~-l_- 1_~ -~- ~ ------

~~~ r_I FUEL SPRAY 2 FUEL-AIR MIXING ZONE ~- _ -------

FLAME FRONT AREA 4 COMBUSTION PRODUCTS

TCCS COMBUSTION SYSTEM

Fig 2-4

3

----==-----~ l~~----bulli r-~ ~-----=-- 1 ~~ ~ -~ ~~ ___-_=gt---l p--- --=-=-_-__71-~-~~ 1-0-- --=---=-- 4 L--_-_-~ P--- ~

25

-c u

f

Cl) 24 gt u _

tgt 23a ~

I

gt-~ 220 2 0 u w 21 _J

lJJ gt LL

2

Texaco TCCS Powered Cricket Vehicle

Max Econ Setting gt A L07 HC

141 CID JQf CR 084 CO 2500 Lb Inertia Wgt

50-so Retard_ 0_73 HC

12 co 051 HC ~ 061 HC

085COA 064CO Retard+ ESPRetard+

EGR

036 HC ~ 115 co Retard +ESP+ EGR

04 06 08 10 12 14 16 18 20 NOx EMISSIONS-GMSMILE (CVS-CH) HtltN1110114

I- 00 -JFig 2-5

-~ ~=- ~ - -i______c_J ~-====c= wr=- ~-~ p--w~~~ rr w -

25

-c u

I

(f)

gt u-lt a_

2

gt-I 20

~ 0 z 0 u LLI

_J

w tJ_

15

I- CJ) CJ)

Turbocharged Texaco TCCS Ml51 Vehicle

Max Econ Adjustment_ HC-3J catalyst Feed C0-70

141 CID 10~1 CR 2750 Inertia Weight 8deg Retard ~

~bull HC-3middot2 catalyst Feed ~~ _ C0-64

_ 5deg Retard HC-0 30 8degRetard LowEGV bullco-11 ~bull HC-3middot6 catalyst Feed WIW21

Med EGR C0-67 1974 Production 33 Average Fuel Economy ~

COmiddoti05 (2750Lb)

I

bull HC-035 co- 141 13deg Retard High EGR

04 10 20 NOx EMISSIONS -GMSMILE (CVS-CH) ~~ts~b~~~74

Fig 2-6

189

Fig 3-1

PRECHAMBER TYPE STRATIFIED CHARGE ENGINE

r Inlet

(Fuel-lean Mixture )

I 0 I

Spark -Prechamber (Fuel-rich mixture)

-Main Chamber

1] HON DA CVCC ENGINE CONCEPT

190

Fig 3-2 Honda CVCC Engine

28 -l u

1

UJ 26 -gt u-(9 CL 24 2-

f

gtshy0gt

22 z ~ _)

u w

20 _J

w ~ LL

18

J= ---- 4 --~~-_----a ~~ _-_bull --~~ 1~~1 ltiil~I ~ ~-r~ ~ -~ ~-~ ~J~-iii-1 ~~1 s _-_ __-

Fuel Economy vs HC Emissions for 3-Valve Prechamber Engines

e NOx-14 15 Liter

bull Honda CVCC 2000 LbsNOx - 12 A Datsun NVCCbull15 Liter

bull ~JOx -09 A 2500 Lbs J LL 1ter NOv -15

2750 Lbs -NOx -17

- I AiJOx -12

0 02 04 06 08 LO 0HYDROCARBON EMiSSlmiddotONS - Glv1 I MILE (CVS-CH) I-

Fig 3-3

J--1

1--Fuel Economy vs NOx Emissions IO N

-- for Honda CVCC Powered Vehiclesr 26 u

l VHc-023 U1 gt umiddot 24_-__

(_IJ o_

~ 22 l

gt-5~-0 z 20 C0-200 u A HC-033w I co -3o_j

_A HC-029w 18 J I C0-27 LL

_ HC-025

HC-017 co -2-3

C0-22

0 -- 02 04 06middot 08 10 12 NOx Ef11SSIONS -GlviS MILE (CVS-CH)

Fig 3-4 middot

I

I

i93

J J

Fig 4-1 Divided Chamber Engine

middot(4) Fuel Injector

1

f J

f ff

f

~ Ii

I f

i

I f ] [

~~

0 0 0 0

i ~ I

1jl

194

E Cl 0

C QJ

CJl 0 _

-1-

z

0

Vl (lJ

-0

X 0

-t-J

V1 ro c X

LLI

Fig ~-2

COMPARISON OF CONVENTIONAL AND DIVIDED COMBUSTION CHAMBER NOx EMISSIONS

5000 MBT Ignition Timing Wide Open Ttl rattle

4000 Conventional Charnber

3000

J = fraction of Total Combustion 2000 Volume in Primary Ct1arnber

Divided Chamber 13 = 0 85

1000

Divided Chamber fo = 0 52

05 06 0 7 08 09 10 11

O~erall Fuel-Air Equivalence Ratio

195

196

AIRBORNE SURVEYS IN URBAN AIR BASINS IMPLICATIONS FOR MODEL DEVELOPMENT

by

Donald L Blumenthal Manager of Program Development

Meteorology Research Inc Altadena California 91001

middotI would like to make several points today First ozonemiddotis basically

a regional long-range problem There is a lot of long range ozone transshy

port and this transport is a normal occurrence The second point is that

ozone is stable in the absence of scavengers Junge mentions in his book

that the residence time of ozone in the troposphere is on the order of a

month Third vertical variations in concentration and ventilation rate are i very important in modeling atmospheres such as Los Angeles Layers aloft

are ventilated down to the surface on occasion and surface pollutants are

ventilated up mountain slopes as Jim Edinger has pointed out before and

often ventilated out of the basin in upper winds Fourth the day to day

carry over of pollutants from one day to the next is a very important considshy

eration in the Los Angeles Basin Finally there is a definite background

level of ozone The geophysical literature says its about O 02 to O 03 ppm (

in various parts of the world Weve seen data varying from 003 to 005 ppm

The difference may be due to calibration differences In any case numbers

like 005 are pretty substantial background levels for ozone

I am going to illustrate the points listed above with some data from

Los Angeles Basin The data were collected during a two-year study funded

by the Air Resources Board some of the analyses were funded by EPA The

study examined the three dimensional distribution of pollutants in the Los

Angeles Basin using airborne sampling systems Coinvestigators on the

project were Dr Ted Smith and Warren White of Meteorology Research Inc (MRI)

197

The first slide shows one of the aircraft we used Its a Cessna 205

which had sampling inlets on the side of the aircraft Figure 2 shows the

instrument system on the inside of the aircraft We were measuring nitrogen

oxides ozone scattering coefficient with a nephelometer condensation nuclei

carbon monoxide and meteorological parameters such as temperature humidity

turbulance Altitude and position were also measured

Figure 4 shows that the typical sampling pattern was a series of spirals

from the top of the mixing layer over an airport virtually to ground level

then we would climb up to the next point on the route and spiral down again

We had three routes (A B C Figure 3) that we would fly We had two airshy

craft and we would fly two of these three routes three times a day any

given day that we could The day I will be talking about September 25~ 1973

we flew what was called the Riverside route (C) and the Los Angeles route

(A) The 25th of July 1973 you might remember was the day before the

federal office buildings were closed in the area here because of smog

Figure 5 shows the surface streamlines at 0300 Pacific Standard Time

about 4 oclock in the morning daylight time on July 25 This streamline

analysis points out the morning stagnation conditions which are a very normal

occurrence in the Los Angeles Basin You start out with very light winds

quite variable maybe a slight off shore flow early in the morning On this

particular day this kind of situation extended well into midday The sea

breeze did not really pick up until up around noon When you have this kind

of a situation and a low radiation inversion at night you have a

long period of accumulation of pollutants all over the Basin espt~cialJy

in the prime source area the southwest portion of the Basin

198

I

Figure 6 shows the streamline pattern at 1600--400 cclock in the

afternoon same day sea breezes develop and with them a transport pattern

that carries pollutants up to the northeast and out toward the eastern por-

tion of the Basin This is a very regular pattern which we see day after l middot

day On July 25 1973 it was a little bit exaggerated The sea breeze was

held off for awhile started a bit late and so there was a very long period

of accumulation in the southwest area and then transport across the Basin

Figure 7 is an average streamline pattern at 1600 PacHic Daylight Time

on low inversion days for August 1970 It is included to show that the pattern

shown before is very typical Flow starts in the western portion of the

Basin and goes right across to the eastern portion This is using surface

data There is a very high average wind velocity in Ontario about 13 m iles

per hour and 23 mph in Riverside This is the average for the whole month

of August at 1600 PDT on low inversion days There is a considerable amount

of transport across the Basin starting relatively slowly in the morning and

accelerating in the afternoon

Figure 8 shows a verticle cross section of the scattering coefficient

The darker areas indicate higher levels of particulates Scattering coefficshy

ient is inversely proportional to visibility In the crosshatched area

visibility is less than about 3 miles In plotting altitude versus distance

inland from the coast you have Santa Monica (SMO) on the coast El Monte (EMT)

Pomona (BRA) Rialto (RIA) Redlands (RED) The lower broken line is surface

ground level The heavy dashed line is the base of the subsidence inversion

that occurred on the two days during this episode The middle line is the

base of the marine inversion There is a large area over in the western

portion of the Basin where emissions accumulate for much of the day At

199

midday the sea breeze has just started ventilating the Santa Monica area

The layer between the inversions is a layer aloft which is fairly well separshy

ated from the surface layer Ozone concentrations for instance in the

layer aloft were on the order of 04 05 ppm using the ARB calibration

method Down in the surface layer they were quite a bit lower in the mornshy

ing due to scavenging

Figure 9 shows that by afternoon the sea breeze starts and you get

kind of a clean air front Sea breeze starts ventilating the whole Basin

the stuff that was over in the west is transported eastward and at approxishy

mately Brackett (BRA) at 1700 PDT there is a clean air front The high conshy

centrations that were over Los Angeles earlier are now centered near Upland

(CAB) The numbers shown over CAB are data taken from a vertical profile

spiral over Upland at about 1600 That turns out to be the time when there

was the worst ozone concentration of the day in the Basin and it did occur

at Upland It could well be a result of the very polluted mass from the

western Basin being transported over the Upland area The layer aloft has

been a bit undercut by the sea breeze and some of the polluted mass has been

around possibly as long as the night before There has been very little

transport in the area aloft ozone concentrations are still very high

Figure 10 shows a trajectory analysis of the air arriving at Upland at

1600 since that was the worst time of the day at Upland We developed a

trajectory envelope using surface wind data and winds aloft so the air

arriving at Upland at 1600 started out somewhere back within this envelope

for example at 1130 PDT We did not go earlier than 1130 because the winds

were pretty much light and variable before that The air that arrives at

Upland at 1600 has been over the western portion of the Basin for much of

200

the morning and q~ite a bit of the evening before Thus there is

a very long period of accumulation and then a transport a pulsing effect

where you have pollutants moved across the Basin

Figure 11 is an isopleth map of surface ozone concentrations Again all

data are corrected to agree with the ARB calibration method Again you can

see that for the hours between 1600 and 1700 using surface data the Upland

area has the highest surface ozone concentrations about 063 ppm The western

area has been well ventilated by the sea breezes and it is cleaned out

The transport is actually pretty much perpendicular to the isopleth line

just about like that

Figure 12 is a vertical profile taken over Upland Cable Airportat

roughly the time of maximum ozone concentration 1636 PDT We are plotting

pollutant concentration on the x-axis versus altitude in meters (since it was

done for an EPA report) Surface leveJ at Upland is a little over 400 meters

the Z line is ozone Ozone concentration within the surface mixing layer

is pegged on the instrument at somewhat above 05 ppm Above the surface

mixing layer it drops off considerably and eventually get down to background

The T line is temperature and you ean see the subsidence inversion

on this day is very nicely documented here and provides a very strong trap

in that area The B line is the scattering coefficient inversely proporshy

tional to visibility Within the surface mixing layer visibility is on the

order of 3 miles or less while up above the surface mixing layer just a few

hundred feet difference visibilities get up to 60 or 80 miles The X is

condensation nuclei the measure of the very fine particles below about 010

micron It is a measure of quite fresh emissions If you have a high condenshy

sation nuclei count there are very fresh combustion emissions If you have

I

201

an aged air mass the condensation nuclei coagulate and the count decreases

considerably You can see that there are still some fresh emissions within

this surface layer as well But up above the surface mixing layer all the

pollutant indicators decrease considerably

Figure 13 is the same type of vertical profile taken over El Monte

which is on the western side of the sea breeze front The sea breeze front

has passed El Monte at this time almost 1700 PDT and again there are

distinct differences between the mass below the mixing layer within the sea

breeze front (below 400 meters) the marine inversion (400 to 800 meters) and

the subsidence inversion The subsidence inversion occurs at about 800 meters

and there is an old layer of very polluted stuff aloft The surface concenshy

trations are lower because of the ventilation by the sea breeze Condensashy

tion nuclei count (X line) within the surface layer is quite high There

are still fresh emissions in the El Monte area The 11 Z line is ozone

about 02 ppm within the surface layer (200 m) but it is 05 ppm up above

the surface mixing layer The scattering coefficient (B line) is very

similar it is lower at the surface and increases to a visibility equivalent

of less than 3 miles above the surface mixing layer The condensation nuclei

count is high in the lower portion of this (eg at 600 m) hut decreases conshy

siderably above This portion of the upper layer (600 m) has been around

at least all morning and condensation nuclei have been scattered from the

area The portion of the upper layer below 600 m has probably just recently

been undercut by the sea breeze and there are still some condensation nuclei

left in it

Figure 14 illustrates a different method of looking at the flushing

problems in the Basin We have tried to develop an objective criteria based

on ground level ozone to show the cleansing of the basin using the time of

202

arrival of clean air We determine the time when the ozone concentrations

drop by a factor of two at any given point The 1600 line means that between

1500 and 1700 the ozone concentration at that point dropped a factor of two

This sort of isopleth chart of when the clean air arrives agrees quite well

with the trajectory analyses although the numbers are a little bit behind

the trajectory analyses for the polluted air Figure 14 again shows the

transport process that takes place across the Basin which is ventilated from

west to east At 1900 some of the fresh ocean air finally gets out to

Redlands

In Figure 15 in order to put this whole flux problem into some perspecshy

tive we looked at the numbers the actual amount of ozone flux across the

basin We calculated the mean trajectory from Torrance towards Redlands

using the surface and upper air data We looked at the flux from the western

basin to the eastern basin basically from Los Angeles and Orange Counties to

Riverside and San Bernardino Counties This is a calculation made at 1700 PDT

We used the winds aloft from Chino as well as the vertical profiles taken at

Pomona and Corona Averaging the ozone concentration throughout the mixing

layer and multiplying by an average wind speed we arrive at a number of 185

metric tons per hour being transported directly from one side of the Basin

to the other If you look at this in terms of actual concentration in the

eastern Basin and assume that the flow was constant for about an hour it

is eno_ugh to fill up the box shown in Figure 15 to 025 ppm ozone which

exceeds the air quality standard by a factor of three (using the ARB calibrashy

tion method) Thus there is a very significant transport of ozone or ozone

precursors from one portion of the Basin to the other side of the Basin One

thing to mention though is that the concentration would not be kept up on a

203

steady state basis because the transport is a result of the pulsing effect

I Illentioned earlier There is a lot of accumulati6n in the western Basin

and these accumulated pollutants are then transported across the Basin This

kind of transport did take place in a couple hours because we also have

measurements from 1500 PDT which give us similar flux numbers

Figure 16 is a trajectory envelope similar to Figure 10 calculated for

Upland at 1600 for the air arriving at Redlands about 600 oclock in the

afternoon I wanted to include this trajectory envelope to show that the

problem is not really simple You cannot say that the air at Redlands came

from Long Beach per se The air at Redlands if you look at the whole

envelope of possible trajectories using upper air data as well as surface

data could have come from anywhere between Downtown Los Angeles and over

the Pacific Ocean south of Long Beach

Another thing to recognize is that the wind actually changes direction

slightly as you go up and down through the mixing layer and the mixing layer

is exactly what it implies There is mixing within the mixing layer so if

you begin with a parcel of air near the surface this parcel may move to the

top of the mixing layer and go one direction for awhile it then may go back

down to the bottom of the mixing layer and move in another direction for

awhile The ratio of the length scales indicata3mixing layer depths of 1500

or 2000 ft and distances on the order of 70 miles This makes it very

difficult for tetroons to follow an air trajectory because they do not go

up and down They stay at one altitude and in one wind regime and yet the

wind regimes are different at different altitudes and the air is continually

mixed up and down through this layer You can often see this on time lapse

photographs

204

The question is where does the pollutant mass go after Redlands Figure

17 is a repeat of Jim Pitts slide from yesterday and it is data for the

same day that we did our analysis It shows the ozone peaks starting at

Pomona and Riverside and on July 25 1973 eventually getting out to Palm

Springs so there is quite a bit of long-range transport The ozone is

stable at 8 00 or 9 00 oclock at night There still are ozone concenshy

trations of 02 ppm it hasnt dissipated even at the surface Ozone does

dilute as the mass moves Other calculations we did were integrations

through the mixing layer of various pollutants such as ozone and CO along

with trajectories that we measured Th~se integrations show just what the

ground data show in Figure 17 The concentrations increase through the western

portion of the Basin and then show a decrease through the eastern portion

of the Basin CO tends to decrease faster than the ozone indicating a

continued production of ozone further east

Figure 18 is a streamline chart on a larger area map for the 16th of

August 1973 It shows the typical streamline patterns that occur for

ventilation from the Basin By mid-afternoon there is flow out through the

major passes to the north and towards Palm Springs (PSP) On this particushy

lar day we had data from Arrowhead showing that the air mass from the Basin

does indeed get up there

Figure 19 shows a vertical profile over Arrowhead early in the morning

16 August 1973 at a time when there was a north wind Ozone level was

about 005 ppm the scattering coefficient was quite low on the order of

probably 60 miles visibility or so Figure 20 is a vertical profile again

over Arrowhead late that afternoon when the winds had switched There is a

flow from the Los Angeles Basin into the Arrowhead area thus one sees a

205

vertical profile that shows a distinct increase near the surface in both the

ozone and the scattering coefficient and in the condensation nuclei Ahove

that you have fairly clean air The top of the polluted level is just about

the top of the mixing level over the Basin

I want to leave the transport now and discuss the complicated vertical

structure that can occur If you want to try to model something try this

one for instance Figure 21 is a vertical profile over Brackett Airport

Pomona about 830 in the morning on 26 July 1973 which is the day after

the episode shown earlier A bit of interpretation shows how complicated

th is can be If one looks at the temperature profile it would be very

difficult to pick out a mixing layer theres a little inversion here another

inversion there several more up here After looking at hundreds of these

profiles though you can start interpreting them What is happening is that

there is a surface mixing layer at about 500 m In this layer there is a

high condensation nuclei (X line) count due to morning traffic The San

Bernardino freeway is quite close to Brackett there is a relatively high

nitrogen oxide count about 02 ppm and the b-scat is fairly high Ozone (Z)

within the surface layer however at this time is quite low The layer beshy

tween 500 m and 700 rn turns out to be the Fontana complex plume Note the

very high b-scat level it is below 3 miles visibility the plume is very

visible especially at this time of the morning when it is fairly stab]e

There is a high nitrogen oxide level (800 m) a high condensation nuclei

level and again a deficit of ozone Above this layer (800 m) you have stuff

that has been left all night very low condensation nuclei indicating a very

aged air mass ozone concentrations about 016 ppm b-scat of about 04 It

has been around all night and not yet had a chance to mix down within the

206

surface layer In fact one good way of determining the surface mixing layer

early in the morning and at night is to look for the ozone deficit Another

thing to mention is that wind reversals occurred for each of these three

layers The winds were fairly light and westerly at the surface slightly

easterly in the 500 m 700 m layer and westerly above 800 m There is a

complicated situation early in the morning but the main problem is that by

the middle of the day there is good surface heating and the pollutants have

all been entrained and mixed down to the ground so in order to modeI what

happens on the second or third day of an episode you must be able to look

at both old pollutants as well as fresh emissions And you need to account

r for ozone that is actually transported down to the surface from layers aloft l

The next slide is a photograph (not included) which is another e xample

of some layers aloft This is due to upslope flow as explained by Jim Edinger

in his publications The mountains are heated during the day in turn heating

the air and making it buoyant there is upslope flow to a point where the

heating cannot overcome the subsidence inversion and the stuff comes right

out from the mountains and spreads out over the Basin The pollutants can

stay up there if the winds aloft are very light and on the subsequent day

will he re-entrained to the surface On the other hand if there are winds

aloft different from those in the surface mixing layer or the wind velocity

aloft is high there can be a very substantial ventilation process for the

Basin Pollutants can be ventilated up the slope and blown away in the upper

winds In the case of the entire July 25th episode winds aloft were quite

light and these upper layers remained

Figure 22 is a vertical profile of one of those upslope flow conditions

in the same location shown in the photograph but on a different day Again

207

there is a relatively high surface concentration of about 03 ppm of ozone

(Z line) a layer of clean air between 900 to 1100 m and then high concenshy

trations of ozone again above 1100 m It has gone up the slopes of the

mountains and then come back out Concentrations in the 1100 to 1300 m area

are just slightly lower than they were at 600 to 800 m area Notice however

that the condensation nuclei count (X line) is quite a bit lower mainly

because the stuff is much more aged above the 1000 m level than it is down

below 900 m

Figure 23 shows the stability of ozone the fact that it can stay around

all night long This is a vertical profile taken over Riverside about 2200

PDT 1000 oclock at night Above the surface mixing layer (600 m) there

are ozone concentrations of about 0 15 ppm (Z line) Within the surface

mixing layer (below 500 m) ozone is completely scavenged decreasing to

zero The nitrogen oxides within this surface layer are being contained and

are around 01 ppm from fresh emissions that occurred during the evening

Condensation nuclei near the surface are very high The temperature profile

is very stable You have a surface based radiation inversion which is a

little strange looking for a radiation inversion~ nevertheless it is quite

stable There is a definite restriction of the mixing--a very difficult

time getting air from below 500 m to above 500 m The ozone that exists in

the 700 m range is in air where the reactions have virtually gone to compleshy

tion and is very stable All the profiles on this night changed very little

the ozone peak stays there High concentrations stay around

Figure 24 is a cross section across theurban plume of the City of St

Louis I wanted to show that this occurrence is not limited to Los Angeles

We have seen ozone formation and transport in other urban plumes These data

l

208

were taken during a project sponsored by EPA in conjunction with R Husar of

Washington University and William Wilson of EPA The dark line on this is

the ozone concentration across the urban plume perpendicular to plume The

dashed line is the scattering coefficient The power plant plume is parallel

to the urban plume The data on the left were taken 35 kilometers down wind

about 1100 oclock in the morning The ozone concentration increases slightly

to 005 ppm in the urban plume there is a deficit of o in the power plant plume3

In the same urban plume same conditions 1500 CDT two hours later further

downwind there has been substantial increase in the ozone in the urban plume

itself The b-scat is very similar to what it was before but the ozone is

now increased quite substantially except in the power plant plume where

there is a strong deficit of ozone due to scavenging by nitrogen oxides So

the formation and transport of ozone and ozone precursors in urban plumes is

a regular occurrence that happens in more places than Los Angeles and as Bob

Neligan showed this morning it can happen over quite a bit longer distances

than we are showing here

To summarize the conclusions as they affect model development first

once ozone is formed in the absence of scavengers ozone is a very stable

compound It remains for long periods of time It can he transported for

very long distances Ozone is a regional problem which cannot be controlled

on a local basis To have effective ozone control middotone must have a regional

control strategy and probably regional type air pollution districts

A second conclusion is that the vertical distribution of pollutants can

be highly complex and models have to include more than just a simple wellshy

mixed surface layer

209

A third conclusion is that layers aloft can persist over night and can

be re-entrained within the surface mixing layer on subsequent days models

should be able to account for old pollution as well as fresh emissions Also

pollutant accumulation and transport can have distinct diurnal patterns that

are strongly dependent on the meteorology Models should be time dependent

and should start at the beginning of the accumulation period In other words

models ought to be able to run for 24 or 48 hours if they have to In this

case in Los Angeles there is often an accumulation of pollutants which starts

in one portion of the Basin at midnight and continues through the next mornshy

ing even before it starts to be transported

As far as recommendations go in many areas a lot of ambient data has

been collected and in some cases the data are actually ahead of some of the

models so I think a research program is needed in developing models that

will account for this vertical structure and the day to day carry over and

the models need to be extended to cover longer distances In addition more

smog chamber work is going to be needed in looking at the effects of carry

over and mixing old pollutants with fresh emissions How people go about

this I leave to the modelers and the smog chamber people They know more

about that than I do

I

210

I

~ INVERTER

AUDIO TAPE

MONIT0R

MONITOR OBSERVER SEAT

MON ITOR

NEPHELOMETFR FLfCTRONICS

j DIGITAL DATA LOGGER

CONDENSATION

VOR DME NEPHELOMETER TUBE

JUNCTION middoteox ASSORTED POWER

AIRBORNE

TEMPERATURE TURBULENCE

middot HUMIDITY

ALTITUDE BOX

__

middotE=-middot RECORDER ----r----------

NUCLEI KJNITOR

CONVERTER

SUPPLIES

INSTRUMENT PACKAGE (

lCO

03

Ndeg

-

-----NEPHELOMETER

BLOWER

Figure 2 Instrumentation Layout for Cessna 205

211

bullubullbullbullbull

Figure 3 Airborne Sampling Routes in the Los Angeles Basin

Figure 4 Vertie al Profile Flight Path

~-~ r~i ~~1 -- ~ ~ ~2-1~ LJ-----~ r~~ ~~ t~~--l

~ ALM l

0 RIA

ec 8v

M

~ Afo

-o

M 0

~IV

ltgt

IN J--1 N

SCALE II fi M I j_ ES 0 3 4 5 =-JSEJ--J~ _middot ~middot- - =- =

I

~

M

N~J

Figure 5 SURFACE STREAMLINE ANALYSIS - 0300 PST 25 July 1973

~~~ ~~-- cp1FJ=D -~~

~ 1

~ ~ 8c

8v

~25

PACIFIC OCEAN

diams Tt

0

9 I 4 5 10 I- m p H - -middotmiddot u 4H__8 middott_

D i6 J4 k W~D SPED llaquotl SNA NJ ~1

SCALE m ICtt84bullmh R v1s1a1L1n (mil 6 ~ CONTOURS REPRESENT

-- 10ml 16km (~() bull ~ ) ~ - 000 ft 3C5

Figure 6 S_cJRFACE WIND STREAMLINES - l 600 PDT JULY 2 S I 8 7 3

l - ~---i ~-=-___-----c---it~~-~~ r----=------1 ~-~~--cpc---_t__A --~ ---llil

~_ - ~-l-cL

34bull vi~-dff

bullbullbullbull bull ~ bull -1 bullbull - -_- L bull-J bull ~bull-bull-ii------~ bullmiddot r_ -~- ~ bullI ~_ bull bull bullbull bull I bull _ - bull -~-~ middotbullbullbull ~ ~ --middot -~- bullbullmiddot ~v ) ~ - -__rl v middotmiddot - 1- ~ -- middot middotmiddot - 1 91 frac12 - ~- lt( middot K i - middot bull - middot - bullmiddot~~-~lJ) obullmiddot~ ~-f- _J_~---Smiddot~middot-~----~~~---gt_middotfY-_middot-~middot --middot-~-~----fJ_middot- middotmiddotbullmiddot u-- bullmiddot ~ ~ -middot L~ bullbull

~bullbullbullbull bullbull l_bull bull bullbullbull EW bullbullbullbull-- ~ __bull f f - middotbull - J middot f bull S bull I ~ -r --

_ bullbull bull- _ bullbull-bull ~ ~ bull bull bull bull I bull bull bull bull bull bull gt - bull middotbulliJ -bull I bull bull _1 bullJ C-- ~-middot _ bull bullbull bullbull bull _____ ~ ~ l _ middot q bull 1 -middot middot ~~middot middot middotbull_ J ~gt - J bull-bullbullbullbull ) _ -middotmiddotbullmiddot J ~middotmiddotmiddot -bullmiddotbull fmiddot 7middot _middotmiddotmiddot bullmiddot(middot Ii~ middotmiddot~_--~middot 1middot__middotmiddotmiddotmiddot middot- gt_ -~ -~-- Imiddotbullmiddotbullbull_ -

- ()_I (w--_ bullbull__(i- bullOmiddotbull bull middotbull -bull-_jlJ middot bull lt 1(middot t gt bull - ~ rbull I bull middot middot- bull41-bull l~r v-middot~- middot middot middot bull_ - middotmiddot ~Jtj (middot~ ~middoti middot middot middot middot middot ~- ~ -tmiddot~ I - middot middot_- ~ - -~ middot_ _- ~bull - _ ~) i bull bullbull bull- middot_ bull middotbull __ ( bull 11bull bull ~ampmiddot ~ l bull bullQ bull - -1 bull JY1 bullbull ~ or bullbullbullbullbull bullbull-bullbull _ ~ - bull bull-bullbullbull middotimiddot middot 91 bull t bull - - tfaw lJ--r- bull bull _ bull middot- - l

f ~~middot--~ middotmiddott ~ltrgtmiddotmiddotJmiddot_bull - ~ - __ middot- LOS ANGELES BASIN - LOW LEVEL -__ jmiddot l-gt bull - bull J iI bullbull bull bull bull _ bullbull _ Jmiddot middotL~_1 middot middot bullbullmiddot ( C middot INVERSION MEAN WIND FLOW _ J

lmiddot - f bullbullbull~ - f 1bullbullbull _ ~)- bull middot- _---_- 7f-~bull~ REGIME _F_~ AUG_UST_~ ~600 P~--- l

-__L-~bull --ncmiddotbull~~-j--bullmiddot~bullmiddot_-bull _fJibullmiddot Imiddotmiddotmiddot-bullmiddot- bullbull ~ bullbullbullbullmiddotmiddotmiddot~middotbull ___ bullJ_ _middot~0))deg bullt t1yensmiddotmiddot ( middot middotmiddot middot middot ~ middot lbullbull1 t_c0 bull -middot---l lt ~middot~- deg bullbull --= bull bull bull I bull bull bull bull bull bull bull bull bullbull _~bull b ---) bullbull-bull ) bulll middotbull middot1middot ) bullT --f bull I bullr ~bullbullbull bullbullbull( - -bull-- ( -o-----_i bull-~-l- i l l J l~-- c middotmiddot _--1 ---I middotmiddot ---- ~bull-bull bulli_ ALT Elmiddot_ bullbullbullbull _- ~~middot bull middot bullbull _ bull middotbull bull~ ~bull middot bull -middot bull--ua_-- bullbull bull

-- 01--- middot_ -middotmiddot hmiddotmiddot __1 ~-- ~ fi~~- ___ - ____ _ -middotmiddotmiddotmiddot~ ) -~-J bull bullbull bull bull 0 uc- -l ~- ~ IT ~~ll ~ bull -middot -middotmiddotmiddotmiddotbullCCAmiddotmiddotmiddot-middot middot bullbullbullbullbull

) i- 5 ~-==-- __ __ - bullbullbull _ bull~ bullbull _ bull bull l T[h4 ------ - 0

i17- o~-lt -(i-_~ 11t~bull-omiddot ~- -- 13 0l~~~bull bull Jbullbull~bull ~ ~bullbullbull bull bull x- middot~---=-~~ -=aJlll8 bull Ibull bull ~~ middotbull rbull~---bull1-~middot-middot _ middotmiddotmiddot-middot 1 0 ~vrbullmiddot ~middot ~ (J~-middot _-_~) ) ~ bull middot

l middot _ POMA_ middot =~~~----ti~ jmiddotmiddotmiddot - middot bull [j

~A ii J0 Vfli middot bullHud __=bt_ bull

CImiddot ~-- ~- middot)middot PACIFIC OCEAN I middot ---- middotmiddot ~

__ middot__ ~ - _ 23~1 middotbull 8 4 1 middot middot ~ middot middot gt ~~- l ~ u middot

bull - bull- I ~------ --1~ i middotmiddotmiddot - n _c-118 1130

~ n r -t ~~gt25) cmiddotbullmiddot

~--lt- ~~- 1-~__( i - t ~ _ middot 0 igt(_J

11bull bull11 ~~ -~[ ~i~gt----gtmiddotmiddotmiddotmiddot--~l_ ~~ ELEVATION

IN FEET bullbull (_- middot bullbullbull -middot middotbull middot ~~ middotmiddot bulltbullbull _ffmiddotmiddot-middot v I )tylt~ -~bullbull1bullbullrbullbull ~-lt -~ ( I~

600~ A0 Cv(A (1829 m AND OVER) deg )_ rJ__~7 middot middot ~--middot L==1 _J bullbullbull - bull -middot~-- rgt ~ middot(Zmiddot- middotbullmiddot middot

Z~C)-tGOO (762 middot 1829 m) 9-N4 __J (r -- lf _ bull bullgt-~~~ ~ _ w _ _ I (1 bullmiddot( middot1 middot -----~~~- middot L-bullmiddotbullW bullbullbull3 STA r I0-4 lODEL

100i -2soo (305~762m) -- Ow - -~1_- i ~~--- bull v~rvt ~~ -middot )) ~--

II gt J (-_bullmiddot middot~ l bull bull tr 1 )~ gt ) bullbull-_bullI-middot -middot bull~0 3 Mor nuq1ENr Wlbull~O JIAtCTIO-bull bull - lbull C---gt bullbull )t bullbull -( I bullf I - 20-00 (61 bull 305 ml J( Jloa xxE- -bullbull00 - -- middot1

0-200 (0middot61m) Wl)7 AVBt~gpound ) bullmiddot-iiNL~ middotntmiddot_ 1 iJJlt( _1J- ~ VAq IA9 IL ITY 0 ~ 10 15 ltS lHPtl

~--_ bull bull I bullbullbullbull 1 ~) J)J ~ bull Is bullmiddot bullbullbullbullbull ~ 3 V IS A VAqlABLE OIR~CTIO- 0 8 16 2-4 km

(SPEEDS SHOWN IN mph 10 mphbull 16 h1llr) -- middot ktr~~~ lt~ ) -middot-SCALE

Figure 7 LOS ANGELES BASIN MEAN WIND FLOW FOR DAYS WITH LOW LEVEL INVERSIONS DURING AUGUST I 970 AT 1600 PDT

-~~~~-=======~middot~-~======~middot--=-==-===gt=---==____________=== ~--=-J~==-- -=-ee----=-------

500

N f-- V

- - - SUBSIDENCE INVERSION

----MARINE INVERSION

bullbull-bull-bullbullGROUND LEVEL

x WINOS ALOFT (kmht)

WESTERN middoteASIN EASTERN BASIN

LAX WINOS EMT IHOS I I

CNO WIHOS

s_ 04 13 1500- 05 02 08

I 06 069 middot

11-1--

04 04 i ~4

06 ~ 4--

I 2

1000 n1 1005 -_E

lll --1 lJ -----------~----

~11

--=i-+- c -- 9 _____ - ~ C

lt I

I 6 4 _r 31

I 6 5 ~~ ~_ bull ---middot- 64 ~li- - middot- bullc - middot-----------

10

SMO (1347 PDT)

EMT (1246 PDT)

BRA CAB (1459 PDT) (1335 PDT

RIA (1349 PDT)

RED (1406PDT)

Figure 8 VERTICAL CROSS-SECTION OF bscat FOR lvflDDAY

T t 10-4 -1)(l n1 s are m

JULY 25 1973

- c - -~

~--~ JC_-_1- ~1pi~ oamp----~JilliiiM~f~-U~ -~--- --~~~ ~~~

-=--~

-E-- O

_ lt

1500 05

06 15

09 __~

1000 --

~- ~---middotmiddot 29

500

oJ11

__a

07

I 07 I

I I

I

09

I

I

I

I 7 ---

11 -----

~ ----- 6

---------------lt- -~middot4 --------

20

29

-

10 10

11 07 08 08

10

08

~8 _____ Y-

N

- - bull SUBSIDENCE INVERSION

----MARINE INVERSION

-bull-bull-bull GROUND LEVEL

WES TERN BASIN EASTERN BASIN x WINOS ALOFT (kmhr)

t t

CNO WINOSILA WllltOS poundMT WINOS

SMO LA EMT BRA CAB RIA RED O (1736 PDT) (1655 PDT) (1707 PDT) (163 PDT) (1823PDT) 1805 PDT)

Figure 9 VERTICAL CROSS-SECTION OF b FOR AFTERlOON OF JULY 25 1973 scat

T bull 1o- 4 - l )(units are m

__~~---iii~~- ~- ~~______ ~~- --~~J---=-~ ~

N ~ -J

PACIFiC OCEAN

0 5 10 15 1111

E 8 4 I 0 8 6 2 ~ bull

SCALE

dh Mes

CONTOURS REPRESENT - 000 ft 305 m

0 SNA

c8s

ec 8v

amp R~b

Figure 10 TRAJECTORY ENVELOPE FOR AIR ARRI1G AT CABLE AIRPORT (CPLAD) 1600 PDT JULY 25 1973

~-~

q_- ~ ------1 H~~~ -~~--~ ___---___--i- __r-=-1--===12---1 ~ ___r~ _==---_ - ~- f~~ ~-- - -5plusmn-at -~middot~

ll~~r1 ri

40

ec 8v

-1 I

amp

0 HQ_

7 0

CAP LAAR) O

VER

PACIFIC OCEAN ~ 0

RLA

4

WHqR d

diams

H ~I

I l

0 COMA

3

L~

LAH

Fa_ f ~~

S ~ LA APCD VALUES ADJUSTED TO AGREE ~

lt

0

5 10 15 mi0 WITH ARB CALIBRATIONE-j I I CONTOURS REPRESENT NZJ ~ 0 a SCALE 6 24 km - 1000 ft 305m COS v~J

______ J 10 ro ( igtf t-i

coFigure 11 SURFACE OZONE CONCENTRATIONS (pphm) I 600- I 700 PDT JULY 25 1973 ~

~~~~~C-~ ------=--~-__-~--~~~=--- ----=--~

N

-E

D1600----------------------------- 1--

14001-------------------------------

1200

I Ground Elevation

1000 middot 445 m ] lampJ

sect ~~ 7 ) SURFACE i6~ 800 MIXED LAYER

~

~ [ J ~ ~ I OZONE CONCENTRATIONS~ 600 E E GREATER THAN

( 50 pohm

400 I C H T Z GROUND LEVEL

200

I PUUloCETER UNIT SnbullBOL

NOc N0 0 ppm01 02 03 04 05 03 z

40 --~45~~ 50 co pm C0 5 10 15 20 25 30 35 I I I I I I I I I I TEIIPERATURE oc T-5 b 5 10 15 20 25 30 35 40 45

I-- 100 RELATIVE HUlillOITY H0 10 20 30 40 50 60 70 60 90 b1eot IOmiddotm- 1 8

CN cmmiddot3 1 IO X0 I 2 3 4 ~ 6 7 8 9 10 URBJLENC-C cm213ue- E

Figure 12 VERTICAL PROFILE OVER CABLE (CAB) J CLY 2 5 l C)7 3 l 63 6 PDT

~ _~ ~--- -

--

1400 I bull bull

1200

1000-5 LampJ 0 ~ I- 800 ~ c(

sooLl

-1-=-1-~--t j --=~c-o-----i-bull 1-~~~ ilt~~ -~-1 lta-abull--~ -c-~---=---r F--- ---- I n_--middot- =~~ ai~IHJ

(~-It

1600 ___________________________________

C r 11 s Ground Elevation t~C E H I~lcc

- ~ 1 90 m

4001 bullc C H

C UNDrnCUTTNG svC ~ Ic- H

SEA BREEZEC II 200

C C

[C -PARAMETER ---UNIT SYMBOL

NOx N0 0 ppm01 02 03 04 05 03 z co ppm C0 5 10 15 20 25 30 35 40 45 50

-5 middot- -~20~----25 TEMPERATURE oc T0 5 10 15 30 35 40 45

100 RELATIVE HUIOITY H0 JO 20 30 40 50 60 70 80 90 bcot 10-4m-1 8

CN crrr3 10 0 I 2 3 4 5 6 7 8 9 10 X TURBULENCE cmZ-13 sec-1 E

N N

_-----=-G--~---

Figure 13 VER TICAL PROFILE AT EL MONTE (EMT) JULY 25 1971 1656 PDT SHOWING UNDERCUTTING BY THE SEA BREEZE

0

middot~_lt ~middotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotbullbull

-~

LACA

0 - )

i r=

-v2v

~

_middot~middot)( I bullbull

bullJ

K~Ji~middot

~~ 61iAS 0

EMT J~J---6~-11 ~orr

PACIFIC OCEAN

WEST 0

SMC

0RLA

14

L~8

R~A

~BL

16 ~ ~

0 5s Pcfrac14A c1i ~ )

wFJfo~J_) ltI~~~

_ff-Clf1ito J )

HILL~

~J U

~ _~~~

~

I o middot

1 1$ ~ 11yen ~middot ~I N

I

N I- I

t

0 --pomiddotmiddot bullmiddot i- 1LO middot Joomiddotmiddotmiddot -- middot middotmiddot -middotmiddot

_middotmiddot 0 middot middotbull MWS r

L4 ( 1 T bull bull __-- -A bullbullbullbull middot

0 i __ bullbull

17 t-J~ N7 a S I ~r ~ 1 rtd ~lt A-~ v- middot ~ - cXa 0

RIA 19

CLO

ltJ~

bull ~ 0

(

--

1

_ _

-2Wl

~s~o -- _)~J0JgtJ~ ___ Q

15 l1JI

0 15 r(A0

CAP

CLARR)~R 1900 1-shyPDT

II (_-L~X L2X I 0~ R[V

0 CCtwA

I

I18=00 POT~ l4 r1

fj

-11J - ----- 11=oomiddotmiddotpor

l~i middotmiddot- o

i

5 10 5 Tl o~1 middot--middotmiddotmiddot middotmiddot

_q it==i--__F-3 9 I I CONTOURS REPRESENT SNA NZJ ~1 o

_- I 0 8 16 24 km I - 1000 ft 305 m middot ~

7 14~CALE --- 2500 ft o2m V lr1 ) middot I i0 _ il o5

16QQ pol(middot v( ____________ _L

I i

Figure 14 APPROXIMATE TIME (PDT) OF ARRIVAL OF SEA BREEZE Jl-LY 25 1973 (Ogt_iective criterion based on ground level ozone concentrations)

~ -___~==~ ~~ - ~ =-~ f7r=~1 _j~-~ --c_~~

u-middot - middot middotmiddotmiddotmiddotmiddot

~- middotmiddot~ ~1 WESTERN BASIN r Joa_middotmiddotmiddotmiddot_ NOxEMISSION RATE ~- 95 METRIC TONShr

-----bull_ ~ ~middot~ I -OUR -----middot )omiddotmiddotmiddot - middot~ l21 (fTI

~ AT middot ~ middotbullmiddot- ~- ~ middot 4bull-middot

I EASTERN BASIN NOx EMISSION RATE 10 METRIC TONS hr

ri r bullbull

t10 Joa

) __ 8v -a_ -- -bull-I O ~AGA -_ ~S ___ _ middotmiddotmiddot -

~ ~v ai- omiddot-middot~-- - ) r -middotmiddotmiddot f middot( ---~ -l A ~ _ (- bull ___

it~ ~~~ middot-middot -- ~-~ ~~~ 0 0 AZU~

AVERAGE CONCEN7RCTi)N iN BOX (IF STEADY STATE)

IS 25 pphm

1 r f--Ji 7 ~Sv PAS ou )V~(~- ~ t i -~ Li_) 03 FLUX THROUGH f~

~ ~JI_~ - amp_ JiM O SHADED BOUNOA~middot~-~ ~~-s-- EMT 185 t 60 METRI~ bull ~ ~ TONShr 0 (m)

c~~~ 1t~CS A~JFP

1000 _29

-i32

_~o tUA

_

1

O~ ~

0 -__rJ( (r- J PACIFIC OCEAN LAX _ C-middotJbull _

l o M R No _

550m

r

A frac14

HAR O HJ LAH

_ o camptA REDLANDS 18QO POT ~ r

I bull ~

RB MEAN TRAJECT~~~y

0

TOA L~S

0 AN

I - ~ 8 OUNOARY ~ ~middotltdeg ~ ~ BETWEEN middot __ WES~ERN ANO- middot middot - ~

I gt I lt bullmiddot bull (EASTERN ~ i middotmiddot middot - - ~

S ~ ~~ ~ - middot-

rt1~1_--t------l

middot1-- BASIN ~-~

1-)~~--middot ~ ~l

~~ ~-bull bull J --

-is-eo -_

0 5 10

j=i r-i C

0 8 ltl

SCALE

5 mi

2~ un

CONTOURS REPRESENT - 1000 ft 3gt5 m

--middotmiddot 2500 ft 1 762 m

~

0SNA

cos 0

_ --~ ----- --- ( bullmiddotmiddotgt

- middotlt- ltgtmiddot t__ Q ~

1 1 rmiddot bullbullbullbullmiddot ~9

NZJ ~ middotmiddot - middot- Alr ---middotmiddot- middot middot( middotmiddotmiddotmiddotv ~ bullbullbullw bullbullbull bullmiddot 1 bullbullr~ ~-- -middot ~--v ~- - I -~

ESTIMATED OZONE FLUX FROM VESTER~ TO EASTER-J BASIN JULY 25 1973 I 700 PDT

C ~IV

N N N

I

l ~

-~~

I

iI

i I

I t

t

~ ---~ --

Figure 15

~Qa llfJD fl(~middot ~ 11f ~I I

l

Lfb ec~s0 CPK v2v 0

ALT 8v Ld~_----1

I

HO-

0 CA

middotLARRv O VE~

1330

ol(Di

A~U

0ENT

~lt

s~e ~ 1530

F8f 1730

~

rbull-~

oc (WljT) -_-~(~~c lt-rw---_

~~ ~-_i~cB~~~

2-~) - ~ ~ l~w-~~ p~- pound)_

0 ojI middot tl-1CfUp I ~ ) 1 ~ J~I i bull middotbull middot~-Li 1)- ) I

DiI ~- 0

i ) 0 l I I

t

A RALc~o JI

C

-~

0 r-iR

~IV 1230 1~

RE PO ~- I - Ftl

) 0 ---~gt- __L8s ~Zi diams ( T~ _middot_ ~~ ~

I AN ~~-~ j t bi 0

~ I

~ I L i

-_gt ji o 5 c 5 Tl middot 0 0 ~-i p__i=r 2=f I_ I 1 NZJSNA 1

1 8 2 4 km )

SCALE I 00 J_(1 CONTOURS REPRESENT cos f

1 0 I --- I - ))) 35

PACIFIC OCEAN

Figure 16 TRAJECTORY E~VELOPE FOR AIR ARRI1gtJG OVER REDL_)DS AT 1800 PDT JULY 23 l =i73

224

JULY 25 1973

LA DOWNTOWN

0sect040 a

~

~ 020 0 X z0 ~ LJ 0 ~ z

~5 040 330POMONA 0 ~ en~ 020 w z _J

w w 0 (9 z O----u-~~-__~_-~~~-------L-~-0--0-0~----- z

ltt~ 040 56 (I)z

0 0o _ RIVERSIDE _J0 20 t6 ~

0~ Qt---0-0--ltrO-ltgt-C~------~~~~ a

LL ~

Rate ~ IO mph___ (I) w

_J~ ~ ~

et~ lt(

3 040 PALM SPRINGS ~

j 020 ~

0------____-----L--___---------L---~--~

105

12 4 8 12 4 8 12 l~-s----am _ pm----1

HOUR OF DAY PST

Figure 17 Diurnal variation July 25 1973 of oxidant concentrations at air monitoring stations at Los Angeles Downtown Pomona Riverside and Palm Springs California Values are corrected data Los Angeles Downtown and Pomona x 11 and Riverside and Palm Springs X 08

CONO S t 1 fRESEIS7

~

~~ 0

ciffmiddotdK ~ ~v~~o

( ~s ~

bull ~r ~ bull 1--~~----Soootl ~ ~ ~ ~ lj i1 d t CJ ~ ampfrsmiddotflt- frac12 ~ middotL~Js _-- ~

_gtgt middot~ ~rroltf~-) ~ 0 s- r

middot-middot- r_~ ~~JtbO ~~bull~Jt ~~~ L r - bull _ ~ I= J 1 ~ ~ ~-~~bullJC ___ -_ middot ~ laquo -poundJ~ ~- middot1~ r-- - V--_1_ ~ I 1 S I

V ~ bullf-uv~ fi -~zumiddot -~middot~ LS gt -tmiddot-F Q~ ~-tv I_~ --- ONT p(_ s ~S ~~~-[ ( 0 c-_ --~ ~~~___d_) lt- ~ I -i-C - -

~----1-1 bull~~POMA ~V BN ) middot-~ f -- s - ~

~VA -middot- ~p AAL a 2~~ ~~middot01 r r ~ middot middot 0-- V

i LAX bull1

~ -~poundJ-i- ltllll _(__1-0~ ~t- degQ-0- ~~ _ _-__~~-qlK ( a_ II ~ ~p-~ ~J

N bull - - 0 r o_ _I ~ -~ ~middot ~ ~amp ~--= ~ ) s ~

- -~- - middotO _a - Tl --0- ov I lHOIO J I bull J -- ~ 6 ~ -__ 2 ~

(__ ~~ _- ~-~ middot8---fl~ -- ~ bull~-abullbull _~ ~-cgt ~ bull bull middot e bull bull l ~ 0

I 1A_ HZJ middoto~J

middot0 (~ ~ S TAA

- ~ - - - --0 () _-j J middotO=c==c-c==cc~~~ l ~~ ~ ~ bull-~---~ ~ bullbull -~ al1 ~ bull __ ~--middotmiddotmiddot

diams Skyforest _ Strawberry Mt Lookout

Figure 18 STRE ~[Ll)ES FOR 1600 PDT on 8 1673

~ ~--

vO 0

N N V1

au

91 V7

-1 ~ -=1 ~~ ~~~~l r=--~d- ---1 _J-_

~E1 ~L1-~f~

3100 ---------------------------------

2900r-----------------------------

T

e w 0

~ 5 Cl Ground Elevation

1560 m

T PARAMETER UNIT SnbullBOL

NOx N 01 02 03 04 05 03

ppm z co ppm C

10 15 20 25 30 35 40 --

45 50

170

I I I z

0 5

-5 - -0~ 5 10 15 20 25 30 35 40 45 TEMPERATURE oc T

0

0

10

I

20

2

30

3

40

4

50

5

60

6

70

7

80

8

90

9

100

o

RELATIVE HUMIDITY

bcot CN

TUR8ULENC~

110-4m-

cm-3 tobull 213 1 cm sec-

H

8 X E N

N OI

Figure 19 VER TI CAL PROFILE OVER ARROWHEAD u-RR_l A CG CST I 6 1973 939 PDT

3100----------------------------------

N2900r----------------------------- -i

N

2700i-------------------------------

2500

e 0 uJ 2300 gt ~ ct

2100

1900i---------------------+--------------

~le 1iation 1360 m) 17001 ~

- -PARA1jETER UNIT SYMBOL

T NOx N1500 o ppm01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50

TEWERATJRE oc T-5 middot --~o--- 5 10 15 20 25 30 35 40 45

IOO RELATIVE HUWIOIT Y H0 10 20 30 40 50 60 70 80 90 bcat 10-~- 1 8

CN cm- 3 104 X0 I 2 3 4 5 6 7 8 9 10 213 1 tURBliiENCE cm sec- E

Figure 20 VERTICAL PROFILE OVER ARROWHEA D -RR 1 --- -AUGlJST 16 I) 16--1S PDT

1-~i w--~i_f l-=--bullC- ---~-4

1600 bull t c- N 8 ff Tbull C[ 8 H 1 bull H z H T ~ C f N 1 H T bull C rn 1 C NE bull-~z Hi400 bull bull tf T bull N ~r --middot _P H -ybull EC N z__e H T i 8 z H Tbull C E HD Z H T POLLUTANTS REMAINING FROM bullt C Hbull L T PREVIOUS DAY1200 Et HO I II -middot-- bull Ct H 9 - H T

___ Hbull( E N 1 a tC N i--_ -1 H

C N Tbull Z HP poundIC C H z_ 1111 1

- bull C H Z l _H_ _J1000 )( cc H -z emiddot ksect bull C N ~ T

)( iz H 8 H TIAI -t XC z 7-- T0 bull pound N t H_8

t-gt

YCpound N 1800 l I-gtltbull - H (Jet

N i -r~Bltt t bull gt- t C X N H T

[ BUOYANT POINT SOURCE PLUMEH 1

N ~z-- -

C H

-bull SUPERIMPOSED ON POLLUTANTSC JZ X H T 600 -~ E c REMAINING FROM PREVIOUS OtY Cl JC t H H f bull cmiddot t HT -fl

C- X t fl _ REMNANT OF NOCTURNAL RADIATION INVERSION(I-----e-C f N K I T H

C Z [ T H x-8 400 _Zc r -H -K SURFACE MIXING LAYERz C II H K 8

C N T pound H M 8 _ I -t ff H E N -9 l

Ground Elevation 305 rn200

PARAMETER UNIT SYMBOL

_ I - I I I NOx N00 ppm01 02 03 04 05 03 z

co ppm C 0 5 IO 15 20 25 30 35 40 45 50

L middot1 TEMPERATURE oc T-5 0 5 IO 15 20 25 30 35 40 45

100 RELATIVE HUPAIDIT y H0 10 20 30 40 50 60 70 80 90 bscot o-4m- 1 B

CN cm-3 x 104 X0 2 3 4 5 6 7 8 9 10 TURBULENC~ cm213sec-1 E N

N co

Figure 21 VERTICAL PROFILE OVER BRACKETT (BRA) JULY 26 1973 0825 PDT SHOWING BUOYANT PLUME AND UNDERCUTTING BY RADIATION INVERSION

N N 01600

___bull C M C

C

1400~~~ t C [ middot H LAYER CAUSED BY

C C H C [ H UPSLOPE FLOWl

1200

1000 ] w

SURFACE MIXING LAYER 0 --= ~ -~~ 6 800~ er

C C

600t-i C C t C

I ~00

Ground Elevation 436 m 2001-------------------------------

PAIUWETU UNIT SYWBOL

NOx N ppm0 0 01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50 I I I I I I I I TEWPERAT1JftE degC T-o b 5 10 15 20 25 30 35 40 45

100 ~EIATIVE HUWIOITY H0 10 20 30 40 50 60 70 80 90 b1tt1 10-m- 8

CN enr3 110 X0 2 3 4 5 6 7 8 9 10 Tu RUL Erct cm23sec- E

Figt1re 22 VERTICAl PROFILE AT RIALTO (RIA) JlJL Y 19 1973 1738 PDT SHOWI=JG LAYER CAUSED BY UPSLOPE FLOW

~~-7 ~ ~- 1 ~iri ~~- ~~-~ ~t ~~ ~ =~middot-1

1200 I t 1 If J-

1000

I C ltTl a_ ~l- t

800

600

L gE __r H

H

400 j (~ c pound N C E I~

t EH -

1-1 M

H H

H M H H

H

H H

11 bull H M H

M H If

H H

H

- C t H ~ C poundmiddot H

I C E I(

200

1600--------------------------- t

T t t T l

l T t

T t_

t 1

l] w ) g f

Tt t

ltt ~ T

t J t T

t J

f 1

t

Klt

H M Cro1nd Elevation 250 m HT X

5Yl80LPAllAlETER ~

NOx N0 0 ppm01 02 03 04 05 03 z

co ppm C0 5 10 io 20 25 30 35 40 45 50

25~--- ---35~~-40 TEMPERATU~E oc T-5 0 5 lO 15 20 30 45

100 RELATIVE HUMIDITY H0 iO 20 30 40 50 60 70 80 90 bact 10--ltllm-1 B

CN cmmiddot3 11 04 X0 I 2 3 4 5 6 7 8 9 10 IURBULENCE cm2hioC-1 E

Figure 23 VERTICAL PROFILE OVER RIVERSIDE (RAL) N

JULY 26 1973 2239 PDT I)

middot==-=-=

0

bull

N w 1--

ii -s~~ l-obull

CJ ~

obull -obull obull

5 02~

bscat

Oa

4l o2J

-I 3 e I 0

--)(

~

Abullu 2

ll

ol

Traverse at 750 m msl 35 km Downwind (SW) of Arch - St Louis Mo 1117 - 1137 CDT

( Power Plant Plume -01 Ibull-[ ~ e

11 bull E I -)(I

I0bull I 1r~ l -

0

I I Io 1 u I

I r- l A bull I i I 1I

H1I I 4 t I II I I

11 I I

I I r I I I

I I qo 01 I I

I I bullJ~viI I middot ~

I

I I

~

Urban Plume

ood 0 10 20 30 40 50

kilometers

o~

02

01

s 1

P

0bull 01

00S~J1 I ti middotmiddot1 middotvmiddotmiddot~ J

Urban Plume

I y

oo 0 10 20 30 40 so

kilometers

Traverse at 750 m msl 46 km Downwind (SVV) of Arch - St Louis Mo 153 0 - J 549 CDT

---- bscat

o-

Power Plant Plume

1l~ 11I 1 t

ill~t fl Ibull I ii

I

lmiddotmiddotrI

I I I I t II

l vrI V

JV-f Jl bull

bull t I bull I

Figure 24

l

232 RELATIVE CONTRIBUTIONS OF STATIONARY ANDMOilILE

SOURCES TO OXIDANT FORMATION IN LOS ANGELES COUN1Y IMPLICATIONS FOR CONTROL STRATEGIES

by Robert G Lunche Air Pollution Control Officer

Los Angeles County Air Pollution Control District Los Angeles California

Introduction

The type of air pollution problem characteristic of the west coast of the

United States and particularly of Southern California has come to be known

as photochemical smog because it is the result of sunlight-energized atmospheric

reations involving oxides of nitrogen and reactive hydrocarbons Its manifesta-

tions- -eye irritation reduced visibility damage to vegetation and accumula-

tion of abnormally high concentrations of ozone or oxidant - -are by now well

known In fact the occurrence of high levels of oxidant which consists almost

entirely of ozone has become the primary indicator for the presence and relative

severity of photochemical smog

During the 25 years since photochemical smog in Los Angeles County was

first identified an extensive program has been underway for control of the responshy

sible contaminant emissions Initially during the 1950 s these programs concenshy

trated on controlling emissions of hydrocarbons from the stationary sources of this

contaminant In the early 60 s programs for the control of hydrocarbon emissions

from motor vehicles in California were begun An exhaust emission control proshy

gram for hydrocarbons and carbon monoxide from new vehicles was begun in 1966

C011trol of oxides of nitrogen emissions from motor vehicles began in 1971

As a result of the overall control program by 1974 emissions of reactive

hydrocarbons from stationary sources have been reduced 70fo from uncontrolled

levels and about the same percentage from mobile sources Oxides of nitrcgen emissions

233

from statjonary sources have been reduced about 53 while emissions from moshy

bile sources are still about 7 above uncontrolled levels due to the increase

in NOx from 1966-1970 models Additional controls already planned for the future

will by 1980 achieve reductions of reactive hydrocarbons from stationary sources

of about 87 from uncontrolled levels and from mobile sources about 93 By

1980 emissions of oxides of nitrogen from stationary sources will have been reshy

duced 53 and from mobile sources 63 from uncontrolled levels The past

present and projected emissions of these contaminants are shown in Figure 1

A I though compliance with the air quality standards has not yet been achieved-shy

and is not likely before 1980- -the results of these programs have been reflected rather

predictably in changes in certain of the manifestations of photochemical smog For

example eye irritation is less frequent and less severe and in some areas js

rarely felt at all any more and damage to vegetation has been markedly reduced

Ozone (or oxidant) concentrations have been decreasing in Southern California

coastal areas since _1964 in areas 10-15 miles from the coast since 1966 and in

inland areas 40-60 miles from the coast since 1970 or 1971 as shown on Figures

2 arrl 3- All of these positive effects have occurred despite the continuing growth

of the area indicating that themiddot control programs are gradually achieving their purpos

a return to clean air

This improvement is al~o refutation of the so-called Big Box -concept which

assumes that the total daily emissions in a given area are somehow uniformly disshy

tributed throughout that area--regardless of its size or of known facts about the

meteorology of the area or the spatial and temporal distribution of its emissions- -

234

and of control strategies based on that concept And since the improvement in

air quality refutes the control strategies based on reductions in total emissions

it thus confirms the value of more recent control strategies which emphasize conshy

trol of motor vehicle emissions and use of a source-effect area concept

Following is a brief listing of the evidence we intend to present as supporting

our views on just what control strategy is appropriate

Examination of relative contributions of HC and NOx from stationarybull and mobile sources demonstrates that motor vehicles are the overwhelming

f source of both contaminants~

I bull Observation of air monitoring data shows that the effects of photochem -

ical smog are not uniformly distributed t_hroughout the county

bull Study of the meteorology of LA County shows consistent paths of trans -

port for various air parcels and consistent relationships between the

areas most seriously affected by photochemical smog and high oxidant

concentrations and certain other areas

bull The upwind areas are found to be source areas--the downwind areas-shy

effect areas

bull Central L A is found to be the predominant source area for the effectI area in which the highest oxidant levels in the SCAB consistently occur

bull The predominant source of emissions in this source area is found to

be motor vehicles

bull Central LA has the highest traffic density I

ij bull Both pr~mary and secondary contaminant concentrations reflect the effects

of the new motor vehicle control program in a predictable fashion 11 I

A strategy based upon these findings is gradually being verified by atmosshybull pheric oxidant data~

235

The Evidence that Motor Vehicle Emissions Are the Principal Source of Oxidant

As seen from Figure 1 at the present time the total daily emissions of I-IC

and_ NOx from all sources in Los Angeles middotcounty are primarily due to the motor

vehicle The problem now is to find the spatial and temporal representation of

emissions which when examined in the light of the known meteorology and geogra -

phy of the Los Angeles region best describes the source of emissions responsible

for the highest observed oxidant readings

In the rollback models used by EPA and others the basin is treated as a

big box with uniformly distributed emissions and peak oxidant is considered to

be proportional to total basinwide hydrocarbon emissions

The fact is that the middotemitted contaminants from which the smog is formed

and the effects which characterize that smog are not evenly distributed throughout

the Los Angeles Basin in other words the basin area under the inversion is not one

large box filled to all corners with homogeneously distributed air contaminants and

photochemical smog

Refutation of Big Box Myth

Examination of atmospheric contaminant concentrations refutes the big box

concept It is found for example that concentrations of djrectly emitted contam -

inants measured at a particular sampling site reflect the emissions within a rather

limited area around that site For this reason contaminant concentration levels

vary from one location to another and each has a characteristic daily pattern which

reflects the daily pattern of emissions in that area

middot 236

The big box concept is further refuted by the fact that peak concentrations

of carbon monoxide and oxides of nitrogen in areas of high traffic density were

fairly static prior to 1966 Thus they did not reflect the 45-50 per cent growth

in motor vehicle registrations and gasoline consumption which occurred in Los

Angeles County between 1955 and 1965 and which caused comparable increases in

total daily emissions of such vehicle-related contaminants This demonstrates

that growth was outward rather than upward so that a larger area of the County

began to be affected by photochemical smog but no area experienced smog ofJ

greater severity than that originally affected by smog formed from the vehicular

emissions which accumulated each weekday in central Los Angeles and were trans-

1 I

ported later that day to the San Gabriel Valley

1 Meteorological Evidence

To verify the geographical dependence of emissions and resulting atmospheric

concentrations let us examine the meteorology of these large areas of Southern

California Both the County and the Basin have many meteorological sub-regions

in which the patterns of wind speed and direction may be similar but within

which the patterns of air transport are parallel with those of adjacent sub-regions

and the respective air parcels do not ever meet or join

The characteristic patterns of inversion height and wind speed and direction

in these sub-regions and their patterns of vehicular emissions together have

created a network of source areas- -those in which the reactant contaminants accu -1T

i ~ mulate in the morning and begin to react--and related receptor areas--those to which

~ the products and associated effects of the photochemical reactions of the contamshy)

inants originally emitted in the source areas are carried by the late morning and

237 middot

afternoon winds ( sea breeze)

Wind-flow patterns show that characteristic patterns of transport for related

source area-effect area combinations are separate and parallel not mixing or

joining Each source area has its own reactor pipeline to its own effect area

or areas

To illustrate this source area-effect area relationship the typical flow of

polluted air from downtown Los Angeles to Pasadena was selected as a worst

case situation for in-depth examination Figure 4 shows that the air in downtown

Los Angeles on the morning of smoggy days moves directly from the central area

to Pasadena

Vehicular traffic is the predominant emission source in both downtown Los

Angeles and Pasadena Thus the air in each locality should contain CO Also

since oxidant would form in the air parcel moving from Los Angeles to Pasadena

oxidant levels would be expected to be higher in Pasadena than in downtown Los

Angeles

Figure 5 shows these relationships for the period 1960-1972 The atmosshy

pheric CO level is similar for the two areas while oxidant levels were higher in

Pasadena than in Los Angeles throughout this time period This demonstrates

that a significant amount of oxidant formed in the air as it moved to Pasadena

containing both the unreactive CO and the photochemical reactants for producing

oxidant Both CO and oxidant show a marked downward trend in each locality since

1965 which emphasizes the effect of vehicle exhaust controls and the correlation

between the localities

238

On a day which is favorable to the formation and accumulation of photoshy

chemical smog a contaminated air parcel normally originates during the

6-9 a m period on a weekday from an area of dense traffic centered just

south and west of Downtown Los Angeles It is oxidant generated within that air

parcel which usually affects Central Los Angeles and the West San Gabriel

middotK IJ l J

Valley area around Pasadena

The traffic area in which this smog had its origin is about the most dense

in Los Angeles County and has been so for the past 25-30 years No area

has a higher effective density thampn-this Using carbon monoxide which

1

is almost entirely attributable to motor vehicles as an indicator of such emis-

sions it is found that the concentrations of emitted vehicular contaminants

middotr i

measured in Central Los Angeles during the past 15 years confirms both this lack

of change in effective density and the absence of any area of any greater effective

density when local differences in inversion are acknowledged

This area the Central Source Area is depicted in Figure 4 The size

and shape of the Central Source Area was ch~sen to be large enough to reduce to

an insignificant level any diffusion or transport into this area from any externally

l generated reactants This conclusion is based in part on the trajectory studies

previously referenced as well as an analysis of the diffusion and transport parashy

meters for the area

239

The Central Source Area has been identified as that geographical region

which contributes essentially all of the primary contaminant emissions giving

rise to the highatmospheric oxidant levels in the West San Gabriel Valley

The proportion of emissions in the CSA due to motor vehicles and that due to

stationary sources is shown in Table 1 For the County as a whole about 80 per

cent of _(6-9) AM reactive hydrocarbons are due to motor vehicle emissions and this

figure rises to 90 per cent for the CSA The same conclusion a pp lies to NOx

emissions The Central Source Area contains the greatest density of vehicle traffic

in the County and thus the greatest density of source emissions Thus it appears

that the source area with the highest density of emissions during the critical (6-9)

AM period is responsible for the highest afternoon oxidant levels observed in Los

A i1geles County and in the South Coast Air Basin These highest oxidant levels

are consistently observed to occur in the San Gabriel Valley This is true whether

the LAAPCD or the ARB oxidant calibration procedure is used

Further the atmospheric concentrations of the primary pollutants can be

identified as originating primarily from the motor vehicle and they reflect the

effects of the motor vehicle emission control program A vehtcular source area

can be identified by its atmospheric levels of CO and NOx Figure 6 compares

measured atmospheric levels with calculated atmospheric levels for CO NOx

and the CONOx ratio in the downtown area

TABLE 1 240

REACTIVE HYDROCARBON EMISSIONS

(6-9) AM

1970

LOS ANGELES COUN1Y middot CENTRAL SOURCE AREA middot SOURCE TONS PER CENT TONS PER CENT

Mobile 1260 81 3 135 91 2

Stationary 290 187 1 3 88

Total 1s~o 1000 148 1000

By 7 -Mode Gallonage

241

The calculated values shown in Figure 6 were derived from a baseline

survey of 1100 vehicles and continued surveillance tests both using the Calishy

fornia 7-Mode test cycle The baseline survey showed that motor vehicles withshy

out exhaust control systems had average exhaust emissions concentrations of 3 4

per cent CO and 1000 parts per million of NOx Baseline emissions data apply

to 1965 and earlier model vehicleg and surveillance data to 1966 and later modelsmiddot

Since it can be concluded from calculations and observations that the dilushy

tion of auto exhaust emissions in the atmosphere on a smoggy day in Los Angeles

is approximately 1000 to 1 the calculated values for CO and NOx prior to 1965 are

34 ppm CO and 1 ppm NOxo After 1965 the changing effect of controlled vehicles

in the total vehicle population is reflected in the calculated values

CO and NOx values measured in the atmosphere are also shown in Figure

6 and confirm the values calculated entirely as diluted vehicular emissions NOx

concentrations measured in the atmosphere tend to be consistently a little lower

than the calculated values probably because photochemical reactions remove some

NOx from the system

The data for CO and NOx calculated and measured show that emissions in

downtown Los Angeles originate almost exclusively from motor vehicles and that

atmospheric concentrations there reflect the average emissions from a representashy

tive vehicle population

The ARB has recently published a report entitled A Trend Study of Two

Indicator Hydrocarbons in the South Coast Air Basin Acetylene was used as a

242

specific indicator of automobile exhaust emissions and it was found to have de-

clined in concentration in the Los Angeles atmosphere at an annual rate of 12 5

per cent since 1970 To quote from this report The California implementation

plan requires an annual average reduction in these emissions (reactive organic

compounds) of 166 tons per day or 11 1 of the 1970 tonnage per year The per cent

reductions in the_ acetylene levels at Los Angeles and Azusa are greater than reshy

quired by the implementation plan Since acetylene is almost entirely associated

J with auto exhaust this demonstrates that the motor vehicle emission control

program is achieving its purpose

To summarize at this point it has been deomonstrated that high oxidant values

are due to motor vehicular emissions of NOx and HC because

NOx and HC are the principal reactants in the oxidant formation process

and they originate primarily from motor vehicle emissions and

The highest oxidant values are recorded in_ effect areas that receive air

from source areas where motor vehicles are clearly identified as the

dominant source of NOx and HC

243

Future Control Strategy

The APCD strategy for achieving and maintaining the oxidant air quality

standard is based upon the fact that high oxidant values are due to motor ve-

hicle emissions of hydrocarlxms arrl nitrogen oxides This strategy is as follows

1 Both Hydrocarbon and Nitrogen Oxides Emissions Must Be Considered To Achieve the Federal Oxidant Standard

There is wide agreement that NOx and HC are the principal reactants in

the oxidant formation process and that vehicular emissions are a major source

of NOx HC and CO

2 Effective Regulation of Atmospheric Concentrations of Both HC and NOx and of the Ratio Between Them is necessary for Attainment of the Federal Air Quality Standard for Oxidant

Basmiddoted on the abundance middotof available experimental evidence it is our firm

position that the most rational approach to solving the photochemical oxidant smog

problem in the South Coast Air Basin (SCAB) is to control the quantities of emissions

from motor vehicles of both smog precursors--Hcmiddot and NOx--their resulting atmosshy

pheric concentrations and the ratios between both contaminants which will result

from these controls

We arc also convinced that the oxidant and nitrogen dioxide air quality stanshy

dards can and will be met not by 1975 or 1977 but by the early 1980 s if the emisshy

sion control program as originally outlined by Ca~ifornia or a slight modification

of it proposed by the District is followed and enforced This should also provide

for continued compliance with these air quality standards at least through 1990

244

It will also allow time for a reappraisal in about 1978 of the whole situation relative

to the ultimate emission standards required and the best approach to their impleshy

mentation

Calculation of the degree of control necessary to attain the air quality

~ standards for oxidant and nitrogen dioxide involves indirect complex methods 1

aimed at determ_ining the degree of control of the primary contaminants directly

emitted by automobiles

The following evidence supports our proposed solution to the problem in

terms of both the atmospheric concentrations of the oxidant precursors NOx

and HC the ratio between them as reflected in their exhaust emission standards

and the resulting atmospheric concentrations of oxidant which comply with the air

quality standards

Chamber Results and Projections to the Atmosphere

The importance of environmental chamberwork cannot be minimized the

j need for and direction of the whole emission control program was based initially

j on the results of chamber experiments In order to understand the importance to

air quality of achieving both the correct low quantities of emissions and the right

ratio we can present several graphic portrayals of analyses of experimental labshy

oratory work together with their relationship to past present and future air quality

in terms of both morning primary reactant concentrations during the morning

traffic peak and the equivalent emissions which would produce them

245

Figure 7 shows maximum ozone levels that were obtained by irradiating

varying amounts of auto exhaust hydrocarbons and oxides of nitrogen in an environshy

mental chamber The corresponding ozone levels then can be found for any comshy

bination of BC and NOx concentrations Thus high ozone is produced with high

emissions of both hydrocarbons and oxides of nitrogen and low oxidant is formed with

low emissions However either low NOx or low HC emissions11 can also produce

low oxidant--graphic and clear evidence of the importance of the NOxHC ratio in

ozone formation Furthermore each and every possible combination of values for

NOx and HC has then a corresponding characteristic maximum chamber ozone

concentration

Using this graph we can estimate what ozone levels would result if certain

atmospheric mixtures of NOx and HC could be injected into the chamber and

irradiated Such estimates were made for 1960 and 1965 using atmospheric data

rlThe points labeles 1960 and 65 show the location of the highest levels of both

HC and NOx found in the air in those years in Downtown Los Angeles (OOLA) area

during the 6-9 AM traffic peak

It has been demonstrated by use of CO and NOx data and CONOx ratios

hnw well the characteristics of vehicle emissions are reflected in the atmosphere

We know what emissions from the average vehicle were then in 1960-1965 both

for HC and NOx so that we can mathematically relate emissions to atmospheric

concentrations for those years and so for future years also knowing or calculating

only what the characteristic emissions will be from the average vehicle

246

The NOx concentrations stayed about the same from 1960 through 1965 because

average vehicle emissions of that contaminant did not change during that time

Mobile source emissions can be shown to have contributed essentially all of this obshy

served result However blow by controls did reduce emissions of HC and the

concentrations dropped accordingly In 1965 the last year before exhaust controls

the point 65 indicates where we were then in terms of maximum ozone formation

to be expected in a chamber with the highest HC and NO concentrations found in the X

air that year Levels of ozone actually measured in the atmosphere however

are higher than those shown on the graph for high NOx and I-IC concentrations for

those years up to the present

The strategy to meet the oxidant standard is obvious--get atmospheric NOx

and HC concentrations out of the area on the chart that produces high ozone levels

and put them in tie areas with the lowest levels This can only be done by implementshy

ing appropriate emission standards

As can be seen that did not happen between 1965 and 1970 because manufacshy

turers used controls on new cars in California which while causing a decrease in

BC (and CO) allowed a large increase in NOx emissions Thus the path line of

the atmosphere on the chart goes up from 65 and diagonally to the left passing

through an area of higher ozone levels The atmospheric concentrations of oxidant

predictably increased during the years 1967 and 1968 By 1970 they dropped to lower

levels - -back to about the same as in 1965- -exactly as predicted by the model The

app14oximate location of the point for 1970 (70) was both predicted on the basis of

247

the mathematical model and confirmed by atm-ospheric measurements of

[)owntown Los Angeles morning summertime NOx and calculated HC values

Again it should be pointed out that those points show the highest possible

concentrations of NOx and HC Years with less restrictive weather conditions

(for accumulating high primary contaminant levels) would cause lower measured

maximum NOx and HC levels but the calculations would still yield the points

shown Thus we are taking the most pessimistic view

Future Projections

In 1973 we were at about the point labeled 73 and ozone levels were beginshy

ning to drop as expected middot It should be emphasized that ozone values plotted on

thi$ graph are for the chamber only- -not the atmosphere The future path the

points 7 4 and on to 90 represents our estimate of future atmospheric levels of

NO and BC expected if the exhaust emission standards are just met While that X -

is optimistic it is all we really can do since performance of future vehicle models

is unknown We will achieve maximum ozone levels at or below the standard by

about 1980-1985 This will only be true however if cars in compliance with the

California interim standards for HC and NOx continue to be added to the vehicle

population at the normal rate These standards provide the optimum ratio of NO X

to HC necessary to provide the nitric oxide (NO) needed for the reaction that re-

moves from the air both oxidant formed photochemically and oxidant which occurs

as natural background which alone may cause the standard to be exceeded This

ratio is about 112 or 2 parts NOx to 1 part HC

248

The optimum NOxHC ratio is a key element in the APCD strategy but will

require a finite time for its attainment Replacement of older cars by newer ones

equipped to meet the most stringent standards is the only reasonable mechanism

which can change it VMT reduction proposed as a prime strategy by EPA cannot

change this crl(ical ratio which is a basic characteristic of the population at any

given time

Validation of the Districts Control Strategy

Figure 8 compares (1) future chamber oxidant levels based upon the

future maximum concentrations of HC and NOx we expect each year with the

California control program (2) calculated atmospheric concentrations using ~ I

our chamber-to-atmasphere empirical translation and (3) actual measured atmos-f 1l pheric oxidant maxima This clearly sets forth the relationship among these three

factors

The chamber concentrations (lower curve) middotare the lowest values shown

The actual atmospheric data (points connected by heavy dotted and solid lines)

vary considerably from year to year partly because of the vagaries of the weather

In all cases the atmospheric oxidant values are higher than the chamber values

because of the addition of vehicle emissions as the air parcel travels from source

to receptor areas The calculated atmospheric data (thin dashed and solid curves)

are shown to be the highest generally exceeding or equalling the actual measured

data and of course always exceeding the chamber data Thus the model paints

the most pessimistic picture possible It can be seen that by about 19801 1985 atmos -

pheric levels should be at or below the Federal air quality standard of 0 08 ppm oxidant

249

3 Motor Vehicle Exhaust Control is the Only Requirement for Achieving the Oxidant Standard by 1980

We can show that the existing motor vehicle control program has resulted

in a significant reduction of oxidant concentrations in the air

The foregoing material explained the relationship between vehicula~ emis -

sions in source areas and the high oxidant levels measured in effect areas This

relationship is exemplified by the downward trend of oxidant levels in the atmosshy

phere and by the similar year-by-year trends of NO and HC emissions from the X

average motor vehicle A projection of these vehicle emissions factors shows that

the associated maximum oxidant level in the atmosphere will meet the oxidant standard

by about 1980-1985

Figure 9 compares by year the number of days that the oxidant air quality

standard was exceeded in three separate areas with the average NO and HC emissions X

per vehicle mile To comply with the air quality regulations the number of days that

this standard is exceeded must be reduced to one per year

The lines plotted on Figure 9 show that a definite relationship exists between

the emissions from the average motor vehicle and the number of days each year that

the oxidant concentration in the air exceeds the clean air standard

The oxidant trendlines for downtown Los Angeles Pasadena arrl Azusa are

all downward and the slopes are about the same This similarity is logical because

the process that results in the suppression of oxidant accumulation simply has been

displaced from one area to another This was a unique one time situation because

of the increase in NOx between 1966 and 1971 After 1971 all areas are down Thus

l

250

the same conclusion is reached that the oxidantstandard will be met in the 1980s

I whether air quality data or vehicle emissions trends are projected middot~ Ul-

This outlook is based on the APCD s belief that future growth in both the

Los Angeles area and SCAB will not create any locality with a traffic density greater

than any traffic density in the area to date For the past 25 years the area around

downtown Los Angeles has been the area of maximum traffic density and therefore

the emissions source area responsible for the maximum effect area measurements

It is assumed that the traffic density in any future source area will be no

greater than the traffic density in downtown Los Angeles Thus since the

vehicular emissions control program will achieve and maintain the air quality

standards in areas affected by vehicular emissions from downtown Los Angeles it

will also achieve and maintain them for any area of SCAB

Summary Conclusions and Recommendations

In conclusion we have shown that a source and effect area analysis of emisshy

sions and resulting oxidant is a more reasonable and accurate representation of

the Los Angeles area for air quality analysis than gross integration metho9s such

as the big box technique It has been shown that motor vehicles are the major and

almost sole contributor to the primary HC and NOx emissions in the downtown source

area which results in the high oxidant levels in the San Gabriel Valley in fact the

highest in SCAB An air quality model and vehicle emissions control strategy has

been suggested to meet the oxidant standard by mid-1980 s

251

We have shown that

bull Only by adjusting the ratio of NOxHC in the motor vehicle emissions to

permit accumulation of sufficient atmospheric NO to sea venge the normal

atmospheric background oxidant can the standard be attained

bull The APCD strategy which provides for implementation of the present

California interim emissions standards for NOx HC and CO for new

motor vehicles in California beginning with the 1975 model vehicles will

result in compliance with the CO N02 and oxidant air quality standards

by the mid 1980 s and will maintain this compliance until 1990 and

possibly longer

bull The effectiveness of the present California motor vehicle control program

is easily demonstrable using air quality data from several areas in Los

Angeles County 1960-1973

bull To assure achievement and maintenance of the air quality goals as now preshy

dicted there must be periodic assessments of the effectiveness of the

motor vehicle control program followed by corrective actions if necessary

What has been accomplished thus far is significant but much more remains

to be done so that the best possible representation of emissions and resulting air

quality may be available for use in this air basin A much better emission inventory

defining the spatial and temporal distribution of both mobile and stationary sources

is needed Better statbnary source information is needed to evaluate the local

effects of these emissions Further detailed studies are needed to establish the

252

true relationship between emissions data from vehicle test cycles and the actual

operation of vehicles neither the 7-mode nor the CVS procedure provides a true

representation of actual vehicle operation Further tracer studies to assess the

transport and dilution of mobile and stationary source emissions from selected

source areas are also needed

253

1111

IUD

a CC I w gt-

1111

1UO

IUD

I 990

IDJO

1180

1111

IUO

FIGURE I

HYDROCARBONS

STATIONARY SOURCES MOTOR VEHICLES

- --

8 12 II 20 742 2l IS 12 I 4

HUNDREDS

HYDROCARBON EMISSIONS STATIONARY SOURCES IN

OXIDES OF

0

OF TONSDAY

FROM MOTOO VEHICLES AND LOS ANGELES COUNTY

NITROGEN

STATIONARY SOURCES

MOTOR VEHICLES

011111111111111111110111bull1111111

IIIIIIHIIIIIIIIIHIUII

llillL Its rd

l1uu~111111u1111111

2 I O 1 J 3

HUND REDS OF TONSDAY

OXIDES OF NITROGEN EMISSIONS FROM MOTOR VEHICLES ANO STATIONARY SOURCES IN LOS ANGELES COUNTY

illl~ -~--~ i~-=i _J~l ~--~ bull_~L- I ~~~-~~--Z ~

6

6S-66 ox

ICS ~A~1 M

i ssmuwmmgt

bullI

e COROyent_

64 ~ IDB RIVERS~

ORAJfD

-

t t 10 miles

bullmiddotsame Avg Cone Both Years

Pigare 2

YEAR OP HIGHEST OXlDANI CONCENTRATIONS

Highest Average of Daily -Maiimum One-Hour Concentrations

During July August amp September 1963-1972

bullLj

I

64

70 s11 3RlU)U0

70

--__ 69bull

N V +=

middot Source Air Resources Board

-200o

t t 10 adlea

tDS ampIJtsect

-1~

-1611ASampXllmiddot bull - bull -z----~------

I ldmmprwJ

IIVERSIDI

~ - 70

OampY -1 U 70 bull L

I

N V1 V

middot-i___

-----------------------------------------------------------i----------------------------

Figure 3

CHANGE OP OXIDANT CONCENTRATIONS

Percent Change from the Highest Three-Year Average to the 1970-72 Average

Of Daily Maximum One-Hour Con~entrationa for JulY August amp September

Source Air Resources Board

256

FIGURE 4 TYPICAL FLOW OF POLLUTED Am PARCEIS CIUGINATING AT DIFFERENT LOCATIONS IN THE LOS ARE~S BASIN - STARTIOO 0900 PST

l I

OAT

TRAJECTORY SUWMATIOl4

----- SMOG ~AVS

I

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullNONbullSlfOG DAYS

ISTARTING Tl~ cgxpsy

~ HAW

(CA

257

FiGURE 5 ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AND OXIDANT IN DOWlflC1N LOS AIDELES (SOURCE AREA) AND PASADENA (EFFECT AREA) 1

1960-1972

LO CARBON MONOXIDE

30

Pasadena

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullbullbullbullbull Downtown Los Angeles

20

10

o_______________________________

OXIDANT

)

2 Down~ Los Angeles

1

o________________________ 1960 1962 196L 1966 1968 1970 1972

YEAR

bullbullbullbullbull

bullbullbullbullbullbullbull

258

FIGURE 6 COMPARISON 01 CALCULATED AND MEASURED ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AN1) OXIDES OF NITROOEN IN DCMNTOWN IDS AIJELES

196o-1972

CARBON MONOXIDE

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ~ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot _-- ---_ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ----middotmiddot-bullw-_~ ---bullbullbull

10

o_______________1111111_____

OXIDES OF NITROGEN25

20

15 bullbullbullbullbullmiddotmiddotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~

1-i 10 middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ---

oS o_______________________

RATIO CONOx

40

50

0 +raquo Cd

p 30

~ 20

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot bullbullbullbullbull middotmiddotmiddotmiddotmiddot-shybullbullbullbullbull 0 u

bullbullbullbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot 10

0 j

ilI 196o 1964 1968 1970 1972 I

YEAR

Measured~D-owntown Los Angeles (90th percentile ofmiddot daily] instantaneous maxima)

Calculated - Aver~ge vehicle emissions - Present control program

259

FIGURE 7

25

t i5

flJ

~ on ~ ~ Q) bO 100 Jo

+gt on z

o5

EFFECT OF CALIFORNIA 1 s AUTO EXHAUST CONTROL ffiOORA M ON MAXIMUM CHAMBER OZONE CONCENTRATION

- PPM

357bullbull

r 76 bull

11 l

30

20

CHAMBER OZONE MAXIMUM

50

10

o___________111111111111______111111111111_____________

0 05 10 15 20 25

Hydrocarbons m-2 (LB-15) - PPM (as Hexane)middot

--

bull bull bull

r--=--~1 ~a==-~ - _~l ~ y--===-- ~~--~-- ~ r---~~

o

o8

~ I

~ 0 H 8 o6 I

c~ ~ 0 z 0 0

8

~ o+ A H gtlto-

02

middoto

Figure 8 Calculated t1ax1mum Levels Instantaneous and Hourly Average

of Atmospheric Oxidant Compared to Measured Los Angeles County Maxima-with Projections to 1990

(California Standards)

~ -Calculated Inst ax ~

f Calculate Max Hr Avg 03

_ bullbull _ _ - i bull

0 bullbull -l bullbull a0Ieasured Inst Lax o3 bull middotmiddotmiddot~bull 0bull _ ____ V ~ ea~ured ~ Hr Avr o3

~~ r---

~ ~ NB r~ima for 197 4 amiddots of 121074--- -_ Chamber Ozone F ~_ _~

- 1L_

~ Federal Primarfo Air ~uality Standard ~6- -UaximumT- our Avera~elr~ppm-------------- --~ ------- -~- -~-- ~

I I I I I I I I I I I I I I I I I N1 O

1960 6i 64 66 ~i middot-o 72 74 76 79 middotso middot92 84 bullg s9 9o

TBAR (end)

0

261 FIGURE -OMPARISON OF ATMOSPHERIC OXIDANT TRENDS WITH AVERAGE NCJx AND

HC EMISSIONS (Grams per Mile from Average Vehicle)

JOO Number of days state oxidant standara wds equalled or exceeded

--- Azusa __ Pasadena ________ Downtown Los Angeles

20

15 u

___ Hydroc_arbons Oxides of Nitrogenbullmiddotmiddotmiddotmiddotmiddotbullbullmiddot 1975 and later-assume middotcalifornia ARB standards

o_ ___________________________11111____

1965 1970 1975middot 198omiddot 198S 1990

143

adverse effect on the lifetime of the cata]_yst This is not so obvious

It is also likely that the higher temperature duty cycle in actual use will

improve the performance of the catalyst in that it will help to regenerate

the catalyst through the removal of contaminants as long as one does not

get into an overheat situation The National Academy of Sciences estimate

was that the number of catalyst failures tn the first 50000 miles would

be on the order of about 7 Thats a very difficult number to estimate in

the absence of any real data A 7 failure still leaves a net gain in

emissions control even if nothing is done about this failure This points

to the problem of what happens after 50000 miles The EPA certification

procedure and control program only addresses the first 50000 miles The

second 50000 miles or slightly less for the average car is the responsishy

bility of the states Unfortunately then~ seems to be very little progress

in the area of mandatory inspection and ma-Lntenance--very little thought

being given to whether the replacement ofthe catalyst at 50000 miles

if it has failed is going to be required and how that is going to be

brought about The area of field performance remains a major problem

area one which obviously needs to be monitored as the California Air

Resources Board has been doing in the past but probably even more carefully

because the unknowns are higher with the catalyst systems

Problem Area Number Two Evaporative hydrocarbons from automobiles

It was identified at least 18 months ago that the evaporative emission

control systems are not working that the evaporative emissions are on the

order of 10 times greater than generally thought In the Los Angeles

area cars which are supposed to be under good evaporative emissions

controls are emitting approximately 19 grams per mile of hydrocarbons

through evaporation This apparently has to do with the test procedure used

144

The EPA is pursuing this The California Air Resources Board does have some

consideration going on for this but it appears that the level of activity

in resolving this problem is simply not adequate If we are to go ahead

to 04 of a gram per mile exhaust emissions standards for hydrocarbons

then it just doesnt make sense to let 19 grams per mile equivalent escape

through evaporative sources

Problem Area Number Three What about the secondary effects of the

catalyst control systems Specifically this is the sulfate emissions

problem and I really do not know the answer to that Our appraisal is

that it is not going to be an immediate problem so we can find out what

the problem is in time to solve it The way to solve it now since the

automobile industry is committed to catalysts and it is unreasonable

to expect that they will reverse that technology in any short period of

time is take the sulfur out of the gasoline The cost of removing sulfur

from gasoline is apparently less than one cent per gallon Therefore if

it becomes necessary to be concerned with sulfate emissions the way to

meet the problem is to take the sulfur out of gasoline Obviously sulfate

emissions need to be monitored very carefully to see what happens The

final appraisal is certainly not now available Another secondary effect

of the catalysts is the introduction of significant quantities of platinum

into an environment where it hasnt existed before Not only through

exhaust emissions which appear to be small but also through the disposal

problem of the catalytic reactors Since the quantity of platinum involved

is quite small the argument is sometimes used that platinum does not

represent much of a problem The fact that the amount of platinum in the

catalyst is so small may also mean that its not economical to recover it

This is probably unfortunate because then the disposal of these catalysts

l Jj

145

I becomes important I will not speak to the medical issues because

am not qualified The evidence is that theuro~ platinum will be emitted in a

form which does not enter into biological cycles--but this is no assurance

that it couldnt later be transformed in such a form What is obviously

needed is a very careful monitoring program which hopefully was started

before the catalysts were put into service If it wasnt then it should

be started today

Problem Area Number Four NO control The big problem with NO X X

control is that nobody seems to know or to be willing to establish what

the emission control level should be It is essential that this be tied

down rapidly and that it be fixed for a reiatively long period of time

because the NO level is going to have a VE~ry important ef feet upon the X

development of advanced engine technology The 20 gm level has been

attained in California with some loss of fuel economy through the use of

EGR and it is not unreasonable in our estimation to go to 15 grams per

mile with very little loss in fuel economy To go to 04 gram per mile

with present technology requires the use of one of two catalytic systems

either the reduction catalyst in tandem with the oxidation catalyst or what

is known as the three-way catalyst Both of these systems require technoshy

logical gains The state of development appears to be roughly that of the

oxidation catalyst two years ago The auto industry will probably say

that it is not quite that advanced but that if it were required to go to

04 gram per mile in 1978 that it could be done With the catalyst systems

the fuel economy penalties would not be great in fact the improvement to

the engine which would be required to make the system work would again

probably even allow a slight improvement in fuel economy What the 04

gram per mile NO catalyst system would appear to do however is to X

146

eliminate the possibility of the introduction of stratified charge engines

both the CVCC and the direction injection system and also diesel engines

It is in the context of the advantages of these advanced engines to meet

emission standards with improved fuel economy that one should be very

cautious about the 04 grammile oxides of nitrogen standards for automoshy

biles My own personal opinion is that the number should not be that

stringent that a number of 1 or 15 gm is appropriate Such a level

would require advancements but would not incur great penalties

Other items which I view as problem areas are less technically

involved and therefore require fewer comments

bull Nonregulated pollutants--again thls is a matter of keeping track

of particulates aldehydes hydrocarbon composition to make

certain that important pollutants ire not being overlooked or

that emission control systems are not increasing the output of

some of these pollutants

bull Fuel economy The pressures of fuel economy are going to be used

as arguments against going ahead wlth emissions control Mostly

these two can be resolved simultaneously We should simply ask

the automobile industry to work harder at this

bull Final problem area New fuels Again it does not appear that

the introduction of new fuels will come about as an emissions

control approach but that they may be introduced because of the

changing fuel availability patterns and the energy crisis These

fuels should be watched carefully for their impact upon emissions

This does middotappear to be an area in which a great deal of study is

going on at the present time It is one problem area perhaps in

which the amount of wprk being done is adequate to the problem

which is involved

147

In sunnnary then the appraisal of the 1975 systems is that they are

a big advancement they will be a lot better than most of us thought and

that we should give the automobile industry credit for the job theyve

done in coming up with their emissions control systems

With that boost for the auto industry which Im very unaccustomed

to Ill entertain your questions

-------=-~ ~~~ U- ~a1

~_~a--~-~ -J~ ~ -~r- _ --=~-- -___ja--~ __1~~ ~-~----=

AIR

1-4 FUEL----1

I I ENGINE

I II

_________ EXHAUST SYSTEM I bull EXHAUST

I I I

+ MIXTURE CONTROL COMBUSTION MODIFICATION EXHAUST TREATMENT

FuelAir Metering Ignition Air Jnjection FuelAir Mixing Chamber Geometry Thermal Reactor Fuel Vaporization Spark Timing Oxidation Catalyst Mixture Distribution Staged Combustion Reduction Catalyst Fuel Characteristics Ex tern almiddot Combustion Three Way Catalyst Exhaust Gas Redrculation Particulate Trap

FIGURE 1 Approaches to the Control of Engine Emissions

~ i 00

149

TABLE I

Average Emissions of 1975 Certification Vehicles (As Corrected Using the 50000-Mile Deterioration Factor)

Emissions in gmi Fraction of Standard HC CO NO HC CO NO

Federal 1975 X X

AMC 065 67 25 043 045 080

Chrysler 074 77 25 049 051 082

Ford 081 92 24 054 061 078

GM 083 80 23 055 053 074

Weighted Average 080 82 24 053 055 076

California 1975

AMC 042 49 17 047 054 087

Chrysler 048 61 16 053 067 082

Ford 052 56 13 058 062 067

GM 065 55 16 0 72 061 082

Weighted Average 058 56 16 064 062 078

kWeighted average assumes the following market shares AMC 3 Chrysler 16 Ford 27 and GM 54

150

TABLE II

Total Number of Vehicles Certified for California 1975 Standard and the Number (and percentage) of These Able to Meet

Certain More Stringent Standards

Calif 1975 Federal 1977 Hypothesized Hypothes ized 099020 04J420 049020 093420

i ~

Manufacturer no () no () no () no ()

AMC 16 (100) 1 ( 6) ti ( 38) 3 (19)

Chrysler 21 (100) 2 ( 9) ( 33) 0 ( O)

Ford 26 (100) 4 (15) -middot ( 15) 5 (19)

l GM 46 (100) 1 ( 2) -1 ( 9) 5 (11)

Foreign 62 (100) 21 (34) 3H (61) 28 (45)

1J

f

-l

151

CURRENT STATUS OF ALTERNATIVE AUTOM)BIIE ENGINE TECHNOLCXY

by

Henry K Newhall Project Leader Fuels Division

Chevron Research CanpanyRicbmmd California

I

iH1middot

10 1ntroduction and General Background

I

11 General

The term stratified ct1arge englne has been used for many

years in connection with a variety of unconventional engine

combustion systems Common to nearly all such systems is

the combustion of fuel-air mixtures havlng a significant

gradation or stratification in fuel- concentration within the

engine combustion chamber Henee the term nstratifled charge

Historically the objective of stratified charge engine designs

has been to permit spark ignition engine operation with average

or overall fuel-air ratios lean beyond the ignition limits of

conventional combustion systems The advantages of this type

of operation will be enumerated shortly Attempts at achieving

this objective date back to the first or second decade of this

century 1

More recently the stratified charge engine has been recognized

as a potential means for control of vehicle pollutant emissions

with minimum loss of fuel economy As a consequence the

various stratified charge concepts have been the focus of

renewed interest

152

12 Advantages and Disadvantages of Lean Mixture Operation

Fuel-lean combustion as achieved in a number of the stratified

charge engine designs receiving current attention has both

advantages and disadvantages wnen considered from the comshy

bined standpoints of emissionsmiddot control vehicle performance

and fuel economy

Advantages of lean mixture operation include the following

Excess oxygen contained in lean mixture combustion

gases helps to promote complete oxidation of hydroshy

carbons (HG) and carbon monoxide (CO) both in the

engine cylinder and in the exhaust system

Lean mixture combustion results in reduced peak

engine cycle temperatures and can therefore yield

lowered nitrogen oxide (NOx) emissions

Thermodynamic properties of lean mixture combustion

products are favorable from the standpoint of engine

cycle thermal efficiency (reduced extent cf dissociashy

tion and higher effective specific heats ratio)

Lean mixture operation caG reduce or eliminate the

need for air throttling as a means of engine load

control The consequent reduction in pumping losses

can result in significantly improved part load fuel

economy

153

Disadvantages of lean mixture operation include the following

Relatively low combustion gas temperatures during

the engine cycle expansion and exhaust processes

are inherent i~ lean mixture operation As a conseshy

quence hydrocarbon oxidation reactions are retarded

and unburned hydrocarbon exhaust emissions can be

excessive

Engine modifications aimed at raising exhaust temperashy

i tures for improved HC emissions control (retarded middot~

ignition timing lowered compression ratlo protrtacted combustion) necessarily impair engine fuel economy1 I

1j bull If lean mixture operation is to be maintained over ~

the entire engine load range maximum power output t l and hence vehicle performance are significantly

impaired

Lean mixture exhaust gases are not amenable to treatshy

ment by existing reducing catalysts for NOx emissions

control

Lean mixture combustion if not carefully controlled

can result in formation of undesirable odorant

materials that appear ln significant concentrations

in the engine exhaust Diesel exhaust odor is typical

of this problem and is thought to derive from lean mixshy

ture regions of the combustion chamber

154

Measures required for control of NOx emissions

to low levels (as example EGR) can accentuate

the above HC and odorant emissions problems

Successful developmentmiddotor the several stratified charge

engine designs now receiving serious attention will depend

very much on the balance that can be achieved among the

foregoing favorable and unfavorable features of lean comshy

bustion This balance will of course depend ultimately on

the standards or goals that are set for emissions control

fuel economy vehicle performance and cost Of particular

importance are the relationships between three factors -

UBHC emissions NOx emissions and fuel economy

13 Stratified Charge Engine Concepts

Charge stratification permitting lean mixture operation has

been achieved in a number of ways using differing concepts

and design configurations

Irrespective of the means used for achieving charge stratifishy

cation two distinct types of combustion process can be idenshy

tified One approach involves ignition of a small and

localized quantity of flammable mixture which in turn serves

to ignite a much larger quantity of adjoining or sur~rounding

fuel-lean mixture - too lean for ignition under normal cirshy

cumstances Requisite m1xture stratification has been achieved

155

in several different ways rangiDg from use of fuel injection

djrectly into open combustion chambers to use of dual

combustion chambers divided physically into rich and lean

mixture regions Under most operating conditions the

overall or average fuel-air ratio is fuel-lean and the

advantages enumerated above for lean operation can be realized

A second approach involves timed staging of the combustion

process An initial rich mj_xture stage in which major comshy

bustion reactions are completed is followed by rapid mixing

of rich mixture combustion products with an excess of air

Mixing and the resultant temperature reduction can in

principle occur so rapidly that minimum opportunity for NO

formation exists and as a consequence NOx emissions are

low Sufficient excess air is made available to encourage

complete oxidation of hydrocarbons and CO in the engine

cylinder and exhaust system The staged combustion concept

has been specifically exploited 1n so-called divided-chamber

or large volume prechamber engine designs But lt will be

seen that staging is also inherent to some degree in other

types of stratified charge engines

The foregoing would indicate that stratified charge engines

can be categorized either as lean burn engines or staged

combustion engines In reality the division between conshy

cepts is not so clear cut Many engines encompass features

of both concepts

156

14 Scope of This Report

During the past several years a large number of engine designs

falling into the broad category of stratified charge engines

have been proposed Many of these have been evaluated by comshy

petent organizations and have been found lacking in one or a

number of important areas A much smaller number of stratified

charge engine designs have shown promise for improved emissions

control and fuel economy with acceptable performance durashy

bility and production feasibility These are currently

receiving intensive research andor development efforts by

major organizations - both domestic and foreign

The purpose of this report is not to enumerate and describe the

many variations of stratified charge engine design that have

been proposed in recent years Rather it is intended to focus

on those engines that are receiving serious development efforts

and for which a reasonably Jarge and sound body of experimental

data has evolved It is hoped that this approach will lead to

a reliable appraisal of the potential for stratified charge

engine systems

20 Open-Chamber Stratified Charge Engines

21 General

From the standpoint of mechanical design stratified charge

engines can be conveniently divided into two types open-chamber

and dual-chamber The open-chamber stratjfied charge engine

has a long history of research lnterest Those crigines

157

reaching the most advanced stages of development are probably

the Ford-programmed c~mbustion process (PROC0) 2 3 and Texacos

controlled combustion process (TCCS) 4 5 Both engines employ a

combination of inlet aar swirl and direct timed combustion

chamber fuel injection to achieve a local fuel-rich ignitable

mixture near the point of ignition _For both engines the overshy

all mixture ratio under most operating conditions is fuel lean

Aside from these general design features that are common to

the two engiries details of their respective engine_cycle proshy

cesses are quite different and these differences reflect

strongly in comparisons of engine performance and emissions

characteristics

22 The Ford PROCO Engin~

221 Description

The Ford PROCO engine is an outgrowth of a stratified charge

development program initiated by Ford in the late 1950s The

development objective at that time was an engine having dieselshy

like fuel economy but with performance noise levels and

driveability comparable to those of conventional engines In

the 1960s objectives were broadened to include exhaust

emissions control

A recent developmental version of the PROCO engine is shown in

Figure 2-1 Fuel is injected directly into the combustion chamber

during the compression stroke resulting in vaporjzation and

formation of a rich mixture cloud or kernel in the immediate

158

vicinity of the spark plug(s) A flame initiated in this rich

mixture region propagates outwardly to the increasingly fuelshy

lean regions of the chamber At the same time high air swirl

velocities resulting from special orientation of the air inlet

system help to promote rapid mixing of fuel-rich combustion

products with excess air contained in the lean region Air

swirl is augmented by the squ1sh action of the piston as it

approaches the combustion chamber roof at the end of the comshy

pression stroke The effect of rapid mixing can be viewed as

promoting a second stage of cori1bustion in which rlch mixture

zone products mix with air contained in lean regions Charge

stratification permits operation with very lean fuel-air mixshy

tures with attendent fuel economy and emissj_ons advantages In

addition charge stratification and direct fuel injection pershy

mit use of high compression ratios with gasolines of moderate

octane quality - again giving a substantial fuel economy

advantage

Present engine operation includes enrichment under maximum

power demand conditions to mixture ratios richer than

stoichiometric Performance therefore closely matches

that of conventionally powered vehicles

Nearly all PROCO development plans at the present time include

use of oxidizing catalysts for HC emissions control For a

given HC emissions standard oxidizing catalyts permit use

of leaner air-fuel ratios (lower exhaust temperatures)

1

l

159

together with fuel injection and ignition timing charactershy

istics optimized for improved fuel economy

222 Emissions and Fuel Economy

Figure 2-2 is a plot of PROCO vehicle fuel economy versus NOx

emissions based or1 the Federal CVS-CH test procedure Also

included are corresponding HC and CO emissions levels Only

the most recent test data have been plotted since these are

most representative of current program directions and also

reflect most accurately current emphasis on improved vehicle

fuel economy 6 7 For comparison purposes average fuel

economies for 1974 production vehicles weighing 4500 pounds

and 5000 pounds have been plotted~ (The CVS-C values

reported in Reference 8 have been adjusted by 5 to obtain

estimated CVS-CH values)

Data points to the left on Figure 2-2 at the o4 gmile

NOx level represent efforts to achieve statutory 1977

emissions levels 6 While the NOx target of o4 gmile was

met the requisite use of exhaust gas recirculation (EGR)

resulted in HC emissions above the statutory level

A redefined NOx target of 2 gn1ile has resulted in the recent

data points appearing in the upper right hand region of

Figure 2-2 7 The HC and CO emissions values listed are

without exhaust oxidation catalysts Assuming catalyst middotl

conversion efficiencies of 50-60 at the end of 50000 miles

of operation HC and CO levels will approach but not meet

160

statutory levels It is clear that excellent fuel economies

have been obtained at the indlcated levels of emissions

control - some 40 to 45 improved re1at1ve to 1974 produc-

tj_on vehicle averages for the same weight class

The cross-hatched horizontal band appearing across the upper

part of Figure 2-2 represents the reductions in NOx emissions

achieveble with use of EGR if HC emissions are unrestricted

The statutory 04 gmile level can apparently be achieved

with this engine with little or no loss of fuel economy but

with significant increases in HC emissions The HC increase

is ascribed to the quenching effect of EGR in lean-middotmixture

regions of the combustion chamber

223 Fuel Requirements

Current PROCO engines operated v1ith 11 1 compression ratio

yield a significant fuel economy advantage over conventional

production engines at current compression ratios According

to Ford engineers the PROCO engine at this compression

ratio j_s satisfied by typical fu1J-boi1ing commercial gasoshy

lines of 91 RON rating Conventional engines are limited to

compression ratios of about 81 and possibly less for

operation on similar fuels

Results of preliminary experiments indicate that the PROCO

engine may be less sensitive to fuel volatility than convenshy

tional engines - m1 important ff1ctor in flextb1 llty from the

standpoint of the fuel supplier

161

224 Present Status

Present development objectives are two-fold

Develop calibrations for alternate emissions target

levels carefully defining the fueleconofuy pbtenshy

tial associated with each level of emissions control

Convert engine and auxiliary systems to designs

feasible for high volume production

23 The Texaco TCCS Stratified Charge Engine

231 General Description

Like the Ford PROCO engine Texacos TCCS system involves_

coordinated air swirl and direct combustion chamber fuel

injection to achieve charge stratification Inlet portshy

induced cylinder air swirl rates typically approach ten times

the rotational engine speed A sectional view of the TCCS

combustion chamber is shown in Figure 2-3

Unlike the PROCO engine fuel injection in the TCCS engine

begins very late in the compression stroke - just before th~

desired time of ignition As shown in Figure 2-4 the first

portion of fuel injected is immediately swept by the swirling

air into the spark plug region where ignition occurs and a

flame front is established The continuing stream of injected

fuel mixes with swirling air and is swept into the flame

region In many respects the Texaco process resembles the

162

spray burning typical of dj_esel combustion ~r1th the difshy

ference that ignition is achieved by energy from an elec-

tric spark rather than by high compression temperatures

The Texaco engine like the diesel engine does not have a

significant fuel octane requirement Further use of positive

spark ignition obviates fuel I

cetane requirements character-

istic of diesel engines The resultant flexibility of the

TCCS engine regarding fuel requirements is a si~1ificant

attribute

In contrast to the TCCS system Fords PROCO system employs

relatively early injection vaporization and mixing of fuel

with air The combustion process more closely resembles the

premixed flame propagation typical of conventional gasoline

engines The PROCO engine therefore has a definite fuel

octane requirement and cannot be considered a multifuel

system

The TCCS engine operates with hi__gh compression ratios and

with little or no inlet air throttling except at idle conshy

ditions As a consequence fuel economy is excellent--both

at full load and under part load operating conditions

232 Exhaust Emissions and Fuel Economv

Low exhaust temperatures characteristlc of the TCCS system

have necessitated use of exhaust oxidation catalysts for

control of HC emissions to low lf~Vels A11 recent development

163

programs have therefore included use of exhaust oxidation

catalysts and most of the data reported here r~present tests

with catalysts installed or with engines tuned for use with

catalysts

Figures 2-5 and 2-6 present fuel economy data at several

exhaust emissions levels for two vehicles--a US Army M-151

vehicle with naturally aspirated 4-cylinder TCCS conversion

and a Plymouth Cricket with turbocharged 4-cylinder TCCS

engine 9 10 1urbocharging has been used to advantage to

increase maximum power output Also plotted in these figures

I are average fuel economies for 1974 production vehicles of

similar weight 8

I When optimized for maximum fuel economy the rrccs vehicles

can meet NOx levels of about 2 gmile It should be noted

that these are relatively lightueight vehicles and that

increasing vehicle weight to the 4000-5000 pound level could

result in significantly increased NOx emissions Figur~s 2-5

and 2-6 both show that engine modifications for reduced NOx

levels including retarded combustion timing EGR and increased

exhaust back pressure result in substantial fuel economy

penalties

For the naturally aspirated engine reducing NOx emissions

from the 2 gmile level to O l~ gmile incurred a fuel

economy penalty of 20 Reducing NOx from the tllrbocharged

164

engine from 15 gmile to 04 gmile gave a 25 fuel economy

penalty Fuel economies for both engines appear to decrease

uniformly as NOx emissions are lowered

For the current TCCS systems most of the fuel economy penalty

associated with emissions control can be ascribed to control

of NOx emissions although several of the measures used for

NOx control (retarded cornbusticn timing and increased exhaust

back pressure) also help to reduce HG emissions HC and CO

emissions ari effectively controlled with oxidation catalysts

resulting in relatively minor reductions in engine efficiency

233 TCCS Fuel Reauirements

The TCCS engine is unique among current stratified charge

systems in its multifuel capability Successful operation

with a nuraber of fuels ranging from gasoline to No 2 diesel

Table 2-I

Emissions and Fuel Economy of Turbocharged TCCS Engine-Powered Vehicle 1

Fuel

Emissions gMile 2 Fuel Economy

mng 2HC co NOx

Gasoline

JP-4

100-600

No 2 Diesel

033

026

014

027

104

109

072

J bull l ~

-

061

050

059

060

197

202

213

230

1M-151 vehicle 8 degrees coffibustion retard 16 light load EGR tw0 catalysts (Ref 10)

2 CVS-CH 2750 pounds tnert1a welght

165

l

has been demonstrated Table ~-I lists emissions levels and

fuel economies obtained with a turbocharged TCCS-powered

M-151 vehicle when operated on each of four different fuels 10

These fuels encompass wide ranges in gravity volatjlity

octane number and cetane leve 1 as middotshown in Table 2-II

Table 2-II

Fuel Specifications for TCCS Emissions Tests (Reference 10)

Gravity 0 API Sulfur

OFDistillation~

Gasolj_ne 100-600 JP-4 No 2

Diesel

88 -

86 124 233 342 388

0024 912

-

486 012

110 170 358 544 615

0002 57 356

541 0020

136 230 314 459 505

-middot --

369 0065

390 435 508 562 594

--

lta 9

IBP 10 50 90 EP

TEL gGal Research Octane Cetane No

Generally the emissions levels were little affected by the

wide variations in fuel properties Vehicle fuel economy

varied in proportion to fuel energy content

As stated above the TCCS engine is unique in its multifuel

capability The results of Tables 2-I and 2-II demonshy

strate that the engine has neither 8ign1ficant fuel octane

nor cetane requirements and further that it can tolerate

166

wide variations j_n fuel volati1tty rhe flexibility offered

by this type of system could be of major importance in

future years

234 Durability Performance Production Readiness

Emissions control system durability has been demonstrated by

mileage accumulation tests Ignltion system service is more

severe than for conventional engines due to heterogeneity of

the fuel-air mixture and also to the high compression ratios

involved The ignition system has been the subject of

intensive development and significant progress in system

reliability has been made

A preproduction prototype engine employing the TCCS process is

now being developed by the Hercules Division of White Motors

Corporation under contract to the US Army Tank Automotive

Command Southwest Research Inr)titute will conduct reliability

tests on the White-developed enGines when installed in Military

vehlcles

30 Small Volume Prechambcr Eng1nes (3-Valve Prechamber Engines Jet Ignition Engines Torch Ignition Engines)

31 General

A number of designs achieve charge stratification through

division of the combustion region into two adjacent chambers

The emissions reduction potentiampl for two types of dualshy

chamber engines has been demonstrated F1 rst ~ j n B desJgn

trad1t1on~JJy caJJld the nrreebrnber engine a 2m211 auxil1ary

167

or ignition chamber equipped w1th a spark plug communicates

with the much larger main combustion chamber located in the

space above the piston (Figure 3-1) The prechamber which

typically contains 5-15 of the total combustion volume

is supplied with a small quantity of fuel-rich ignitable

fuel-air mixture while a large quantity of very lean and

normally unignitable mixture is applied to the main chamber

above the piston Expansion of high temperature flame

products from the prechamber leads to ignition and burning

of the lean maj_n chamber fuel-a_r charge Ignitionmiddot and

combustion in the lean main chamber region are promoted both

by the high temperatures of prechamber gases and bythe

mixing that accompanies the jet-like motion of prechamber

products into the main chamber

I jl

I i j

I

Operation with lean overall mixtures tends to limit peak comshy

bustion temperatures thus minimizing the formation of nitric

oxide Further lean mixture combustion products contain

sufficient oxygen for complete oxidation of HC and CO in the

engine cylinder and exhaust system

It should be reemphasized here that a iraditional problem

with lean mixture engines has been low exhaust temperatures

which tend to quench HC oxidation reactions leading to

excessive emissions

Control of HC emissions to low levels requires a retarded or

slowly developing combustion process The consequent extenshy

sion of heat release j nto 1ate porttt)ns of the engtne cycle

168

tends to raise exhaust gas temperatures thus promoting

complete oxidation of hydrocarbons and carbon monoxide

32 Historical Background and Current Status

321 Early Developm9nt Objectives and Engine Def igns

The prechamber stratified charge engine has existed in various

forms for many years Early work by Ricardo 1 indicated that

the engine could perform very efficiently within a limited

range of carefully controlled operating conditions Both

fuel-injected and carbureted prechambcr engines have been

built A fuel-injected design Lnittally conceived by

Brodersen 11 was the subject of extensive study at the

University of Rochester for nearly a decade 12 13 Unforshy

tunately the University of Rochester work was undertaken prior

to widespread recognition of the automobile emissions problem

and as a consequence emission characteristics of the

Brodersen engine were not determined Another prechamber

engine receiving attention in the early 1960s is that conshy

ceived by R M Heintz 14 bull The objectives of this design

were reduced HC emissions incr0ased fuel economy and more

flexible fuel requirements

Experiments with a prechamber engine design called the torch

ignition enginen were reported n the USSR by Nilov 15

and later by Kerimov and Mekhtier 16 This designation

refers to the torchlike jet of hot comhust1on gases issuing

169

from the precombustion chamber upon j_gnj_ tion In a recent

publication 17 Varshaoski et al have presented emissions

data obtained with a torch ignition engine These data show

significant pollutant reductions relative to conventional

engines however their interpretation in terms of requireshy

ments based on the Federal emissions test procedure is not

clear

l

3 2 2 Current DeveloJ)ments

A carbureted middotthree-valve prechamber engine the Honda CVCC

system has received considerable recent attention as a

potential low emissions power plant 18 This system is

illustrated in Figure 3-2 Hondas current design employs a

conventional engine block and piston assembly Only_ the

cylinder head and fuel inlet system differ from current

automotive practice Each cylinder is equipped with a small

precombustion chamber communicating by means of an orifice

with the main combustion chambe situated above the piston lj

ij_ A small inlet valve is located in each precharnber Larger

inlet and exhaust valves typical of conventlonal automotive

practice are located in the main combustion chamber Proper

proportioning of fuel-air mixture between prechamber and

main chamber is achieved by a combination of throttle conshy

trol and appropriate inlet valve timing A relatively slow

and uniform burning process gjvjng rise to elevated combusshy

tion temperatures late in the expansion stroke and during

the exhaust procezs is achieved H1 gh tewperaturr--s in thin

part of the engine cycle ar-e necessary to promote complete

170

oxidation of HC and CO It si1ould be no~ed that these

elevated exhaust temperatures are necessarily obtained at

the expense of a fuel economy penalty

To reduce HC and CO emissions to required levels it has been

necessary for Honda to employ specially designed inlet and

exhaust systems Supply of extremely rich fuel-air mixtures

to the precombustion chambers requires extensive inlet manifold

heating to provide adequate fuel vaporization This is accomshy

plished with a heat exchange system between inlet and exhaust

streams

To promote maximum oxidation of HC and CO in the lean mixture

CVCC engine exhaust gases it has been necessary to conserve

as much exhaust heat as possible and also to increase exhaust

manifold residence time This has been done by using a relashy

tively large exhaust manifold fitted with an internal heat

shield or liner to minimize heat losses In additj_on the

exhaust ports are equipped with thin metallic liners to

minimize loss of heat from exhaust gases to the cylinder

head casting

Engines similar in concept to the Honda CVCC system are under

development by other companies including Ttyota and Nissan

in Japan and General Motors and Fo~d in the United States

Honda presently markets a CVCC-powered vehicle tn tTapan and

plans US introduction in 1975 Othe~ manufactur~rs

includlnr General Motors and Forgtd 1n thr U S havf~ stated

171

that CVCC-type engines could be manufactured for use in limited

numbers of vehicles by as early as 1977 or 1978

33 Emissions and Fuel Economywith CVCC-Type Engines

331 Recent Emissions Test Results

Results of emissions tests with the Honda engine have been very

promising The emissions levels shown in Table 3-I are typical

and demonstate that the Honda engine can meet statutory 1975-1976

HC and CO stindards and can approach the statutory 1976 NOx

standard 19 Of particular importance durability of this

system appears excellent as evidenced by the high mileage

emissions levels reported in Table 3-I Any deterioration of

l emissions after 50000 miles of engine operation was slight

and apparently insignificant

I Table 3-I

Honda Compound Vortex-Controlled Combustion-Powered Vehicle 1 Emissions

Fuel Economy

Emissions 2 mpg gMile 1972

HC 1975 FTP FTPco NOv

210 50000-Mile Car+ No 2034 Low Mileage Car 3 No 3652 018 212 221089

024 065 198 1976 Standards

213175 20o41 34 - -04o411977 Standards 34 - -

1Honda Civic vehicles 2 1975 CVS C-H procedure with 2000-lb inertia weight3Average of five tests aAverage of four tests

172

Recently the EPA has tested a larger vehicle conve~ted to the

Honda system 20 This vehicle a 1973 Chevrolet Impala with

a 350-CID V-8 engine was equipped with cylinder heads and

induction system built by Honda The vehicle met the present

1976 interim Federal emissions standards though NOx levels

were substantially higher than for the much lighter weight

Honda Civic vehicles

Results of development tests conducted by General Motors are

shown in Table 3-II 21 These tests involved a 5000-pound

Chevrolet Impala with stratified charge engine conversion

HC and CO emissions were below 1977 statutory limits while

NOx emissions ranged from 15 to 2 gmile Average CVS-CH

fuel ec9nomy was 112 miles per gallon

Table 3-II

Emissions and Fuel Economy for Chevrolet Impala Strmiddotatified

Charge Engine Conversion (Ref 21)

Test

Exhaust Emlssions

gMile 1 Fuel

Economy mpgHC co NOx

1 2 3 4 5

Average

020 026 020 029 0 18

023

25 29 31 32 28

29

17 15 19 1 6 19

17

108 117 114 109 111

112

1cvs-CH 5000-lb inertia weight

173

I

332 HC Control Has a Significant Impact on Fuel Economy

In Figure 3-3 fuel economy data for several levels of hydroshy

carbon emissions from QVCC-type stratified charge engines

are plotted 22 23 ~ 24 At the 1 gmile HC level stratified

charge engine fuel economy appears better than the average

fuel economy for 1973-74 production vehicles of equivalent

weight Reduction of HC emissions below the 1-gram level

necessitates lowered compression ratios andor retarded

ignition timing with a consequent loss of efficiencymiddot For

the light-weight (2000-pound) vehicles the O~ gmile IIC

emissions standard can be met with a fuel economy of 25 mpg

a level approximately equal to the average of 1973 producshy

tion vehicles in this weight class 8 For heavier cars the

HC emissions versus fuel economy trade-off appears less

favorable A fuel economy penalty of 10 relative to 1974

production vehicles in the 2750-pound weight class is

required to meet the statutory 04 gmile HC level

333 Effect of NOx Emissions Control on Fuel Economy

Data showing the effect of NOx emissions control appear in

Figure 3-~ 22 These data are based on modifications of a Honda

CVCC-powered Civic vehicle (2000-pound test weight) to meet

increasingly stringent NOx standards ranging from 12 gmile

to as low as 03 gmile For all tests HC and CO emissions

are within the statutory 1977 standards

NOx control as shown in Figure 3-4 has been effected by use

of exhaust gas recirculation 1n comb1nation w1th retarded

174

ignj_tion timing It is clear that control of rmx emissions

to levels below l to 1 5 gmile results in stgnificant fuel

economy penalties The penalty increases uniformly as NOx

emissions are reduced ~nd appears to be 25 or more as the

04 gmile NOx level is approached

It should be emphasized that the data of Fisure 3-4 apply

specifically to a 2000-pound vehicle With increased vehicle

weight NOx emissions control becomes more difficult and the

fuel economy penalty more severe The effect of vehicle

weight on NOx emissions is apparent when comparing the data

of Table 3-I for 2000-pound vehicles with that of Table 3-II

for a 5000-pound vehicle While HC and CO emissio~s for the

two vehicles are roughly comparable there is over a factor

of two difference in average NOx emissions

34 Fuel Requirements

To meet present and future US emissions control standards

compression ratio and maximum ignltion advance are limited

by HC emissions control rather than by the octane quality of

existing gasolines CVCC engines tuned to meet 1975 California

emissions standards appear to be easily satisfied with

presently available 91 RON commercial unleaded gasolines

CVCC engines are lead tolerant and have completed emissions

certification test programs using leaded gasolines However

with the low octane requirement of the CVCC engine as noted

above the economic benefits of lead antlknock compoundt ar-euromiddot

not realized

175

It is possible that fuel volatLLity characteristlcs may be of

importance in relation to vaporization within the high

temperature fuel-rich regions of the prechamber cup inlet

port and prechamber iQlet manifold However experimental

data on this question aomiddot not appear to be available at

present

~O Divided-Chamber Staged Combustion Engines (Large-Volume Prechamber Engines Fuel-Injected Blind Prechamber Engines)

41 General

Dual-chamber engines of a type often called divided-chamber

or large-volume prechamber engines employ a two-stage comshy

bustion process Here initial r~ich mixture combustion and

heat release (first stage of combustion) are followed by rapid

dilution of combustion products with relatively low temperature

air (second stage of combustion) The object of this engine

design is to effect the transitjon from overall rich combustion

products to overall lean products with sufficient speed that

time is not available for formation of significant quantities

of NO During the second low temperature lean stage of

combustion oxidation of HC and CO goes to completion

An experimental divided-chamber engine design that has been

built and tested is represented schematically in Figure ~-1 25 26

A dividing orifice (3) separates the primary combustion

chamber (1) from the secondary combustion chamber (2) which

includes the cylinder volume above the piston top A fuel

injector (4) supplies fuel to the primary chamber only

176

Injection timing is arranged such that fuel continuously

mixes with air entering the primary chamber during the

compression stroke At the end of compression as the

piston nears its top center position the primary chamber

contains an ignitable fuel-air mixture while the secondary

chamber adjacent to the piston top contains only air

Following ignition of the primary chamber mixture by a spark

plug (6) located near the dividing orifice high temperature

rich mixture combustion products expand rapidly into and mix

with the relatively cool air contained in the secondary

chamber The resulting dilution of combustion products with

attendant temperature reduction rapidly suppresses formation

of NO At the same time the presence of excess air in the

secondary chamber tends to promote complete oxidation of HC

and CO

42 Exhaust Emissions and Fuel Economy

Results of limited research conducted both by university and

industrial laboratories indicat~ that NOx reductions of as

much as 80-95 relative to conventional engines are possible

with the divided-chamber staged combustion process Typical

experimentally determined NOx emissions levels are presented

in Figure 4-2 27 Here NOx emissions for two different

divided-chamber configurations 8re compared with typical

emissions levels for conventional uncontrolled automobile

engines The volume ratio 8 appearing as a parameter in

Figure 4-2 represents the fraction of total combustion volume

contained in the primary chamber For a values approaching

I

i J_

177

1

05 or lower NOx emissions reach extremely low levels Howshy

ever maximum power output capability for a given engine size

decreases with decreasing 6 values Optimum primary chamber

volume must ultimately_represent a compromise between low

emissions levels and desired maximum power output

HC and particularly CO emissions from the divided-chamber

engine are substantially lower than eonventional engine

levels However further detailed work with combustion

chamber geometries and fuel injection systems will be necesshy

sary to fully evaluate the potential for reduction of these

emissions

i Recent tests by Ford Motor Company show that the large volume

prechamber engine may be capable of better HC emissions conshy

trol and fuel economy than their PROCO engine This is shown

by the laboratory engine test comparison of Table 4-I 19

Table 4-I

Single-Cylinder Low Emissions middot11 ~ _____En____g__~ne __middot _e_s_-_s_____

Engine

NO--X Reduction

Method

Em1ssions g1 hp-Hr

Fuel Economy

Lb1 hp-HrNOv HC- co

PROCO

Divided Chamber

PROCO

Divided Chamber

EGR

None

EGR

None

10 30

10 04

05 ~o

o J_o 75

130

25

l 1i bull 0

33

0377

0378

0383

0377

178

Fuel injection spray characteristics are critical to control

of HC emissions from this type of engine and Fords success

in this regard is probably due in part to use of the already

highly developed PROCO-gasoline injection system Figure 4-3

is a cutaway view of Fords adaptation of a 400-CID V-8 engine

to the divided-chamber system 2 e

Volkswagen (VW) has recently published results of a program

aimed at development of a large volume precharnber engine 29

In the Volkswagen adaptation the primary chamber which comshy

prises about 30 of the total clearance volume is fueled by a

direct timed injection system and auxiliary fuel for high

power output conditions is supplied to the cylinder region by

a carburetor

Table 4-II presents emissions data for both air-cooled and

water-cooled versions of VW s dtvided-middotchamber engine 3 0

Emissions levels while quite low do not meet the ultimate

1978 statutory US standards

179

Table 4-II

Volkswagen Jarge Volume _Jrechamber Er[ Lne Emissions

Exhaust Emissions

_ _gMile 1

___E_n_gi_n_e__t--H_C___c_o__N_O_x____E_ng__i_n_e_S_p_e_c_i_f_i_c_a_tmiddot_1_middoto_n_s__

20 50 09 841 compression ratio Air-Cooled 16-Liter

prechamber volume 28 of total clearance volume conventional exhaust manishyfold direct prechamber fuel injection

20-Liter 10 40 10 91 compression ratio Water-Cooled prechamber volume 28 of

total clearance volume simple exhaust manifold reactor direct prechamber fuel injection

1cvs c-H

Toyota also has experimented wlth ___a large volume prechamber

engine using direct prechamber fuel injection and has

reported emissions levels comparable to those of Table 4-II 31

43 Problem Areas

A number of major problems inherent in the large volume

prechamber engine remain to be 3olved I~ These problems include the following II

Fuel injection spray characteristics are critically

important to achieving acceptable HC emissions

The feasibility of producing asatisfactory injecshy

tion system hasnot been estab1ished

180

Combustion noise due to high turbulence levels and

hence high rates of heat release and pres[-ure rise

in the prechamber can be excessive It has been

shown that the-noise level can be modified through

careful chamber design and combustion event timing

If the engine is operated with prechamber fuel

injection as the sole fuel source maximum engine

power output is limited This might be overcome

by a~xiliary carburetion of the air inlet for maximum

power demand or possibly by turbocharging Either

approach adds to system complexity

The engine is charmiddotaeter1zed by low exhaust temperatures

typical of most lean mixture engines

References

1 Ricardo H R Recent Research Work on the Internal Combustion Engine 11 SAE Journal Vol 10 p 305-336 (1922)

2 Bishop I N and Simko A Society of Automotive Engineers Paper 680041 (1968)

3 Simko A Choma M A and Repco L L Society of Automotive Engineers Paper 720052 (1972)

4 Mitchell E Cobb JM and Frost R A Society of Automotive Engineers Paper 680042 (1968)

5 Mitchell E Alperstein M and Cobb JM Society of Automotive Engineers Paper 720051 (1972)

6 1975-77 Emission Control Program Status Report submitted to EPA by Ford Motor Company November 26 1973

181

if

7 consultant Report on Emissions Control of Engine Systems National Academy of Sciences Committee on Motor Vehicle Emissions Washington DC September 1974

8 Austin T C and Hellman K H Society of Automotive Engineers Paper 730790 (1973)

9 See Ref 7

10 Alperstein M Schafer G H and Villforth F J Iiil SAE Paper 740563 (1974)

11 US Patent No 2615437 and No 2690741 Method of Operating Internal Combustion Engines Neil O Broderson Rochester New York

12 Conta L~ D and Pandeli American Society of Mechanical Engineers Paper 59-SA-25 (1959)

13 Canta L D and Pandeli American Society of Mechanical Engineers Paper 60-WA-314 (1960)

14 US Patent No 2884913 0 Internal Combustion Engine R Mi Heintz i

15 Nilov N A Automobilnaya Promyshlennost No 8 (1958)

l 16 Kerimov N A and Metehtiev R I Automobilnoya Promyshlennost No 1 p8-11 (1967)

17 Varshaoski I L Konev B F and Klatskin V B Automobilnaya Promyshlennost No 4 (1970)

18 An Evaluation of Three Honda Compound Vortex Controlled Combustion (CVCC) Powered Vehicles Report B-11 issued by Test and Evaluation Branch Environmental Protection Agency December 1972

19 Automotive Spark Ignition Engine Emission Control Systems to Meet Requirements of the 1970 Clean Air Amendments report of the Emissions Control Systems Panel to the Committee on Motor Vehicle Emissions National Academy of Sciences May 1973

20 An Evaluation of a 300-CID Compound Vortex Controlled Combustion (CVCC) Powered Chevrolet Impala Report 74-13 DWP issued by Test and Evaluation Branch Environmental Protection Agency October 1973

21 See Ref 7

22 See Ref 7

23 See Ref 7

24 See Ref 7

182

25 Newhall H K and El-Messiri I A Combustion and Flame 14 p 155-158 (1970)

26 Newhall H K and El-Messiri I A Society of Automotive Engineers Transaction Ford 78 Paper 700491 (1970)

27 El-Messiri I A and Newhall H K Proc Intersociety Energy Conversion Engineering Conference p 63 (1971)

28 See Ref 7

29 Decker G and Brandstetter W MTZ Motortechnische Zeitschrift Vol 34 No 10 p 317-322 (1973)

30 See Ref 7

31 See Ref 7

183

Fig 2-1 FORD PROCO ENGINE

l

Ford Proco Engine Fuel Economy and Emissions _ 15 _ f--1

00 +

I ~ x X gt( X _ x A 7- ~ X x~ ~c - l4catalyst Feed u NOx vs ruel Econ with 1 C0-71 CJ) 14 x x Ynn H( RP c tr ir-t irm vltgtZ G I HC - C0-127 _ A txcessve c

13 Approx W EG R

~ C~~r 351 CID 5000 Lb Inertia Weight

Q 21 A L 0 u w II _j

LJ =gt LL

10

35i CD 4500 Lb Inertia Weight

~ 1974 Production Average Fuel Economy

4 soo _b r-r-r-----z~lt_~~---7--_~--r--1r-7-r1--~-rz7-w~~

150 0 0 Lb PU221ufrac122-1 I

LO 20 30

NOx EMISSIONS-GMSMILE (CVS-CH) Revised216174

0

HKN 71074

Fig 2-2

l

~___-~ ~--=---~ ~=---__---~1 f-=-----1__middot-_~J ~-----------1 ~bull-=-=- (-~-~ LJii-ZJj ~ ~~-~ ~~ -__c~~ 1--~~ ~----~--1 ---------s___-c--1 ~~~-~~~bull r~~-~--middot1 ____c__ J~ p- ~

Texaco TCCS Engine

Shrouded Intake Valve

~ Intakemiddot r~ )p__-- Fuel Nozzle Fuel Nozzte Port ~ -- -yen -_~

X f -J J ( ~1 I --- ~ f middotmiddotj_Ja 1(~-~_ frff 1-Cylinderv~ v_ r--L~ I (~~)J ~- Intake 1 - ------L- middotmiddot - middotmiddot -1 H0 ad middot --- - -- 1 Po rt I 1 I ~~ ) ~ ~ ~~~ -A- I ------

- I _ ---_ ~ P1ston-mgt-lt_ffrac12 T_77~~~--1 i- r_-~J N

- ~- i~-L - _ _ - IExhaust - - I ~ - 1-_ r- bullsect ~ ----lt_ ~ I PortJ~bJ lt 7A--7~ ~1 ~j --~ ~ yl ind er

-__~lli- klmiddot ~ro v_t_gt11J1bull Bti Or K__ - middot ~

I t--tL pgt-- Ultmiddot middot- - Spark Plugr- -1 --U2middot- ~-~

LHorizont al Projections of Nozzle and Spark Plug Centerlines

Fig 2-3 i--1 00 U1

---~---~-~ -------c- --~--- 7middot-r---c-- ~- -~~~==---~~~~~- srsr RZIIEF7 11t111-~-----==-----=-~--~-~~---c=rmiddot=

OPEN CHAMBER TYPE STRATI Fl ED CHARGE ENGINE i-shyCj

DIRECTIONAl~Fsw7 Q

NOZZLE P

I

~J~treg lt-_(__(lt-(11

c_-- _7- -

SPARK PLUG_ l 1__- -_ - l --_ ~ ----__ lt_ lt_ -- --

ltlt_I_--- _

~ gt - _____- -- --~ ~-l_- 1_~ -~- ~ ------

~~~ r_I FUEL SPRAY 2 FUEL-AIR MIXING ZONE ~- _ -------

FLAME FRONT AREA 4 COMBUSTION PRODUCTS

TCCS COMBUSTION SYSTEM

Fig 2-4

3

----==-----~ l~~----bulli r-~ ~-----=-- 1 ~~ ~ -~ ~~ ___-_=gt---l p--- --=-=-_-__71-~-~~ 1-0-- --=---=-- 4 L--_-_-~ P--- ~

25

-c u

f

Cl) 24 gt u _

tgt 23a ~

I

gt-~ 220 2 0 u w 21 _J

lJJ gt LL

2

Texaco TCCS Powered Cricket Vehicle

Max Econ Setting gt A L07 HC

141 CID JQf CR 084 CO 2500 Lb Inertia Wgt

50-so Retard_ 0_73 HC

12 co 051 HC ~ 061 HC

085COA 064CO Retard+ ESPRetard+

EGR

036 HC ~ 115 co Retard +ESP+ EGR

04 06 08 10 12 14 16 18 20 NOx EMISSIONS-GMSMILE (CVS-CH) HtltN1110114

I- 00 -JFig 2-5

-~ ~=- ~ - -i______c_J ~-====c= wr=- ~-~ p--w~~~ rr w -

25

-c u

I

(f)

gt u-lt a_

2

gt-I 20

~ 0 z 0 u LLI

_J

w tJ_

15

I- CJ) CJ)

Turbocharged Texaco TCCS Ml51 Vehicle

Max Econ Adjustment_ HC-3J catalyst Feed C0-70

141 CID 10~1 CR 2750 Inertia Weight 8deg Retard ~

~bull HC-3middot2 catalyst Feed ~~ _ C0-64

_ 5deg Retard HC-0 30 8degRetard LowEGV bullco-11 ~bull HC-3middot6 catalyst Feed WIW21

Med EGR C0-67 1974 Production 33 Average Fuel Economy ~

COmiddoti05 (2750Lb)

I

bull HC-035 co- 141 13deg Retard High EGR

04 10 20 NOx EMISSIONS -GMSMILE (CVS-CH) ~~ts~b~~~74

Fig 2-6

189

Fig 3-1

PRECHAMBER TYPE STRATIFIED CHARGE ENGINE

r Inlet

(Fuel-lean Mixture )

I 0 I

Spark -Prechamber (Fuel-rich mixture)

-Main Chamber

1] HON DA CVCC ENGINE CONCEPT

190

Fig 3-2 Honda CVCC Engine

28 -l u

1

UJ 26 -gt u-(9 CL 24 2-

f

gtshy0gt

22 z ~ _)

u w

20 _J

w ~ LL

18

J= ---- 4 --~~-_----a ~~ _-_bull --~~ 1~~1 ltiil~I ~ ~-r~ ~ -~ ~-~ ~J~-iii-1 ~~1 s _-_ __-

Fuel Economy vs HC Emissions for 3-Valve Prechamber Engines

e NOx-14 15 Liter

bull Honda CVCC 2000 LbsNOx - 12 A Datsun NVCCbull15 Liter

bull ~JOx -09 A 2500 Lbs J LL 1ter NOv -15

2750 Lbs -NOx -17

- I AiJOx -12

0 02 04 06 08 LO 0HYDROCARBON EMiSSlmiddotONS - Glv1 I MILE (CVS-CH) I-

Fig 3-3

J--1

1--Fuel Economy vs NOx Emissions IO N

-- for Honda CVCC Powered Vehiclesr 26 u

l VHc-023 U1 gt umiddot 24_-__

(_IJ o_

~ 22 l

gt-5~-0 z 20 C0-200 u A HC-033w I co -3o_j

_A HC-029w 18 J I C0-27 LL

_ HC-025

HC-017 co -2-3

C0-22

0 -- 02 04 06middot 08 10 12 NOx Ef11SSIONS -GlviS MILE (CVS-CH)

Fig 3-4 middot

I

I

i93

J J

Fig 4-1 Divided Chamber Engine

middot(4) Fuel Injector

1

f J

f ff

f

~ Ii

I f

i

I f ] [

~~

0 0 0 0

i ~ I

1jl

194

E Cl 0

C QJ

CJl 0 _

-1-

z

0

Vl (lJ

-0

X 0

-t-J

V1 ro c X

LLI

Fig ~-2

COMPARISON OF CONVENTIONAL AND DIVIDED COMBUSTION CHAMBER NOx EMISSIONS

5000 MBT Ignition Timing Wide Open Ttl rattle

4000 Conventional Charnber

3000

J = fraction of Total Combustion 2000 Volume in Primary Ct1arnber

Divided Chamber 13 = 0 85

1000

Divided Chamber fo = 0 52

05 06 0 7 08 09 10 11

O~erall Fuel-Air Equivalence Ratio

195

196

AIRBORNE SURVEYS IN URBAN AIR BASINS IMPLICATIONS FOR MODEL DEVELOPMENT

by

Donald L Blumenthal Manager of Program Development

Meteorology Research Inc Altadena California 91001

middotI would like to make several points today First ozonemiddotis basically

a regional long-range problem There is a lot of long range ozone transshy

port and this transport is a normal occurrence The second point is that

ozone is stable in the absence of scavengers Junge mentions in his book

that the residence time of ozone in the troposphere is on the order of a

month Third vertical variations in concentration and ventilation rate are i very important in modeling atmospheres such as Los Angeles Layers aloft

are ventilated down to the surface on occasion and surface pollutants are

ventilated up mountain slopes as Jim Edinger has pointed out before and

often ventilated out of the basin in upper winds Fourth the day to day

carry over of pollutants from one day to the next is a very important considshy

eration in the Los Angeles Basin Finally there is a definite background

level of ozone The geophysical literature says its about O 02 to O 03 ppm (

in various parts of the world Weve seen data varying from 003 to 005 ppm

The difference may be due to calibration differences In any case numbers

like 005 are pretty substantial background levels for ozone

I am going to illustrate the points listed above with some data from

Los Angeles Basin The data were collected during a two-year study funded

by the Air Resources Board some of the analyses were funded by EPA The

study examined the three dimensional distribution of pollutants in the Los

Angeles Basin using airborne sampling systems Coinvestigators on the

project were Dr Ted Smith and Warren White of Meteorology Research Inc (MRI)

197

The first slide shows one of the aircraft we used Its a Cessna 205

which had sampling inlets on the side of the aircraft Figure 2 shows the

instrument system on the inside of the aircraft We were measuring nitrogen

oxides ozone scattering coefficient with a nephelometer condensation nuclei

carbon monoxide and meteorological parameters such as temperature humidity

turbulance Altitude and position were also measured

Figure 4 shows that the typical sampling pattern was a series of spirals

from the top of the mixing layer over an airport virtually to ground level

then we would climb up to the next point on the route and spiral down again

We had three routes (A B C Figure 3) that we would fly We had two airshy

craft and we would fly two of these three routes three times a day any

given day that we could The day I will be talking about September 25~ 1973

we flew what was called the Riverside route (C) and the Los Angeles route

(A) The 25th of July 1973 you might remember was the day before the

federal office buildings were closed in the area here because of smog

Figure 5 shows the surface streamlines at 0300 Pacific Standard Time

about 4 oclock in the morning daylight time on July 25 This streamline

analysis points out the morning stagnation conditions which are a very normal

occurrence in the Los Angeles Basin You start out with very light winds

quite variable maybe a slight off shore flow early in the morning On this

particular day this kind of situation extended well into midday The sea

breeze did not really pick up until up around noon When you have this kind

of a situation and a low radiation inversion at night you have a

long period of accumulation of pollutants all over the Basin espt~cialJy

in the prime source area the southwest portion of the Basin

198

I

Figure 6 shows the streamline pattern at 1600--400 cclock in the

afternoon same day sea breezes develop and with them a transport pattern

that carries pollutants up to the northeast and out toward the eastern por-

tion of the Basin This is a very regular pattern which we see day after l middot

day On July 25 1973 it was a little bit exaggerated The sea breeze was

held off for awhile started a bit late and so there was a very long period

of accumulation in the southwest area and then transport across the Basin

Figure 7 is an average streamline pattern at 1600 PacHic Daylight Time

on low inversion days for August 1970 It is included to show that the pattern

shown before is very typical Flow starts in the western portion of the

Basin and goes right across to the eastern portion This is using surface

data There is a very high average wind velocity in Ontario about 13 m iles

per hour and 23 mph in Riverside This is the average for the whole month

of August at 1600 PDT on low inversion days There is a considerable amount

of transport across the Basin starting relatively slowly in the morning and

accelerating in the afternoon

Figure 8 shows a verticle cross section of the scattering coefficient

The darker areas indicate higher levels of particulates Scattering coefficshy

ient is inversely proportional to visibility In the crosshatched area

visibility is less than about 3 miles In plotting altitude versus distance

inland from the coast you have Santa Monica (SMO) on the coast El Monte (EMT)

Pomona (BRA) Rialto (RIA) Redlands (RED) The lower broken line is surface

ground level The heavy dashed line is the base of the subsidence inversion

that occurred on the two days during this episode The middle line is the

base of the marine inversion There is a large area over in the western

portion of the Basin where emissions accumulate for much of the day At

199

midday the sea breeze has just started ventilating the Santa Monica area

The layer between the inversions is a layer aloft which is fairly well separshy

ated from the surface layer Ozone concentrations for instance in the

layer aloft were on the order of 04 05 ppm using the ARB calibration

method Down in the surface layer they were quite a bit lower in the mornshy

ing due to scavenging

Figure 9 shows that by afternoon the sea breeze starts and you get

kind of a clean air front Sea breeze starts ventilating the whole Basin

the stuff that was over in the west is transported eastward and at approxishy

mately Brackett (BRA) at 1700 PDT there is a clean air front The high conshy

centrations that were over Los Angeles earlier are now centered near Upland

(CAB) The numbers shown over CAB are data taken from a vertical profile

spiral over Upland at about 1600 That turns out to be the time when there

was the worst ozone concentration of the day in the Basin and it did occur

at Upland It could well be a result of the very polluted mass from the

western Basin being transported over the Upland area The layer aloft has

been a bit undercut by the sea breeze and some of the polluted mass has been

around possibly as long as the night before There has been very little

transport in the area aloft ozone concentrations are still very high

Figure 10 shows a trajectory analysis of the air arriving at Upland at

1600 since that was the worst time of the day at Upland We developed a

trajectory envelope using surface wind data and winds aloft so the air

arriving at Upland at 1600 started out somewhere back within this envelope

for example at 1130 PDT We did not go earlier than 1130 because the winds

were pretty much light and variable before that The air that arrives at

Upland at 1600 has been over the western portion of the Basin for much of

200

the morning and q~ite a bit of the evening before Thus there is

a very long period of accumulation and then a transport a pulsing effect

where you have pollutants moved across the Basin

Figure 11 is an isopleth map of surface ozone concentrations Again all

data are corrected to agree with the ARB calibration method Again you can

see that for the hours between 1600 and 1700 using surface data the Upland

area has the highest surface ozone concentrations about 063 ppm The western

area has been well ventilated by the sea breezes and it is cleaned out

The transport is actually pretty much perpendicular to the isopleth line

just about like that

Figure 12 is a vertical profile taken over Upland Cable Airportat

roughly the time of maximum ozone concentration 1636 PDT We are plotting

pollutant concentration on the x-axis versus altitude in meters (since it was

done for an EPA report) Surface leveJ at Upland is a little over 400 meters

the Z line is ozone Ozone concentration within the surface mixing layer

is pegged on the instrument at somewhat above 05 ppm Above the surface

mixing layer it drops off considerably and eventually get down to background

The T line is temperature and you ean see the subsidence inversion

on this day is very nicely documented here and provides a very strong trap

in that area The B line is the scattering coefficient inversely proporshy

tional to visibility Within the surface mixing layer visibility is on the

order of 3 miles or less while up above the surface mixing layer just a few

hundred feet difference visibilities get up to 60 or 80 miles The X is

condensation nuclei the measure of the very fine particles below about 010

micron It is a measure of quite fresh emissions If you have a high condenshy

sation nuclei count there are very fresh combustion emissions If you have

I

201

an aged air mass the condensation nuclei coagulate and the count decreases

considerably You can see that there are still some fresh emissions within

this surface layer as well But up above the surface mixing layer all the

pollutant indicators decrease considerably

Figure 13 is the same type of vertical profile taken over El Monte

which is on the western side of the sea breeze front The sea breeze front

has passed El Monte at this time almost 1700 PDT and again there are

distinct differences between the mass below the mixing layer within the sea

breeze front (below 400 meters) the marine inversion (400 to 800 meters) and

the subsidence inversion The subsidence inversion occurs at about 800 meters

and there is an old layer of very polluted stuff aloft The surface concenshy

trations are lower because of the ventilation by the sea breeze Condensashy

tion nuclei count (X line) within the surface layer is quite high There

are still fresh emissions in the El Monte area The 11 Z line is ozone

about 02 ppm within the surface layer (200 m) but it is 05 ppm up above

the surface mixing layer The scattering coefficient (B line) is very

similar it is lower at the surface and increases to a visibility equivalent

of less than 3 miles above the surface mixing layer The condensation nuclei

count is high in the lower portion of this (eg at 600 m) hut decreases conshy

siderably above This portion of the upper layer (600 m) has been around

at least all morning and condensation nuclei have been scattered from the

area The portion of the upper layer below 600 m has probably just recently

been undercut by the sea breeze and there are still some condensation nuclei

left in it

Figure 14 illustrates a different method of looking at the flushing

problems in the Basin We have tried to develop an objective criteria based

on ground level ozone to show the cleansing of the basin using the time of

202

arrival of clean air We determine the time when the ozone concentrations

drop by a factor of two at any given point The 1600 line means that between

1500 and 1700 the ozone concentration at that point dropped a factor of two

This sort of isopleth chart of when the clean air arrives agrees quite well

with the trajectory analyses although the numbers are a little bit behind

the trajectory analyses for the polluted air Figure 14 again shows the

transport process that takes place across the Basin which is ventilated from

west to east At 1900 some of the fresh ocean air finally gets out to

Redlands

In Figure 15 in order to put this whole flux problem into some perspecshy

tive we looked at the numbers the actual amount of ozone flux across the

basin We calculated the mean trajectory from Torrance towards Redlands

using the surface and upper air data We looked at the flux from the western

basin to the eastern basin basically from Los Angeles and Orange Counties to

Riverside and San Bernardino Counties This is a calculation made at 1700 PDT

We used the winds aloft from Chino as well as the vertical profiles taken at

Pomona and Corona Averaging the ozone concentration throughout the mixing

layer and multiplying by an average wind speed we arrive at a number of 185

metric tons per hour being transported directly from one side of the Basin

to the other If you look at this in terms of actual concentration in the

eastern Basin and assume that the flow was constant for about an hour it

is eno_ugh to fill up the box shown in Figure 15 to 025 ppm ozone which

exceeds the air quality standard by a factor of three (using the ARB calibrashy

tion method) Thus there is a very significant transport of ozone or ozone

precursors from one portion of the Basin to the other side of the Basin One

thing to mention though is that the concentration would not be kept up on a

203

steady state basis because the transport is a result of the pulsing effect

I Illentioned earlier There is a lot of accumulati6n in the western Basin

and these accumulated pollutants are then transported across the Basin This

kind of transport did take place in a couple hours because we also have

measurements from 1500 PDT which give us similar flux numbers

Figure 16 is a trajectory envelope similar to Figure 10 calculated for

Upland at 1600 for the air arriving at Redlands about 600 oclock in the

afternoon I wanted to include this trajectory envelope to show that the

problem is not really simple You cannot say that the air at Redlands came

from Long Beach per se The air at Redlands if you look at the whole

envelope of possible trajectories using upper air data as well as surface

data could have come from anywhere between Downtown Los Angeles and over

the Pacific Ocean south of Long Beach

Another thing to recognize is that the wind actually changes direction

slightly as you go up and down through the mixing layer and the mixing layer

is exactly what it implies There is mixing within the mixing layer so if

you begin with a parcel of air near the surface this parcel may move to the

top of the mixing layer and go one direction for awhile it then may go back

down to the bottom of the mixing layer and move in another direction for

awhile The ratio of the length scales indicata3mixing layer depths of 1500

or 2000 ft and distances on the order of 70 miles This makes it very

difficult for tetroons to follow an air trajectory because they do not go

up and down They stay at one altitude and in one wind regime and yet the

wind regimes are different at different altitudes and the air is continually

mixed up and down through this layer You can often see this on time lapse

photographs

204

The question is where does the pollutant mass go after Redlands Figure

17 is a repeat of Jim Pitts slide from yesterday and it is data for the

same day that we did our analysis It shows the ozone peaks starting at

Pomona and Riverside and on July 25 1973 eventually getting out to Palm

Springs so there is quite a bit of long-range transport The ozone is

stable at 8 00 or 9 00 oclock at night There still are ozone concenshy

trations of 02 ppm it hasnt dissipated even at the surface Ozone does

dilute as the mass moves Other calculations we did were integrations

through the mixing layer of various pollutants such as ozone and CO along

with trajectories that we measured Th~se integrations show just what the

ground data show in Figure 17 The concentrations increase through the western

portion of the Basin and then show a decrease through the eastern portion

of the Basin CO tends to decrease faster than the ozone indicating a

continued production of ozone further east

Figure 18 is a streamline chart on a larger area map for the 16th of

August 1973 It shows the typical streamline patterns that occur for

ventilation from the Basin By mid-afternoon there is flow out through the

major passes to the north and towards Palm Springs (PSP) On this particushy

lar day we had data from Arrowhead showing that the air mass from the Basin

does indeed get up there

Figure 19 shows a vertical profile over Arrowhead early in the morning

16 August 1973 at a time when there was a north wind Ozone level was

about 005 ppm the scattering coefficient was quite low on the order of

probably 60 miles visibility or so Figure 20 is a vertical profile again

over Arrowhead late that afternoon when the winds had switched There is a

flow from the Los Angeles Basin into the Arrowhead area thus one sees a

205

vertical profile that shows a distinct increase near the surface in both the

ozone and the scattering coefficient and in the condensation nuclei Ahove

that you have fairly clean air The top of the polluted level is just about

the top of the mixing level over the Basin

I want to leave the transport now and discuss the complicated vertical

structure that can occur If you want to try to model something try this

one for instance Figure 21 is a vertical profile over Brackett Airport

Pomona about 830 in the morning on 26 July 1973 which is the day after

the episode shown earlier A bit of interpretation shows how complicated

th is can be If one looks at the temperature profile it would be very

difficult to pick out a mixing layer theres a little inversion here another

inversion there several more up here After looking at hundreds of these

profiles though you can start interpreting them What is happening is that

there is a surface mixing layer at about 500 m In this layer there is a

high condensation nuclei (X line) count due to morning traffic The San

Bernardino freeway is quite close to Brackett there is a relatively high

nitrogen oxide count about 02 ppm and the b-scat is fairly high Ozone (Z)

within the surface layer however at this time is quite low The layer beshy

tween 500 m and 700 rn turns out to be the Fontana complex plume Note the

very high b-scat level it is below 3 miles visibility the plume is very

visible especially at this time of the morning when it is fairly stab]e

There is a high nitrogen oxide level (800 m) a high condensation nuclei

level and again a deficit of ozone Above this layer (800 m) you have stuff

that has been left all night very low condensation nuclei indicating a very

aged air mass ozone concentrations about 016 ppm b-scat of about 04 It

has been around all night and not yet had a chance to mix down within the

206

surface layer In fact one good way of determining the surface mixing layer

early in the morning and at night is to look for the ozone deficit Another

thing to mention is that wind reversals occurred for each of these three

layers The winds were fairly light and westerly at the surface slightly

easterly in the 500 m 700 m layer and westerly above 800 m There is a

complicated situation early in the morning but the main problem is that by

the middle of the day there is good surface heating and the pollutants have

all been entrained and mixed down to the ground so in order to modeI what

happens on the second or third day of an episode you must be able to look

at both old pollutants as well as fresh emissions And you need to account

r for ozone that is actually transported down to the surface from layers aloft l

The next slide is a photograph (not included) which is another e xample

of some layers aloft This is due to upslope flow as explained by Jim Edinger

in his publications The mountains are heated during the day in turn heating

the air and making it buoyant there is upslope flow to a point where the

heating cannot overcome the subsidence inversion and the stuff comes right

out from the mountains and spreads out over the Basin The pollutants can

stay up there if the winds aloft are very light and on the subsequent day

will he re-entrained to the surface On the other hand if there are winds

aloft different from those in the surface mixing layer or the wind velocity

aloft is high there can be a very substantial ventilation process for the

Basin Pollutants can be ventilated up the slope and blown away in the upper

winds In the case of the entire July 25th episode winds aloft were quite

light and these upper layers remained

Figure 22 is a vertical profile of one of those upslope flow conditions

in the same location shown in the photograph but on a different day Again

207

there is a relatively high surface concentration of about 03 ppm of ozone

(Z line) a layer of clean air between 900 to 1100 m and then high concenshy

trations of ozone again above 1100 m It has gone up the slopes of the

mountains and then come back out Concentrations in the 1100 to 1300 m area

are just slightly lower than they were at 600 to 800 m area Notice however

that the condensation nuclei count (X line) is quite a bit lower mainly

because the stuff is much more aged above the 1000 m level than it is down

below 900 m

Figure 23 shows the stability of ozone the fact that it can stay around

all night long This is a vertical profile taken over Riverside about 2200

PDT 1000 oclock at night Above the surface mixing layer (600 m) there

are ozone concentrations of about 0 15 ppm (Z line) Within the surface

mixing layer (below 500 m) ozone is completely scavenged decreasing to

zero The nitrogen oxides within this surface layer are being contained and

are around 01 ppm from fresh emissions that occurred during the evening

Condensation nuclei near the surface are very high The temperature profile

is very stable You have a surface based radiation inversion which is a

little strange looking for a radiation inversion~ nevertheless it is quite

stable There is a definite restriction of the mixing--a very difficult

time getting air from below 500 m to above 500 m The ozone that exists in

the 700 m range is in air where the reactions have virtually gone to compleshy

tion and is very stable All the profiles on this night changed very little

the ozone peak stays there High concentrations stay around

Figure 24 is a cross section across theurban plume of the City of St

Louis I wanted to show that this occurrence is not limited to Los Angeles

We have seen ozone formation and transport in other urban plumes These data

l

208

were taken during a project sponsored by EPA in conjunction with R Husar of

Washington University and William Wilson of EPA The dark line on this is

the ozone concentration across the urban plume perpendicular to plume The

dashed line is the scattering coefficient The power plant plume is parallel

to the urban plume The data on the left were taken 35 kilometers down wind

about 1100 oclock in the morning The ozone concentration increases slightly

to 005 ppm in the urban plume there is a deficit of o in the power plant plume3

In the same urban plume same conditions 1500 CDT two hours later further

downwind there has been substantial increase in the ozone in the urban plume

itself The b-scat is very similar to what it was before but the ozone is

now increased quite substantially except in the power plant plume where

there is a strong deficit of ozone due to scavenging by nitrogen oxides So

the formation and transport of ozone and ozone precursors in urban plumes is

a regular occurrence that happens in more places than Los Angeles and as Bob

Neligan showed this morning it can happen over quite a bit longer distances

than we are showing here

To summarize the conclusions as they affect model development first

once ozone is formed in the absence of scavengers ozone is a very stable

compound It remains for long periods of time It can he transported for

very long distances Ozone is a regional problem which cannot be controlled

on a local basis To have effective ozone control middotone must have a regional

control strategy and probably regional type air pollution districts

A second conclusion is that the vertical distribution of pollutants can

be highly complex and models have to include more than just a simple wellshy

mixed surface layer

209

A third conclusion is that layers aloft can persist over night and can

be re-entrained within the surface mixing layer on subsequent days models

should be able to account for old pollution as well as fresh emissions Also

pollutant accumulation and transport can have distinct diurnal patterns that

are strongly dependent on the meteorology Models should be time dependent

and should start at the beginning of the accumulation period In other words

models ought to be able to run for 24 or 48 hours if they have to In this

case in Los Angeles there is often an accumulation of pollutants which starts

in one portion of the Basin at midnight and continues through the next mornshy

ing even before it starts to be transported

As far as recommendations go in many areas a lot of ambient data has

been collected and in some cases the data are actually ahead of some of the

models so I think a research program is needed in developing models that

will account for this vertical structure and the day to day carry over and

the models need to be extended to cover longer distances In addition more

smog chamber work is going to be needed in looking at the effects of carry

over and mixing old pollutants with fresh emissions How people go about

this I leave to the modelers and the smog chamber people They know more

about that than I do

I

210

I

~ INVERTER

AUDIO TAPE

MONIT0R

MONITOR OBSERVER SEAT

MON ITOR

NEPHELOMETFR FLfCTRONICS

j DIGITAL DATA LOGGER

CONDENSATION

VOR DME NEPHELOMETER TUBE

JUNCTION middoteox ASSORTED POWER

AIRBORNE

TEMPERATURE TURBULENCE

middot HUMIDITY

ALTITUDE BOX

__

middotE=-middot RECORDER ----r----------

NUCLEI KJNITOR

CONVERTER

SUPPLIES

INSTRUMENT PACKAGE (

lCO

03

Ndeg

-

-----NEPHELOMETER

BLOWER

Figure 2 Instrumentation Layout for Cessna 205

211

bullubullbullbullbull

Figure 3 Airborne Sampling Routes in the Los Angeles Basin

Figure 4 Vertie al Profile Flight Path

~-~ r~i ~~1 -- ~ ~ ~2-1~ LJ-----~ r~~ ~~ t~~--l

~ ALM l

0 RIA

ec 8v

M

~ Afo

-o

M 0

~IV

ltgt

IN J--1 N

SCALE II fi M I j_ ES 0 3 4 5 =-JSEJ--J~ _middot ~middot- - =- =

I

~

M

N~J

Figure 5 SURFACE STREAMLINE ANALYSIS - 0300 PST 25 July 1973

~~~ ~~-- cp1FJ=D -~~

~ 1

~ ~ 8c

8v

~25

PACIFIC OCEAN

diams Tt

0

9 I 4 5 10 I- m p H - -middotmiddot u 4H__8 middott_

D i6 J4 k W~D SPED llaquotl SNA NJ ~1

SCALE m ICtt84bullmh R v1s1a1L1n (mil 6 ~ CONTOURS REPRESENT

-- 10ml 16km (~() bull ~ ) ~ - 000 ft 3C5

Figure 6 S_cJRFACE WIND STREAMLINES - l 600 PDT JULY 2 S I 8 7 3

l - ~---i ~-=-___-----c---it~~-~~ r----=------1 ~-~~--cpc---_t__A --~ ---llil

~_ - ~-l-cL

34bull vi~-dff

bullbullbullbull bull ~ bull -1 bullbull - -_- L bull-J bull ~bull-bull-ii------~ bullmiddot r_ -~- ~ bullI ~_ bull bull bullbull bull I bull _ - bull -~-~ middotbullbullbull ~ ~ --middot -~- bullbullmiddot ~v ) ~ - -__rl v middotmiddot - 1- ~ -- middot middotmiddot - 1 91 frac12 - ~- lt( middot K i - middot bull - middot - bullmiddot~~-~lJ) obullmiddot~ ~-f- _J_~---Smiddot~middot-~----~~~---gt_middotfY-_middot-~middot --middot-~-~----fJ_middot- middotmiddotbullmiddot u-- bullmiddot ~ ~ -middot L~ bullbull

~bullbullbullbull bullbull l_bull bull bullbullbull EW bullbullbullbull-- ~ __bull f f - middotbull - J middot f bull S bull I ~ -r --

_ bullbull bull- _ bullbull-bull ~ ~ bull bull bull bull I bull bull bull bull bull bull gt - bull middotbulliJ -bull I bull bull _1 bullJ C-- ~-middot _ bull bullbull bullbull bull _____ ~ ~ l _ middot q bull 1 -middot middot ~~middot middot middotbull_ J ~gt - J bull-bullbullbullbull ) _ -middotmiddotbullmiddot J ~middotmiddotmiddot -bullmiddotbull fmiddot 7middot _middotmiddotmiddot bullmiddot(middot Ii~ middotmiddot~_--~middot 1middot__middotmiddotmiddotmiddot middot- gt_ -~ -~-- Imiddotbullmiddotbullbull_ -

- ()_I (w--_ bullbull__(i- bullOmiddotbull bull middotbull -bull-_jlJ middot bull lt 1(middot t gt bull - ~ rbull I bull middot middot- bull41-bull l~r v-middot~- middot middot middot bull_ - middotmiddot ~Jtj (middot~ ~middoti middot middot middot middot middot ~- ~ -tmiddot~ I - middot middot_- ~ - -~ middot_ _- ~bull - _ ~) i bull bullbull bull- middot_ bull middotbull __ ( bull 11bull bull ~ampmiddot ~ l bull bullQ bull - -1 bull JY1 bullbull ~ or bullbullbullbullbull bullbull-bullbull _ ~ - bull bull-bullbullbull middotimiddot middot 91 bull t bull - - tfaw lJ--r- bull bull _ bull middot- - l

f ~~middot--~ middotmiddott ~ltrgtmiddotmiddotJmiddot_bull - ~ - __ middot- LOS ANGELES BASIN - LOW LEVEL -__ jmiddot l-gt bull - bull J iI bullbull bull bull bull _ bullbull _ Jmiddot middotL~_1 middot middot bullbullmiddot ( C middot INVERSION MEAN WIND FLOW _ J

lmiddot - f bullbullbull~ - f 1bullbullbull _ ~)- bull middot- _---_- 7f-~bull~ REGIME _F_~ AUG_UST_~ ~600 P~--- l

-__L-~bull --ncmiddotbull~~-j--bullmiddot~bullmiddot_-bull _fJibullmiddot Imiddotmiddotmiddot-bullmiddot- bullbull ~ bullbullbullbullmiddotmiddotmiddot~middotbull ___ bullJ_ _middot~0))deg bullt t1yensmiddotmiddot ( middot middotmiddot middot middot ~ middot lbullbull1 t_c0 bull -middot---l lt ~middot~- deg bullbull --= bull bull bull I bull bull bull bull bull bull bull bull bullbull _~bull b ---) bullbull-bull ) bulll middotbull middot1middot ) bullT --f bull I bullr ~bullbullbull bullbullbull( - -bull-- ( -o-----_i bull-~-l- i l l J l~-- c middotmiddot _--1 ---I middotmiddot ---- ~bull-bull bulli_ ALT Elmiddot_ bullbullbullbull _- ~~middot bull middot bullbull _ bull middotbull bull~ ~bull middot bull -middot bull--ua_-- bullbull bull

-- 01--- middot_ -middotmiddot hmiddotmiddot __1 ~-- ~ fi~~- ___ - ____ _ -middotmiddotmiddotmiddot~ ) -~-J bull bullbull bull bull 0 uc- -l ~- ~ IT ~~ll ~ bull -middot -middotmiddotmiddotmiddotbullCCAmiddotmiddotmiddot-middot middot bullbullbullbullbull

) i- 5 ~-==-- __ __ - bullbullbull _ bull~ bullbull _ bull bull l T[h4 ------ - 0

i17- o~-lt -(i-_~ 11t~bull-omiddot ~- -- 13 0l~~~bull bull Jbullbull~bull ~ ~bullbullbull bull bull x- middot~---=-~~ -=aJlll8 bull Ibull bull ~~ middotbull rbull~---bull1-~middot-middot _ middotmiddotmiddot-middot 1 0 ~vrbullmiddot ~middot ~ (J~-middot _-_~) ) ~ bull middot

l middot _ POMA_ middot =~~~----ti~ jmiddotmiddotmiddot - middot bull [j

~A ii J0 Vfli middot bullHud __=bt_ bull

CImiddot ~-- ~- middot)middot PACIFIC OCEAN I middot ---- middotmiddot ~

__ middot__ ~ - _ 23~1 middotbull 8 4 1 middot middot ~ middot middot gt ~~- l ~ u middot

bull - bull- I ~------ --1~ i middotmiddotmiddot - n _c-118 1130

~ n r -t ~~gt25) cmiddotbullmiddot

~--lt- ~~- 1-~__( i - t ~ _ middot 0 igt(_J

11bull bull11 ~~ -~[ ~i~gt----gtmiddotmiddotmiddotmiddot--~l_ ~~ ELEVATION

IN FEET bullbull (_- middot bullbullbull -middot middotbull middot ~~ middotmiddot bulltbullbull _ffmiddotmiddot-middot v I )tylt~ -~bullbull1bullbullrbullbull ~-lt -~ ( I~

600~ A0 Cv(A (1829 m AND OVER) deg )_ rJ__~7 middot middot ~--middot L==1 _J bullbullbull - bull -middot~-- rgt ~ middot(Zmiddot- middotbullmiddot middot

Z~C)-tGOO (762 middot 1829 m) 9-N4 __J (r -- lf _ bull bullgt-~~~ ~ _ w _ _ I (1 bullmiddot( middot1 middot -----~~~- middot L-bullmiddotbullW bullbullbull3 STA r I0-4 lODEL

100i -2soo (305~762m) -- Ow - -~1_- i ~~--- bull v~rvt ~~ -middot )) ~--

II gt J (-_bullmiddot middot~ l bull bull tr 1 )~ gt ) bullbull-_bullI-middot -middot bull~0 3 Mor nuq1ENr Wlbull~O JIAtCTIO-bull bull - lbull C---gt bullbull )t bullbull -( I bullf I - 20-00 (61 bull 305 ml J( Jloa xxE- -bullbull00 - -- middot1

0-200 (0middot61m) Wl)7 AVBt~gpound ) bullmiddot-iiNL~ middotntmiddot_ 1 iJJlt( _1J- ~ VAq IA9 IL ITY 0 ~ 10 15 ltS lHPtl

~--_ bull bull I bullbullbullbull 1 ~) J)J ~ bull Is bullmiddot bullbullbullbullbull ~ 3 V IS A VAqlABLE OIR~CTIO- 0 8 16 2-4 km

(SPEEDS SHOWN IN mph 10 mphbull 16 h1llr) -- middot ktr~~~ lt~ ) -middot-SCALE

Figure 7 LOS ANGELES BASIN MEAN WIND FLOW FOR DAYS WITH LOW LEVEL INVERSIONS DURING AUGUST I 970 AT 1600 PDT

-~~~~-=======~middot~-~======~middot--=-==-===gt=---==____________=== ~--=-J~==-- -=-ee----=-------

500

N f-- V

- - - SUBSIDENCE INVERSION

----MARINE INVERSION

bullbull-bull-bullbullGROUND LEVEL

x WINOS ALOFT (kmht)

WESTERN middoteASIN EASTERN BASIN

LAX WINOS EMT IHOS I I

CNO WIHOS

s_ 04 13 1500- 05 02 08

I 06 069 middot

11-1--

04 04 i ~4

06 ~ 4--

I 2

1000 n1 1005 -_E

lll --1 lJ -----------~----

~11

--=i-+- c -- 9 _____ - ~ C

lt I

I 6 4 _r 31

I 6 5 ~~ ~_ bull ---middot- 64 ~li- - middot- bullc - middot-----------

10

SMO (1347 PDT)

EMT (1246 PDT)

BRA CAB (1459 PDT) (1335 PDT

RIA (1349 PDT)

RED (1406PDT)

Figure 8 VERTICAL CROSS-SECTION OF bscat FOR lvflDDAY

T t 10-4 -1)(l n1 s are m

JULY 25 1973

- c - -~

~--~ JC_-_1- ~1pi~ oamp----~JilliiiM~f~-U~ -~--- --~~~ ~~~

-=--~

-E-- O

_ lt

1500 05

06 15

09 __~

1000 --

~- ~---middotmiddot 29

500

oJ11

__a

07

I 07 I

I I

I

09

I

I

I

I 7 ---

11 -----

~ ----- 6

---------------lt- -~middot4 --------

20

29

-

10 10

11 07 08 08

10

08

~8 _____ Y-

N

- - bull SUBSIDENCE INVERSION

----MARINE INVERSION

-bull-bull-bull GROUND LEVEL

WES TERN BASIN EASTERN BASIN x WINOS ALOFT (kmhr)

t t

CNO WINOSILA WllltOS poundMT WINOS

SMO LA EMT BRA CAB RIA RED O (1736 PDT) (1655 PDT) (1707 PDT) (163 PDT) (1823PDT) 1805 PDT)

Figure 9 VERTICAL CROSS-SECTION OF b FOR AFTERlOON OF JULY 25 1973 scat

T bull 1o- 4 - l )(units are m

__~~---iii~~- ~- ~~______ ~~- --~~J---=-~ ~

N ~ -J

PACIFiC OCEAN

0 5 10 15 1111

E 8 4 I 0 8 6 2 ~ bull

SCALE

dh Mes

CONTOURS REPRESENT - 000 ft 305 m

0 SNA

c8s

ec 8v

amp R~b

Figure 10 TRAJECTORY ENVELOPE FOR AIR ARRI1G AT CABLE AIRPORT (CPLAD) 1600 PDT JULY 25 1973

~-~

q_- ~ ------1 H~~~ -~~--~ ___---___--i- __r-=-1--===12---1 ~ ___r~ _==---_ - ~- f~~ ~-- - -5plusmn-at -~middot~

ll~~r1 ri

40

ec 8v

-1 I

amp

0 HQ_

7 0

CAP LAAR) O

VER

PACIFIC OCEAN ~ 0

RLA

4

WHqR d

diams

H ~I

I l

0 COMA

3

L~

LAH

Fa_ f ~~

S ~ LA APCD VALUES ADJUSTED TO AGREE ~

lt

0

5 10 15 mi0 WITH ARB CALIBRATIONE-j I I CONTOURS REPRESENT NZJ ~ 0 a SCALE 6 24 km - 1000 ft 305m COS v~J

______ J 10 ro ( igtf t-i

coFigure 11 SURFACE OZONE CONCENTRATIONS (pphm) I 600- I 700 PDT JULY 25 1973 ~

~~~~~C-~ ------=--~-__-~--~~~=--- ----=--~

N

-E

D1600----------------------------- 1--

14001-------------------------------

1200

I Ground Elevation

1000 middot 445 m ] lampJ

sect ~~ 7 ) SURFACE i6~ 800 MIXED LAYER

~

~ [ J ~ ~ I OZONE CONCENTRATIONS~ 600 E E GREATER THAN

( 50 pohm

400 I C H T Z GROUND LEVEL

200

I PUUloCETER UNIT SnbullBOL

NOc N0 0 ppm01 02 03 04 05 03 z

40 --~45~~ 50 co pm C0 5 10 15 20 25 30 35 I I I I I I I I I I TEIIPERATURE oc T-5 b 5 10 15 20 25 30 35 40 45

I-- 100 RELATIVE HUlillOITY H0 10 20 30 40 50 60 70 60 90 b1eot IOmiddotm- 1 8

CN cmmiddot3 1 IO X0 I 2 3 4 ~ 6 7 8 9 10 URBJLENC-C cm213ue- E

Figure 12 VERTICAL PROFILE OVER CABLE (CAB) J CLY 2 5 l C)7 3 l 63 6 PDT

~ _~ ~--- -

--

1400 I bull bull

1200

1000-5 LampJ 0 ~ I- 800 ~ c(

sooLl

-1-=-1-~--t j --=~c-o-----i-bull 1-~~~ ilt~~ -~-1 lta-abull--~ -c-~---=---r F--- ---- I n_--middot- =~~ ai~IHJ

(~-It

1600 ___________________________________

C r 11 s Ground Elevation t~C E H I~lcc

- ~ 1 90 m

4001 bullc C H

C UNDrnCUTTNG svC ~ Ic- H

SEA BREEZEC II 200

C C

[C -PARAMETER ---UNIT SYMBOL

NOx N0 0 ppm01 02 03 04 05 03 z co ppm C0 5 10 15 20 25 30 35 40 45 50

-5 middot- -~20~----25 TEMPERATURE oc T0 5 10 15 30 35 40 45

100 RELATIVE HUIOITY H0 JO 20 30 40 50 60 70 80 90 bcot 10-4m-1 8

CN crrr3 10 0 I 2 3 4 5 6 7 8 9 10 X TURBULENCE cmZ-13 sec-1 E

N N

_-----=-G--~---

Figure 13 VER TICAL PROFILE AT EL MONTE (EMT) JULY 25 1971 1656 PDT SHOWING UNDERCUTTING BY THE SEA BREEZE

0

middot~_lt ~middotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotbullbull

-~

LACA

0 - )

i r=

-v2v

~

_middot~middot)( I bullbull

bullJ

K~Ji~middot

~~ 61iAS 0

EMT J~J---6~-11 ~orr

PACIFIC OCEAN

WEST 0

SMC

0RLA

14

L~8

R~A

~BL

16 ~ ~

0 5s Pcfrac14A c1i ~ )

wFJfo~J_) ltI~~~

_ff-Clf1ito J )

HILL~

~J U

~ _~~~

~

I o middot

1 1$ ~ 11yen ~middot ~I N

I

N I- I

t

0 --pomiddotmiddot bullmiddot i- 1LO middot Joomiddotmiddotmiddot -- middot middotmiddot -middotmiddot

_middotmiddot 0 middot middotbull MWS r

L4 ( 1 T bull bull __-- -A bullbullbullbull middot

0 i __ bullbull

17 t-J~ N7 a S I ~r ~ 1 rtd ~lt A-~ v- middot ~ - cXa 0

RIA 19

CLO

ltJ~

bull ~ 0

(

--

1

_ _

-2Wl

~s~o -- _)~J0JgtJ~ ___ Q

15 l1JI

0 15 r(A0

CAP

CLARR)~R 1900 1-shyPDT

II (_-L~X L2X I 0~ R[V

0 CCtwA

I

I18=00 POT~ l4 r1

fj

-11J - ----- 11=oomiddotmiddotpor

l~i middotmiddot- o

i

5 10 5 Tl o~1 middot--middotmiddotmiddot middotmiddot

_q it==i--__F-3 9 I I CONTOURS REPRESENT SNA NZJ ~1 o

_- I 0 8 16 24 km I - 1000 ft 305 m middot ~

7 14~CALE --- 2500 ft o2m V lr1 ) middot I i0 _ il o5

16QQ pol(middot v( ____________ _L

I i

Figure 14 APPROXIMATE TIME (PDT) OF ARRIVAL OF SEA BREEZE Jl-LY 25 1973 (Ogt_iective criterion based on ground level ozone concentrations)

~ -___~==~ ~~ - ~ =-~ f7r=~1 _j~-~ --c_~~

u-middot - middot middotmiddotmiddotmiddotmiddot

~- middotmiddot~ ~1 WESTERN BASIN r Joa_middotmiddotmiddotmiddot_ NOxEMISSION RATE ~- 95 METRIC TONShr

-----bull_ ~ ~middot~ I -OUR -----middot )omiddotmiddotmiddot - middot~ l21 (fTI

~ AT middot ~ middotbullmiddot- ~- ~ middot 4bull-middot

I EASTERN BASIN NOx EMISSION RATE 10 METRIC TONS hr

ri r bullbull

t10 Joa

) __ 8v -a_ -- -bull-I O ~AGA -_ ~S ___ _ middotmiddotmiddot -

~ ~v ai- omiddot-middot~-- - ) r -middotmiddotmiddot f middot( ---~ -l A ~ _ (- bull ___

it~ ~~~ middot-middot -- ~-~ ~~~ 0 0 AZU~

AVERAGE CONCEN7RCTi)N iN BOX (IF STEADY STATE)

IS 25 pphm

1 r f--Ji 7 ~Sv PAS ou )V~(~- ~ t i -~ Li_) 03 FLUX THROUGH f~

~ ~JI_~ - amp_ JiM O SHADED BOUNOA~middot~-~ ~~-s-- EMT 185 t 60 METRI~ bull ~ ~ TONShr 0 (m)

c~~~ 1t~CS A~JFP

1000 _29

-i32

_~o tUA

_

1

O~ ~

0 -__rJ( (r- J PACIFIC OCEAN LAX _ C-middotJbull _

l o M R No _

550m

r

A frac14

HAR O HJ LAH

_ o camptA REDLANDS 18QO POT ~ r

I bull ~

RB MEAN TRAJECT~~~y

0

TOA L~S

0 AN

I - ~ 8 OUNOARY ~ ~middotltdeg ~ ~ BETWEEN middot __ WES~ERN ANO- middot middot - ~

I gt I lt bullmiddot bull (EASTERN ~ i middotmiddot middot - - ~

S ~ ~~ ~ - middot-

rt1~1_--t------l

middot1-- BASIN ~-~

1-)~~--middot ~ ~l

~~ ~-bull bull J --

-is-eo -_

0 5 10

j=i r-i C

0 8 ltl

SCALE

5 mi

2~ un

CONTOURS REPRESENT - 1000 ft 3gt5 m

--middotmiddot 2500 ft 1 762 m

~

0SNA

cos 0

_ --~ ----- --- ( bullmiddotmiddotgt

- middotlt- ltgtmiddot t__ Q ~

1 1 rmiddot bullbullbullbullmiddot ~9

NZJ ~ middotmiddot - middot- Alr ---middotmiddot- middot middot( middotmiddotmiddotmiddotv ~ bullbullbullw bullbullbull bullmiddot 1 bullbullr~ ~-- -middot ~--v ~- - I -~

ESTIMATED OZONE FLUX FROM VESTER~ TO EASTER-J BASIN JULY 25 1973 I 700 PDT

C ~IV

N N N

I

l ~

-~~

I

iI

i I

I t

t

~ ---~ --

Figure 15

~Qa llfJD fl(~middot ~ 11f ~I I

l

Lfb ec~s0 CPK v2v 0

ALT 8v Ld~_----1

I

HO-

0 CA

middotLARRv O VE~

1330

ol(Di

A~U

0ENT

~lt

s~e ~ 1530

F8f 1730

~

rbull-~

oc (WljT) -_-~(~~c lt-rw---_

~~ ~-_i~cB~~~

2-~) - ~ ~ l~w-~~ p~- pound)_

0 ojI middot tl-1CfUp I ~ ) 1 ~ J~I i bull middotbull middot~-Li 1)- ) I

DiI ~- 0

i ) 0 l I I

t

A RALc~o JI

C

-~

0 r-iR

~IV 1230 1~

RE PO ~- I - Ftl

) 0 ---~gt- __L8s ~Zi diams ( T~ _middot_ ~~ ~

I AN ~~-~ j t bi 0

~ I

~ I L i

-_gt ji o 5 c 5 Tl middot 0 0 ~-i p__i=r 2=f I_ I 1 NZJSNA 1

1 8 2 4 km )

SCALE I 00 J_(1 CONTOURS REPRESENT cos f

1 0 I --- I - ))) 35

PACIFIC OCEAN

Figure 16 TRAJECTORY E~VELOPE FOR AIR ARRI1gtJG OVER REDL_)DS AT 1800 PDT JULY 23 l =i73

224

JULY 25 1973

LA DOWNTOWN

0sect040 a

~

~ 020 0 X z0 ~ LJ 0 ~ z

~5 040 330POMONA 0 ~ en~ 020 w z _J

w w 0 (9 z O----u-~~-__~_-~~~-------L-~-0--0-0~----- z

ltt~ 040 56 (I)z

0 0o _ RIVERSIDE _J0 20 t6 ~

0~ Qt---0-0--ltrO-ltgt-C~------~~~~ a

LL ~

Rate ~ IO mph___ (I) w

_J~ ~ ~

et~ lt(

3 040 PALM SPRINGS ~

j 020 ~

0------____-----L--___---------L---~--~

105

12 4 8 12 4 8 12 l~-s----am _ pm----1

HOUR OF DAY PST

Figure 17 Diurnal variation July 25 1973 of oxidant concentrations at air monitoring stations at Los Angeles Downtown Pomona Riverside and Palm Springs California Values are corrected data Los Angeles Downtown and Pomona x 11 and Riverside and Palm Springs X 08

CONO S t 1 fRESEIS7

~

~~ 0

ciffmiddotdK ~ ~v~~o

( ~s ~

bull ~r ~ bull 1--~~----Soootl ~ ~ ~ ~ lj i1 d t CJ ~ ampfrsmiddotflt- frac12 ~ middotL~Js _-- ~

_gtgt middot~ ~rroltf~-) ~ 0 s- r

middot-middot- r_~ ~~JtbO ~~bull~Jt ~~~ L r - bull _ ~ I= J 1 ~ ~ ~-~~bullJC ___ -_ middot ~ laquo -poundJ~ ~- middot1~ r-- - V--_1_ ~ I 1 S I

V ~ bullf-uv~ fi -~zumiddot -~middot~ LS gt -tmiddot-F Q~ ~-tv I_~ --- ONT p(_ s ~S ~~~-[ ( 0 c-_ --~ ~~~___d_) lt- ~ I -i-C - -

~----1-1 bull~~POMA ~V BN ) middot-~ f -- s - ~

~VA -middot- ~p AAL a 2~~ ~~middot01 r r ~ middot middot 0-- V

i LAX bull1

~ -~poundJ-i- ltllll _(__1-0~ ~t- degQ-0- ~~ _ _-__~~-qlK ( a_ II ~ ~p-~ ~J

N bull - - 0 r o_ _I ~ -~ ~middot ~ ~amp ~--= ~ ) s ~

- -~- - middotO _a - Tl --0- ov I lHOIO J I bull J -- ~ 6 ~ -__ 2 ~

(__ ~~ _- ~-~ middot8---fl~ -- ~ bull~-abullbull _~ ~-cgt ~ bull bull middot e bull bull l ~ 0

I 1A_ HZJ middoto~J

middot0 (~ ~ S TAA

- ~ - - - --0 () _-j J middotO=c==c-c==cc~~~ l ~~ ~ ~ bull-~---~ ~ bullbull -~ al1 ~ bull __ ~--middotmiddotmiddot

diams Skyforest _ Strawberry Mt Lookout

Figure 18 STRE ~[Ll)ES FOR 1600 PDT on 8 1673

~ ~--

vO 0

N N V1

au

91 V7

-1 ~ -=1 ~~ ~~~~l r=--~d- ---1 _J-_

~E1 ~L1-~f~

3100 ---------------------------------

2900r-----------------------------

T

e w 0

~ 5 Cl Ground Elevation

1560 m

T PARAMETER UNIT SnbullBOL

NOx N 01 02 03 04 05 03

ppm z co ppm C

10 15 20 25 30 35 40 --

45 50

170

I I I z

0 5

-5 - -0~ 5 10 15 20 25 30 35 40 45 TEMPERATURE oc T

0

0

10

I

20

2

30

3

40

4

50

5

60

6

70

7

80

8

90

9

100

o

RELATIVE HUMIDITY

bcot CN

TUR8ULENC~

110-4m-

cm-3 tobull 213 1 cm sec-

H

8 X E N

N OI

Figure 19 VER TI CAL PROFILE OVER ARROWHEAD u-RR_l A CG CST I 6 1973 939 PDT

3100----------------------------------

N2900r----------------------------- -i

N

2700i-------------------------------

2500

e 0 uJ 2300 gt ~ ct

2100

1900i---------------------+--------------

~le 1iation 1360 m) 17001 ~

- -PARA1jETER UNIT SYMBOL

T NOx N1500 o ppm01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50

TEWERATJRE oc T-5 middot --~o--- 5 10 15 20 25 30 35 40 45

IOO RELATIVE HUWIOIT Y H0 10 20 30 40 50 60 70 80 90 bcat 10-~- 1 8

CN cm- 3 104 X0 I 2 3 4 5 6 7 8 9 10 213 1 tURBliiENCE cm sec- E

Figure 20 VERTICAL PROFILE OVER ARROWHEA D -RR 1 --- -AUGlJST 16 I) 16--1S PDT

1-~i w--~i_f l-=--bullC- ---~-4

1600 bull t c- N 8 ff Tbull C[ 8 H 1 bull H z H T ~ C f N 1 H T bull C rn 1 C NE bull-~z Hi400 bull bull tf T bull N ~r --middot _P H -ybull EC N z__e H T i 8 z H Tbull C E HD Z H T POLLUTANTS REMAINING FROM bullt C Hbull L T PREVIOUS DAY1200 Et HO I II -middot-- bull Ct H 9 - H T

___ Hbull( E N 1 a tC N i--_ -1 H

C N Tbull Z HP poundIC C H z_ 1111 1

- bull C H Z l _H_ _J1000 )( cc H -z emiddot ksect bull C N ~ T

)( iz H 8 H TIAI -t XC z 7-- T0 bull pound N t H_8

t-gt

YCpound N 1800 l I-gtltbull - H (Jet

N i -r~Bltt t bull gt- t C X N H T

[ BUOYANT POINT SOURCE PLUMEH 1

N ~z-- -

C H

-bull SUPERIMPOSED ON POLLUTANTSC JZ X H T 600 -~ E c REMAINING FROM PREVIOUS OtY Cl JC t H H f bull cmiddot t HT -fl

C- X t fl _ REMNANT OF NOCTURNAL RADIATION INVERSION(I-----e-C f N K I T H

C Z [ T H x-8 400 _Zc r -H -K SURFACE MIXING LAYERz C II H K 8

C N T pound H M 8 _ I -t ff H E N -9 l

Ground Elevation 305 rn200

PARAMETER UNIT SYMBOL

_ I - I I I NOx N00 ppm01 02 03 04 05 03 z

co ppm C 0 5 IO 15 20 25 30 35 40 45 50

L middot1 TEMPERATURE oc T-5 0 5 IO 15 20 25 30 35 40 45

100 RELATIVE HUPAIDIT y H0 10 20 30 40 50 60 70 80 90 bscot o-4m- 1 B

CN cm-3 x 104 X0 2 3 4 5 6 7 8 9 10 TURBULENC~ cm213sec-1 E N

N co

Figure 21 VERTICAL PROFILE OVER BRACKETT (BRA) JULY 26 1973 0825 PDT SHOWING BUOYANT PLUME AND UNDERCUTTING BY RADIATION INVERSION

N N 01600

___bull C M C

C

1400~~~ t C [ middot H LAYER CAUSED BY

C C H C [ H UPSLOPE FLOWl

1200

1000 ] w

SURFACE MIXING LAYER 0 --= ~ -~~ 6 800~ er

C C

600t-i C C t C

I ~00

Ground Elevation 436 m 2001-------------------------------

PAIUWETU UNIT SYWBOL

NOx N ppm0 0 01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50 I I I I I I I I TEWPERAT1JftE degC T-o b 5 10 15 20 25 30 35 40 45

100 ~EIATIVE HUWIOITY H0 10 20 30 40 50 60 70 80 90 b1tt1 10-m- 8

CN enr3 110 X0 2 3 4 5 6 7 8 9 10 Tu RUL Erct cm23sec- E

Figt1re 22 VERTICAl PROFILE AT RIALTO (RIA) JlJL Y 19 1973 1738 PDT SHOWI=JG LAYER CAUSED BY UPSLOPE FLOW

~~-7 ~ ~- 1 ~iri ~~- ~~-~ ~t ~~ ~ =~middot-1

1200 I t 1 If J-

1000

I C ltTl a_ ~l- t

800

600

L gE __r H

H

400 j (~ c pound N C E I~

t EH -

1-1 M

H H

H M H H

H

H H

11 bull H M H

M H If

H H

H

- C t H ~ C poundmiddot H

I C E I(

200

1600--------------------------- t

T t t T l

l T t

T t_

t 1

l] w ) g f

Tt t

ltt ~ T

t J t T

t J

f 1

t

Klt

H M Cro1nd Elevation 250 m HT X

5Yl80LPAllAlETER ~

NOx N0 0 ppm01 02 03 04 05 03 z

co ppm C0 5 10 io 20 25 30 35 40 45 50

25~--- ---35~~-40 TEMPERATU~E oc T-5 0 5 lO 15 20 30 45

100 RELATIVE HUMIDITY H0 iO 20 30 40 50 60 70 80 90 bact 10--ltllm-1 B

CN cmmiddot3 11 04 X0 I 2 3 4 5 6 7 8 9 10 IURBULENCE cm2hioC-1 E

Figure 23 VERTICAL PROFILE OVER RIVERSIDE (RAL) N

JULY 26 1973 2239 PDT I)

middot==-=-=

0

bull

N w 1--

ii -s~~ l-obull

CJ ~

obull -obull obull

5 02~

bscat

Oa

4l o2J

-I 3 e I 0

--)(

~

Abullu 2

ll

ol

Traverse at 750 m msl 35 km Downwind (SW) of Arch - St Louis Mo 1117 - 1137 CDT

( Power Plant Plume -01 Ibull-[ ~ e

11 bull E I -)(I

I0bull I 1r~ l -

0

I I Io 1 u I

I r- l A bull I i I 1I

H1I I 4 t I II I I

11 I I

I I r I I I

I I qo 01 I I

I I bullJ~viI I middot ~

I

I I

~

Urban Plume

ood 0 10 20 30 40 50

kilometers

o~

02

01

s 1

P

0bull 01

00S~J1 I ti middotmiddot1 middotvmiddotmiddot~ J

Urban Plume

I y

oo 0 10 20 30 40 so

kilometers

Traverse at 750 m msl 46 km Downwind (SVV) of Arch - St Louis Mo 153 0 - J 549 CDT

---- bscat

o-

Power Plant Plume

1l~ 11I 1 t

ill~t fl Ibull I ii

I

lmiddotmiddotrI

I I I I t II

l vrI V

JV-f Jl bull

bull t I bull I

Figure 24

l

232 RELATIVE CONTRIBUTIONS OF STATIONARY ANDMOilILE

SOURCES TO OXIDANT FORMATION IN LOS ANGELES COUN1Y IMPLICATIONS FOR CONTROL STRATEGIES

by Robert G Lunche Air Pollution Control Officer

Los Angeles County Air Pollution Control District Los Angeles California

Introduction

The type of air pollution problem characteristic of the west coast of the

United States and particularly of Southern California has come to be known

as photochemical smog because it is the result of sunlight-energized atmospheric

reations involving oxides of nitrogen and reactive hydrocarbons Its manifesta-

tions- -eye irritation reduced visibility damage to vegetation and accumula-

tion of abnormally high concentrations of ozone or oxidant - -are by now well

known In fact the occurrence of high levels of oxidant which consists almost

entirely of ozone has become the primary indicator for the presence and relative

severity of photochemical smog

During the 25 years since photochemical smog in Los Angeles County was

first identified an extensive program has been underway for control of the responshy

sible contaminant emissions Initially during the 1950 s these programs concenshy

trated on controlling emissions of hydrocarbons from the stationary sources of this

contaminant In the early 60 s programs for the control of hydrocarbon emissions

from motor vehicles in California were begun An exhaust emission control proshy

gram for hydrocarbons and carbon monoxide from new vehicles was begun in 1966

C011trol of oxides of nitrogen emissions from motor vehicles began in 1971

As a result of the overall control program by 1974 emissions of reactive

hydrocarbons from stationary sources have been reduced 70fo from uncontrolled

levels and about the same percentage from mobile sources Oxides of nitrcgen emissions

233

from statjonary sources have been reduced about 53 while emissions from moshy

bile sources are still about 7 above uncontrolled levels due to the increase

in NOx from 1966-1970 models Additional controls already planned for the future

will by 1980 achieve reductions of reactive hydrocarbons from stationary sources

of about 87 from uncontrolled levels and from mobile sources about 93 By

1980 emissions of oxides of nitrogen from stationary sources will have been reshy

duced 53 and from mobile sources 63 from uncontrolled levels The past

present and projected emissions of these contaminants are shown in Figure 1

A I though compliance with the air quality standards has not yet been achieved-shy

and is not likely before 1980- -the results of these programs have been reflected rather

predictably in changes in certain of the manifestations of photochemical smog For

example eye irritation is less frequent and less severe and in some areas js

rarely felt at all any more and damage to vegetation has been markedly reduced

Ozone (or oxidant) concentrations have been decreasing in Southern California

coastal areas since _1964 in areas 10-15 miles from the coast since 1966 and in

inland areas 40-60 miles from the coast since 1970 or 1971 as shown on Figures

2 arrl 3- All of these positive effects have occurred despite the continuing growth

of the area indicating that themiddot control programs are gradually achieving their purpos

a return to clean air

This improvement is al~o refutation of the so-called Big Box -concept which

assumes that the total daily emissions in a given area are somehow uniformly disshy

tributed throughout that area--regardless of its size or of known facts about the

meteorology of the area or the spatial and temporal distribution of its emissions- -

234

and of control strategies based on that concept And since the improvement in

air quality refutes the control strategies based on reductions in total emissions

it thus confirms the value of more recent control strategies which emphasize conshy

trol of motor vehicle emissions and use of a source-effect area concept

Following is a brief listing of the evidence we intend to present as supporting

our views on just what control strategy is appropriate

Examination of relative contributions of HC and NOx from stationarybull and mobile sources demonstrates that motor vehicles are the overwhelming

f source of both contaminants~

I bull Observation of air monitoring data shows that the effects of photochem -

ical smog are not uniformly distributed t_hroughout the county

bull Study of the meteorology of LA County shows consistent paths of trans -

port for various air parcels and consistent relationships between the

areas most seriously affected by photochemical smog and high oxidant

concentrations and certain other areas

bull The upwind areas are found to be source areas--the downwind areas-shy

effect areas

bull Central L A is found to be the predominant source area for the effectI area in which the highest oxidant levels in the SCAB consistently occur

bull The predominant source of emissions in this source area is found to

be motor vehicles

bull Central LA has the highest traffic density I

ij bull Both pr~mary and secondary contaminant concentrations reflect the effects

of the new motor vehicle control program in a predictable fashion 11 I

A strategy based upon these findings is gradually being verified by atmosshybull pheric oxidant data~

235

The Evidence that Motor Vehicle Emissions Are the Principal Source of Oxidant

As seen from Figure 1 at the present time the total daily emissions of I-IC

and_ NOx from all sources in Los Angeles middotcounty are primarily due to the motor

vehicle The problem now is to find the spatial and temporal representation of

emissions which when examined in the light of the known meteorology and geogra -

phy of the Los Angeles region best describes the source of emissions responsible

for the highest observed oxidant readings

In the rollback models used by EPA and others the basin is treated as a

big box with uniformly distributed emissions and peak oxidant is considered to

be proportional to total basinwide hydrocarbon emissions

The fact is that the middotemitted contaminants from which the smog is formed

and the effects which characterize that smog are not evenly distributed throughout

the Los Angeles Basin in other words the basin area under the inversion is not one

large box filled to all corners with homogeneously distributed air contaminants and

photochemical smog

Refutation of Big Box Myth

Examination of atmospheric contaminant concentrations refutes the big box

concept It is found for example that concentrations of djrectly emitted contam -

inants measured at a particular sampling site reflect the emissions within a rather

limited area around that site For this reason contaminant concentration levels

vary from one location to another and each has a characteristic daily pattern which

reflects the daily pattern of emissions in that area

middot 236

The big box concept is further refuted by the fact that peak concentrations

of carbon monoxide and oxides of nitrogen in areas of high traffic density were

fairly static prior to 1966 Thus they did not reflect the 45-50 per cent growth

in motor vehicle registrations and gasoline consumption which occurred in Los

Angeles County between 1955 and 1965 and which caused comparable increases in

total daily emissions of such vehicle-related contaminants This demonstrates

that growth was outward rather than upward so that a larger area of the County

began to be affected by photochemical smog but no area experienced smog ofJ

greater severity than that originally affected by smog formed from the vehicular

emissions which accumulated each weekday in central Los Angeles and were trans-

1 I

ported later that day to the San Gabriel Valley

1 Meteorological Evidence

To verify the geographical dependence of emissions and resulting atmospheric

concentrations let us examine the meteorology of these large areas of Southern

California Both the County and the Basin have many meteorological sub-regions

in which the patterns of wind speed and direction may be similar but within

which the patterns of air transport are parallel with those of adjacent sub-regions

and the respective air parcels do not ever meet or join

The characteristic patterns of inversion height and wind speed and direction

in these sub-regions and their patterns of vehicular emissions together have

created a network of source areas- -those in which the reactant contaminants accu -1T

i ~ mulate in the morning and begin to react--and related receptor areas--those to which

~ the products and associated effects of the photochemical reactions of the contamshy)

inants originally emitted in the source areas are carried by the late morning and

237 middot

afternoon winds ( sea breeze)

Wind-flow patterns show that characteristic patterns of transport for related

source area-effect area combinations are separate and parallel not mixing or

joining Each source area has its own reactor pipeline to its own effect area

or areas

To illustrate this source area-effect area relationship the typical flow of

polluted air from downtown Los Angeles to Pasadena was selected as a worst

case situation for in-depth examination Figure 4 shows that the air in downtown

Los Angeles on the morning of smoggy days moves directly from the central area

to Pasadena

Vehicular traffic is the predominant emission source in both downtown Los

Angeles and Pasadena Thus the air in each locality should contain CO Also

since oxidant would form in the air parcel moving from Los Angeles to Pasadena

oxidant levels would be expected to be higher in Pasadena than in downtown Los

Angeles

Figure 5 shows these relationships for the period 1960-1972 The atmosshy

pheric CO level is similar for the two areas while oxidant levels were higher in

Pasadena than in Los Angeles throughout this time period This demonstrates

that a significant amount of oxidant formed in the air as it moved to Pasadena

containing both the unreactive CO and the photochemical reactants for producing

oxidant Both CO and oxidant show a marked downward trend in each locality since

1965 which emphasizes the effect of vehicle exhaust controls and the correlation

between the localities

238

On a day which is favorable to the formation and accumulation of photoshy

chemical smog a contaminated air parcel normally originates during the

6-9 a m period on a weekday from an area of dense traffic centered just

south and west of Downtown Los Angeles It is oxidant generated within that air

parcel which usually affects Central Los Angeles and the West San Gabriel

middotK IJ l J

Valley area around Pasadena

The traffic area in which this smog had its origin is about the most dense

in Los Angeles County and has been so for the past 25-30 years No area

has a higher effective density thampn-this Using carbon monoxide which

1

is almost entirely attributable to motor vehicles as an indicator of such emis-

sions it is found that the concentrations of emitted vehicular contaminants

middotr i

measured in Central Los Angeles during the past 15 years confirms both this lack

of change in effective density and the absence of any area of any greater effective

density when local differences in inversion are acknowledged

This area the Central Source Area is depicted in Figure 4 The size

and shape of the Central Source Area was ch~sen to be large enough to reduce to

an insignificant level any diffusion or transport into this area from any externally

l generated reactants This conclusion is based in part on the trajectory studies

previously referenced as well as an analysis of the diffusion and transport parashy

meters for the area

239

The Central Source Area has been identified as that geographical region

which contributes essentially all of the primary contaminant emissions giving

rise to the highatmospheric oxidant levels in the West San Gabriel Valley

The proportion of emissions in the CSA due to motor vehicles and that due to

stationary sources is shown in Table 1 For the County as a whole about 80 per

cent of _(6-9) AM reactive hydrocarbons are due to motor vehicle emissions and this

figure rises to 90 per cent for the CSA The same conclusion a pp lies to NOx

emissions The Central Source Area contains the greatest density of vehicle traffic

in the County and thus the greatest density of source emissions Thus it appears

that the source area with the highest density of emissions during the critical (6-9)

AM period is responsible for the highest afternoon oxidant levels observed in Los

A i1geles County and in the South Coast Air Basin These highest oxidant levels

are consistently observed to occur in the San Gabriel Valley This is true whether

the LAAPCD or the ARB oxidant calibration procedure is used

Further the atmospheric concentrations of the primary pollutants can be

identified as originating primarily from the motor vehicle and they reflect the

effects of the motor vehicle emission control program A vehtcular source area

can be identified by its atmospheric levels of CO and NOx Figure 6 compares

measured atmospheric levels with calculated atmospheric levels for CO NOx

and the CONOx ratio in the downtown area

TABLE 1 240

REACTIVE HYDROCARBON EMISSIONS

(6-9) AM

1970

LOS ANGELES COUN1Y middot CENTRAL SOURCE AREA middot SOURCE TONS PER CENT TONS PER CENT

Mobile 1260 81 3 135 91 2

Stationary 290 187 1 3 88

Total 1s~o 1000 148 1000

By 7 -Mode Gallonage

241

The calculated values shown in Figure 6 were derived from a baseline

survey of 1100 vehicles and continued surveillance tests both using the Calishy

fornia 7-Mode test cycle The baseline survey showed that motor vehicles withshy

out exhaust control systems had average exhaust emissions concentrations of 3 4

per cent CO and 1000 parts per million of NOx Baseline emissions data apply

to 1965 and earlier model vehicleg and surveillance data to 1966 and later modelsmiddot

Since it can be concluded from calculations and observations that the dilushy

tion of auto exhaust emissions in the atmosphere on a smoggy day in Los Angeles

is approximately 1000 to 1 the calculated values for CO and NOx prior to 1965 are

34 ppm CO and 1 ppm NOxo After 1965 the changing effect of controlled vehicles

in the total vehicle population is reflected in the calculated values

CO and NOx values measured in the atmosphere are also shown in Figure

6 and confirm the values calculated entirely as diluted vehicular emissions NOx

concentrations measured in the atmosphere tend to be consistently a little lower

than the calculated values probably because photochemical reactions remove some

NOx from the system

The data for CO and NOx calculated and measured show that emissions in

downtown Los Angeles originate almost exclusively from motor vehicles and that

atmospheric concentrations there reflect the average emissions from a representashy

tive vehicle population

The ARB has recently published a report entitled A Trend Study of Two

Indicator Hydrocarbons in the South Coast Air Basin Acetylene was used as a

242

specific indicator of automobile exhaust emissions and it was found to have de-

clined in concentration in the Los Angeles atmosphere at an annual rate of 12 5

per cent since 1970 To quote from this report The California implementation

plan requires an annual average reduction in these emissions (reactive organic

compounds) of 166 tons per day or 11 1 of the 1970 tonnage per year The per cent

reductions in the_ acetylene levels at Los Angeles and Azusa are greater than reshy

quired by the implementation plan Since acetylene is almost entirely associated

J with auto exhaust this demonstrates that the motor vehicle emission control

program is achieving its purpose

To summarize at this point it has been deomonstrated that high oxidant values

are due to motor vehicular emissions of NOx and HC because

NOx and HC are the principal reactants in the oxidant formation process

and they originate primarily from motor vehicle emissions and

The highest oxidant values are recorded in_ effect areas that receive air

from source areas where motor vehicles are clearly identified as the

dominant source of NOx and HC

243

Future Control Strategy

The APCD strategy for achieving and maintaining the oxidant air quality

standard is based upon the fact that high oxidant values are due to motor ve-

hicle emissions of hydrocarlxms arrl nitrogen oxides This strategy is as follows

1 Both Hydrocarbon and Nitrogen Oxides Emissions Must Be Considered To Achieve the Federal Oxidant Standard

There is wide agreement that NOx and HC are the principal reactants in

the oxidant formation process and that vehicular emissions are a major source

of NOx HC and CO

2 Effective Regulation of Atmospheric Concentrations of Both HC and NOx and of the Ratio Between Them is necessary for Attainment of the Federal Air Quality Standard for Oxidant

Basmiddoted on the abundance middotof available experimental evidence it is our firm

position that the most rational approach to solving the photochemical oxidant smog

problem in the South Coast Air Basin (SCAB) is to control the quantities of emissions

from motor vehicles of both smog precursors--Hcmiddot and NOx--their resulting atmosshy

pheric concentrations and the ratios between both contaminants which will result

from these controls

We arc also convinced that the oxidant and nitrogen dioxide air quality stanshy

dards can and will be met not by 1975 or 1977 but by the early 1980 s if the emisshy

sion control program as originally outlined by Ca~ifornia or a slight modification

of it proposed by the District is followed and enforced This should also provide

for continued compliance with these air quality standards at least through 1990

244

It will also allow time for a reappraisal in about 1978 of the whole situation relative

to the ultimate emission standards required and the best approach to their impleshy

mentation

Calculation of the degree of control necessary to attain the air quality

~ standards for oxidant and nitrogen dioxide involves indirect complex methods 1

aimed at determ_ining the degree of control of the primary contaminants directly

emitted by automobiles

The following evidence supports our proposed solution to the problem in

terms of both the atmospheric concentrations of the oxidant precursors NOx

and HC the ratio between them as reflected in their exhaust emission standards

and the resulting atmospheric concentrations of oxidant which comply with the air

quality standards

Chamber Results and Projections to the Atmosphere

The importance of environmental chamberwork cannot be minimized the

j need for and direction of the whole emission control program was based initially

j on the results of chamber experiments In order to understand the importance to

air quality of achieving both the correct low quantities of emissions and the right

ratio we can present several graphic portrayals of analyses of experimental labshy

oratory work together with their relationship to past present and future air quality

in terms of both morning primary reactant concentrations during the morning

traffic peak and the equivalent emissions which would produce them

245

Figure 7 shows maximum ozone levels that were obtained by irradiating

varying amounts of auto exhaust hydrocarbons and oxides of nitrogen in an environshy

mental chamber The corresponding ozone levels then can be found for any comshy

bination of BC and NOx concentrations Thus high ozone is produced with high

emissions of both hydrocarbons and oxides of nitrogen and low oxidant is formed with

low emissions However either low NOx or low HC emissions11 can also produce

low oxidant--graphic and clear evidence of the importance of the NOxHC ratio in

ozone formation Furthermore each and every possible combination of values for

NOx and HC has then a corresponding characteristic maximum chamber ozone

concentration

Using this graph we can estimate what ozone levels would result if certain

atmospheric mixtures of NOx and HC could be injected into the chamber and

irradiated Such estimates were made for 1960 and 1965 using atmospheric data

rlThe points labeles 1960 and 65 show the location of the highest levels of both

HC and NOx found in the air in those years in Downtown Los Angeles (OOLA) area

during the 6-9 AM traffic peak

It has been demonstrated by use of CO and NOx data and CONOx ratios

hnw well the characteristics of vehicle emissions are reflected in the atmosphere

We know what emissions from the average vehicle were then in 1960-1965 both

for HC and NOx so that we can mathematically relate emissions to atmospheric

concentrations for those years and so for future years also knowing or calculating

only what the characteristic emissions will be from the average vehicle

246

The NOx concentrations stayed about the same from 1960 through 1965 because

average vehicle emissions of that contaminant did not change during that time

Mobile source emissions can be shown to have contributed essentially all of this obshy

served result However blow by controls did reduce emissions of HC and the

concentrations dropped accordingly In 1965 the last year before exhaust controls

the point 65 indicates where we were then in terms of maximum ozone formation

to be expected in a chamber with the highest HC and NO concentrations found in the X

air that year Levels of ozone actually measured in the atmosphere however

are higher than those shown on the graph for high NOx and I-IC concentrations for

those years up to the present

The strategy to meet the oxidant standard is obvious--get atmospheric NOx

and HC concentrations out of the area on the chart that produces high ozone levels

and put them in tie areas with the lowest levels This can only be done by implementshy

ing appropriate emission standards

As can be seen that did not happen between 1965 and 1970 because manufacshy

turers used controls on new cars in California which while causing a decrease in

BC (and CO) allowed a large increase in NOx emissions Thus the path line of

the atmosphere on the chart goes up from 65 and diagonally to the left passing

through an area of higher ozone levels The atmospheric concentrations of oxidant

predictably increased during the years 1967 and 1968 By 1970 they dropped to lower

levels - -back to about the same as in 1965- -exactly as predicted by the model The

app14oximate location of the point for 1970 (70) was both predicted on the basis of

247

the mathematical model and confirmed by atm-ospheric measurements of

[)owntown Los Angeles morning summertime NOx and calculated HC values

Again it should be pointed out that those points show the highest possible

concentrations of NOx and HC Years with less restrictive weather conditions

(for accumulating high primary contaminant levels) would cause lower measured

maximum NOx and HC levels but the calculations would still yield the points

shown Thus we are taking the most pessimistic view

Future Projections

In 1973 we were at about the point labeled 73 and ozone levels were beginshy

ning to drop as expected middot It should be emphasized that ozone values plotted on

thi$ graph are for the chamber only- -not the atmosphere The future path the

points 7 4 and on to 90 represents our estimate of future atmospheric levels of

NO and BC expected if the exhaust emission standards are just met While that X -

is optimistic it is all we really can do since performance of future vehicle models

is unknown We will achieve maximum ozone levels at or below the standard by

about 1980-1985 This will only be true however if cars in compliance with the

California interim standards for HC and NOx continue to be added to the vehicle

population at the normal rate These standards provide the optimum ratio of NO X

to HC necessary to provide the nitric oxide (NO) needed for the reaction that re-

moves from the air both oxidant formed photochemically and oxidant which occurs

as natural background which alone may cause the standard to be exceeded This

ratio is about 112 or 2 parts NOx to 1 part HC

248

The optimum NOxHC ratio is a key element in the APCD strategy but will

require a finite time for its attainment Replacement of older cars by newer ones

equipped to meet the most stringent standards is the only reasonable mechanism

which can change it VMT reduction proposed as a prime strategy by EPA cannot

change this crl(ical ratio which is a basic characteristic of the population at any

given time

Validation of the Districts Control Strategy

Figure 8 compares (1) future chamber oxidant levels based upon the

future maximum concentrations of HC and NOx we expect each year with the

California control program (2) calculated atmospheric concentrations using ~ I

our chamber-to-atmasphere empirical translation and (3) actual measured atmos-f 1l pheric oxidant maxima This clearly sets forth the relationship among these three

factors

The chamber concentrations (lower curve) middotare the lowest values shown

The actual atmospheric data (points connected by heavy dotted and solid lines)

vary considerably from year to year partly because of the vagaries of the weather

In all cases the atmospheric oxidant values are higher than the chamber values

because of the addition of vehicle emissions as the air parcel travels from source

to receptor areas The calculated atmospheric data (thin dashed and solid curves)

are shown to be the highest generally exceeding or equalling the actual measured

data and of course always exceeding the chamber data Thus the model paints

the most pessimistic picture possible It can be seen that by about 19801 1985 atmos -

pheric levels should be at or below the Federal air quality standard of 0 08 ppm oxidant

249

3 Motor Vehicle Exhaust Control is the Only Requirement for Achieving the Oxidant Standard by 1980

We can show that the existing motor vehicle control program has resulted

in a significant reduction of oxidant concentrations in the air

The foregoing material explained the relationship between vehicula~ emis -

sions in source areas and the high oxidant levels measured in effect areas This

relationship is exemplified by the downward trend of oxidant levels in the atmosshy

phere and by the similar year-by-year trends of NO and HC emissions from the X

average motor vehicle A projection of these vehicle emissions factors shows that

the associated maximum oxidant level in the atmosphere will meet the oxidant standard

by about 1980-1985

Figure 9 compares by year the number of days that the oxidant air quality

standard was exceeded in three separate areas with the average NO and HC emissions X

per vehicle mile To comply with the air quality regulations the number of days that

this standard is exceeded must be reduced to one per year

The lines plotted on Figure 9 show that a definite relationship exists between

the emissions from the average motor vehicle and the number of days each year that

the oxidant concentration in the air exceeds the clean air standard

The oxidant trendlines for downtown Los Angeles Pasadena arrl Azusa are

all downward and the slopes are about the same This similarity is logical because

the process that results in the suppression of oxidant accumulation simply has been

displaced from one area to another This was a unique one time situation because

of the increase in NOx between 1966 and 1971 After 1971 all areas are down Thus

l

250

the same conclusion is reached that the oxidantstandard will be met in the 1980s

I whether air quality data or vehicle emissions trends are projected middot~ Ul-

This outlook is based on the APCD s belief that future growth in both the

Los Angeles area and SCAB will not create any locality with a traffic density greater

than any traffic density in the area to date For the past 25 years the area around

downtown Los Angeles has been the area of maximum traffic density and therefore

the emissions source area responsible for the maximum effect area measurements

It is assumed that the traffic density in any future source area will be no

greater than the traffic density in downtown Los Angeles Thus since the

vehicular emissions control program will achieve and maintain the air quality

standards in areas affected by vehicular emissions from downtown Los Angeles it

will also achieve and maintain them for any area of SCAB

Summary Conclusions and Recommendations

In conclusion we have shown that a source and effect area analysis of emisshy

sions and resulting oxidant is a more reasonable and accurate representation of

the Los Angeles area for air quality analysis than gross integration metho9s such

as the big box technique It has been shown that motor vehicles are the major and

almost sole contributor to the primary HC and NOx emissions in the downtown source

area which results in the high oxidant levels in the San Gabriel Valley in fact the

highest in SCAB An air quality model and vehicle emissions control strategy has

been suggested to meet the oxidant standard by mid-1980 s

251

We have shown that

bull Only by adjusting the ratio of NOxHC in the motor vehicle emissions to

permit accumulation of sufficient atmospheric NO to sea venge the normal

atmospheric background oxidant can the standard be attained

bull The APCD strategy which provides for implementation of the present

California interim emissions standards for NOx HC and CO for new

motor vehicles in California beginning with the 1975 model vehicles will

result in compliance with the CO N02 and oxidant air quality standards

by the mid 1980 s and will maintain this compliance until 1990 and

possibly longer

bull The effectiveness of the present California motor vehicle control program

is easily demonstrable using air quality data from several areas in Los

Angeles County 1960-1973

bull To assure achievement and maintenance of the air quality goals as now preshy

dicted there must be periodic assessments of the effectiveness of the

motor vehicle control program followed by corrective actions if necessary

What has been accomplished thus far is significant but much more remains

to be done so that the best possible representation of emissions and resulting air

quality may be available for use in this air basin A much better emission inventory

defining the spatial and temporal distribution of both mobile and stationary sources

is needed Better statbnary source information is needed to evaluate the local

effects of these emissions Further detailed studies are needed to establish the

252

true relationship between emissions data from vehicle test cycles and the actual

operation of vehicles neither the 7-mode nor the CVS procedure provides a true

representation of actual vehicle operation Further tracer studies to assess the

transport and dilution of mobile and stationary source emissions from selected

source areas are also needed

253

1111

IUD

a CC I w gt-

1111

1UO

IUD

I 990

IDJO

1180

1111

IUO

FIGURE I

HYDROCARBONS

STATIONARY SOURCES MOTOR VEHICLES

- --

8 12 II 20 742 2l IS 12 I 4

HUNDREDS

HYDROCARBON EMISSIONS STATIONARY SOURCES IN

OXIDES OF

0

OF TONSDAY

FROM MOTOO VEHICLES AND LOS ANGELES COUNTY

NITROGEN

STATIONARY SOURCES

MOTOR VEHICLES

011111111111111111110111bull1111111

IIIIIIHIIIIIIIIIHIUII

llillL Its rd

l1uu~111111u1111111

2 I O 1 J 3

HUND REDS OF TONSDAY

OXIDES OF NITROGEN EMISSIONS FROM MOTOR VEHICLES ANO STATIONARY SOURCES IN LOS ANGELES COUNTY

illl~ -~--~ i~-=i _J~l ~--~ bull_~L- I ~~~-~~--Z ~

6

6S-66 ox

ICS ~A~1 M

i ssmuwmmgt

bullI

e COROyent_

64 ~ IDB RIVERS~

ORAJfD

-

t t 10 miles

bullmiddotsame Avg Cone Both Years

Pigare 2

YEAR OP HIGHEST OXlDANI CONCENTRATIONS

Highest Average of Daily -Maiimum One-Hour Concentrations

During July August amp September 1963-1972

bullLj

I

64

70 s11 3RlU)U0

70

--__ 69bull

N V +=

middot Source Air Resources Board

-200o

t t 10 adlea

tDS ampIJtsect

-1~

-1611ASampXllmiddot bull - bull -z----~------

I ldmmprwJ

IIVERSIDI

~ - 70

OampY -1 U 70 bull L

I

N V1 V

middot-i___

-----------------------------------------------------------i----------------------------

Figure 3

CHANGE OP OXIDANT CONCENTRATIONS

Percent Change from the Highest Three-Year Average to the 1970-72 Average

Of Daily Maximum One-Hour Con~entrationa for JulY August amp September

Source Air Resources Board

256

FIGURE 4 TYPICAL FLOW OF POLLUTED Am PARCEIS CIUGINATING AT DIFFERENT LOCATIONS IN THE LOS ARE~S BASIN - STARTIOO 0900 PST

l I

OAT

TRAJECTORY SUWMATIOl4

----- SMOG ~AVS

I

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullNONbullSlfOG DAYS

ISTARTING Tl~ cgxpsy

~ HAW

(CA

257

FiGURE 5 ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AND OXIDANT IN DOWlflC1N LOS AIDELES (SOURCE AREA) AND PASADENA (EFFECT AREA) 1

1960-1972

LO CARBON MONOXIDE

30

Pasadena

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullbullbullbullbull Downtown Los Angeles

20

10

o_______________________________

OXIDANT

)

2 Down~ Los Angeles

1

o________________________ 1960 1962 196L 1966 1968 1970 1972

YEAR

bullbullbullbullbull

bullbullbullbullbullbullbull

258

FIGURE 6 COMPARISON 01 CALCULATED AND MEASURED ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AN1) OXIDES OF NITROOEN IN DCMNTOWN IDS AIJELES

196o-1972

CARBON MONOXIDE

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ~ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot _-- ---_ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ----middotmiddot-bullw-_~ ---bullbullbull

10

o_______________1111111_____

OXIDES OF NITROGEN25

20

15 bullbullbullbullbullmiddotmiddotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~

1-i 10 middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ---

oS o_______________________

RATIO CONOx

40

50

0 +raquo Cd

p 30

~ 20

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot bullbullbullbullbull middotmiddotmiddotmiddotmiddot-shybullbullbullbullbull 0 u

bullbullbullbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot 10

0 j

ilI 196o 1964 1968 1970 1972 I

YEAR

Measured~D-owntown Los Angeles (90th percentile ofmiddot daily] instantaneous maxima)

Calculated - Aver~ge vehicle emissions - Present control program

259

FIGURE 7

25

t i5

flJ

~ on ~ ~ Q) bO 100 Jo

+gt on z

o5

EFFECT OF CALIFORNIA 1 s AUTO EXHAUST CONTROL ffiOORA M ON MAXIMUM CHAMBER OZONE CONCENTRATION

- PPM

357bullbull

r 76 bull

11 l

30

20

CHAMBER OZONE MAXIMUM

50

10

o___________111111111111______111111111111_____________

0 05 10 15 20 25

Hydrocarbons m-2 (LB-15) - PPM (as Hexane)middot

--

bull bull bull

r--=--~1 ~a==-~ - _~l ~ y--===-- ~~--~-- ~ r---~~

o

o8

~ I

~ 0 H 8 o6 I

c~ ~ 0 z 0 0

8

~ o+ A H gtlto-

02

middoto

Figure 8 Calculated t1ax1mum Levels Instantaneous and Hourly Average

of Atmospheric Oxidant Compared to Measured Los Angeles County Maxima-with Projections to 1990

(California Standards)

~ -Calculated Inst ax ~

f Calculate Max Hr Avg 03

_ bullbull _ _ - i bull

0 bullbull -l bullbull a0Ieasured Inst Lax o3 bull middotmiddotmiddot~bull 0bull _ ____ V ~ ea~ured ~ Hr Avr o3

~~ r---

~ ~ NB r~ima for 197 4 amiddots of 121074--- -_ Chamber Ozone F ~_ _~

- 1L_

~ Federal Primarfo Air ~uality Standard ~6- -UaximumT- our Avera~elr~ppm-------------- --~ ------- -~- -~-- ~

I I I I I I I I I I I I I I I I I N1 O

1960 6i 64 66 ~i middot-o 72 74 76 79 middotso middot92 84 bullg s9 9o

TBAR (end)

0

261 FIGURE -OMPARISON OF ATMOSPHERIC OXIDANT TRENDS WITH AVERAGE NCJx AND

HC EMISSIONS (Grams per Mile from Average Vehicle)

JOO Number of days state oxidant standara wds equalled or exceeded

--- Azusa __ Pasadena ________ Downtown Los Angeles

20

15 u

___ Hydroc_arbons Oxides of Nitrogenbullmiddotmiddotmiddotmiddotmiddotbullbullmiddot 1975 and later-assume middotcalifornia ARB standards

o_ ___________________________11111____

1965 1970 1975middot 198omiddot 198S 1990

144

The EPA is pursuing this The California Air Resources Board does have some

consideration going on for this but it appears that the level of activity

in resolving this problem is simply not adequate If we are to go ahead

to 04 of a gram per mile exhaust emissions standards for hydrocarbons

then it just doesnt make sense to let 19 grams per mile equivalent escape

through evaporative sources

Problem Area Number Three What about the secondary effects of the

catalyst control systems Specifically this is the sulfate emissions

problem and I really do not know the answer to that Our appraisal is

that it is not going to be an immediate problem so we can find out what

the problem is in time to solve it The way to solve it now since the

automobile industry is committed to catalysts and it is unreasonable

to expect that they will reverse that technology in any short period of

time is take the sulfur out of the gasoline The cost of removing sulfur

from gasoline is apparently less than one cent per gallon Therefore if

it becomes necessary to be concerned with sulfate emissions the way to

meet the problem is to take the sulfur out of gasoline Obviously sulfate

emissions need to be monitored very carefully to see what happens The

final appraisal is certainly not now available Another secondary effect

of the catalysts is the introduction of significant quantities of platinum

into an environment where it hasnt existed before Not only through

exhaust emissions which appear to be small but also through the disposal

problem of the catalytic reactors Since the quantity of platinum involved

is quite small the argument is sometimes used that platinum does not

represent much of a problem The fact that the amount of platinum in the

catalyst is so small may also mean that its not economical to recover it

This is probably unfortunate because then the disposal of these catalysts

l Jj

145

I becomes important I will not speak to the medical issues because

am not qualified The evidence is that theuro~ platinum will be emitted in a

form which does not enter into biological cycles--but this is no assurance

that it couldnt later be transformed in such a form What is obviously

needed is a very careful monitoring program which hopefully was started

before the catalysts were put into service If it wasnt then it should

be started today

Problem Area Number Four NO control The big problem with NO X X

control is that nobody seems to know or to be willing to establish what

the emission control level should be It is essential that this be tied

down rapidly and that it be fixed for a reiatively long period of time

because the NO level is going to have a VE~ry important ef feet upon the X

development of advanced engine technology The 20 gm level has been

attained in California with some loss of fuel economy through the use of

EGR and it is not unreasonable in our estimation to go to 15 grams per

mile with very little loss in fuel economy To go to 04 gram per mile

with present technology requires the use of one of two catalytic systems

either the reduction catalyst in tandem with the oxidation catalyst or what

is known as the three-way catalyst Both of these systems require technoshy

logical gains The state of development appears to be roughly that of the

oxidation catalyst two years ago The auto industry will probably say

that it is not quite that advanced but that if it were required to go to

04 gram per mile in 1978 that it could be done With the catalyst systems

the fuel economy penalties would not be great in fact the improvement to

the engine which would be required to make the system work would again

probably even allow a slight improvement in fuel economy What the 04

gram per mile NO catalyst system would appear to do however is to X

146

eliminate the possibility of the introduction of stratified charge engines

both the CVCC and the direction injection system and also diesel engines

It is in the context of the advantages of these advanced engines to meet

emission standards with improved fuel economy that one should be very

cautious about the 04 grammile oxides of nitrogen standards for automoshy

biles My own personal opinion is that the number should not be that

stringent that a number of 1 or 15 gm is appropriate Such a level

would require advancements but would not incur great penalties

Other items which I view as problem areas are less technically

involved and therefore require fewer comments

bull Nonregulated pollutants--again thls is a matter of keeping track

of particulates aldehydes hydrocarbon composition to make

certain that important pollutants ire not being overlooked or

that emission control systems are not increasing the output of

some of these pollutants

bull Fuel economy The pressures of fuel economy are going to be used

as arguments against going ahead wlth emissions control Mostly

these two can be resolved simultaneously We should simply ask

the automobile industry to work harder at this

bull Final problem area New fuels Again it does not appear that

the introduction of new fuels will come about as an emissions

control approach but that they may be introduced because of the

changing fuel availability patterns and the energy crisis These

fuels should be watched carefully for their impact upon emissions

This does middotappear to be an area in which a great deal of study is

going on at the present time It is one problem area perhaps in

which the amount of wprk being done is adequate to the problem

which is involved

147

In sunnnary then the appraisal of the 1975 systems is that they are

a big advancement they will be a lot better than most of us thought and

that we should give the automobile industry credit for the job theyve

done in coming up with their emissions control systems

With that boost for the auto industry which Im very unaccustomed

to Ill entertain your questions

-------=-~ ~~~ U- ~a1

~_~a--~-~ -J~ ~ -~r- _ --=~-- -___ja--~ __1~~ ~-~----=

AIR

1-4 FUEL----1

I I ENGINE

I II

_________ EXHAUST SYSTEM I bull EXHAUST

I I I

+ MIXTURE CONTROL COMBUSTION MODIFICATION EXHAUST TREATMENT

FuelAir Metering Ignition Air Jnjection FuelAir Mixing Chamber Geometry Thermal Reactor Fuel Vaporization Spark Timing Oxidation Catalyst Mixture Distribution Staged Combustion Reduction Catalyst Fuel Characteristics Ex tern almiddot Combustion Three Way Catalyst Exhaust Gas Redrculation Particulate Trap

FIGURE 1 Approaches to the Control of Engine Emissions

~ i 00

149

TABLE I

Average Emissions of 1975 Certification Vehicles (As Corrected Using the 50000-Mile Deterioration Factor)

Emissions in gmi Fraction of Standard HC CO NO HC CO NO

Federal 1975 X X

AMC 065 67 25 043 045 080

Chrysler 074 77 25 049 051 082

Ford 081 92 24 054 061 078

GM 083 80 23 055 053 074

Weighted Average 080 82 24 053 055 076

California 1975

AMC 042 49 17 047 054 087

Chrysler 048 61 16 053 067 082

Ford 052 56 13 058 062 067

GM 065 55 16 0 72 061 082

Weighted Average 058 56 16 064 062 078

kWeighted average assumes the following market shares AMC 3 Chrysler 16 Ford 27 and GM 54

150

TABLE II

Total Number of Vehicles Certified for California 1975 Standard and the Number (and percentage) of These Able to Meet

Certain More Stringent Standards

Calif 1975 Federal 1977 Hypothesized Hypothes ized 099020 04J420 049020 093420

i ~

Manufacturer no () no () no () no ()

AMC 16 (100) 1 ( 6) ti ( 38) 3 (19)

Chrysler 21 (100) 2 ( 9) ( 33) 0 ( O)

Ford 26 (100) 4 (15) -middot ( 15) 5 (19)

l GM 46 (100) 1 ( 2) -1 ( 9) 5 (11)

Foreign 62 (100) 21 (34) 3H (61) 28 (45)

1J

f

-l

151

CURRENT STATUS OF ALTERNATIVE AUTOM)BIIE ENGINE TECHNOLCXY

by

Henry K Newhall Project Leader Fuels Division

Chevron Research CanpanyRicbmmd California

I

iH1middot

10 1ntroduction and General Background

I

11 General

The term stratified ct1arge englne has been used for many

years in connection with a variety of unconventional engine

combustion systems Common to nearly all such systems is

the combustion of fuel-air mixtures havlng a significant

gradation or stratification in fuel- concentration within the

engine combustion chamber Henee the term nstratifled charge

Historically the objective of stratified charge engine designs

has been to permit spark ignition engine operation with average

or overall fuel-air ratios lean beyond the ignition limits of

conventional combustion systems The advantages of this type

of operation will be enumerated shortly Attempts at achieving

this objective date back to the first or second decade of this

century 1

More recently the stratified charge engine has been recognized

as a potential means for control of vehicle pollutant emissions

with minimum loss of fuel economy As a consequence the

various stratified charge concepts have been the focus of

renewed interest

152

12 Advantages and Disadvantages of Lean Mixture Operation

Fuel-lean combustion as achieved in a number of the stratified

charge engine designs receiving current attention has both

advantages and disadvantages wnen considered from the comshy

bined standpoints of emissionsmiddot control vehicle performance

and fuel economy

Advantages of lean mixture operation include the following

Excess oxygen contained in lean mixture combustion

gases helps to promote complete oxidation of hydroshy

carbons (HG) and carbon monoxide (CO) both in the

engine cylinder and in the exhaust system

Lean mixture combustion results in reduced peak

engine cycle temperatures and can therefore yield

lowered nitrogen oxide (NOx) emissions

Thermodynamic properties of lean mixture combustion

products are favorable from the standpoint of engine

cycle thermal efficiency (reduced extent cf dissociashy

tion and higher effective specific heats ratio)

Lean mixture operation caG reduce or eliminate the

need for air throttling as a means of engine load

control The consequent reduction in pumping losses

can result in significantly improved part load fuel

economy

153

Disadvantages of lean mixture operation include the following

Relatively low combustion gas temperatures during

the engine cycle expansion and exhaust processes

are inherent i~ lean mixture operation As a conseshy

quence hydrocarbon oxidation reactions are retarded

and unburned hydrocarbon exhaust emissions can be

excessive

Engine modifications aimed at raising exhaust temperashy

i tures for improved HC emissions control (retarded middot~

ignition timing lowered compression ratlo protrtacted combustion) necessarily impair engine fuel economy1 I

1j bull If lean mixture operation is to be maintained over ~

the entire engine load range maximum power output t l and hence vehicle performance are significantly

impaired

Lean mixture exhaust gases are not amenable to treatshy

ment by existing reducing catalysts for NOx emissions

control

Lean mixture combustion if not carefully controlled

can result in formation of undesirable odorant

materials that appear ln significant concentrations

in the engine exhaust Diesel exhaust odor is typical

of this problem and is thought to derive from lean mixshy

ture regions of the combustion chamber

154

Measures required for control of NOx emissions

to low levels (as example EGR) can accentuate

the above HC and odorant emissions problems

Successful developmentmiddotor the several stratified charge

engine designs now receiving serious attention will depend

very much on the balance that can be achieved among the

foregoing favorable and unfavorable features of lean comshy

bustion This balance will of course depend ultimately on

the standards or goals that are set for emissions control

fuel economy vehicle performance and cost Of particular

importance are the relationships between three factors -

UBHC emissions NOx emissions and fuel economy

13 Stratified Charge Engine Concepts

Charge stratification permitting lean mixture operation has

been achieved in a number of ways using differing concepts

and design configurations

Irrespective of the means used for achieving charge stratifishy

cation two distinct types of combustion process can be idenshy

tified One approach involves ignition of a small and

localized quantity of flammable mixture which in turn serves

to ignite a much larger quantity of adjoining or sur~rounding

fuel-lean mixture - too lean for ignition under normal cirshy

cumstances Requisite m1xture stratification has been achieved

155

in several different ways rangiDg from use of fuel injection

djrectly into open combustion chambers to use of dual

combustion chambers divided physically into rich and lean

mixture regions Under most operating conditions the

overall or average fuel-air ratio is fuel-lean and the

advantages enumerated above for lean operation can be realized

A second approach involves timed staging of the combustion

process An initial rich mj_xture stage in which major comshy

bustion reactions are completed is followed by rapid mixing

of rich mixture combustion products with an excess of air

Mixing and the resultant temperature reduction can in

principle occur so rapidly that minimum opportunity for NO

formation exists and as a consequence NOx emissions are

low Sufficient excess air is made available to encourage

complete oxidation of hydrocarbons and CO in the engine

cylinder and exhaust system The staged combustion concept

has been specifically exploited 1n so-called divided-chamber

or large volume prechamber engine designs But lt will be

seen that staging is also inherent to some degree in other

types of stratified charge engines

The foregoing would indicate that stratified charge engines

can be categorized either as lean burn engines or staged

combustion engines In reality the division between conshy

cepts is not so clear cut Many engines encompass features

of both concepts

156

14 Scope of This Report

During the past several years a large number of engine designs

falling into the broad category of stratified charge engines

have been proposed Many of these have been evaluated by comshy

petent organizations and have been found lacking in one or a

number of important areas A much smaller number of stratified

charge engine designs have shown promise for improved emissions

control and fuel economy with acceptable performance durashy

bility and production feasibility These are currently

receiving intensive research andor development efforts by

major organizations - both domestic and foreign

The purpose of this report is not to enumerate and describe the

many variations of stratified charge engine design that have

been proposed in recent years Rather it is intended to focus

on those engines that are receiving serious development efforts

and for which a reasonably Jarge and sound body of experimental

data has evolved It is hoped that this approach will lead to

a reliable appraisal of the potential for stratified charge

engine systems

20 Open-Chamber Stratified Charge Engines

21 General

From the standpoint of mechanical design stratified charge

engines can be conveniently divided into two types open-chamber

and dual-chamber The open-chamber stratjfied charge engine

has a long history of research lnterest Those crigines

157

reaching the most advanced stages of development are probably

the Ford-programmed c~mbustion process (PROC0) 2 3 and Texacos

controlled combustion process (TCCS) 4 5 Both engines employ a

combination of inlet aar swirl and direct timed combustion

chamber fuel injection to achieve a local fuel-rich ignitable

mixture near the point of ignition _For both engines the overshy

all mixture ratio under most operating conditions is fuel lean

Aside from these general design features that are common to

the two engiries details of their respective engine_cycle proshy

cesses are quite different and these differences reflect

strongly in comparisons of engine performance and emissions

characteristics

22 The Ford PROCO Engin~

221 Description

The Ford PROCO engine is an outgrowth of a stratified charge

development program initiated by Ford in the late 1950s The

development objective at that time was an engine having dieselshy

like fuel economy but with performance noise levels and

driveability comparable to those of conventional engines In

the 1960s objectives were broadened to include exhaust

emissions control

A recent developmental version of the PROCO engine is shown in

Figure 2-1 Fuel is injected directly into the combustion chamber

during the compression stroke resulting in vaporjzation and

formation of a rich mixture cloud or kernel in the immediate

158

vicinity of the spark plug(s) A flame initiated in this rich

mixture region propagates outwardly to the increasingly fuelshy

lean regions of the chamber At the same time high air swirl

velocities resulting from special orientation of the air inlet

system help to promote rapid mixing of fuel-rich combustion

products with excess air contained in the lean region Air

swirl is augmented by the squ1sh action of the piston as it

approaches the combustion chamber roof at the end of the comshy

pression stroke The effect of rapid mixing can be viewed as

promoting a second stage of cori1bustion in which rlch mixture

zone products mix with air contained in lean regions Charge

stratification permits operation with very lean fuel-air mixshy

tures with attendent fuel economy and emissj_ons advantages In

addition charge stratification and direct fuel injection pershy

mit use of high compression ratios with gasolines of moderate

octane quality - again giving a substantial fuel economy

advantage

Present engine operation includes enrichment under maximum

power demand conditions to mixture ratios richer than

stoichiometric Performance therefore closely matches

that of conventionally powered vehicles

Nearly all PROCO development plans at the present time include

use of oxidizing catalysts for HC emissions control For a

given HC emissions standard oxidizing catalyts permit use

of leaner air-fuel ratios (lower exhaust temperatures)

1

l

159

together with fuel injection and ignition timing charactershy

istics optimized for improved fuel economy

222 Emissions and Fuel Economy

Figure 2-2 is a plot of PROCO vehicle fuel economy versus NOx

emissions based or1 the Federal CVS-CH test procedure Also

included are corresponding HC and CO emissions levels Only

the most recent test data have been plotted since these are

most representative of current program directions and also

reflect most accurately current emphasis on improved vehicle

fuel economy 6 7 For comparison purposes average fuel

economies for 1974 production vehicles weighing 4500 pounds

and 5000 pounds have been plotted~ (The CVS-C values

reported in Reference 8 have been adjusted by 5 to obtain

estimated CVS-CH values)

Data points to the left on Figure 2-2 at the o4 gmile

NOx level represent efforts to achieve statutory 1977

emissions levels 6 While the NOx target of o4 gmile was

met the requisite use of exhaust gas recirculation (EGR)

resulted in HC emissions above the statutory level

A redefined NOx target of 2 gn1ile has resulted in the recent

data points appearing in the upper right hand region of

Figure 2-2 7 The HC and CO emissions values listed are

without exhaust oxidation catalysts Assuming catalyst middotl

conversion efficiencies of 50-60 at the end of 50000 miles

of operation HC and CO levels will approach but not meet

160

statutory levels It is clear that excellent fuel economies

have been obtained at the indlcated levels of emissions

control - some 40 to 45 improved re1at1ve to 1974 produc-

tj_on vehicle averages for the same weight class

The cross-hatched horizontal band appearing across the upper

part of Figure 2-2 represents the reductions in NOx emissions

achieveble with use of EGR if HC emissions are unrestricted

The statutory 04 gmile level can apparently be achieved

with this engine with little or no loss of fuel economy but

with significant increases in HC emissions The HC increase

is ascribed to the quenching effect of EGR in lean-middotmixture

regions of the combustion chamber

223 Fuel Requirements

Current PROCO engines operated v1ith 11 1 compression ratio

yield a significant fuel economy advantage over conventional

production engines at current compression ratios According

to Ford engineers the PROCO engine at this compression

ratio j_s satisfied by typical fu1J-boi1ing commercial gasoshy

lines of 91 RON rating Conventional engines are limited to

compression ratios of about 81 and possibly less for

operation on similar fuels

Results of preliminary experiments indicate that the PROCO

engine may be less sensitive to fuel volatility than convenshy

tional engines - m1 important ff1ctor in flextb1 llty from the

standpoint of the fuel supplier

161

224 Present Status

Present development objectives are two-fold

Develop calibrations for alternate emissions target

levels carefully defining the fueleconofuy pbtenshy

tial associated with each level of emissions control

Convert engine and auxiliary systems to designs

feasible for high volume production

23 The Texaco TCCS Stratified Charge Engine

231 General Description

Like the Ford PROCO engine Texacos TCCS system involves_

coordinated air swirl and direct combustion chamber fuel

injection to achieve charge stratification Inlet portshy

induced cylinder air swirl rates typically approach ten times

the rotational engine speed A sectional view of the TCCS

combustion chamber is shown in Figure 2-3

Unlike the PROCO engine fuel injection in the TCCS engine

begins very late in the compression stroke - just before th~

desired time of ignition As shown in Figure 2-4 the first

portion of fuel injected is immediately swept by the swirling

air into the spark plug region where ignition occurs and a

flame front is established The continuing stream of injected

fuel mixes with swirling air and is swept into the flame

region In many respects the Texaco process resembles the

162

spray burning typical of dj_esel combustion ~r1th the difshy

ference that ignition is achieved by energy from an elec-

tric spark rather than by high compression temperatures

The Texaco engine like the diesel engine does not have a

significant fuel octane requirement Further use of positive

spark ignition obviates fuel I

cetane requirements character-

istic of diesel engines The resultant flexibility of the

TCCS engine regarding fuel requirements is a si~1ificant

attribute

In contrast to the TCCS system Fords PROCO system employs

relatively early injection vaporization and mixing of fuel

with air The combustion process more closely resembles the

premixed flame propagation typical of conventional gasoline

engines The PROCO engine therefore has a definite fuel

octane requirement and cannot be considered a multifuel

system

The TCCS engine operates with hi__gh compression ratios and

with little or no inlet air throttling except at idle conshy

ditions As a consequence fuel economy is excellent--both

at full load and under part load operating conditions

232 Exhaust Emissions and Fuel Economv

Low exhaust temperatures characteristlc of the TCCS system

have necessitated use of exhaust oxidation catalysts for

control of HC emissions to low lf~Vels A11 recent development

163

programs have therefore included use of exhaust oxidation

catalysts and most of the data reported here r~present tests

with catalysts installed or with engines tuned for use with

catalysts

Figures 2-5 and 2-6 present fuel economy data at several

exhaust emissions levels for two vehicles--a US Army M-151

vehicle with naturally aspirated 4-cylinder TCCS conversion

and a Plymouth Cricket with turbocharged 4-cylinder TCCS

engine 9 10 1urbocharging has been used to advantage to

increase maximum power output Also plotted in these figures

I are average fuel economies for 1974 production vehicles of

similar weight 8

I When optimized for maximum fuel economy the rrccs vehicles

can meet NOx levels of about 2 gmile It should be noted

that these are relatively lightueight vehicles and that

increasing vehicle weight to the 4000-5000 pound level could

result in significantly increased NOx emissions Figur~s 2-5

and 2-6 both show that engine modifications for reduced NOx

levels including retarded combustion timing EGR and increased

exhaust back pressure result in substantial fuel economy

penalties

For the naturally aspirated engine reducing NOx emissions

from the 2 gmile level to O l~ gmile incurred a fuel

economy penalty of 20 Reducing NOx from the tllrbocharged

164

engine from 15 gmile to 04 gmile gave a 25 fuel economy

penalty Fuel economies for both engines appear to decrease

uniformly as NOx emissions are lowered

For the current TCCS systems most of the fuel economy penalty

associated with emissions control can be ascribed to control

of NOx emissions although several of the measures used for

NOx control (retarded cornbusticn timing and increased exhaust

back pressure) also help to reduce HG emissions HC and CO

emissions ari effectively controlled with oxidation catalysts

resulting in relatively minor reductions in engine efficiency

233 TCCS Fuel Reauirements

The TCCS engine is unique among current stratified charge

systems in its multifuel capability Successful operation

with a nuraber of fuels ranging from gasoline to No 2 diesel

Table 2-I

Emissions and Fuel Economy of Turbocharged TCCS Engine-Powered Vehicle 1

Fuel

Emissions gMile 2 Fuel Economy

mng 2HC co NOx

Gasoline

JP-4

100-600

No 2 Diesel

033

026

014

027

104

109

072

J bull l ~

-

061

050

059

060

197

202

213

230

1M-151 vehicle 8 degrees coffibustion retard 16 light load EGR tw0 catalysts (Ref 10)

2 CVS-CH 2750 pounds tnert1a welght

165

l

has been demonstrated Table ~-I lists emissions levels and

fuel economies obtained with a turbocharged TCCS-powered

M-151 vehicle when operated on each of four different fuels 10

These fuels encompass wide ranges in gravity volatjlity

octane number and cetane leve 1 as middotshown in Table 2-II

Table 2-II

Fuel Specifications for TCCS Emissions Tests (Reference 10)

Gravity 0 API Sulfur

OFDistillation~

Gasolj_ne 100-600 JP-4 No 2

Diesel

88 -

86 124 233 342 388

0024 912

-

486 012

110 170 358 544 615

0002 57 356

541 0020

136 230 314 459 505

-middot --

369 0065

390 435 508 562 594

--

lta 9

IBP 10 50 90 EP

TEL gGal Research Octane Cetane No

Generally the emissions levels were little affected by the

wide variations in fuel properties Vehicle fuel economy

varied in proportion to fuel energy content

As stated above the TCCS engine is unique in its multifuel

capability The results of Tables 2-I and 2-II demonshy

strate that the engine has neither 8ign1ficant fuel octane

nor cetane requirements and further that it can tolerate

166

wide variations j_n fuel volati1tty rhe flexibility offered

by this type of system could be of major importance in

future years

234 Durability Performance Production Readiness

Emissions control system durability has been demonstrated by

mileage accumulation tests Ignltion system service is more

severe than for conventional engines due to heterogeneity of

the fuel-air mixture and also to the high compression ratios

involved The ignition system has been the subject of

intensive development and significant progress in system

reliability has been made

A preproduction prototype engine employing the TCCS process is

now being developed by the Hercules Division of White Motors

Corporation under contract to the US Army Tank Automotive

Command Southwest Research Inr)titute will conduct reliability

tests on the White-developed enGines when installed in Military

vehlcles

30 Small Volume Prechambcr Eng1nes (3-Valve Prechamber Engines Jet Ignition Engines Torch Ignition Engines)

31 General

A number of designs achieve charge stratification through

division of the combustion region into two adjacent chambers

The emissions reduction potentiampl for two types of dualshy

chamber engines has been demonstrated F1 rst ~ j n B desJgn

trad1t1on~JJy caJJld the nrreebrnber engine a 2m211 auxil1ary

167

or ignition chamber equipped w1th a spark plug communicates

with the much larger main combustion chamber located in the

space above the piston (Figure 3-1) The prechamber which

typically contains 5-15 of the total combustion volume

is supplied with a small quantity of fuel-rich ignitable

fuel-air mixture while a large quantity of very lean and

normally unignitable mixture is applied to the main chamber

above the piston Expansion of high temperature flame

products from the prechamber leads to ignition and burning

of the lean maj_n chamber fuel-a_r charge Ignitionmiddot and

combustion in the lean main chamber region are promoted both

by the high temperatures of prechamber gases and bythe

mixing that accompanies the jet-like motion of prechamber

products into the main chamber

I jl

I i j

I

Operation with lean overall mixtures tends to limit peak comshy

bustion temperatures thus minimizing the formation of nitric

oxide Further lean mixture combustion products contain

sufficient oxygen for complete oxidation of HC and CO in the

engine cylinder and exhaust system

It should be reemphasized here that a iraditional problem

with lean mixture engines has been low exhaust temperatures

which tend to quench HC oxidation reactions leading to

excessive emissions

Control of HC emissions to low levels requires a retarded or

slowly developing combustion process The consequent extenshy

sion of heat release j nto 1ate porttt)ns of the engtne cycle

168

tends to raise exhaust gas temperatures thus promoting

complete oxidation of hydrocarbons and carbon monoxide

32 Historical Background and Current Status

321 Early Developm9nt Objectives and Engine Def igns

The prechamber stratified charge engine has existed in various

forms for many years Early work by Ricardo 1 indicated that

the engine could perform very efficiently within a limited

range of carefully controlled operating conditions Both

fuel-injected and carbureted prechambcr engines have been

built A fuel-injected design Lnittally conceived by

Brodersen 11 was the subject of extensive study at the

University of Rochester for nearly a decade 12 13 Unforshy

tunately the University of Rochester work was undertaken prior

to widespread recognition of the automobile emissions problem

and as a consequence emission characteristics of the

Brodersen engine were not determined Another prechamber

engine receiving attention in the early 1960s is that conshy

ceived by R M Heintz 14 bull The objectives of this design

were reduced HC emissions incr0ased fuel economy and more

flexible fuel requirements

Experiments with a prechamber engine design called the torch

ignition enginen were reported n the USSR by Nilov 15

and later by Kerimov and Mekhtier 16 This designation

refers to the torchlike jet of hot comhust1on gases issuing

169

from the precombustion chamber upon j_gnj_ tion In a recent

publication 17 Varshaoski et al have presented emissions

data obtained with a torch ignition engine These data show

significant pollutant reductions relative to conventional

engines however their interpretation in terms of requireshy

ments based on the Federal emissions test procedure is not

clear

l

3 2 2 Current DeveloJ)ments

A carbureted middotthree-valve prechamber engine the Honda CVCC

system has received considerable recent attention as a

potential low emissions power plant 18 This system is

illustrated in Figure 3-2 Hondas current design employs a

conventional engine block and piston assembly Only_ the

cylinder head and fuel inlet system differ from current

automotive practice Each cylinder is equipped with a small

precombustion chamber communicating by means of an orifice

with the main combustion chambe situated above the piston lj

ij_ A small inlet valve is located in each precharnber Larger

inlet and exhaust valves typical of conventlonal automotive

practice are located in the main combustion chamber Proper

proportioning of fuel-air mixture between prechamber and

main chamber is achieved by a combination of throttle conshy

trol and appropriate inlet valve timing A relatively slow

and uniform burning process gjvjng rise to elevated combusshy

tion temperatures late in the expansion stroke and during

the exhaust procezs is achieved H1 gh tewperaturr--s in thin

part of the engine cycle ar-e necessary to promote complete

170

oxidation of HC and CO It si1ould be no~ed that these

elevated exhaust temperatures are necessarily obtained at

the expense of a fuel economy penalty

To reduce HC and CO emissions to required levels it has been

necessary for Honda to employ specially designed inlet and

exhaust systems Supply of extremely rich fuel-air mixtures

to the precombustion chambers requires extensive inlet manifold

heating to provide adequate fuel vaporization This is accomshy

plished with a heat exchange system between inlet and exhaust

streams

To promote maximum oxidation of HC and CO in the lean mixture

CVCC engine exhaust gases it has been necessary to conserve

as much exhaust heat as possible and also to increase exhaust

manifold residence time This has been done by using a relashy

tively large exhaust manifold fitted with an internal heat

shield or liner to minimize heat losses In additj_on the

exhaust ports are equipped with thin metallic liners to

minimize loss of heat from exhaust gases to the cylinder

head casting

Engines similar in concept to the Honda CVCC system are under

development by other companies including Ttyota and Nissan

in Japan and General Motors and Fo~d in the United States

Honda presently markets a CVCC-powered vehicle tn tTapan and

plans US introduction in 1975 Othe~ manufactur~rs

includlnr General Motors and Forgtd 1n thr U S havf~ stated

171

that CVCC-type engines could be manufactured for use in limited

numbers of vehicles by as early as 1977 or 1978

33 Emissions and Fuel Economywith CVCC-Type Engines

331 Recent Emissions Test Results

Results of emissions tests with the Honda engine have been very

promising The emissions levels shown in Table 3-I are typical

and demonstate that the Honda engine can meet statutory 1975-1976

HC and CO stindards and can approach the statutory 1976 NOx

standard 19 Of particular importance durability of this

system appears excellent as evidenced by the high mileage

emissions levels reported in Table 3-I Any deterioration of

l emissions after 50000 miles of engine operation was slight

and apparently insignificant

I Table 3-I

Honda Compound Vortex-Controlled Combustion-Powered Vehicle 1 Emissions

Fuel Economy

Emissions 2 mpg gMile 1972

HC 1975 FTP FTPco NOv

210 50000-Mile Car+ No 2034 Low Mileage Car 3 No 3652 018 212 221089

024 065 198 1976 Standards

213175 20o41 34 - -04o411977 Standards 34 - -

1Honda Civic vehicles 2 1975 CVS C-H procedure with 2000-lb inertia weight3Average of five tests aAverage of four tests

172

Recently the EPA has tested a larger vehicle conve~ted to the

Honda system 20 This vehicle a 1973 Chevrolet Impala with

a 350-CID V-8 engine was equipped with cylinder heads and

induction system built by Honda The vehicle met the present

1976 interim Federal emissions standards though NOx levels

were substantially higher than for the much lighter weight

Honda Civic vehicles

Results of development tests conducted by General Motors are

shown in Table 3-II 21 These tests involved a 5000-pound

Chevrolet Impala with stratified charge engine conversion

HC and CO emissions were below 1977 statutory limits while

NOx emissions ranged from 15 to 2 gmile Average CVS-CH

fuel ec9nomy was 112 miles per gallon

Table 3-II

Emissions and Fuel Economy for Chevrolet Impala Strmiddotatified

Charge Engine Conversion (Ref 21)

Test

Exhaust Emlssions

gMile 1 Fuel

Economy mpgHC co NOx

1 2 3 4 5

Average

020 026 020 029 0 18

023

25 29 31 32 28

29

17 15 19 1 6 19

17

108 117 114 109 111

112

1cvs-CH 5000-lb inertia weight

173

I

332 HC Control Has a Significant Impact on Fuel Economy

In Figure 3-3 fuel economy data for several levels of hydroshy

carbon emissions from QVCC-type stratified charge engines

are plotted 22 23 ~ 24 At the 1 gmile HC level stratified

charge engine fuel economy appears better than the average

fuel economy for 1973-74 production vehicles of equivalent

weight Reduction of HC emissions below the 1-gram level

necessitates lowered compression ratios andor retarded

ignition timing with a consequent loss of efficiencymiddot For

the light-weight (2000-pound) vehicles the O~ gmile IIC

emissions standard can be met with a fuel economy of 25 mpg

a level approximately equal to the average of 1973 producshy

tion vehicles in this weight class 8 For heavier cars the

HC emissions versus fuel economy trade-off appears less

favorable A fuel economy penalty of 10 relative to 1974

production vehicles in the 2750-pound weight class is

required to meet the statutory 04 gmile HC level

333 Effect of NOx Emissions Control on Fuel Economy

Data showing the effect of NOx emissions control appear in

Figure 3-~ 22 These data are based on modifications of a Honda

CVCC-powered Civic vehicle (2000-pound test weight) to meet

increasingly stringent NOx standards ranging from 12 gmile

to as low as 03 gmile For all tests HC and CO emissions

are within the statutory 1977 standards

NOx control as shown in Figure 3-4 has been effected by use

of exhaust gas recirculation 1n comb1nation w1th retarded

174

ignj_tion timing It is clear that control of rmx emissions

to levels below l to 1 5 gmile results in stgnificant fuel

economy penalties The penalty increases uniformly as NOx

emissions are reduced ~nd appears to be 25 or more as the

04 gmile NOx level is approached

It should be emphasized that the data of Fisure 3-4 apply

specifically to a 2000-pound vehicle With increased vehicle

weight NOx emissions control becomes more difficult and the

fuel economy penalty more severe The effect of vehicle

weight on NOx emissions is apparent when comparing the data

of Table 3-I for 2000-pound vehicles with that of Table 3-II

for a 5000-pound vehicle While HC and CO emissio~s for the

two vehicles are roughly comparable there is over a factor

of two difference in average NOx emissions

34 Fuel Requirements

To meet present and future US emissions control standards

compression ratio and maximum ignltion advance are limited

by HC emissions control rather than by the octane quality of

existing gasolines CVCC engines tuned to meet 1975 California

emissions standards appear to be easily satisfied with

presently available 91 RON commercial unleaded gasolines

CVCC engines are lead tolerant and have completed emissions

certification test programs using leaded gasolines However

with the low octane requirement of the CVCC engine as noted

above the economic benefits of lead antlknock compoundt ar-euromiddot

not realized

175

It is possible that fuel volatLLity characteristlcs may be of

importance in relation to vaporization within the high

temperature fuel-rich regions of the prechamber cup inlet

port and prechamber iQlet manifold However experimental

data on this question aomiddot not appear to be available at

present

~O Divided-Chamber Staged Combustion Engines (Large-Volume Prechamber Engines Fuel-Injected Blind Prechamber Engines)

41 General

Dual-chamber engines of a type often called divided-chamber

or large-volume prechamber engines employ a two-stage comshy

bustion process Here initial r~ich mixture combustion and

heat release (first stage of combustion) are followed by rapid

dilution of combustion products with relatively low temperature

air (second stage of combustion) The object of this engine

design is to effect the transitjon from overall rich combustion

products to overall lean products with sufficient speed that

time is not available for formation of significant quantities

of NO During the second low temperature lean stage of

combustion oxidation of HC and CO goes to completion

An experimental divided-chamber engine design that has been

built and tested is represented schematically in Figure ~-1 25 26

A dividing orifice (3) separates the primary combustion

chamber (1) from the secondary combustion chamber (2) which

includes the cylinder volume above the piston top A fuel

injector (4) supplies fuel to the primary chamber only

176

Injection timing is arranged such that fuel continuously

mixes with air entering the primary chamber during the

compression stroke At the end of compression as the

piston nears its top center position the primary chamber

contains an ignitable fuel-air mixture while the secondary

chamber adjacent to the piston top contains only air

Following ignition of the primary chamber mixture by a spark

plug (6) located near the dividing orifice high temperature

rich mixture combustion products expand rapidly into and mix

with the relatively cool air contained in the secondary

chamber The resulting dilution of combustion products with

attendant temperature reduction rapidly suppresses formation

of NO At the same time the presence of excess air in the

secondary chamber tends to promote complete oxidation of HC

and CO

42 Exhaust Emissions and Fuel Economy

Results of limited research conducted both by university and

industrial laboratories indicat~ that NOx reductions of as

much as 80-95 relative to conventional engines are possible

with the divided-chamber staged combustion process Typical

experimentally determined NOx emissions levels are presented

in Figure 4-2 27 Here NOx emissions for two different

divided-chamber configurations 8re compared with typical

emissions levels for conventional uncontrolled automobile

engines The volume ratio 8 appearing as a parameter in

Figure 4-2 represents the fraction of total combustion volume

contained in the primary chamber For a values approaching

I

i J_

177

1

05 or lower NOx emissions reach extremely low levels Howshy

ever maximum power output capability for a given engine size

decreases with decreasing 6 values Optimum primary chamber

volume must ultimately_represent a compromise between low

emissions levels and desired maximum power output

HC and particularly CO emissions from the divided-chamber

engine are substantially lower than eonventional engine

levels However further detailed work with combustion

chamber geometries and fuel injection systems will be necesshy

sary to fully evaluate the potential for reduction of these

emissions

i Recent tests by Ford Motor Company show that the large volume

prechamber engine may be capable of better HC emissions conshy

trol and fuel economy than their PROCO engine This is shown

by the laboratory engine test comparison of Table 4-I 19

Table 4-I

Single-Cylinder Low Emissions middot11 ~ _____En____g__~ne __middot _e_s_-_s_____

Engine

NO--X Reduction

Method

Em1ssions g1 hp-Hr

Fuel Economy

Lb1 hp-HrNOv HC- co

PROCO

Divided Chamber

PROCO

Divided Chamber

EGR

None

EGR

None

10 30

10 04

05 ~o

o J_o 75

130

25

l 1i bull 0

33

0377

0378

0383

0377

178

Fuel injection spray characteristics are critical to control

of HC emissions from this type of engine and Fords success

in this regard is probably due in part to use of the already

highly developed PROCO-gasoline injection system Figure 4-3

is a cutaway view of Fords adaptation of a 400-CID V-8 engine

to the divided-chamber system 2 e

Volkswagen (VW) has recently published results of a program

aimed at development of a large volume precharnber engine 29

In the Volkswagen adaptation the primary chamber which comshy

prises about 30 of the total clearance volume is fueled by a

direct timed injection system and auxiliary fuel for high

power output conditions is supplied to the cylinder region by

a carburetor

Table 4-II presents emissions data for both air-cooled and

water-cooled versions of VW s dtvided-middotchamber engine 3 0

Emissions levels while quite low do not meet the ultimate

1978 statutory US standards

179

Table 4-II

Volkswagen Jarge Volume _Jrechamber Er[ Lne Emissions

Exhaust Emissions

_ _gMile 1

___E_n_gi_n_e__t--H_C___c_o__N_O_x____E_ng__i_n_e_S_p_e_c_i_f_i_c_a_tmiddot_1_middoto_n_s__

20 50 09 841 compression ratio Air-Cooled 16-Liter

prechamber volume 28 of total clearance volume conventional exhaust manishyfold direct prechamber fuel injection

20-Liter 10 40 10 91 compression ratio Water-Cooled prechamber volume 28 of

total clearance volume simple exhaust manifold reactor direct prechamber fuel injection

1cvs c-H

Toyota also has experimented wlth ___a large volume prechamber

engine using direct prechamber fuel injection and has

reported emissions levels comparable to those of Table 4-II 31

43 Problem Areas

A number of major problems inherent in the large volume

prechamber engine remain to be 3olved I~ These problems include the following II

Fuel injection spray characteristics are critically

important to achieving acceptable HC emissions

The feasibility of producing asatisfactory injecshy

tion system hasnot been estab1ished

180

Combustion noise due to high turbulence levels and

hence high rates of heat release and pres[-ure rise

in the prechamber can be excessive It has been

shown that the-noise level can be modified through

careful chamber design and combustion event timing

If the engine is operated with prechamber fuel

injection as the sole fuel source maximum engine

power output is limited This might be overcome

by a~xiliary carburetion of the air inlet for maximum

power demand or possibly by turbocharging Either

approach adds to system complexity

The engine is charmiddotaeter1zed by low exhaust temperatures

typical of most lean mixture engines

References

1 Ricardo H R Recent Research Work on the Internal Combustion Engine 11 SAE Journal Vol 10 p 305-336 (1922)

2 Bishop I N and Simko A Society of Automotive Engineers Paper 680041 (1968)

3 Simko A Choma M A and Repco L L Society of Automotive Engineers Paper 720052 (1972)

4 Mitchell E Cobb JM and Frost R A Society of Automotive Engineers Paper 680042 (1968)

5 Mitchell E Alperstein M and Cobb JM Society of Automotive Engineers Paper 720051 (1972)

6 1975-77 Emission Control Program Status Report submitted to EPA by Ford Motor Company November 26 1973

181

if

7 consultant Report on Emissions Control of Engine Systems National Academy of Sciences Committee on Motor Vehicle Emissions Washington DC September 1974

8 Austin T C and Hellman K H Society of Automotive Engineers Paper 730790 (1973)

9 See Ref 7

10 Alperstein M Schafer G H and Villforth F J Iiil SAE Paper 740563 (1974)

11 US Patent No 2615437 and No 2690741 Method of Operating Internal Combustion Engines Neil O Broderson Rochester New York

12 Conta L~ D and Pandeli American Society of Mechanical Engineers Paper 59-SA-25 (1959)

13 Canta L D and Pandeli American Society of Mechanical Engineers Paper 60-WA-314 (1960)

14 US Patent No 2884913 0 Internal Combustion Engine R Mi Heintz i

15 Nilov N A Automobilnaya Promyshlennost No 8 (1958)

l 16 Kerimov N A and Metehtiev R I Automobilnoya Promyshlennost No 1 p8-11 (1967)

17 Varshaoski I L Konev B F and Klatskin V B Automobilnaya Promyshlennost No 4 (1970)

18 An Evaluation of Three Honda Compound Vortex Controlled Combustion (CVCC) Powered Vehicles Report B-11 issued by Test and Evaluation Branch Environmental Protection Agency December 1972

19 Automotive Spark Ignition Engine Emission Control Systems to Meet Requirements of the 1970 Clean Air Amendments report of the Emissions Control Systems Panel to the Committee on Motor Vehicle Emissions National Academy of Sciences May 1973

20 An Evaluation of a 300-CID Compound Vortex Controlled Combustion (CVCC) Powered Chevrolet Impala Report 74-13 DWP issued by Test and Evaluation Branch Environmental Protection Agency October 1973

21 See Ref 7

22 See Ref 7

23 See Ref 7

24 See Ref 7

182

25 Newhall H K and El-Messiri I A Combustion and Flame 14 p 155-158 (1970)

26 Newhall H K and El-Messiri I A Society of Automotive Engineers Transaction Ford 78 Paper 700491 (1970)

27 El-Messiri I A and Newhall H K Proc Intersociety Energy Conversion Engineering Conference p 63 (1971)

28 See Ref 7

29 Decker G and Brandstetter W MTZ Motortechnische Zeitschrift Vol 34 No 10 p 317-322 (1973)

30 See Ref 7

31 See Ref 7

183

Fig 2-1 FORD PROCO ENGINE

l

Ford Proco Engine Fuel Economy and Emissions _ 15 _ f--1

00 +

I ~ x X gt( X _ x A 7- ~ X x~ ~c - l4catalyst Feed u NOx vs ruel Econ with 1 C0-71 CJ) 14 x x Ynn H( RP c tr ir-t irm vltgtZ G I HC - C0-127 _ A txcessve c

13 Approx W EG R

~ C~~r 351 CID 5000 Lb Inertia Weight

Q 21 A L 0 u w II _j

LJ =gt LL

10

35i CD 4500 Lb Inertia Weight

~ 1974 Production Average Fuel Economy

4 soo _b r-r-r-----z~lt_~~---7--_~--r--1r-7-r1--~-rz7-w~~

150 0 0 Lb PU221ufrac122-1 I

LO 20 30

NOx EMISSIONS-GMSMILE (CVS-CH) Revised216174

0

HKN 71074

Fig 2-2

l

~___-~ ~--=---~ ~=---__---~1 f-=-----1__middot-_~J ~-----------1 ~bull-=-=- (-~-~ LJii-ZJj ~ ~~-~ ~~ -__c~~ 1--~~ ~----~--1 ---------s___-c--1 ~~~-~~~bull r~~-~--middot1 ____c__ J~ p- ~

Texaco TCCS Engine

Shrouded Intake Valve

~ Intakemiddot r~ )p__-- Fuel Nozzle Fuel Nozzte Port ~ -- -yen -_~

X f -J J ( ~1 I --- ~ f middotmiddotj_Ja 1(~-~_ frff 1-Cylinderv~ v_ r--L~ I (~~)J ~- Intake 1 - ------L- middotmiddot - middotmiddot -1 H0 ad middot --- - -- 1 Po rt I 1 I ~~ ) ~ ~ ~~~ -A- I ------

- I _ ---_ ~ P1ston-mgt-lt_ffrac12 T_77~~~--1 i- r_-~J N

- ~- i~-L - _ _ - IExhaust - - I ~ - 1-_ r- bullsect ~ ----lt_ ~ I PortJ~bJ lt 7A--7~ ~1 ~j --~ ~ yl ind er

-__~lli- klmiddot ~ro v_t_gt11J1bull Bti Or K__ - middot ~

I t--tL pgt-- Ultmiddot middot- - Spark Plugr- -1 --U2middot- ~-~

LHorizont al Projections of Nozzle and Spark Plug Centerlines

Fig 2-3 i--1 00 U1

---~---~-~ -------c- --~--- 7middot-r---c-- ~- -~~~==---~~~~~- srsr RZIIEF7 11t111-~-----==-----=-~--~-~~---c=rmiddot=

OPEN CHAMBER TYPE STRATI Fl ED CHARGE ENGINE i-shyCj

DIRECTIONAl~Fsw7 Q

NOZZLE P

I

~J~treg lt-_(__(lt-(11

c_-- _7- -

SPARK PLUG_ l 1__- -_ - l --_ ~ ----__ lt_ lt_ -- --

ltlt_I_--- _

~ gt - _____- -- --~ ~-l_- 1_~ -~- ~ ------

~~~ r_I FUEL SPRAY 2 FUEL-AIR MIXING ZONE ~- _ -------

FLAME FRONT AREA 4 COMBUSTION PRODUCTS

TCCS COMBUSTION SYSTEM

Fig 2-4

3

----==-----~ l~~----bulli r-~ ~-----=-- 1 ~~ ~ -~ ~~ ___-_=gt---l p--- --=-=-_-__71-~-~~ 1-0-- --=---=-- 4 L--_-_-~ P--- ~

25

-c u

f

Cl) 24 gt u _

tgt 23a ~

I

gt-~ 220 2 0 u w 21 _J

lJJ gt LL

2

Texaco TCCS Powered Cricket Vehicle

Max Econ Setting gt A L07 HC

141 CID JQf CR 084 CO 2500 Lb Inertia Wgt

50-so Retard_ 0_73 HC

12 co 051 HC ~ 061 HC

085COA 064CO Retard+ ESPRetard+

EGR

036 HC ~ 115 co Retard +ESP+ EGR

04 06 08 10 12 14 16 18 20 NOx EMISSIONS-GMSMILE (CVS-CH) HtltN1110114

I- 00 -JFig 2-5

-~ ~=- ~ - -i______c_J ~-====c= wr=- ~-~ p--w~~~ rr w -

25

-c u

I

(f)

gt u-lt a_

2

gt-I 20

~ 0 z 0 u LLI

_J

w tJ_

15

I- CJ) CJ)

Turbocharged Texaco TCCS Ml51 Vehicle

Max Econ Adjustment_ HC-3J catalyst Feed C0-70

141 CID 10~1 CR 2750 Inertia Weight 8deg Retard ~

~bull HC-3middot2 catalyst Feed ~~ _ C0-64

_ 5deg Retard HC-0 30 8degRetard LowEGV bullco-11 ~bull HC-3middot6 catalyst Feed WIW21

Med EGR C0-67 1974 Production 33 Average Fuel Economy ~

COmiddoti05 (2750Lb)

I

bull HC-035 co- 141 13deg Retard High EGR

04 10 20 NOx EMISSIONS -GMSMILE (CVS-CH) ~~ts~b~~~74

Fig 2-6

189

Fig 3-1

PRECHAMBER TYPE STRATIFIED CHARGE ENGINE

r Inlet

(Fuel-lean Mixture )

I 0 I

Spark -Prechamber (Fuel-rich mixture)

-Main Chamber

1] HON DA CVCC ENGINE CONCEPT

190

Fig 3-2 Honda CVCC Engine

28 -l u

1

UJ 26 -gt u-(9 CL 24 2-

f

gtshy0gt

22 z ~ _)

u w

20 _J

w ~ LL

18

J= ---- 4 --~~-_----a ~~ _-_bull --~~ 1~~1 ltiil~I ~ ~-r~ ~ -~ ~-~ ~J~-iii-1 ~~1 s _-_ __-

Fuel Economy vs HC Emissions for 3-Valve Prechamber Engines

e NOx-14 15 Liter

bull Honda CVCC 2000 LbsNOx - 12 A Datsun NVCCbull15 Liter

bull ~JOx -09 A 2500 Lbs J LL 1ter NOv -15

2750 Lbs -NOx -17

- I AiJOx -12

0 02 04 06 08 LO 0HYDROCARBON EMiSSlmiddotONS - Glv1 I MILE (CVS-CH) I-

Fig 3-3

J--1

1--Fuel Economy vs NOx Emissions IO N

-- for Honda CVCC Powered Vehiclesr 26 u

l VHc-023 U1 gt umiddot 24_-__

(_IJ o_

~ 22 l

gt-5~-0 z 20 C0-200 u A HC-033w I co -3o_j

_A HC-029w 18 J I C0-27 LL

_ HC-025

HC-017 co -2-3

C0-22

0 -- 02 04 06middot 08 10 12 NOx Ef11SSIONS -GlviS MILE (CVS-CH)

Fig 3-4 middot

I

I

i93

J J

Fig 4-1 Divided Chamber Engine

middot(4) Fuel Injector

1

f J

f ff

f

~ Ii

I f

i

I f ] [

~~

0 0 0 0

i ~ I

1jl

194

E Cl 0

C QJ

CJl 0 _

-1-

z

0

Vl (lJ

-0

X 0

-t-J

V1 ro c X

LLI

Fig ~-2

COMPARISON OF CONVENTIONAL AND DIVIDED COMBUSTION CHAMBER NOx EMISSIONS

5000 MBT Ignition Timing Wide Open Ttl rattle

4000 Conventional Charnber

3000

J = fraction of Total Combustion 2000 Volume in Primary Ct1arnber

Divided Chamber 13 = 0 85

1000

Divided Chamber fo = 0 52

05 06 0 7 08 09 10 11

O~erall Fuel-Air Equivalence Ratio

195

196

AIRBORNE SURVEYS IN URBAN AIR BASINS IMPLICATIONS FOR MODEL DEVELOPMENT

by

Donald L Blumenthal Manager of Program Development

Meteorology Research Inc Altadena California 91001

middotI would like to make several points today First ozonemiddotis basically

a regional long-range problem There is a lot of long range ozone transshy

port and this transport is a normal occurrence The second point is that

ozone is stable in the absence of scavengers Junge mentions in his book

that the residence time of ozone in the troposphere is on the order of a

month Third vertical variations in concentration and ventilation rate are i very important in modeling atmospheres such as Los Angeles Layers aloft

are ventilated down to the surface on occasion and surface pollutants are

ventilated up mountain slopes as Jim Edinger has pointed out before and

often ventilated out of the basin in upper winds Fourth the day to day

carry over of pollutants from one day to the next is a very important considshy

eration in the Los Angeles Basin Finally there is a definite background

level of ozone The geophysical literature says its about O 02 to O 03 ppm (

in various parts of the world Weve seen data varying from 003 to 005 ppm

The difference may be due to calibration differences In any case numbers

like 005 are pretty substantial background levels for ozone

I am going to illustrate the points listed above with some data from

Los Angeles Basin The data were collected during a two-year study funded

by the Air Resources Board some of the analyses were funded by EPA The

study examined the three dimensional distribution of pollutants in the Los

Angeles Basin using airborne sampling systems Coinvestigators on the

project were Dr Ted Smith and Warren White of Meteorology Research Inc (MRI)

197

The first slide shows one of the aircraft we used Its a Cessna 205

which had sampling inlets on the side of the aircraft Figure 2 shows the

instrument system on the inside of the aircraft We were measuring nitrogen

oxides ozone scattering coefficient with a nephelometer condensation nuclei

carbon monoxide and meteorological parameters such as temperature humidity

turbulance Altitude and position were also measured

Figure 4 shows that the typical sampling pattern was a series of spirals

from the top of the mixing layer over an airport virtually to ground level

then we would climb up to the next point on the route and spiral down again

We had three routes (A B C Figure 3) that we would fly We had two airshy

craft and we would fly two of these three routes three times a day any

given day that we could The day I will be talking about September 25~ 1973

we flew what was called the Riverside route (C) and the Los Angeles route

(A) The 25th of July 1973 you might remember was the day before the

federal office buildings were closed in the area here because of smog

Figure 5 shows the surface streamlines at 0300 Pacific Standard Time

about 4 oclock in the morning daylight time on July 25 This streamline

analysis points out the morning stagnation conditions which are a very normal

occurrence in the Los Angeles Basin You start out with very light winds

quite variable maybe a slight off shore flow early in the morning On this

particular day this kind of situation extended well into midday The sea

breeze did not really pick up until up around noon When you have this kind

of a situation and a low radiation inversion at night you have a

long period of accumulation of pollutants all over the Basin espt~cialJy

in the prime source area the southwest portion of the Basin

198

I

Figure 6 shows the streamline pattern at 1600--400 cclock in the

afternoon same day sea breezes develop and with them a transport pattern

that carries pollutants up to the northeast and out toward the eastern por-

tion of the Basin This is a very regular pattern which we see day after l middot

day On July 25 1973 it was a little bit exaggerated The sea breeze was

held off for awhile started a bit late and so there was a very long period

of accumulation in the southwest area and then transport across the Basin

Figure 7 is an average streamline pattern at 1600 PacHic Daylight Time

on low inversion days for August 1970 It is included to show that the pattern

shown before is very typical Flow starts in the western portion of the

Basin and goes right across to the eastern portion This is using surface

data There is a very high average wind velocity in Ontario about 13 m iles

per hour and 23 mph in Riverside This is the average for the whole month

of August at 1600 PDT on low inversion days There is a considerable amount

of transport across the Basin starting relatively slowly in the morning and

accelerating in the afternoon

Figure 8 shows a verticle cross section of the scattering coefficient

The darker areas indicate higher levels of particulates Scattering coefficshy

ient is inversely proportional to visibility In the crosshatched area

visibility is less than about 3 miles In plotting altitude versus distance

inland from the coast you have Santa Monica (SMO) on the coast El Monte (EMT)

Pomona (BRA) Rialto (RIA) Redlands (RED) The lower broken line is surface

ground level The heavy dashed line is the base of the subsidence inversion

that occurred on the two days during this episode The middle line is the

base of the marine inversion There is a large area over in the western

portion of the Basin where emissions accumulate for much of the day At

199

midday the sea breeze has just started ventilating the Santa Monica area

The layer between the inversions is a layer aloft which is fairly well separshy

ated from the surface layer Ozone concentrations for instance in the

layer aloft were on the order of 04 05 ppm using the ARB calibration

method Down in the surface layer they were quite a bit lower in the mornshy

ing due to scavenging

Figure 9 shows that by afternoon the sea breeze starts and you get

kind of a clean air front Sea breeze starts ventilating the whole Basin

the stuff that was over in the west is transported eastward and at approxishy

mately Brackett (BRA) at 1700 PDT there is a clean air front The high conshy

centrations that were over Los Angeles earlier are now centered near Upland

(CAB) The numbers shown over CAB are data taken from a vertical profile

spiral over Upland at about 1600 That turns out to be the time when there

was the worst ozone concentration of the day in the Basin and it did occur

at Upland It could well be a result of the very polluted mass from the

western Basin being transported over the Upland area The layer aloft has

been a bit undercut by the sea breeze and some of the polluted mass has been

around possibly as long as the night before There has been very little

transport in the area aloft ozone concentrations are still very high

Figure 10 shows a trajectory analysis of the air arriving at Upland at

1600 since that was the worst time of the day at Upland We developed a

trajectory envelope using surface wind data and winds aloft so the air

arriving at Upland at 1600 started out somewhere back within this envelope

for example at 1130 PDT We did not go earlier than 1130 because the winds

were pretty much light and variable before that The air that arrives at

Upland at 1600 has been over the western portion of the Basin for much of

200

the morning and q~ite a bit of the evening before Thus there is

a very long period of accumulation and then a transport a pulsing effect

where you have pollutants moved across the Basin

Figure 11 is an isopleth map of surface ozone concentrations Again all

data are corrected to agree with the ARB calibration method Again you can

see that for the hours between 1600 and 1700 using surface data the Upland

area has the highest surface ozone concentrations about 063 ppm The western

area has been well ventilated by the sea breezes and it is cleaned out

The transport is actually pretty much perpendicular to the isopleth line

just about like that

Figure 12 is a vertical profile taken over Upland Cable Airportat

roughly the time of maximum ozone concentration 1636 PDT We are plotting

pollutant concentration on the x-axis versus altitude in meters (since it was

done for an EPA report) Surface leveJ at Upland is a little over 400 meters

the Z line is ozone Ozone concentration within the surface mixing layer

is pegged on the instrument at somewhat above 05 ppm Above the surface

mixing layer it drops off considerably and eventually get down to background

The T line is temperature and you ean see the subsidence inversion

on this day is very nicely documented here and provides a very strong trap

in that area The B line is the scattering coefficient inversely proporshy

tional to visibility Within the surface mixing layer visibility is on the

order of 3 miles or less while up above the surface mixing layer just a few

hundred feet difference visibilities get up to 60 or 80 miles The X is

condensation nuclei the measure of the very fine particles below about 010

micron It is a measure of quite fresh emissions If you have a high condenshy

sation nuclei count there are very fresh combustion emissions If you have

I

201

an aged air mass the condensation nuclei coagulate and the count decreases

considerably You can see that there are still some fresh emissions within

this surface layer as well But up above the surface mixing layer all the

pollutant indicators decrease considerably

Figure 13 is the same type of vertical profile taken over El Monte

which is on the western side of the sea breeze front The sea breeze front

has passed El Monte at this time almost 1700 PDT and again there are

distinct differences between the mass below the mixing layer within the sea

breeze front (below 400 meters) the marine inversion (400 to 800 meters) and

the subsidence inversion The subsidence inversion occurs at about 800 meters

and there is an old layer of very polluted stuff aloft The surface concenshy

trations are lower because of the ventilation by the sea breeze Condensashy

tion nuclei count (X line) within the surface layer is quite high There

are still fresh emissions in the El Monte area The 11 Z line is ozone

about 02 ppm within the surface layer (200 m) but it is 05 ppm up above

the surface mixing layer The scattering coefficient (B line) is very

similar it is lower at the surface and increases to a visibility equivalent

of less than 3 miles above the surface mixing layer The condensation nuclei

count is high in the lower portion of this (eg at 600 m) hut decreases conshy

siderably above This portion of the upper layer (600 m) has been around

at least all morning and condensation nuclei have been scattered from the

area The portion of the upper layer below 600 m has probably just recently

been undercut by the sea breeze and there are still some condensation nuclei

left in it

Figure 14 illustrates a different method of looking at the flushing

problems in the Basin We have tried to develop an objective criteria based

on ground level ozone to show the cleansing of the basin using the time of

202

arrival of clean air We determine the time when the ozone concentrations

drop by a factor of two at any given point The 1600 line means that between

1500 and 1700 the ozone concentration at that point dropped a factor of two

This sort of isopleth chart of when the clean air arrives agrees quite well

with the trajectory analyses although the numbers are a little bit behind

the trajectory analyses for the polluted air Figure 14 again shows the

transport process that takes place across the Basin which is ventilated from

west to east At 1900 some of the fresh ocean air finally gets out to

Redlands

In Figure 15 in order to put this whole flux problem into some perspecshy

tive we looked at the numbers the actual amount of ozone flux across the

basin We calculated the mean trajectory from Torrance towards Redlands

using the surface and upper air data We looked at the flux from the western

basin to the eastern basin basically from Los Angeles and Orange Counties to

Riverside and San Bernardino Counties This is a calculation made at 1700 PDT

We used the winds aloft from Chino as well as the vertical profiles taken at

Pomona and Corona Averaging the ozone concentration throughout the mixing

layer and multiplying by an average wind speed we arrive at a number of 185

metric tons per hour being transported directly from one side of the Basin

to the other If you look at this in terms of actual concentration in the

eastern Basin and assume that the flow was constant for about an hour it

is eno_ugh to fill up the box shown in Figure 15 to 025 ppm ozone which

exceeds the air quality standard by a factor of three (using the ARB calibrashy

tion method) Thus there is a very significant transport of ozone or ozone

precursors from one portion of the Basin to the other side of the Basin One

thing to mention though is that the concentration would not be kept up on a

203

steady state basis because the transport is a result of the pulsing effect

I Illentioned earlier There is a lot of accumulati6n in the western Basin

and these accumulated pollutants are then transported across the Basin This

kind of transport did take place in a couple hours because we also have

measurements from 1500 PDT which give us similar flux numbers

Figure 16 is a trajectory envelope similar to Figure 10 calculated for

Upland at 1600 for the air arriving at Redlands about 600 oclock in the

afternoon I wanted to include this trajectory envelope to show that the

problem is not really simple You cannot say that the air at Redlands came

from Long Beach per se The air at Redlands if you look at the whole

envelope of possible trajectories using upper air data as well as surface

data could have come from anywhere between Downtown Los Angeles and over

the Pacific Ocean south of Long Beach

Another thing to recognize is that the wind actually changes direction

slightly as you go up and down through the mixing layer and the mixing layer

is exactly what it implies There is mixing within the mixing layer so if

you begin with a parcel of air near the surface this parcel may move to the

top of the mixing layer and go one direction for awhile it then may go back

down to the bottom of the mixing layer and move in another direction for

awhile The ratio of the length scales indicata3mixing layer depths of 1500

or 2000 ft and distances on the order of 70 miles This makes it very

difficult for tetroons to follow an air trajectory because they do not go

up and down They stay at one altitude and in one wind regime and yet the

wind regimes are different at different altitudes and the air is continually

mixed up and down through this layer You can often see this on time lapse

photographs

204

The question is where does the pollutant mass go after Redlands Figure

17 is a repeat of Jim Pitts slide from yesterday and it is data for the

same day that we did our analysis It shows the ozone peaks starting at

Pomona and Riverside and on July 25 1973 eventually getting out to Palm

Springs so there is quite a bit of long-range transport The ozone is

stable at 8 00 or 9 00 oclock at night There still are ozone concenshy

trations of 02 ppm it hasnt dissipated even at the surface Ozone does

dilute as the mass moves Other calculations we did were integrations

through the mixing layer of various pollutants such as ozone and CO along

with trajectories that we measured Th~se integrations show just what the

ground data show in Figure 17 The concentrations increase through the western

portion of the Basin and then show a decrease through the eastern portion

of the Basin CO tends to decrease faster than the ozone indicating a

continued production of ozone further east

Figure 18 is a streamline chart on a larger area map for the 16th of

August 1973 It shows the typical streamline patterns that occur for

ventilation from the Basin By mid-afternoon there is flow out through the

major passes to the north and towards Palm Springs (PSP) On this particushy

lar day we had data from Arrowhead showing that the air mass from the Basin

does indeed get up there

Figure 19 shows a vertical profile over Arrowhead early in the morning

16 August 1973 at a time when there was a north wind Ozone level was

about 005 ppm the scattering coefficient was quite low on the order of

probably 60 miles visibility or so Figure 20 is a vertical profile again

over Arrowhead late that afternoon when the winds had switched There is a

flow from the Los Angeles Basin into the Arrowhead area thus one sees a

205

vertical profile that shows a distinct increase near the surface in both the

ozone and the scattering coefficient and in the condensation nuclei Ahove

that you have fairly clean air The top of the polluted level is just about

the top of the mixing level over the Basin

I want to leave the transport now and discuss the complicated vertical

structure that can occur If you want to try to model something try this

one for instance Figure 21 is a vertical profile over Brackett Airport

Pomona about 830 in the morning on 26 July 1973 which is the day after

the episode shown earlier A bit of interpretation shows how complicated

th is can be If one looks at the temperature profile it would be very

difficult to pick out a mixing layer theres a little inversion here another

inversion there several more up here After looking at hundreds of these

profiles though you can start interpreting them What is happening is that

there is a surface mixing layer at about 500 m In this layer there is a

high condensation nuclei (X line) count due to morning traffic The San

Bernardino freeway is quite close to Brackett there is a relatively high

nitrogen oxide count about 02 ppm and the b-scat is fairly high Ozone (Z)

within the surface layer however at this time is quite low The layer beshy

tween 500 m and 700 rn turns out to be the Fontana complex plume Note the

very high b-scat level it is below 3 miles visibility the plume is very

visible especially at this time of the morning when it is fairly stab]e

There is a high nitrogen oxide level (800 m) a high condensation nuclei

level and again a deficit of ozone Above this layer (800 m) you have stuff

that has been left all night very low condensation nuclei indicating a very

aged air mass ozone concentrations about 016 ppm b-scat of about 04 It

has been around all night and not yet had a chance to mix down within the

206

surface layer In fact one good way of determining the surface mixing layer

early in the morning and at night is to look for the ozone deficit Another

thing to mention is that wind reversals occurred for each of these three

layers The winds were fairly light and westerly at the surface slightly

easterly in the 500 m 700 m layer and westerly above 800 m There is a

complicated situation early in the morning but the main problem is that by

the middle of the day there is good surface heating and the pollutants have

all been entrained and mixed down to the ground so in order to modeI what

happens on the second or third day of an episode you must be able to look

at both old pollutants as well as fresh emissions And you need to account

r for ozone that is actually transported down to the surface from layers aloft l

The next slide is a photograph (not included) which is another e xample

of some layers aloft This is due to upslope flow as explained by Jim Edinger

in his publications The mountains are heated during the day in turn heating

the air and making it buoyant there is upslope flow to a point where the

heating cannot overcome the subsidence inversion and the stuff comes right

out from the mountains and spreads out over the Basin The pollutants can

stay up there if the winds aloft are very light and on the subsequent day

will he re-entrained to the surface On the other hand if there are winds

aloft different from those in the surface mixing layer or the wind velocity

aloft is high there can be a very substantial ventilation process for the

Basin Pollutants can be ventilated up the slope and blown away in the upper

winds In the case of the entire July 25th episode winds aloft were quite

light and these upper layers remained

Figure 22 is a vertical profile of one of those upslope flow conditions

in the same location shown in the photograph but on a different day Again

207

there is a relatively high surface concentration of about 03 ppm of ozone

(Z line) a layer of clean air between 900 to 1100 m and then high concenshy

trations of ozone again above 1100 m It has gone up the slopes of the

mountains and then come back out Concentrations in the 1100 to 1300 m area

are just slightly lower than they were at 600 to 800 m area Notice however

that the condensation nuclei count (X line) is quite a bit lower mainly

because the stuff is much more aged above the 1000 m level than it is down

below 900 m

Figure 23 shows the stability of ozone the fact that it can stay around

all night long This is a vertical profile taken over Riverside about 2200

PDT 1000 oclock at night Above the surface mixing layer (600 m) there

are ozone concentrations of about 0 15 ppm (Z line) Within the surface

mixing layer (below 500 m) ozone is completely scavenged decreasing to

zero The nitrogen oxides within this surface layer are being contained and

are around 01 ppm from fresh emissions that occurred during the evening

Condensation nuclei near the surface are very high The temperature profile

is very stable You have a surface based radiation inversion which is a

little strange looking for a radiation inversion~ nevertheless it is quite

stable There is a definite restriction of the mixing--a very difficult

time getting air from below 500 m to above 500 m The ozone that exists in

the 700 m range is in air where the reactions have virtually gone to compleshy

tion and is very stable All the profiles on this night changed very little

the ozone peak stays there High concentrations stay around

Figure 24 is a cross section across theurban plume of the City of St

Louis I wanted to show that this occurrence is not limited to Los Angeles

We have seen ozone formation and transport in other urban plumes These data

l

208

were taken during a project sponsored by EPA in conjunction with R Husar of

Washington University and William Wilson of EPA The dark line on this is

the ozone concentration across the urban plume perpendicular to plume The

dashed line is the scattering coefficient The power plant plume is parallel

to the urban plume The data on the left were taken 35 kilometers down wind

about 1100 oclock in the morning The ozone concentration increases slightly

to 005 ppm in the urban plume there is a deficit of o in the power plant plume3

In the same urban plume same conditions 1500 CDT two hours later further

downwind there has been substantial increase in the ozone in the urban plume

itself The b-scat is very similar to what it was before but the ozone is

now increased quite substantially except in the power plant plume where

there is a strong deficit of ozone due to scavenging by nitrogen oxides So

the formation and transport of ozone and ozone precursors in urban plumes is

a regular occurrence that happens in more places than Los Angeles and as Bob

Neligan showed this morning it can happen over quite a bit longer distances

than we are showing here

To summarize the conclusions as they affect model development first

once ozone is formed in the absence of scavengers ozone is a very stable

compound It remains for long periods of time It can he transported for

very long distances Ozone is a regional problem which cannot be controlled

on a local basis To have effective ozone control middotone must have a regional

control strategy and probably regional type air pollution districts

A second conclusion is that the vertical distribution of pollutants can

be highly complex and models have to include more than just a simple wellshy

mixed surface layer

209

A third conclusion is that layers aloft can persist over night and can

be re-entrained within the surface mixing layer on subsequent days models

should be able to account for old pollution as well as fresh emissions Also

pollutant accumulation and transport can have distinct diurnal patterns that

are strongly dependent on the meteorology Models should be time dependent

and should start at the beginning of the accumulation period In other words

models ought to be able to run for 24 or 48 hours if they have to In this

case in Los Angeles there is often an accumulation of pollutants which starts

in one portion of the Basin at midnight and continues through the next mornshy

ing even before it starts to be transported

As far as recommendations go in many areas a lot of ambient data has

been collected and in some cases the data are actually ahead of some of the

models so I think a research program is needed in developing models that

will account for this vertical structure and the day to day carry over and

the models need to be extended to cover longer distances In addition more

smog chamber work is going to be needed in looking at the effects of carry

over and mixing old pollutants with fresh emissions How people go about

this I leave to the modelers and the smog chamber people They know more

about that than I do

I

210

I

~ INVERTER

AUDIO TAPE

MONIT0R

MONITOR OBSERVER SEAT

MON ITOR

NEPHELOMETFR FLfCTRONICS

j DIGITAL DATA LOGGER

CONDENSATION

VOR DME NEPHELOMETER TUBE

JUNCTION middoteox ASSORTED POWER

AIRBORNE

TEMPERATURE TURBULENCE

middot HUMIDITY

ALTITUDE BOX

__

middotE=-middot RECORDER ----r----------

NUCLEI KJNITOR

CONVERTER

SUPPLIES

INSTRUMENT PACKAGE (

lCO

03

Ndeg

-

-----NEPHELOMETER

BLOWER

Figure 2 Instrumentation Layout for Cessna 205

211

bullubullbullbullbull

Figure 3 Airborne Sampling Routes in the Los Angeles Basin

Figure 4 Vertie al Profile Flight Path

~-~ r~i ~~1 -- ~ ~ ~2-1~ LJ-----~ r~~ ~~ t~~--l

~ ALM l

0 RIA

ec 8v

M

~ Afo

-o

M 0

~IV

ltgt

IN J--1 N

SCALE II fi M I j_ ES 0 3 4 5 =-JSEJ--J~ _middot ~middot- - =- =

I

~

M

N~J

Figure 5 SURFACE STREAMLINE ANALYSIS - 0300 PST 25 July 1973

~~~ ~~-- cp1FJ=D -~~

~ 1

~ ~ 8c

8v

~25

PACIFIC OCEAN

diams Tt

0

9 I 4 5 10 I- m p H - -middotmiddot u 4H__8 middott_

D i6 J4 k W~D SPED llaquotl SNA NJ ~1

SCALE m ICtt84bullmh R v1s1a1L1n (mil 6 ~ CONTOURS REPRESENT

-- 10ml 16km (~() bull ~ ) ~ - 000 ft 3C5

Figure 6 S_cJRFACE WIND STREAMLINES - l 600 PDT JULY 2 S I 8 7 3

l - ~---i ~-=-___-----c---it~~-~~ r----=------1 ~-~~--cpc---_t__A --~ ---llil

~_ - ~-l-cL

34bull vi~-dff

bullbullbullbull bull ~ bull -1 bullbull - -_- L bull-J bull ~bull-bull-ii------~ bullmiddot r_ -~- ~ bullI ~_ bull bull bullbull bull I bull _ - bull -~-~ middotbullbullbull ~ ~ --middot -~- bullbullmiddot ~v ) ~ - -__rl v middotmiddot - 1- ~ -- middot middotmiddot - 1 91 frac12 - ~- lt( middot K i - middot bull - middot - bullmiddot~~-~lJ) obullmiddot~ ~-f- _J_~---Smiddot~middot-~----~~~---gt_middotfY-_middot-~middot --middot-~-~----fJ_middot- middotmiddotbullmiddot u-- bullmiddot ~ ~ -middot L~ bullbull

~bullbullbullbull bullbull l_bull bull bullbullbull EW bullbullbullbull-- ~ __bull f f - middotbull - J middot f bull S bull I ~ -r --

_ bullbull bull- _ bullbull-bull ~ ~ bull bull bull bull I bull bull bull bull bull bull gt - bull middotbulliJ -bull I bull bull _1 bullJ C-- ~-middot _ bull bullbull bullbull bull _____ ~ ~ l _ middot q bull 1 -middot middot ~~middot middot middotbull_ J ~gt - J bull-bullbullbullbull ) _ -middotmiddotbullmiddot J ~middotmiddotmiddot -bullmiddotbull fmiddot 7middot _middotmiddotmiddot bullmiddot(middot Ii~ middotmiddot~_--~middot 1middot__middotmiddotmiddotmiddot middot- gt_ -~ -~-- Imiddotbullmiddotbullbull_ -

- ()_I (w--_ bullbull__(i- bullOmiddotbull bull middotbull -bull-_jlJ middot bull lt 1(middot t gt bull - ~ rbull I bull middot middot- bull41-bull l~r v-middot~- middot middot middot bull_ - middotmiddot ~Jtj (middot~ ~middoti middot middot middot middot middot ~- ~ -tmiddot~ I - middot middot_- ~ - -~ middot_ _- ~bull - _ ~) i bull bullbull bull- middot_ bull middotbull __ ( bull 11bull bull ~ampmiddot ~ l bull bullQ bull - -1 bull JY1 bullbull ~ or bullbullbullbullbull bullbull-bullbull _ ~ - bull bull-bullbullbull middotimiddot middot 91 bull t bull - - tfaw lJ--r- bull bull _ bull middot- - l

f ~~middot--~ middotmiddott ~ltrgtmiddotmiddotJmiddot_bull - ~ - __ middot- LOS ANGELES BASIN - LOW LEVEL -__ jmiddot l-gt bull - bull J iI bullbull bull bull bull _ bullbull _ Jmiddot middotL~_1 middot middot bullbullmiddot ( C middot INVERSION MEAN WIND FLOW _ J

lmiddot - f bullbullbull~ - f 1bullbullbull _ ~)- bull middot- _---_- 7f-~bull~ REGIME _F_~ AUG_UST_~ ~600 P~--- l

-__L-~bull --ncmiddotbull~~-j--bullmiddot~bullmiddot_-bull _fJibullmiddot Imiddotmiddotmiddot-bullmiddot- bullbull ~ bullbullbullbullmiddotmiddotmiddot~middotbull ___ bullJ_ _middot~0))deg bullt t1yensmiddotmiddot ( middot middotmiddot middot middot ~ middot lbullbull1 t_c0 bull -middot---l lt ~middot~- deg bullbull --= bull bull bull I bull bull bull bull bull bull bull bull bullbull _~bull b ---) bullbull-bull ) bulll middotbull middot1middot ) bullT --f bull I bullr ~bullbullbull bullbullbull( - -bull-- ( -o-----_i bull-~-l- i l l J l~-- c middotmiddot _--1 ---I middotmiddot ---- ~bull-bull bulli_ ALT Elmiddot_ bullbullbullbull _- ~~middot bull middot bullbull _ bull middotbull bull~ ~bull middot bull -middot bull--ua_-- bullbull bull

-- 01--- middot_ -middotmiddot hmiddotmiddot __1 ~-- ~ fi~~- ___ - ____ _ -middotmiddotmiddotmiddot~ ) -~-J bull bullbull bull bull 0 uc- -l ~- ~ IT ~~ll ~ bull -middot -middotmiddotmiddotmiddotbullCCAmiddotmiddotmiddot-middot middot bullbullbullbullbull

) i- 5 ~-==-- __ __ - bullbullbull _ bull~ bullbull _ bull bull l T[h4 ------ - 0

i17- o~-lt -(i-_~ 11t~bull-omiddot ~- -- 13 0l~~~bull bull Jbullbull~bull ~ ~bullbullbull bull bull x- middot~---=-~~ -=aJlll8 bull Ibull bull ~~ middotbull rbull~---bull1-~middot-middot _ middotmiddotmiddot-middot 1 0 ~vrbullmiddot ~middot ~ (J~-middot _-_~) ) ~ bull middot

l middot _ POMA_ middot =~~~----ti~ jmiddotmiddotmiddot - middot bull [j

~A ii J0 Vfli middot bullHud __=bt_ bull

CImiddot ~-- ~- middot)middot PACIFIC OCEAN I middot ---- middotmiddot ~

__ middot__ ~ - _ 23~1 middotbull 8 4 1 middot middot ~ middot middot gt ~~- l ~ u middot

bull - bull- I ~------ --1~ i middotmiddotmiddot - n _c-118 1130

~ n r -t ~~gt25) cmiddotbullmiddot

~--lt- ~~- 1-~__( i - t ~ _ middot 0 igt(_J

11bull bull11 ~~ -~[ ~i~gt----gtmiddotmiddotmiddotmiddot--~l_ ~~ ELEVATION

IN FEET bullbull (_- middot bullbullbull -middot middotbull middot ~~ middotmiddot bulltbullbull _ffmiddotmiddot-middot v I )tylt~ -~bullbull1bullbullrbullbull ~-lt -~ ( I~

600~ A0 Cv(A (1829 m AND OVER) deg )_ rJ__~7 middot middot ~--middot L==1 _J bullbullbull - bull -middot~-- rgt ~ middot(Zmiddot- middotbullmiddot middot

Z~C)-tGOO (762 middot 1829 m) 9-N4 __J (r -- lf _ bull bullgt-~~~ ~ _ w _ _ I (1 bullmiddot( middot1 middot -----~~~- middot L-bullmiddotbullW bullbullbull3 STA r I0-4 lODEL

100i -2soo (305~762m) -- Ow - -~1_- i ~~--- bull v~rvt ~~ -middot )) ~--

II gt J (-_bullmiddot middot~ l bull bull tr 1 )~ gt ) bullbull-_bullI-middot -middot bull~0 3 Mor nuq1ENr Wlbull~O JIAtCTIO-bull bull - lbull C---gt bullbull )t bullbull -( I bullf I - 20-00 (61 bull 305 ml J( Jloa xxE- -bullbull00 - -- middot1

0-200 (0middot61m) Wl)7 AVBt~gpound ) bullmiddot-iiNL~ middotntmiddot_ 1 iJJlt( _1J- ~ VAq IA9 IL ITY 0 ~ 10 15 ltS lHPtl

~--_ bull bull I bullbullbullbull 1 ~) J)J ~ bull Is bullmiddot bullbullbullbullbull ~ 3 V IS A VAqlABLE OIR~CTIO- 0 8 16 2-4 km

(SPEEDS SHOWN IN mph 10 mphbull 16 h1llr) -- middot ktr~~~ lt~ ) -middot-SCALE

Figure 7 LOS ANGELES BASIN MEAN WIND FLOW FOR DAYS WITH LOW LEVEL INVERSIONS DURING AUGUST I 970 AT 1600 PDT

-~~~~-=======~middot~-~======~middot--=-==-===gt=---==____________=== ~--=-J~==-- -=-ee----=-------

500

N f-- V

- - - SUBSIDENCE INVERSION

----MARINE INVERSION

bullbull-bull-bullbullGROUND LEVEL

x WINOS ALOFT (kmht)

WESTERN middoteASIN EASTERN BASIN

LAX WINOS EMT IHOS I I

CNO WIHOS

s_ 04 13 1500- 05 02 08

I 06 069 middot

11-1--

04 04 i ~4

06 ~ 4--

I 2

1000 n1 1005 -_E

lll --1 lJ -----------~----

~11

--=i-+- c -- 9 _____ - ~ C

lt I

I 6 4 _r 31

I 6 5 ~~ ~_ bull ---middot- 64 ~li- - middot- bullc - middot-----------

10

SMO (1347 PDT)

EMT (1246 PDT)

BRA CAB (1459 PDT) (1335 PDT

RIA (1349 PDT)

RED (1406PDT)

Figure 8 VERTICAL CROSS-SECTION OF bscat FOR lvflDDAY

T t 10-4 -1)(l n1 s are m

JULY 25 1973

- c - -~

~--~ JC_-_1- ~1pi~ oamp----~JilliiiM~f~-U~ -~--- --~~~ ~~~

-=--~

-E-- O

_ lt

1500 05

06 15

09 __~

1000 --

~- ~---middotmiddot 29

500

oJ11

__a

07

I 07 I

I I

I

09

I

I

I

I 7 ---

11 -----

~ ----- 6

---------------lt- -~middot4 --------

20

29

-

10 10

11 07 08 08

10

08

~8 _____ Y-

N

- - bull SUBSIDENCE INVERSION

----MARINE INVERSION

-bull-bull-bull GROUND LEVEL

WES TERN BASIN EASTERN BASIN x WINOS ALOFT (kmhr)

t t

CNO WINOSILA WllltOS poundMT WINOS

SMO LA EMT BRA CAB RIA RED O (1736 PDT) (1655 PDT) (1707 PDT) (163 PDT) (1823PDT) 1805 PDT)

Figure 9 VERTICAL CROSS-SECTION OF b FOR AFTERlOON OF JULY 25 1973 scat

T bull 1o- 4 - l )(units are m

__~~---iii~~- ~- ~~______ ~~- --~~J---=-~ ~

N ~ -J

PACIFiC OCEAN

0 5 10 15 1111

E 8 4 I 0 8 6 2 ~ bull

SCALE

dh Mes

CONTOURS REPRESENT - 000 ft 305 m

0 SNA

c8s

ec 8v

amp R~b

Figure 10 TRAJECTORY ENVELOPE FOR AIR ARRI1G AT CABLE AIRPORT (CPLAD) 1600 PDT JULY 25 1973

~-~

q_- ~ ------1 H~~~ -~~--~ ___---___--i- __r-=-1--===12---1 ~ ___r~ _==---_ - ~- f~~ ~-- - -5plusmn-at -~middot~

ll~~r1 ri

40

ec 8v

-1 I

amp

0 HQ_

7 0

CAP LAAR) O

VER

PACIFIC OCEAN ~ 0

RLA

4

WHqR d

diams

H ~I

I l

0 COMA

3

L~

LAH

Fa_ f ~~

S ~ LA APCD VALUES ADJUSTED TO AGREE ~

lt

0

5 10 15 mi0 WITH ARB CALIBRATIONE-j I I CONTOURS REPRESENT NZJ ~ 0 a SCALE 6 24 km - 1000 ft 305m COS v~J

______ J 10 ro ( igtf t-i

coFigure 11 SURFACE OZONE CONCENTRATIONS (pphm) I 600- I 700 PDT JULY 25 1973 ~

~~~~~C-~ ------=--~-__-~--~~~=--- ----=--~

N

-E

D1600----------------------------- 1--

14001-------------------------------

1200

I Ground Elevation

1000 middot 445 m ] lampJ

sect ~~ 7 ) SURFACE i6~ 800 MIXED LAYER

~

~ [ J ~ ~ I OZONE CONCENTRATIONS~ 600 E E GREATER THAN

( 50 pohm

400 I C H T Z GROUND LEVEL

200

I PUUloCETER UNIT SnbullBOL

NOc N0 0 ppm01 02 03 04 05 03 z

40 --~45~~ 50 co pm C0 5 10 15 20 25 30 35 I I I I I I I I I I TEIIPERATURE oc T-5 b 5 10 15 20 25 30 35 40 45

I-- 100 RELATIVE HUlillOITY H0 10 20 30 40 50 60 70 60 90 b1eot IOmiddotm- 1 8

CN cmmiddot3 1 IO X0 I 2 3 4 ~ 6 7 8 9 10 URBJLENC-C cm213ue- E

Figure 12 VERTICAL PROFILE OVER CABLE (CAB) J CLY 2 5 l C)7 3 l 63 6 PDT

~ _~ ~--- -

--

1400 I bull bull

1200

1000-5 LampJ 0 ~ I- 800 ~ c(

sooLl

-1-=-1-~--t j --=~c-o-----i-bull 1-~~~ ilt~~ -~-1 lta-abull--~ -c-~---=---r F--- ---- I n_--middot- =~~ ai~IHJ

(~-It

1600 ___________________________________

C r 11 s Ground Elevation t~C E H I~lcc

- ~ 1 90 m

4001 bullc C H

C UNDrnCUTTNG svC ~ Ic- H

SEA BREEZEC II 200

C C

[C -PARAMETER ---UNIT SYMBOL

NOx N0 0 ppm01 02 03 04 05 03 z co ppm C0 5 10 15 20 25 30 35 40 45 50

-5 middot- -~20~----25 TEMPERATURE oc T0 5 10 15 30 35 40 45

100 RELATIVE HUIOITY H0 JO 20 30 40 50 60 70 80 90 bcot 10-4m-1 8

CN crrr3 10 0 I 2 3 4 5 6 7 8 9 10 X TURBULENCE cmZ-13 sec-1 E

N N

_-----=-G--~---

Figure 13 VER TICAL PROFILE AT EL MONTE (EMT) JULY 25 1971 1656 PDT SHOWING UNDERCUTTING BY THE SEA BREEZE

0

middot~_lt ~middotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotbullbull

-~

LACA

0 - )

i r=

-v2v

~

_middot~middot)( I bullbull

bullJ

K~Ji~middot

~~ 61iAS 0

EMT J~J---6~-11 ~orr

PACIFIC OCEAN

WEST 0

SMC

0RLA

14

L~8

R~A

~BL

16 ~ ~

0 5s Pcfrac14A c1i ~ )

wFJfo~J_) ltI~~~

_ff-Clf1ito J )

HILL~

~J U

~ _~~~

~

I o middot

1 1$ ~ 11yen ~middot ~I N

I

N I- I

t

0 --pomiddotmiddot bullmiddot i- 1LO middot Joomiddotmiddotmiddot -- middot middotmiddot -middotmiddot

_middotmiddot 0 middot middotbull MWS r

L4 ( 1 T bull bull __-- -A bullbullbullbull middot

0 i __ bullbull

17 t-J~ N7 a S I ~r ~ 1 rtd ~lt A-~ v- middot ~ - cXa 0

RIA 19

CLO

ltJ~

bull ~ 0

(

--

1

_ _

-2Wl

~s~o -- _)~J0JgtJ~ ___ Q

15 l1JI

0 15 r(A0

CAP

CLARR)~R 1900 1-shyPDT

II (_-L~X L2X I 0~ R[V

0 CCtwA

I

I18=00 POT~ l4 r1

fj

-11J - ----- 11=oomiddotmiddotpor

l~i middotmiddot- o

i

5 10 5 Tl o~1 middot--middotmiddotmiddot middotmiddot

_q it==i--__F-3 9 I I CONTOURS REPRESENT SNA NZJ ~1 o

_- I 0 8 16 24 km I - 1000 ft 305 m middot ~

7 14~CALE --- 2500 ft o2m V lr1 ) middot I i0 _ il o5

16QQ pol(middot v( ____________ _L

I i

Figure 14 APPROXIMATE TIME (PDT) OF ARRIVAL OF SEA BREEZE Jl-LY 25 1973 (Ogt_iective criterion based on ground level ozone concentrations)

~ -___~==~ ~~ - ~ =-~ f7r=~1 _j~-~ --c_~~

u-middot - middot middotmiddotmiddotmiddotmiddot

~- middotmiddot~ ~1 WESTERN BASIN r Joa_middotmiddotmiddotmiddot_ NOxEMISSION RATE ~- 95 METRIC TONShr

-----bull_ ~ ~middot~ I -OUR -----middot )omiddotmiddotmiddot - middot~ l21 (fTI

~ AT middot ~ middotbullmiddot- ~- ~ middot 4bull-middot

I EASTERN BASIN NOx EMISSION RATE 10 METRIC TONS hr

ri r bullbull

t10 Joa

) __ 8v -a_ -- -bull-I O ~AGA -_ ~S ___ _ middotmiddotmiddot -

~ ~v ai- omiddot-middot~-- - ) r -middotmiddotmiddot f middot( ---~ -l A ~ _ (- bull ___

it~ ~~~ middot-middot -- ~-~ ~~~ 0 0 AZU~

AVERAGE CONCEN7RCTi)N iN BOX (IF STEADY STATE)

IS 25 pphm

1 r f--Ji 7 ~Sv PAS ou )V~(~- ~ t i -~ Li_) 03 FLUX THROUGH f~

~ ~JI_~ - amp_ JiM O SHADED BOUNOA~middot~-~ ~~-s-- EMT 185 t 60 METRI~ bull ~ ~ TONShr 0 (m)

c~~~ 1t~CS A~JFP

1000 _29

-i32

_~o tUA

_

1

O~ ~

0 -__rJ( (r- J PACIFIC OCEAN LAX _ C-middotJbull _

l o M R No _

550m

r

A frac14

HAR O HJ LAH

_ o camptA REDLANDS 18QO POT ~ r

I bull ~

RB MEAN TRAJECT~~~y

0

TOA L~S

0 AN

I - ~ 8 OUNOARY ~ ~middotltdeg ~ ~ BETWEEN middot __ WES~ERN ANO- middot middot - ~

I gt I lt bullmiddot bull (EASTERN ~ i middotmiddot middot - - ~

S ~ ~~ ~ - middot-

rt1~1_--t------l

middot1-- BASIN ~-~

1-)~~--middot ~ ~l

~~ ~-bull bull J --

-is-eo -_

0 5 10

j=i r-i C

0 8 ltl

SCALE

5 mi

2~ un

CONTOURS REPRESENT - 1000 ft 3gt5 m

--middotmiddot 2500 ft 1 762 m

~

0SNA

cos 0

_ --~ ----- --- ( bullmiddotmiddotgt

- middotlt- ltgtmiddot t__ Q ~

1 1 rmiddot bullbullbullbullmiddot ~9

NZJ ~ middotmiddot - middot- Alr ---middotmiddot- middot middot( middotmiddotmiddotmiddotv ~ bullbullbullw bullbullbull bullmiddot 1 bullbullr~ ~-- -middot ~--v ~- - I -~

ESTIMATED OZONE FLUX FROM VESTER~ TO EASTER-J BASIN JULY 25 1973 I 700 PDT

C ~IV

N N N

I

l ~

-~~

I

iI

i I

I t

t

~ ---~ --

Figure 15

~Qa llfJD fl(~middot ~ 11f ~I I

l

Lfb ec~s0 CPK v2v 0

ALT 8v Ld~_----1

I

HO-

0 CA

middotLARRv O VE~

1330

ol(Di

A~U

0ENT

~lt

s~e ~ 1530

F8f 1730

~

rbull-~

oc (WljT) -_-~(~~c lt-rw---_

~~ ~-_i~cB~~~

2-~) - ~ ~ l~w-~~ p~- pound)_

0 ojI middot tl-1CfUp I ~ ) 1 ~ J~I i bull middotbull middot~-Li 1)- ) I

DiI ~- 0

i ) 0 l I I

t

A RALc~o JI

C

-~

0 r-iR

~IV 1230 1~

RE PO ~- I - Ftl

) 0 ---~gt- __L8s ~Zi diams ( T~ _middot_ ~~ ~

I AN ~~-~ j t bi 0

~ I

~ I L i

-_gt ji o 5 c 5 Tl middot 0 0 ~-i p__i=r 2=f I_ I 1 NZJSNA 1

1 8 2 4 km )

SCALE I 00 J_(1 CONTOURS REPRESENT cos f

1 0 I --- I - ))) 35

PACIFIC OCEAN

Figure 16 TRAJECTORY E~VELOPE FOR AIR ARRI1gtJG OVER REDL_)DS AT 1800 PDT JULY 23 l =i73

224

JULY 25 1973

LA DOWNTOWN

0sect040 a

~

~ 020 0 X z0 ~ LJ 0 ~ z

~5 040 330POMONA 0 ~ en~ 020 w z _J

w w 0 (9 z O----u-~~-__~_-~~~-------L-~-0--0-0~----- z

ltt~ 040 56 (I)z

0 0o _ RIVERSIDE _J0 20 t6 ~

0~ Qt---0-0--ltrO-ltgt-C~------~~~~ a

LL ~

Rate ~ IO mph___ (I) w

_J~ ~ ~

et~ lt(

3 040 PALM SPRINGS ~

j 020 ~

0------____-----L--___---------L---~--~

105

12 4 8 12 4 8 12 l~-s----am _ pm----1

HOUR OF DAY PST

Figure 17 Diurnal variation July 25 1973 of oxidant concentrations at air monitoring stations at Los Angeles Downtown Pomona Riverside and Palm Springs California Values are corrected data Los Angeles Downtown and Pomona x 11 and Riverside and Palm Springs X 08

CONO S t 1 fRESEIS7

~

~~ 0

ciffmiddotdK ~ ~v~~o

( ~s ~

bull ~r ~ bull 1--~~----Soootl ~ ~ ~ ~ lj i1 d t CJ ~ ampfrsmiddotflt- frac12 ~ middotL~Js _-- ~

_gtgt middot~ ~rroltf~-) ~ 0 s- r

middot-middot- r_~ ~~JtbO ~~bull~Jt ~~~ L r - bull _ ~ I= J 1 ~ ~ ~-~~bullJC ___ -_ middot ~ laquo -poundJ~ ~- middot1~ r-- - V--_1_ ~ I 1 S I

V ~ bullf-uv~ fi -~zumiddot -~middot~ LS gt -tmiddot-F Q~ ~-tv I_~ --- ONT p(_ s ~S ~~~-[ ( 0 c-_ --~ ~~~___d_) lt- ~ I -i-C - -

~----1-1 bull~~POMA ~V BN ) middot-~ f -- s - ~

~VA -middot- ~p AAL a 2~~ ~~middot01 r r ~ middot middot 0-- V

i LAX bull1

~ -~poundJ-i- ltllll _(__1-0~ ~t- degQ-0- ~~ _ _-__~~-qlK ( a_ II ~ ~p-~ ~J

N bull - - 0 r o_ _I ~ -~ ~middot ~ ~amp ~--= ~ ) s ~

- -~- - middotO _a - Tl --0- ov I lHOIO J I bull J -- ~ 6 ~ -__ 2 ~

(__ ~~ _- ~-~ middot8---fl~ -- ~ bull~-abullbull _~ ~-cgt ~ bull bull middot e bull bull l ~ 0

I 1A_ HZJ middoto~J

middot0 (~ ~ S TAA

- ~ - - - --0 () _-j J middotO=c==c-c==cc~~~ l ~~ ~ ~ bull-~---~ ~ bullbull -~ al1 ~ bull __ ~--middotmiddotmiddot

diams Skyforest _ Strawberry Mt Lookout

Figure 18 STRE ~[Ll)ES FOR 1600 PDT on 8 1673

~ ~--

vO 0

N N V1

au

91 V7

-1 ~ -=1 ~~ ~~~~l r=--~d- ---1 _J-_

~E1 ~L1-~f~

3100 ---------------------------------

2900r-----------------------------

T

e w 0

~ 5 Cl Ground Elevation

1560 m

T PARAMETER UNIT SnbullBOL

NOx N 01 02 03 04 05 03

ppm z co ppm C

10 15 20 25 30 35 40 --

45 50

170

I I I z

0 5

-5 - -0~ 5 10 15 20 25 30 35 40 45 TEMPERATURE oc T

0

0

10

I

20

2

30

3

40

4

50

5

60

6

70

7

80

8

90

9

100

o

RELATIVE HUMIDITY

bcot CN

TUR8ULENC~

110-4m-

cm-3 tobull 213 1 cm sec-

H

8 X E N

N OI

Figure 19 VER TI CAL PROFILE OVER ARROWHEAD u-RR_l A CG CST I 6 1973 939 PDT

3100----------------------------------

N2900r----------------------------- -i

N

2700i-------------------------------

2500

e 0 uJ 2300 gt ~ ct

2100

1900i---------------------+--------------

~le 1iation 1360 m) 17001 ~

- -PARA1jETER UNIT SYMBOL

T NOx N1500 o ppm01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50

TEWERATJRE oc T-5 middot --~o--- 5 10 15 20 25 30 35 40 45

IOO RELATIVE HUWIOIT Y H0 10 20 30 40 50 60 70 80 90 bcat 10-~- 1 8

CN cm- 3 104 X0 I 2 3 4 5 6 7 8 9 10 213 1 tURBliiENCE cm sec- E

Figure 20 VERTICAL PROFILE OVER ARROWHEA D -RR 1 --- -AUGlJST 16 I) 16--1S PDT

1-~i w--~i_f l-=--bullC- ---~-4

1600 bull t c- N 8 ff Tbull C[ 8 H 1 bull H z H T ~ C f N 1 H T bull C rn 1 C NE bull-~z Hi400 bull bull tf T bull N ~r --middot _P H -ybull EC N z__e H T i 8 z H Tbull C E HD Z H T POLLUTANTS REMAINING FROM bullt C Hbull L T PREVIOUS DAY1200 Et HO I II -middot-- bull Ct H 9 - H T

___ Hbull( E N 1 a tC N i--_ -1 H

C N Tbull Z HP poundIC C H z_ 1111 1

- bull C H Z l _H_ _J1000 )( cc H -z emiddot ksect bull C N ~ T

)( iz H 8 H TIAI -t XC z 7-- T0 bull pound N t H_8

t-gt

YCpound N 1800 l I-gtltbull - H (Jet

N i -r~Bltt t bull gt- t C X N H T

[ BUOYANT POINT SOURCE PLUMEH 1

N ~z-- -

C H

-bull SUPERIMPOSED ON POLLUTANTSC JZ X H T 600 -~ E c REMAINING FROM PREVIOUS OtY Cl JC t H H f bull cmiddot t HT -fl

C- X t fl _ REMNANT OF NOCTURNAL RADIATION INVERSION(I-----e-C f N K I T H

C Z [ T H x-8 400 _Zc r -H -K SURFACE MIXING LAYERz C II H K 8

C N T pound H M 8 _ I -t ff H E N -9 l

Ground Elevation 305 rn200

PARAMETER UNIT SYMBOL

_ I - I I I NOx N00 ppm01 02 03 04 05 03 z

co ppm C 0 5 IO 15 20 25 30 35 40 45 50

L middot1 TEMPERATURE oc T-5 0 5 IO 15 20 25 30 35 40 45

100 RELATIVE HUPAIDIT y H0 10 20 30 40 50 60 70 80 90 bscot o-4m- 1 B

CN cm-3 x 104 X0 2 3 4 5 6 7 8 9 10 TURBULENC~ cm213sec-1 E N

N co

Figure 21 VERTICAL PROFILE OVER BRACKETT (BRA) JULY 26 1973 0825 PDT SHOWING BUOYANT PLUME AND UNDERCUTTING BY RADIATION INVERSION

N N 01600

___bull C M C

C

1400~~~ t C [ middot H LAYER CAUSED BY

C C H C [ H UPSLOPE FLOWl

1200

1000 ] w

SURFACE MIXING LAYER 0 --= ~ -~~ 6 800~ er

C C

600t-i C C t C

I ~00

Ground Elevation 436 m 2001-------------------------------

PAIUWETU UNIT SYWBOL

NOx N ppm0 0 01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50 I I I I I I I I TEWPERAT1JftE degC T-o b 5 10 15 20 25 30 35 40 45

100 ~EIATIVE HUWIOITY H0 10 20 30 40 50 60 70 80 90 b1tt1 10-m- 8

CN enr3 110 X0 2 3 4 5 6 7 8 9 10 Tu RUL Erct cm23sec- E

Figt1re 22 VERTICAl PROFILE AT RIALTO (RIA) JlJL Y 19 1973 1738 PDT SHOWI=JG LAYER CAUSED BY UPSLOPE FLOW

~~-7 ~ ~- 1 ~iri ~~- ~~-~ ~t ~~ ~ =~middot-1

1200 I t 1 If J-

1000

I C ltTl a_ ~l- t

800

600

L gE __r H

H

400 j (~ c pound N C E I~

t EH -

1-1 M

H H

H M H H

H

H H

11 bull H M H

M H If

H H

H

- C t H ~ C poundmiddot H

I C E I(

200

1600--------------------------- t

T t t T l

l T t

T t_

t 1

l] w ) g f

Tt t

ltt ~ T

t J t T

t J

f 1

t

Klt

H M Cro1nd Elevation 250 m HT X

5Yl80LPAllAlETER ~

NOx N0 0 ppm01 02 03 04 05 03 z

co ppm C0 5 10 io 20 25 30 35 40 45 50

25~--- ---35~~-40 TEMPERATU~E oc T-5 0 5 lO 15 20 30 45

100 RELATIVE HUMIDITY H0 iO 20 30 40 50 60 70 80 90 bact 10--ltllm-1 B

CN cmmiddot3 11 04 X0 I 2 3 4 5 6 7 8 9 10 IURBULENCE cm2hioC-1 E

Figure 23 VERTICAL PROFILE OVER RIVERSIDE (RAL) N

JULY 26 1973 2239 PDT I)

middot==-=-=

0

bull

N w 1--

ii -s~~ l-obull

CJ ~

obull -obull obull

5 02~

bscat

Oa

4l o2J

-I 3 e I 0

--)(

~

Abullu 2

ll

ol

Traverse at 750 m msl 35 km Downwind (SW) of Arch - St Louis Mo 1117 - 1137 CDT

( Power Plant Plume -01 Ibull-[ ~ e

11 bull E I -)(I

I0bull I 1r~ l -

0

I I Io 1 u I

I r- l A bull I i I 1I

H1I I 4 t I II I I

11 I I

I I r I I I

I I qo 01 I I

I I bullJ~viI I middot ~

I

I I

~

Urban Plume

ood 0 10 20 30 40 50

kilometers

o~

02

01

s 1

P

0bull 01

00S~J1 I ti middotmiddot1 middotvmiddotmiddot~ J

Urban Plume

I y

oo 0 10 20 30 40 so

kilometers

Traverse at 750 m msl 46 km Downwind (SVV) of Arch - St Louis Mo 153 0 - J 549 CDT

---- bscat

o-

Power Plant Plume

1l~ 11I 1 t

ill~t fl Ibull I ii

I

lmiddotmiddotrI

I I I I t II

l vrI V

JV-f Jl bull

bull t I bull I

Figure 24

l

232 RELATIVE CONTRIBUTIONS OF STATIONARY ANDMOilILE

SOURCES TO OXIDANT FORMATION IN LOS ANGELES COUN1Y IMPLICATIONS FOR CONTROL STRATEGIES

by Robert G Lunche Air Pollution Control Officer

Los Angeles County Air Pollution Control District Los Angeles California

Introduction

The type of air pollution problem characteristic of the west coast of the

United States and particularly of Southern California has come to be known

as photochemical smog because it is the result of sunlight-energized atmospheric

reations involving oxides of nitrogen and reactive hydrocarbons Its manifesta-

tions- -eye irritation reduced visibility damage to vegetation and accumula-

tion of abnormally high concentrations of ozone or oxidant - -are by now well

known In fact the occurrence of high levels of oxidant which consists almost

entirely of ozone has become the primary indicator for the presence and relative

severity of photochemical smog

During the 25 years since photochemical smog in Los Angeles County was

first identified an extensive program has been underway for control of the responshy

sible contaminant emissions Initially during the 1950 s these programs concenshy

trated on controlling emissions of hydrocarbons from the stationary sources of this

contaminant In the early 60 s programs for the control of hydrocarbon emissions

from motor vehicles in California were begun An exhaust emission control proshy

gram for hydrocarbons and carbon monoxide from new vehicles was begun in 1966

C011trol of oxides of nitrogen emissions from motor vehicles began in 1971

As a result of the overall control program by 1974 emissions of reactive

hydrocarbons from stationary sources have been reduced 70fo from uncontrolled

levels and about the same percentage from mobile sources Oxides of nitrcgen emissions

233

from statjonary sources have been reduced about 53 while emissions from moshy

bile sources are still about 7 above uncontrolled levels due to the increase

in NOx from 1966-1970 models Additional controls already planned for the future

will by 1980 achieve reductions of reactive hydrocarbons from stationary sources

of about 87 from uncontrolled levels and from mobile sources about 93 By

1980 emissions of oxides of nitrogen from stationary sources will have been reshy

duced 53 and from mobile sources 63 from uncontrolled levels The past

present and projected emissions of these contaminants are shown in Figure 1

A I though compliance with the air quality standards has not yet been achieved-shy

and is not likely before 1980- -the results of these programs have been reflected rather

predictably in changes in certain of the manifestations of photochemical smog For

example eye irritation is less frequent and less severe and in some areas js

rarely felt at all any more and damage to vegetation has been markedly reduced

Ozone (or oxidant) concentrations have been decreasing in Southern California

coastal areas since _1964 in areas 10-15 miles from the coast since 1966 and in

inland areas 40-60 miles from the coast since 1970 or 1971 as shown on Figures

2 arrl 3- All of these positive effects have occurred despite the continuing growth

of the area indicating that themiddot control programs are gradually achieving their purpos

a return to clean air

This improvement is al~o refutation of the so-called Big Box -concept which

assumes that the total daily emissions in a given area are somehow uniformly disshy

tributed throughout that area--regardless of its size or of known facts about the

meteorology of the area or the spatial and temporal distribution of its emissions- -

234

and of control strategies based on that concept And since the improvement in

air quality refutes the control strategies based on reductions in total emissions

it thus confirms the value of more recent control strategies which emphasize conshy

trol of motor vehicle emissions and use of a source-effect area concept

Following is a brief listing of the evidence we intend to present as supporting

our views on just what control strategy is appropriate

Examination of relative contributions of HC and NOx from stationarybull and mobile sources demonstrates that motor vehicles are the overwhelming

f source of both contaminants~

I bull Observation of air monitoring data shows that the effects of photochem -

ical smog are not uniformly distributed t_hroughout the county

bull Study of the meteorology of LA County shows consistent paths of trans -

port for various air parcels and consistent relationships between the

areas most seriously affected by photochemical smog and high oxidant

concentrations and certain other areas

bull The upwind areas are found to be source areas--the downwind areas-shy

effect areas

bull Central L A is found to be the predominant source area for the effectI area in which the highest oxidant levels in the SCAB consistently occur

bull The predominant source of emissions in this source area is found to

be motor vehicles

bull Central LA has the highest traffic density I

ij bull Both pr~mary and secondary contaminant concentrations reflect the effects

of the new motor vehicle control program in a predictable fashion 11 I

A strategy based upon these findings is gradually being verified by atmosshybull pheric oxidant data~

235

The Evidence that Motor Vehicle Emissions Are the Principal Source of Oxidant

As seen from Figure 1 at the present time the total daily emissions of I-IC

and_ NOx from all sources in Los Angeles middotcounty are primarily due to the motor

vehicle The problem now is to find the spatial and temporal representation of

emissions which when examined in the light of the known meteorology and geogra -

phy of the Los Angeles region best describes the source of emissions responsible

for the highest observed oxidant readings

In the rollback models used by EPA and others the basin is treated as a

big box with uniformly distributed emissions and peak oxidant is considered to

be proportional to total basinwide hydrocarbon emissions

The fact is that the middotemitted contaminants from which the smog is formed

and the effects which characterize that smog are not evenly distributed throughout

the Los Angeles Basin in other words the basin area under the inversion is not one

large box filled to all corners with homogeneously distributed air contaminants and

photochemical smog

Refutation of Big Box Myth

Examination of atmospheric contaminant concentrations refutes the big box

concept It is found for example that concentrations of djrectly emitted contam -

inants measured at a particular sampling site reflect the emissions within a rather

limited area around that site For this reason contaminant concentration levels

vary from one location to another and each has a characteristic daily pattern which

reflects the daily pattern of emissions in that area

middot 236

The big box concept is further refuted by the fact that peak concentrations

of carbon monoxide and oxides of nitrogen in areas of high traffic density were

fairly static prior to 1966 Thus they did not reflect the 45-50 per cent growth

in motor vehicle registrations and gasoline consumption which occurred in Los

Angeles County between 1955 and 1965 and which caused comparable increases in

total daily emissions of such vehicle-related contaminants This demonstrates

that growth was outward rather than upward so that a larger area of the County

began to be affected by photochemical smog but no area experienced smog ofJ

greater severity than that originally affected by smog formed from the vehicular

emissions which accumulated each weekday in central Los Angeles and were trans-

1 I

ported later that day to the San Gabriel Valley

1 Meteorological Evidence

To verify the geographical dependence of emissions and resulting atmospheric

concentrations let us examine the meteorology of these large areas of Southern

California Both the County and the Basin have many meteorological sub-regions

in which the patterns of wind speed and direction may be similar but within

which the patterns of air transport are parallel with those of adjacent sub-regions

and the respective air parcels do not ever meet or join

The characteristic patterns of inversion height and wind speed and direction

in these sub-regions and their patterns of vehicular emissions together have

created a network of source areas- -those in which the reactant contaminants accu -1T

i ~ mulate in the morning and begin to react--and related receptor areas--those to which

~ the products and associated effects of the photochemical reactions of the contamshy)

inants originally emitted in the source areas are carried by the late morning and

237 middot

afternoon winds ( sea breeze)

Wind-flow patterns show that characteristic patterns of transport for related

source area-effect area combinations are separate and parallel not mixing or

joining Each source area has its own reactor pipeline to its own effect area

or areas

To illustrate this source area-effect area relationship the typical flow of

polluted air from downtown Los Angeles to Pasadena was selected as a worst

case situation for in-depth examination Figure 4 shows that the air in downtown

Los Angeles on the morning of smoggy days moves directly from the central area

to Pasadena

Vehicular traffic is the predominant emission source in both downtown Los

Angeles and Pasadena Thus the air in each locality should contain CO Also

since oxidant would form in the air parcel moving from Los Angeles to Pasadena

oxidant levels would be expected to be higher in Pasadena than in downtown Los

Angeles

Figure 5 shows these relationships for the period 1960-1972 The atmosshy

pheric CO level is similar for the two areas while oxidant levels were higher in

Pasadena than in Los Angeles throughout this time period This demonstrates

that a significant amount of oxidant formed in the air as it moved to Pasadena

containing both the unreactive CO and the photochemical reactants for producing

oxidant Both CO and oxidant show a marked downward trend in each locality since

1965 which emphasizes the effect of vehicle exhaust controls and the correlation

between the localities

238

On a day which is favorable to the formation and accumulation of photoshy

chemical smog a contaminated air parcel normally originates during the

6-9 a m period on a weekday from an area of dense traffic centered just

south and west of Downtown Los Angeles It is oxidant generated within that air

parcel which usually affects Central Los Angeles and the West San Gabriel

middotK IJ l J

Valley area around Pasadena

The traffic area in which this smog had its origin is about the most dense

in Los Angeles County and has been so for the past 25-30 years No area

has a higher effective density thampn-this Using carbon monoxide which

1

is almost entirely attributable to motor vehicles as an indicator of such emis-

sions it is found that the concentrations of emitted vehicular contaminants

middotr i

measured in Central Los Angeles during the past 15 years confirms both this lack

of change in effective density and the absence of any area of any greater effective

density when local differences in inversion are acknowledged

This area the Central Source Area is depicted in Figure 4 The size

and shape of the Central Source Area was ch~sen to be large enough to reduce to

an insignificant level any diffusion or transport into this area from any externally

l generated reactants This conclusion is based in part on the trajectory studies

previously referenced as well as an analysis of the diffusion and transport parashy

meters for the area

239

The Central Source Area has been identified as that geographical region

which contributes essentially all of the primary contaminant emissions giving

rise to the highatmospheric oxidant levels in the West San Gabriel Valley

The proportion of emissions in the CSA due to motor vehicles and that due to

stationary sources is shown in Table 1 For the County as a whole about 80 per

cent of _(6-9) AM reactive hydrocarbons are due to motor vehicle emissions and this

figure rises to 90 per cent for the CSA The same conclusion a pp lies to NOx

emissions The Central Source Area contains the greatest density of vehicle traffic

in the County and thus the greatest density of source emissions Thus it appears

that the source area with the highest density of emissions during the critical (6-9)

AM period is responsible for the highest afternoon oxidant levels observed in Los

A i1geles County and in the South Coast Air Basin These highest oxidant levels

are consistently observed to occur in the San Gabriel Valley This is true whether

the LAAPCD or the ARB oxidant calibration procedure is used

Further the atmospheric concentrations of the primary pollutants can be

identified as originating primarily from the motor vehicle and they reflect the

effects of the motor vehicle emission control program A vehtcular source area

can be identified by its atmospheric levels of CO and NOx Figure 6 compares

measured atmospheric levels with calculated atmospheric levels for CO NOx

and the CONOx ratio in the downtown area

TABLE 1 240

REACTIVE HYDROCARBON EMISSIONS

(6-9) AM

1970

LOS ANGELES COUN1Y middot CENTRAL SOURCE AREA middot SOURCE TONS PER CENT TONS PER CENT

Mobile 1260 81 3 135 91 2

Stationary 290 187 1 3 88

Total 1s~o 1000 148 1000

By 7 -Mode Gallonage

241

The calculated values shown in Figure 6 were derived from a baseline

survey of 1100 vehicles and continued surveillance tests both using the Calishy

fornia 7-Mode test cycle The baseline survey showed that motor vehicles withshy

out exhaust control systems had average exhaust emissions concentrations of 3 4

per cent CO and 1000 parts per million of NOx Baseline emissions data apply

to 1965 and earlier model vehicleg and surveillance data to 1966 and later modelsmiddot

Since it can be concluded from calculations and observations that the dilushy

tion of auto exhaust emissions in the atmosphere on a smoggy day in Los Angeles

is approximately 1000 to 1 the calculated values for CO and NOx prior to 1965 are

34 ppm CO and 1 ppm NOxo After 1965 the changing effect of controlled vehicles

in the total vehicle population is reflected in the calculated values

CO and NOx values measured in the atmosphere are also shown in Figure

6 and confirm the values calculated entirely as diluted vehicular emissions NOx

concentrations measured in the atmosphere tend to be consistently a little lower

than the calculated values probably because photochemical reactions remove some

NOx from the system

The data for CO and NOx calculated and measured show that emissions in

downtown Los Angeles originate almost exclusively from motor vehicles and that

atmospheric concentrations there reflect the average emissions from a representashy

tive vehicle population

The ARB has recently published a report entitled A Trend Study of Two

Indicator Hydrocarbons in the South Coast Air Basin Acetylene was used as a

242

specific indicator of automobile exhaust emissions and it was found to have de-

clined in concentration in the Los Angeles atmosphere at an annual rate of 12 5

per cent since 1970 To quote from this report The California implementation

plan requires an annual average reduction in these emissions (reactive organic

compounds) of 166 tons per day or 11 1 of the 1970 tonnage per year The per cent

reductions in the_ acetylene levels at Los Angeles and Azusa are greater than reshy

quired by the implementation plan Since acetylene is almost entirely associated

J with auto exhaust this demonstrates that the motor vehicle emission control

program is achieving its purpose

To summarize at this point it has been deomonstrated that high oxidant values

are due to motor vehicular emissions of NOx and HC because

NOx and HC are the principal reactants in the oxidant formation process

and they originate primarily from motor vehicle emissions and

The highest oxidant values are recorded in_ effect areas that receive air

from source areas where motor vehicles are clearly identified as the

dominant source of NOx and HC

243

Future Control Strategy

The APCD strategy for achieving and maintaining the oxidant air quality

standard is based upon the fact that high oxidant values are due to motor ve-

hicle emissions of hydrocarlxms arrl nitrogen oxides This strategy is as follows

1 Both Hydrocarbon and Nitrogen Oxides Emissions Must Be Considered To Achieve the Federal Oxidant Standard

There is wide agreement that NOx and HC are the principal reactants in

the oxidant formation process and that vehicular emissions are a major source

of NOx HC and CO

2 Effective Regulation of Atmospheric Concentrations of Both HC and NOx and of the Ratio Between Them is necessary for Attainment of the Federal Air Quality Standard for Oxidant

Basmiddoted on the abundance middotof available experimental evidence it is our firm

position that the most rational approach to solving the photochemical oxidant smog

problem in the South Coast Air Basin (SCAB) is to control the quantities of emissions

from motor vehicles of both smog precursors--Hcmiddot and NOx--their resulting atmosshy

pheric concentrations and the ratios between both contaminants which will result

from these controls

We arc also convinced that the oxidant and nitrogen dioxide air quality stanshy

dards can and will be met not by 1975 or 1977 but by the early 1980 s if the emisshy

sion control program as originally outlined by Ca~ifornia or a slight modification

of it proposed by the District is followed and enforced This should also provide

for continued compliance with these air quality standards at least through 1990

244

It will also allow time for a reappraisal in about 1978 of the whole situation relative

to the ultimate emission standards required and the best approach to their impleshy

mentation

Calculation of the degree of control necessary to attain the air quality

~ standards for oxidant and nitrogen dioxide involves indirect complex methods 1

aimed at determ_ining the degree of control of the primary contaminants directly

emitted by automobiles

The following evidence supports our proposed solution to the problem in

terms of both the atmospheric concentrations of the oxidant precursors NOx

and HC the ratio between them as reflected in their exhaust emission standards

and the resulting atmospheric concentrations of oxidant which comply with the air

quality standards

Chamber Results and Projections to the Atmosphere

The importance of environmental chamberwork cannot be minimized the

j need for and direction of the whole emission control program was based initially

j on the results of chamber experiments In order to understand the importance to

air quality of achieving both the correct low quantities of emissions and the right

ratio we can present several graphic portrayals of analyses of experimental labshy

oratory work together with their relationship to past present and future air quality

in terms of both morning primary reactant concentrations during the morning

traffic peak and the equivalent emissions which would produce them

245

Figure 7 shows maximum ozone levels that were obtained by irradiating

varying amounts of auto exhaust hydrocarbons and oxides of nitrogen in an environshy

mental chamber The corresponding ozone levels then can be found for any comshy

bination of BC and NOx concentrations Thus high ozone is produced with high

emissions of both hydrocarbons and oxides of nitrogen and low oxidant is formed with

low emissions However either low NOx or low HC emissions11 can also produce

low oxidant--graphic and clear evidence of the importance of the NOxHC ratio in

ozone formation Furthermore each and every possible combination of values for

NOx and HC has then a corresponding characteristic maximum chamber ozone

concentration

Using this graph we can estimate what ozone levels would result if certain

atmospheric mixtures of NOx and HC could be injected into the chamber and

irradiated Such estimates were made for 1960 and 1965 using atmospheric data

rlThe points labeles 1960 and 65 show the location of the highest levels of both

HC and NOx found in the air in those years in Downtown Los Angeles (OOLA) area

during the 6-9 AM traffic peak

It has been demonstrated by use of CO and NOx data and CONOx ratios

hnw well the characteristics of vehicle emissions are reflected in the atmosphere

We know what emissions from the average vehicle were then in 1960-1965 both

for HC and NOx so that we can mathematically relate emissions to atmospheric

concentrations for those years and so for future years also knowing or calculating

only what the characteristic emissions will be from the average vehicle

246

The NOx concentrations stayed about the same from 1960 through 1965 because

average vehicle emissions of that contaminant did not change during that time

Mobile source emissions can be shown to have contributed essentially all of this obshy

served result However blow by controls did reduce emissions of HC and the

concentrations dropped accordingly In 1965 the last year before exhaust controls

the point 65 indicates where we were then in terms of maximum ozone formation

to be expected in a chamber with the highest HC and NO concentrations found in the X

air that year Levels of ozone actually measured in the atmosphere however

are higher than those shown on the graph for high NOx and I-IC concentrations for

those years up to the present

The strategy to meet the oxidant standard is obvious--get atmospheric NOx

and HC concentrations out of the area on the chart that produces high ozone levels

and put them in tie areas with the lowest levels This can only be done by implementshy

ing appropriate emission standards

As can be seen that did not happen between 1965 and 1970 because manufacshy

turers used controls on new cars in California which while causing a decrease in

BC (and CO) allowed a large increase in NOx emissions Thus the path line of

the atmosphere on the chart goes up from 65 and diagonally to the left passing

through an area of higher ozone levels The atmospheric concentrations of oxidant

predictably increased during the years 1967 and 1968 By 1970 they dropped to lower

levels - -back to about the same as in 1965- -exactly as predicted by the model The

app14oximate location of the point for 1970 (70) was both predicted on the basis of

247

the mathematical model and confirmed by atm-ospheric measurements of

[)owntown Los Angeles morning summertime NOx and calculated HC values

Again it should be pointed out that those points show the highest possible

concentrations of NOx and HC Years with less restrictive weather conditions

(for accumulating high primary contaminant levels) would cause lower measured

maximum NOx and HC levels but the calculations would still yield the points

shown Thus we are taking the most pessimistic view

Future Projections

In 1973 we were at about the point labeled 73 and ozone levels were beginshy

ning to drop as expected middot It should be emphasized that ozone values plotted on

thi$ graph are for the chamber only- -not the atmosphere The future path the

points 7 4 and on to 90 represents our estimate of future atmospheric levels of

NO and BC expected if the exhaust emission standards are just met While that X -

is optimistic it is all we really can do since performance of future vehicle models

is unknown We will achieve maximum ozone levels at or below the standard by

about 1980-1985 This will only be true however if cars in compliance with the

California interim standards for HC and NOx continue to be added to the vehicle

population at the normal rate These standards provide the optimum ratio of NO X

to HC necessary to provide the nitric oxide (NO) needed for the reaction that re-

moves from the air both oxidant formed photochemically and oxidant which occurs

as natural background which alone may cause the standard to be exceeded This

ratio is about 112 or 2 parts NOx to 1 part HC

248

The optimum NOxHC ratio is a key element in the APCD strategy but will

require a finite time for its attainment Replacement of older cars by newer ones

equipped to meet the most stringent standards is the only reasonable mechanism

which can change it VMT reduction proposed as a prime strategy by EPA cannot

change this crl(ical ratio which is a basic characteristic of the population at any

given time

Validation of the Districts Control Strategy

Figure 8 compares (1) future chamber oxidant levels based upon the

future maximum concentrations of HC and NOx we expect each year with the

California control program (2) calculated atmospheric concentrations using ~ I

our chamber-to-atmasphere empirical translation and (3) actual measured atmos-f 1l pheric oxidant maxima This clearly sets forth the relationship among these three

factors

The chamber concentrations (lower curve) middotare the lowest values shown

The actual atmospheric data (points connected by heavy dotted and solid lines)

vary considerably from year to year partly because of the vagaries of the weather

In all cases the atmospheric oxidant values are higher than the chamber values

because of the addition of vehicle emissions as the air parcel travels from source

to receptor areas The calculated atmospheric data (thin dashed and solid curves)

are shown to be the highest generally exceeding or equalling the actual measured

data and of course always exceeding the chamber data Thus the model paints

the most pessimistic picture possible It can be seen that by about 19801 1985 atmos -

pheric levels should be at or below the Federal air quality standard of 0 08 ppm oxidant

249

3 Motor Vehicle Exhaust Control is the Only Requirement for Achieving the Oxidant Standard by 1980

We can show that the existing motor vehicle control program has resulted

in a significant reduction of oxidant concentrations in the air

The foregoing material explained the relationship between vehicula~ emis -

sions in source areas and the high oxidant levels measured in effect areas This

relationship is exemplified by the downward trend of oxidant levels in the atmosshy

phere and by the similar year-by-year trends of NO and HC emissions from the X

average motor vehicle A projection of these vehicle emissions factors shows that

the associated maximum oxidant level in the atmosphere will meet the oxidant standard

by about 1980-1985

Figure 9 compares by year the number of days that the oxidant air quality

standard was exceeded in three separate areas with the average NO and HC emissions X

per vehicle mile To comply with the air quality regulations the number of days that

this standard is exceeded must be reduced to one per year

The lines plotted on Figure 9 show that a definite relationship exists between

the emissions from the average motor vehicle and the number of days each year that

the oxidant concentration in the air exceeds the clean air standard

The oxidant trendlines for downtown Los Angeles Pasadena arrl Azusa are

all downward and the slopes are about the same This similarity is logical because

the process that results in the suppression of oxidant accumulation simply has been

displaced from one area to another This was a unique one time situation because

of the increase in NOx between 1966 and 1971 After 1971 all areas are down Thus

l

250

the same conclusion is reached that the oxidantstandard will be met in the 1980s

I whether air quality data or vehicle emissions trends are projected middot~ Ul-

This outlook is based on the APCD s belief that future growth in both the

Los Angeles area and SCAB will not create any locality with a traffic density greater

than any traffic density in the area to date For the past 25 years the area around

downtown Los Angeles has been the area of maximum traffic density and therefore

the emissions source area responsible for the maximum effect area measurements

It is assumed that the traffic density in any future source area will be no

greater than the traffic density in downtown Los Angeles Thus since the

vehicular emissions control program will achieve and maintain the air quality

standards in areas affected by vehicular emissions from downtown Los Angeles it

will also achieve and maintain them for any area of SCAB

Summary Conclusions and Recommendations

In conclusion we have shown that a source and effect area analysis of emisshy

sions and resulting oxidant is a more reasonable and accurate representation of

the Los Angeles area for air quality analysis than gross integration metho9s such

as the big box technique It has been shown that motor vehicles are the major and

almost sole contributor to the primary HC and NOx emissions in the downtown source

area which results in the high oxidant levels in the San Gabriel Valley in fact the

highest in SCAB An air quality model and vehicle emissions control strategy has

been suggested to meet the oxidant standard by mid-1980 s

251

We have shown that

bull Only by adjusting the ratio of NOxHC in the motor vehicle emissions to

permit accumulation of sufficient atmospheric NO to sea venge the normal

atmospheric background oxidant can the standard be attained

bull The APCD strategy which provides for implementation of the present

California interim emissions standards for NOx HC and CO for new

motor vehicles in California beginning with the 1975 model vehicles will

result in compliance with the CO N02 and oxidant air quality standards

by the mid 1980 s and will maintain this compliance until 1990 and

possibly longer

bull The effectiveness of the present California motor vehicle control program

is easily demonstrable using air quality data from several areas in Los

Angeles County 1960-1973

bull To assure achievement and maintenance of the air quality goals as now preshy

dicted there must be periodic assessments of the effectiveness of the

motor vehicle control program followed by corrective actions if necessary

What has been accomplished thus far is significant but much more remains

to be done so that the best possible representation of emissions and resulting air

quality may be available for use in this air basin A much better emission inventory

defining the spatial and temporal distribution of both mobile and stationary sources

is needed Better statbnary source information is needed to evaluate the local

effects of these emissions Further detailed studies are needed to establish the

252

true relationship between emissions data from vehicle test cycles and the actual

operation of vehicles neither the 7-mode nor the CVS procedure provides a true

representation of actual vehicle operation Further tracer studies to assess the

transport and dilution of mobile and stationary source emissions from selected

source areas are also needed

253

1111

IUD

a CC I w gt-

1111

1UO

IUD

I 990

IDJO

1180

1111

IUO

FIGURE I

HYDROCARBONS

STATIONARY SOURCES MOTOR VEHICLES

- --

8 12 II 20 742 2l IS 12 I 4

HUNDREDS

HYDROCARBON EMISSIONS STATIONARY SOURCES IN

OXIDES OF

0

OF TONSDAY

FROM MOTOO VEHICLES AND LOS ANGELES COUNTY

NITROGEN

STATIONARY SOURCES

MOTOR VEHICLES

011111111111111111110111bull1111111

IIIIIIHIIIIIIIIIHIUII

llillL Its rd

l1uu~111111u1111111

2 I O 1 J 3

HUND REDS OF TONSDAY

OXIDES OF NITROGEN EMISSIONS FROM MOTOR VEHICLES ANO STATIONARY SOURCES IN LOS ANGELES COUNTY

illl~ -~--~ i~-=i _J~l ~--~ bull_~L- I ~~~-~~--Z ~

6

6S-66 ox

ICS ~A~1 M

i ssmuwmmgt

bullI

e COROyent_

64 ~ IDB RIVERS~

ORAJfD

-

t t 10 miles

bullmiddotsame Avg Cone Both Years

Pigare 2

YEAR OP HIGHEST OXlDANI CONCENTRATIONS

Highest Average of Daily -Maiimum One-Hour Concentrations

During July August amp September 1963-1972

bullLj

I

64

70 s11 3RlU)U0

70

--__ 69bull

N V +=

middot Source Air Resources Board

-200o

t t 10 adlea

tDS ampIJtsect

-1~

-1611ASampXllmiddot bull - bull -z----~------

I ldmmprwJ

IIVERSIDI

~ - 70

OampY -1 U 70 bull L

I

N V1 V

middot-i___

-----------------------------------------------------------i----------------------------

Figure 3

CHANGE OP OXIDANT CONCENTRATIONS

Percent Change from the Highest Three-Year Average to the 1970-72 Average

Of Daily Maximum One-Hour Con~entrationa for JulY August amp September

Source Air Resources Board

256

FIGURE 4 TYPICAL FLOW OF POLLUTED Am PARCEIS CIUGINATING AT DIFFERENT LOCATIONS IN THE LOS ARE~S BASIN - STARTIOO 0900 PST

l I

OAT

TRAJECTORY SUWMATIOl4

----- SMOG ~AVS

I

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullNONbullSlfOG DAYS

ISTARTING Tl~ cgxpsy

~ HAW

(CA

257

FiGURE 5 ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AND OXIDANT IN DOWlflC1N LOS AIDELES (SOURCE AREA) AND PASADENA (EFFECT AREA) 1

1960-1972

LO CARBON MONOXIDE

30

Pasadena

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullbullbullbullbull Downtown Los Angeles

20

10

o_______________________________

OXIDANT

)

2 Down~ Los Angeles

1

o________________________ 1960 1962 196L 1966 1968 1970 1972

YEAR

bullbullbullbullbull

bullbullbullbullbullbullbull

258

FIGURE 6 COMPARISON 01 CALCULATED AND MEASURED ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AN1) OXIDES OF NITROOEN IN DCMNTOWN IDS AIJELES

196o-1972

CARBON MONOXIDE

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ~ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot _-- ---_ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ----middotmiddot-bullw-_~ ---bullbullbull

10

o_______________1111111_____

OXIDES OF NITROGEN25

20

15 bullbullbullbullbullmiddotmiddotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~

1-i 10 middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ---

oS o_______________________

RATIO CONOx

40

50

0 +raquo Cd

p 30

~ 20

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot bullbullbullbullbull middotmiddotmiddotmiddotmiddot-shybullbullbullbullbull 0 u

bullbullbullbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot 10

0 j

ilI 196o 1964 1968 1970 1972 I

YEAR

Measured~D-owntown Los Angeles (90th percentile ofmiddot daily] instantaneous maxima)

Calculated - Aver~ge vehicle emissions - Present control program

259

FIGURE 7

25

t i5

flJ

~ on ~ ~ Q) bO 100 Jo

+gt on z

o5

EFFECT OF CALIFORNIA 1 s AUTO EXHAUST CONTROL ffiOORA M ON MAXIMUM CHAMBER OZONE CONCENTRATION

- PPM

357bullbull

r 76 bull

11 l

30

20

CHAMBER OZONE MAXIMUM

50

10

o___________111111111111______111111111111_____________

0 05 10 15 20 25

Hydrocarbons m-2 (LB-15) - PPM (as Hexane)middot

--

bull bull bull

r--=--~1 ~a==-~ - _~l ~ y--===-- ~~--~-- ~ r---~~

o

o8

~ I

~ 0 H 8 o6 I

c~ ~ 0 z 0 0

8

~ o+ A H gtlto-

02

middoto

Figure 8 Calculated t1ax1mum Levels Instantaneous and Hourly Average

of Atmospheric Oxidant Compared to Measured Los Angeles County Maxima-with Projections to 1990

(California Standards)

~ -Calculated Inst ax ~

f Calculate Max Hr Avg 03

_ bullbull _ _ - i bull

0 bullbull -l bullbull a0Ieasured Inst Lax o3 bull middotmiddotmiddot~bull 0bull _ ____ V ~ ea~ured ~ Hr Avr o3

~~ r---

~ ~ NB r~ima for 197 4 amiddots of 121074--- -_ Chamber Ozone F ~_ _~

- 1L_

~ Federal Primarfo Air ~uality Standard ~6- -UaximumT- our Avera~elr~ppm-------------- --~ ------- -~- -~-- ~

I I I I I I I I I I I I I I I I I N1 O

1960 6i 64 66 ~i middot-o 72 74 76 79 middotso middot92 84 bullg s9 9o

TBAR (end)

0

261 FIGURE -OMPARISON OF ATMOSPHERIC OXIDANT TRENDS WITH AVERAGE NCJx AND

HC EMISSIONS (Grams per Mile from Average Vehicle)

JOO Number of days state oxidant standara wds equalled or exceeded

--- Azusa __ Pasadena ________ Downtown Los Angeles

20

15 u

___ Hydroc_arbons Oxides of Nitrogenbullmiddotmiddotmiddotmiddotmiddotbullbullmiddot 1975 and later-assume middotcalifornia ARB standards

o_ ___________________________11111____

1965 1970 1975middot 198omiddot 198S 1990

145

I becomes important I will not speak to the medical issues because

am not qualified The evidence is that theuro~ platinum will be emitted in a

form which does not enter into biological cycles--but this is no assurance

that it couldnt later be transformed in such a form What is obviously

needed is a very careful monitoring program which hopefully was started

before the catalysts were put into service If it wasnt then it should

be started today

Problem Area Number Four NO control The big problem with NO X X

control is that nobody seems to know or to be willing to establish what

the emission control level should be It is essential that this be tied

down rapidly and that it be fixed for a reiatively long period of time

because the NO level is going to have a VE~ry important ef feet upon the X

development of advanced engine technology The 20 gm level has been

attained in California with some loss of fuel economy through the use of

EGR and it is not unreasonable in our estimation to go to 15 grams per

mile with very little loss in fuel economy To go to 04 gram per mile

with present technology requires the use of one of two catalytic systems

either the reduction catalyst in tandem with the oxidation catalyst or what

is known as the three-way catalyst Both of these systems require technoshy

logical gains The state of development appears to be roughly that of the

oxidation catalyst two years ago The auto industry will probably say

that it is not quite that advanced but that if it were required to go to

04 gram per mile in 1978 that it could be done With the catalyst systems

the fuel economy penalties would not be great in fact the improvement to

the engine which would be required to make the system work would again

probably even allow a slight improvement in fuel economy What the 04

gram per mile NO catalyst system would appear to do however is to X

146

eliminate the possibility of the introduction of stratified charge engines

both the CVCC and the direction injection system and also diesel engines

It is in the context of the advantages of these advanced engines to meet

emission standards with improved fuel economy that one should be very

cautious about the 04 grammile oxides of nitrogen standards for automoshy

biles My own personal opinion is that the number should not be that

stringent that a number of 1 or 15 gm is appropriate Such a level

would require advancements but would not incur great penalties

Other items which I view as problem areas are less technically

involved and therefore require fewer comments

bull Nonregulated pollutants--again thls is a matter of keeping track

of particulates aldehydes hydrocarbon composition to make

certain that important pollutants ire not being overlooked or

that emission control systems are not increasing the output of

some of these pollutants

bull Fuel economy The pressures of fuel economy are going to be used

as arguments against going ahead wlth emissions control Mostly

these two can be resolved simultaneously We should simply ask

the automobile industry to work harder at this

bull Final problem area New fuels Again it does not appear that

the introduction of new fuels will come about as an emissions

control approach but that they may be introduced because of the

changing fuel availability patterns and the energy crisis These

fuels should be watched carefully for their impact upon emissions

This does middotappear to be an area in which a great deal of study is

going on at the present time It is one problem area perhaps in

which the amount of wprk being done is adequate to the problem

which is involved

147

In sunnnary then the appraisal of the 1975 systems is that they are

a big advancement they will be a lot better than most of us thought and

that we should give the automobile industry credit for the job theyve

done in coming up with their emissions control systems

With that boost for the auto industry which Im very unaccustomed

to Ill entertain your questions

-------=-~ ~~~ U- ~a1

~_~a--~-~ -J~ ~ -~r- _ --=~-- -___ja--~ __1~~ ~-~----=

AIR

1-4 FUEL----1

I I ENGINE

I II

_________ EXHAUST SYSTEM I bull EXHAUST

I I I

+ MIXTURE CONTROL COMBUSTION MODIFICATION EXHAUST TREATMENT

FuelAir Metering Ignition Air Jnjection FuelAir Mixing Chamber Geometry Thermal Reactor Fuel Vaporization Spark Timing Oxidation Catalyst Mixture Distribution Staged Combustion Reduction Catalyst Fuel Characteristics Ex tern almiddot Combustion Three Way Catalyst Exhaust Gas Redrculation Particulate Trap

FIGURE 1 Approaches to the Control of Engine Emissions

~ i 00

149

TABLE I

Average Emissions of 1975 Certification Vehicles (As Corrected Using the 50000-Mile Deterioration Factor)

Emissions in gmi Fraction of Standard HC CO NO HC CO NO

Federal 1975 X X

AMC 065 67 25 043 045 080

Chrysler 074 77 25 049 051 082

Ford 081 92 24 054 061 078

GM 083 80 23 055 053 074

Weighted Average 080 82 24 053 055 076

California 1975

AMC 042 49 17 047 054 087

Chrysler 048 61 16 053 067 082

Ford 052 56 13 058 062 067

GM 065 55 16 0 72 061 082

Weighted Average 058 56 16 064 062 078

kWeighted average assumes the following market shares AMC 3 Chrysler 16 Ford 27 and GM 54

150

TABLE II

Total Number of Vehicles Certified for California 1975 Standard and the Number (and percentage) of These Able to Meet

Certain More Stringent Standards

Calif 1975 Federal 1977 Hypothesized Hypothes ized 099020 04J420 049020 093420

i ~

Manufacturer no () no () no () no ()

AMC 16 (100) 1 ( 6) ti ( 38) 3 (19)

Chrysler 21 (100) 2 ( 9) ( 33) 0 ( O)

Ford 26 (100) 4 (15) -middot ( 15) 5 (19)

l GM 46 (100) 1 ( 2) -1 ( 9) 5 (11)

Foreign 62 (100) 21 (34) 3H (61) 28 (45)

1J

f

-l

151

CURRENT STATUS OF ALTERNATIVE AUTOM)BIIE ENGINE TECHNOLCXY

by

Henry K Newhall Project Leader Fuels Division

Chevron Research CanpanyRicbmmd California

I

iH1middot

10 1ntroduction and General Background

I

11 General

The term stratified ct1arge englne has been used for many

years in connection with a variety of unconventional engine

combustion systems Common to nearly all such systems is

the combustion of fuel-air mixtures havlng a significant

gradation or stratification in fuel- concentration within the

engine combustion chamber Henee the term nstratifled charge

Historically the objective of stratified charge engine designs

has been to permit spark ignition engine operation with average

or overall fuel-air ratios lean beyond the ignition limits of

conventional combustion systems The advantages of this type

of operation will be enumerated shortly Attempts at achieving

this objective date back to the first or second decade of this

century 1

More recently the stratified charge engine has been recognized

as a potential means for control of vehicle pollutant emissions

with minimum loss of fuel economy As a consequence the

various stratified charge concepts have been the focus of

renewed interest

152

12 Advantages and Disadvantages of Lean Mixture Operation

Fuel-lean combustion as achieved in a number of the stratified

charge engine designs receiving current attention has both

advantages and disadvantages wnen considered from the comshy

bined standpoints of emissionsmiddot control vehicle performance

and fuel economy

Advantages of lean mixture operation include the following

Excess oxygen contained in lean mixture combustion

gases helps to promote complete oxidation of hydroshy

carbons (HG) and carbon monoxide (CO) both in the

engine cylinder and in the exhaust system

Lean mixture combustion results in reduced peak

engine cycle temperatures and can therefore yield

lowered nitrogen oxide (NOx) emissions

Thermodynamic properties of lean mixture combustion

products are favorable from the standpoint of engine

cycle thermal efficiency (reduced extent cf dissociashy

tion and higher effective specific heats ratio)

Lean mixture operation caG reduce or eliminate the

need for air throttling as a means of engine load

control The consequent reduction in pumping losses

can result in significantly improved part load fuel

economy

153

Disadvantages of lean mixture operation include the following

Relatively low combustion gas temperatures during

the engine cycle expansion and exhaust processes

are inherent i~ lean mixture operation As a conseshy

quence hydrocarbon oxidation reactions are retarded

and unburned hydrocarbon exhaust emissions can be

excessive

Engine modifications aimed at raising exhaust temperashy

i tures for improved HC emissions control (retarded middot~

ignition timing lowered compression ratlo protrtacted combustion) necessarily impair engine fuel economy1 I

1j bull If lean mixture operation is to be maintained over ~

the entire engine load range maximum power output t l and hence vehicle performance are significantly

impaired

Lean mixture exhaust gases are not amenable to treatshy

ment by existing reducing catalysts for NOx emissions

control

Lean mixture combustion if not carefully controlled

can result in formation of undesirable odorant

materials that appear ln significant concentrations

in the engine exhaust Diesel exhaust odor is typical

of this problem and is thought to derive from lean mixshy

ture regions of the combustion chamber

154

Measures required for control of NOx emissions

to low levels (as example EGR) can accentuate

the above HC and odorant emissions problems

Successful developmentmiddotor the several stratified charge

engine designs now receiving serious attention will depend

very much on the balance that can be achieved among the

foregoing favorable and unfavorable features of lean comshy

bustion This balance will of course depend ultimately on

the standards or goals that are set for emissions control

fuel economy vehicle performance and cost Of particular

importance are the relationships between three factors -

UBHC emissions NOx emissions and fuel economy

13 Stratified Charge Engine Concepts

Charge stratification permitting lean mixture operation has

been achieved in a number of ways using differing concepts

and design configurations

Irrespective of the means used for achieving charge stratifishy

cation two distinct types of combustion process can be idenshy

tified One approach involves ignition of a small and

localized quantity of flammable mixture which in turn serves

to ignite a much larger quantity of adjoining or sur~rounding

fuel-lean mixture - too lean for ignition under normal cirshy

cumstances Requisite m1xture stratification has been achieved

155

in several different ways rangiDg from use of fuel injection

djrectly into open combustion chambers to use of dual

combustion chambers divided physically into rich and lean

mixture regions Under most operating conditions the

overall or average fuel-air ratio is fuel-lean and the

advantages enumerated above for lean operation can be realized

A second approach involves timed staging of the combustion

process An initial rich mj_xture stage in which major comshy

bustion reactions are completed is followed by rapid mixing

of rich mixture combustion products with an excess of air

Mixing and the resultant temperature reduction can in

principle occur so rapidly that minimum opportunity for NO

formation exists and as a consequence NOx emissions are

low Sufficient excess air is made available to encourage

complete oxidation of hydrocarbons and CO in the engine

cylinder and exhaust system The staged combustion concept

has been specifically exploited 1n so-called divided-chamber

or large volume prechamber engine designs But lt will be

seen that staging is also inherent to some degree in other

types of stratified charge engines

The foregoing would indicate that stratified charge engines

can be categorized either as lean burn engines or staged

combustion engines In reality the division between conshy

cepts is not so clear cut Many engines encompass features

of both concepts

156

14 Scope of This Report

During the past several years a large number of engine designs

falling into the broad category of stratified charge engines

have been proposed Many of these have been evaluated by comshy

petent organizations and have been found lacking in one or a

number of important areas A much smaller number of stratified

charge engine designs have shown promise for improved emissions

control and fuel economy with acceptable performance durashy

bility and production feasibility These are currently

receiving intensive research andor development efforts by

major organizations - both domestic and foreign

The purpose of this report is not to enumerate and describe the

many variations of stratified charge engine design that have

been proposed in recent years Rather it is intended to focus

on those engines that are receiving serious development efforts

and for which a reasonably Jarge and sound body of experimental

data has evolved It is hoped that this approach will lead to

a reliable appraisal of the potential for stratified charge

engine systems

20 Open-Chamber Stratified Charge Engines

21 General

From the standpoint of mechanical design stratified charge

engines can be conveniently divided into two types open-chamber

and dual-chamber The open-chamber stratjfied charge engine

has a long history of research lnterest Those crigines

157

reaching the most advanced stages of development are probably

the Ford-programmed c~mbustion process (PROC0) 2 3 and Texacos

controlled combustion process (TCCS) 4 5 Both engines employ a

combination of inlet aar swirl and direct timed combustion

chamber fuel injection to achieve a local fuel-rich ignitable

mixture near the point of ignition _For both engines the overshy

all mixture ratio under most operating conditions is fuel lean

Aside from these general design features that are common to

the two engiries details of their respective engine_cycle proshy

cesses are quite different and these differences reflect

strongly in comparisons of engine performance and emissions

characteristics

22 The Ford PROCO Engin~

221 Description

The Ford PROCO engine is an outgrowth of a stratified charge

development program initiated by Ford in the late 1950s The

development objective at that time was an engine having dieselshy

like fuel economy but with performance noise levels and

driveability comparable to those of conventional engines In

the 1960s objectives were broadened to include exhaust

emissions control

A recent developmental version of the PROCO engine is shown in

Figure 2-1 Fuel is injected directly into the combustion chamber

during the compression stroke resulting in vaporjzation and

formation of a rich mixture cloud or kernel in the immediate

158

vicinity of the spark plug(s) A flame initiated in this rich

mixture region propagates outwardly to the increasingly fuelshy

lean regions of the chamber At the same time high air swirl

velocities resulting from special orientation of the air inlet

system help to promote rapid mixing of fuel-rich combustion

products with excess air contained in the lean region Air

swirl is augmented by the squ1sh action of the piston as it

approaches the combustion chamber roof at the end of the comshy

pression stroke The effect of rapid mixing can be viewed as

promoting a second stage of cori1bustion in which rlch mixture

zone products mix with air contained in lean regions Charge

stratification permits operation with very lean fuel-air mixshy

tures with attendent fuel economy and emissj_ons advantages In

addition charge stratification and direct fuel injection pershy

mit use of high compression ratios with gasolines of moderate

octane quality - again giving a substantial fuel economy

advantage

Present engine operation includes enrichment under maximum

power demand conditions to mixture ratios richer than

stoichiometric Performance therefore closely matches

that of conventionally powered vehicles

Nearly all PROCO development plans at the present time include

use of oxidizing catalysts for HC emissions control For a

given HC emissions standard oxidizing catalyts permit use

of leaner air-fuel ratios (lower exhaust temperatures)

1

l

159

together with fuel injection and ignition timing charactershy

istics optimized for improved fuel economy

222 Emissions and Fuel Economy

Figure 2-2 is a plot of PROCO vehicle fuel economy versus NOx

emissions based or1 the Federal CVS-CH test procedure Also

included are corresponding HC and CO emissions levels Only

the most recent test data have been plotted since these are

most representative of current program directions and also

reflect most accurately current emphasis on improved vehicle

fuel economy 6 7 For comparison purposes average fuel

economies for 1974 production vehicles weighing 4500 pounds

and 5000 pounds have been plotted~ (The CVS-C values

reported in Reference 8 have been adjusted by 5 to obtain

estimated CVS-CH values)

Data points to the left on Figure 2-2 at the o4 gmile

NOx level represent efforts to achieve statutory 1977

emissions levels 6 While the NOx target of o4 gmile was

met the requisite use of exhaust gas recirculation (EGR)

resulted in HC emissions above the statutory level

A redefined NOx target of 2 gn1ile has resulted in the recent

data points appearing in the upper right hand region of

Figure 2-2 7 The HC and CO emissions values listed are

without exhaust oxidation catalysts Assuming catalyst middotl

conversion efficiencies of 50-60 at the end of 50000 miles

of operation HC and CO levels will approach but not meet

160

statutory levels It is clear that excellent fuel economies

have been obtained at the indlcated levels of emissions

control - some 40 to 45 improved re1at1ve to 1974 produc-

tj_on vehicle averages for the same weight class

The cross-hatched horizontal band appearing across the upper

part of Figure 2-2 represents the reductions in NOx emissions

achieveble with use of EGR if HC emissions are unrestricted

The statutory 04 gmile level can apparently be achieved

with this engine with little or no loss of fuel economy but

with significant increases in HC emissions The HC increase

is ascribed to the quenching effect of EGR in lean-middotmixture

regions of the combustion chamber

223 Fuel Requirements

Current PROCO engines operated v1ith 11 1 compression ratio

yield a significant fuel economy advantage over conventional

production engines at current compression ratios According

to Ford engineers the PROCO engine at this compression

ratio j_s satisfied by typical fu1J-boi1ing commercial gasoshy

lines of 91 RON rating Conventional engines are limited to

compression ratios of about 81 and possibly less for

operation on similar fuels

Results of preliminary experiments indicate that the PROCO

engine may be less sensitive to fuel volatility than convenshy

tional engines - m1 important ff1ctor in flextb1 llty from the

standpoint of the fuel supplier

161

224 Present Status

Present development objectives are two-fold

Develop calibrations for alternate emissions target

levels carefully defining the fueleconofuy pbtenshy

tial associated with each level of emissions control

Convert engine and auxiliary systems to designs

feasible for high volume production

23 The Texaco TCCS Stratified Charge Engine

231 General Description

Like the Ford PROCO engine Texacos TCCS system involves_

coordinated air swirl and direct combustion chamber fuel

injection to achieve charge stratification Inlet portshy

induced cylinder air swirl rates typically approach ten times

the rotational engine speed A sectional view of the TCCS

combustion chamber is shown in Figure 2-3

Unlike the PROCO engine fuel injection in the TCCS engine

begins very late in the compression stroke - just before th~

desired time of ignition As shown in Figure 2-4 the first

portion of fuel injected is immediately swept by the swirling

air into the spark plug region where ignition occurs and a

flame front is established The continuing stream of injected

fuel mixes with swirling air and is swept into the flame

region In many respects the Texaco process resembles the

162

spray burning typical of dj_esel combustion ~r1th the difshy

ference that ignition is achieved by energy from an elec-

tric spark rather than by high compression temperatures

The Texaco engine like the diesel engine does not have a

significant fuel octane requirement Further use of positive

spark ignition obviates fuel I

cetane requirements character-

istic of diesel engines The resultant flexibility of the

TCCS engine regarding fuel requirements is a si~1ificant

attribute

In contrast to the TCCS system Fords PROCO system employs

relatively early injection vaporization and mixing of fuel

with air The combustion process more closely resembles the

premixed flame propagation typical of conventional gasoline

engines The PROCO engine therefore has a definite fuel

octane requirement and cannot be considered a multifuel

system

The TCCS engine operates with hi__gh compression ratios and

with little or no inlet air throttling except at idle conshy

ditions As a consequence fuel economy is excellent--both

at full load and under part load operating conditions

232 Exhaust Emissions and Fuel Economv

Low exhaust temperatures characteristlc of the TCCS system

have necessitated use of exhaust oxidation catalysts for

control of HC emissions to low lf~Vels A11 recent development

163

programs have therefore included use of exhaust oxidation

catalysts and most of the data reported here r~present tests

with catalysts installed or with engines tuned for use with

catalysts

Figures 2-5 and 2-6 present fuel economy data at several

exhaust emissions levels for two vehicles--a US Army M-151

vehicle with naturally aspirated 4-cylinder TCCS conversion

and a Plymouth Cricket with turbocharged 4-cylinder TCCS

engine 9 10 1urbocharging has been used to advantage to

increase maximum power output Also plotted in these figures

I are average fuel economies for 1974 production vehicles of

similar weight 8

I When optimized for maximum fuel economy the rrccs vehicles

can meet NOx levels of about 2 gmile It should be noted

that these are relatively lightueight vehicles and that

increasing vehicle weight to the 4000-5000 pound level could

result in significantly increased NOx emissions Figur~s 2-5

and 2-6 both show that engine modifications for reduced NOx

levels including retarded combustion timing EGR and increased

exhaust back pressure result in substantial fuel economy

penalties

For the naturally aspirated engine reducing NOx emissions

from the 2 gmile level to O l~ gmile incurred a fuel

economy penalty of 20 Reducing NOx from the tllrbocharged

164

engine from 15 gmile to 04 gmile gave a 25 fuel economy

penalty Fuel economies for both engines appear to decrease

uniformly as NOx emissions are lowered

For the current TCCS systems most of the fuel economy penalty

associated with emissions control can be ascribed to control

of NOx emissions although several of the measures used for

NOx control (retarded cornbusticn timing and increased exhaust

back pressure) also help to reduce HG emissions HC and CO

emissions ari effectively controlled with oxidation catalysts

resulting in relatively minor reductions in engine efficiency

233 TCCS Fuel Reauirements

The TCCS engine is unique among current stratified charge

systems in its multifuel capability Successful operation

with a nuraber of fuels ranging from gasoline to No 2 diesel

Table 2-I

Emissions and Fuel Economy of Turbocharged TCCS Engine-Powered Vehicle 1

Fuel

Emissions gMile 2 Fuel Economy

mng 2HC co NOx

Gasoline

JP-4

100-600

No 2 Diesel

033

026

014

027

104

109

072

J bull l ~

-

061

050

059

060

197

202

213

230

1M-151 vehicle 8 degrees coffibustion retard 16 light load EGR tw0 catalysts (Ref 10)

2 CVS-CH 2750 pounds tnert1a welght

165

l

has been demonstrated Table ~-I lists emissions levels and

fuel economies obtained with a turbocharged TCCS-powered

M-151 vehicle when operated on each of four different fuels 10

These fuels encompass wide ranges in gravity volatjlity

octane number and cetane leve 1 as middotshown in Table 2-II

Table 2-II

Fuel Specifications for TCCS Emissions Tests (Reference 10)

Gravity 0 API Sulfur

OFDistillation~

Gasolj_ne 100-600 JP-4 No 2

Diesel

88 -

86 124 233 342 388

0024 912

-

486 012

110 170 358 544 615

0002 57 356

541 0020

136 230 314 459 505

-middot --

369 0065

390 435 508 562 594

--

lta 9

IBP 10 50 90 EP

TEL gGal Research Octane Cetane No

Generally the emissions levels were little affected by the

wide variations in fuel properties Vehicle fuel economy

varied in proportion to fuel energy content

As stated above the TCCS engine is unique in its multifuel

capability The results of Tables 2-I and 2-II demonshy

strate that the engine has neither 8ign1ficant fuel octane

nor cetane requirements and further that it can tolerate

166

wide variations j_n fuel volati1tty rhe flexibility offered

by this type of system could be of major importance in

future years

234 Durability Performance Production Readiness

Emissions control system durability has been demonstrated by

mileage accumulation tests Ignltion system service is more

severe than for conventional engines due to heterogeneity of

the fuel-air mixture and also to the high compression ratios

involved The ignition system has been the subject of

intensive development and significant progress in system

reliability has been made

A preproduction prototype engine employing the TCCS process is

now being developed by the Hercules Division of White Motors

Corporation under contract to the US Army Tank Automotive

Command Southwest Research Inr)titute will conduct reliability

tests on the White-developed enGines when installed in Military

vehlcles

30 Small Volume Prechambcr Eng1nes (3-Valve Prechamber Engines Jet Ignition Engines Torch Ignition Engines)

31 General

A number of designs achieve charge stratification through

division of the combustion region into two adjacent chambers

The emissions reduction potentiampl for two types of dualshy

chamber engines has been demonstrated F1 rst ~ j n B desJgn

trad1t1on~JJy caJJld the nrreebrnber engine a 2m211 auxil1ary

167

or ignition chamber equipped w1th a spark plug communicates

with the much larger main combustion chamber located in the

space above the piston (Figure 3-1) The prechamber which

typically contains 5-15 of the total combustion volume

is supplied with a small quantity of fuel-rich ignitable

fuel-air mixture while a large quantity of very lean and

normally unignitable mixture is applied to the main chamber

above the piston Expansion of high temperature flame

products from the prechamber leads to ignition and burning

of the lean maj_n chamber fuel-a_r charge Ignitionmiddot and

combustion in the lean main chamber region are promoted both

by the high temperatures of prechamber gases and bythe

mixing that accompanies the jet-like motion of prechamber

products into the main chamber

I jl

I i j

I

Operation with lean overall mixtures tends to limit peak comshy

bustion temperatures thus minimizing the formation of nitric

oxide Further lean mixture combustion products contain

sufficient oxygen for complete oxidation of HC and CO in the

engine cylinder and exhaust system

It should be reemphasized here that a iraditional problem

with lean mixture engines has been low exhaust temperatures

which tend to quench HC oxidation reactions leading to

excessive emissions

Control of HC emissions to low levels requires a retarded or

slowly developing combustion process The consequent extenshy

sion of heat release j nto 1ate porttt)ns of the engtne cycle

168

tends to raise exhaust gas temperatures thus promoting

complete oxidation of hydrocarbons and carbon monoxide

32 Historical Background and Current Status

321 Early Developm9nt Objectives and Engine Def igns

The prechamber stratified charge engine has existed in various

forms for many years Early work by Ricardo 1 indicated that

the engine could perform very efficiently within a limited

range of carefully controlled operating conditions Both

fuel-injected and carbureted prechambcr engines have been

built A fuel-injected design Lnittally conceived by

Brodersen 11 was the subject of extensive study at the

University of Rochester for nearly a decade 12 13 Unforshy

tunately the University of Rochester work was undertaken prior

to widespread recognition of the automobile emissions problem

and as a consequence emission characteristics of the

Brodersen engine were not determined Another prechamber

engine receiving attention in the early 1960s is that conshy

ceived by R M Heintz 14 bull The objectives of this design

were reduced HC emissions incr0ased fuel economy and more

flexible fuel requirements

Experiments with a prechamber engine design called the torch

ignition enginen were reported n the USSR by Nilov 15

and later by Kerimov and Mekhtier 16 This designation

refers to the torchlike jet of hot comhust1on gases issuing

169

from the precombustion chamber upon j_gnj_ tion In a recent

publication 17 Varshaoski et al have presented emissions

data obtained with a torch ignition engine These data show

significant pollutant reductions relative to conventional

engines however their interpretation in terms of requireshy

ments based on the Federal emissions test procedure is not

clear

l

3 2 2 Current DeveloJ)ments

A carbureted middotthree-valve prechamber engine the Honda CVCC

system has received considerable recent attention as a

potential low emissions power plant 18 This system is

illustrated in Figure 3-2 Hondas current design employs a

conventional engine block and piston assembly Only_ the

cylinder head and fuel inlet system differ from current

automotive practice Each cylinder is equipped with a small

precombustion chamber communicating by means of an orifice

with the main combustion chambe situated above the piston lj

ij_ A small inlet valve is located in each precharnber Larger

inlet and exhaust valves typical of conventlonal automotive

practice are located in the main combustion chamber Proper

proportioning of fuel-air mixture between prechamber and

main chamber is achieved by a combination of throttle conshy

trol and appropriate inlet valve timing A relatively slow

and uniform burning process gjvjng rise to elevated combusshy

tion temperatures late in the expansion stroke and during

the exhaust procezs is achieved H1 gh tewperaturr--s in thin

part of the engine cycle ar-e necessary to promote complete

170

oxidation of HC and CO It si1ould be no~ed that these

elevated exhaust temperatures are necessarily obtained at

the expense of a fuel economy penalty

To reduce HC and CO emissions to required levels it has been

necessary for Honda to employ specially designed inlet and

exhaust systems Supply of extremely rich fuel-air mixtures

to the precombustion chambers requires extensive inlet manifold

heating to provide adequate fuel vaporization This is accomshy

plished with a heat exchange system between inlet and exhaust

streams

To promote maximum oxidation of HC and CO in the lean mixture

CVCC engine exhaust gases it has been necessary to conserve

as much exhaust heat as possible and also to increase exhaust

manifold residence time This has been done by using a relashy

tively large exhaust manifold fitted with an internal heat

shield or liner to minimize heat losses In additj_on the

exhaust ports are equipped with thin metallic liners to

minimize loss of heat from exhaust gases to the cylinder

head casting

Engines similar in concept to the Honda CVCC system are under

development by other companies including Ttyota and Nissan

in Japan and General Motors and Fo~d in the United States

Honda presently markets a CVCC-powered vehicle tn tTapan and

plans US introduction in 1975 Othe~ manufactur~rs

includlnr General Motors and Forgtd 1n thr U S havf~ stated

171

that CVCC-type engines could be manufactured for use in limited

numbers of vehicles by as early as 1977 or 1978

33 Emissions and Fuel Economywith CVCC-Type Engines

331 Recent Emissions Test Results

Results of emissions tests with the Honda engine have been very

promising The emissions levels shown in Table 3-I are typical

and demonstate that the Honda engine can meet statutory 1975-1976

HC and CO stindards and can approach the statutory 1976 NOx

standard 19 Of particular importance durability of this

system appears excellent as evidenced by the high mileage

emissions levels reported in Table 3-I Any deterioration of

l emissions after 50000 miles of engine operation was slight

and apparently insignificant

I Table 3-I

Honda Compound Vortex-Controlled Combustion-Powered Vehicle 1 Emissions

Fuel Economy

Emissions 2 mpg gMile 1972

HC 1975 FTP FTPco NOv

210 50000-Mile Car+ No 2034 Low Mileage Car 3 No 3652 018 212 221089

024 065 198 1976 Standards

213175 20o41 34 - -04o411977 Standards 34 - -

1Honda Civic vehicles 2 1975 CVS C-H procedure with 2000-lb inertia weight3Average of five tests aAverage of four tests

172

Recently the EPA has tested a larger vehicle conve~ted to the

Honda system 20 This vehicle a 1973 Chevrolet Impala with

a 350-CID V-8 engine was equipped with cylinder heads and

induction system built by Honda The vehicle met the present

1976 interim Federal emissions standards though NOx levels

were substantially higher than for the much lighter weight

Honda Civic vehicles

Results of development tests conducted by General Motors are

shown in Table 3-II 21 These tests involved a 5000-pound

Chevrolet Impala with stratified charge engine conversion

HC and CO emissions were below 1977 statutory limits while

NOx emissions ranged from 15 to 2 gmile Average CVS-CH

fuel ec9nomy was 112 miles per gallon

Table 3-II

Emissions and Fuel Economy for Chevrolet Impala Strmiddotatified

Charge Engine Conversion (Ref 21)

Test

Exhaust Emlssions

gMile 1 Fuel

Economy mpgHC co NOx

1 2 3 4 5

Average

020 026 020 029 0 18

023

25 29 31 32 28

29

17 15 19 1 6 19

17

108 117 114 109 111

112

1cvs-CH 5000-lb inertia weight

173

I

332 HC Control Has a Significant Impact on Fuel Economy

In Figure 3-3 fuel economy data for several levels of hydroshy

carbon emissions from QVCC-type stratified charge engines

are plotted 22 23 ~ 24 At the 1 gmile HC level stratified

charge engine fuel economy appears better than the average

fuel economy for 1973-74 production vehicles of equivalent

weight Reduction of HC emissions below the 1-gram level

necessitates lowered compression ratios andor retarded

ignition timing with a consequent loss of efficiencymiddot For

the light-weight (2000-pound) vehicles the O~ gmile IIC

emissions standard can be met with a fuel economy of 25 mpg

a level approximately equal to the average of 1973 producshy

tion vehicles in this weight class 8 For heavier cars the

HC emissions versus fuel economy trade-off appears less

favorable A fuel economy penalty of 10 relative to 1974

production vehicles in the 2750-pound weight class is

required to meet the statutory 04 gmile HC level

333 Effect of NOx Emissions Control on Fuel Economy

Data showing the effect of NOx emissions control appear in

Figure 3-~ 22 These data are based on modifications of a Honda

CVCC-powered Civic vehicle (2000-pound test weight) to meet

increasingly stringent NOx standards ranging from 12 gmile

to as low as 03 gmile For all tests HC and CO emissions

are within the statutory 1977 standards

NOx control as shown in Figure 3-4 has been effected by use

of exhaust gas recirculation 1n comb1nation w1th retarded

174

ignj_tion timing It is clear that control of rmx emissions

to levels below l to 1 5 gmile results in stgnificant fuel

economy penalties The penalty increases uniformly as NOx

emissions are reduced ~nd appears to be 25 or more as the

04 gmile NOx level is approached

It should be emphasized that the data of Fisure 3-4 apply

specifically to a 2000-pound vehicle With increased vehicle

weight NOx emissions control becomes more difficult and the

fuel economy penalty more severe The effect of vehicle

weight on NOx emissions is apparent when comparing the data

of Table 3-I for 2000-pound vehicles with that of Table 3-II

for a 5000-pound vehicle While HC and CO emissio~s for the

two vehicles are roughly comparable there is over a factor

of two difference in average NOx emissions

34 Fuel Requirements

To meet present and future US emissions control standards

compression ratio and maximum ignltion advance are limited

by HC emissions control rather than by the octane quality of

existing gasolines CVCC engines tuned to meet 1975 California

emissions standards appear to be easily satisfied with

presently available 91 RON commercial unleaded gasolines

CVCC engines are lead tolerant and have completed emissions

certification test programs using leaded gasolines However

with the low octane requirement of the CVCC engine as noted

above the economic benefits of lead antlknock compoundt ar-euromiddot

not realized

175

It is possible that fuel volatLLity characteristlcs may be of

importance in relation to vaporization within the high

temperature fuel-rich regions of the prechamber cup inlet

port and prechamber iQlet manifold However experimental

data on this question aomiddot not appear to be available at

present

~O Divided-Chamber Staged Combustion Engines (Large-Volume Prechamber Engines Fuel-Injected Blind Prechamber Engines)

41 General

Dual-chamber engines of a type often called divided-chamber

or large-volume prechamber engines employ a two-stage comshy

bustion process Here initial r~ich mixture combustion and

heat release (first stage of combustion) are followed by rapid

dilution of combustion products with relatively low temperature

air (second stage of combustion) The object of this engine

design is to effect the transitjon from overall rich combustion

products to overall lean products with sufficient speed that

time is not available for formation of significant quantities

of NO During the second low temperature lean stage of

combustion oxidation of HC and CO goes to completion

An experimental divided-chamber engine design that has been

built and tested is represented schematically in Figure ~-1 25 26

A dividing orifice (3) separates the primary combustion

chamber (1) from the secondary combustion chamber (2) which

includes the cylinder volume above the piston top A fuel

injector (4) supplies fuel to the primary chamber only

176

Injection timing is arranged such that fuel continuously

mixes with air entering the primary chamber during the

compression stroke At the end of compression as the

piston nears its top center position the primary chamber

contains an ignitable fuel-air mixture while the secondary

chamber adjacent to the piston top contains only air

Following ignition of the primary chamber mixture by a spark

plug (6) located near the dividing orifice high temperature

rich mixture combustion products expand rapidly into and mix

with the relatively cool air contained in the secondary

chamber The resulting dilution of combustion products with

attendant temperature reduction rapidly suppresses formation

of NO At the same time the presence of excess air in the

secondary chamber tends to promote complete oxidation of HC

and CO

42 Exhaust Emissions and Fuel Economy

Results of limited research conducted both by university and

industrial laboratories indicat~ that NOx reductions of as

much as 80-95 relative to conventional engines are possible

with the divided-chamber staged combustion process Typical

experimentally determined NOx emissions levels are presented

in Figure 4-2 27 Here NOx emissions for two different

divided-chamber configurations 8re compared with typical

emissions levels for conventional uncontrolled automobile

engines The volume ratio 8 appearing as a parameter in

Figure 4-2 represents the fraction of total combustion volume

contained in the primary chamber For a values approaching

I

i J_

177

1

05 or lower NOx emissions reach extremely low levels Howshy

ever maximum power output capability for a given engine size

decreases with decreasing 6 values Optimum primary chamber

volume must ultimately_represent a compromise between low

emissions levels and desired maximum power output

HC and particularly CO emissions from the divided-chamber

engine are substantially lower than eonventional engine

levels However further detailed work with combustion

chamber geometries and fuel injection systems will be necesshy

sary to fully evaluate the potential for reduction of these

emissions

i Recent tests by Ford Motor Company show that the large volume

prechamber engine may be capable of better HC emissions conshy

trol and fuel economy than their PROCO engine This is shown

by the laboratory engine test comparison of Table 4-I 19

Table 4-I

Single-Cylinder Low Emissions middot11 ~ _____En____g__~ne __middot _e_s_-_s_____

Engine

NO--X Reduction

Method

Em1ssions g1 hp-Hr

Fuel Economy

Lb1 hp-HrNOv HC- co

PROCO

Divided Chamber

PROCO

Divided Chamber

EGR

None

EGR

None

10 30

10 04

05 ~o

o J_o 75

130

25

l 1i bull 0

33

0377

0378

0383

0377

178

Fuel injection spray characteristics are critical to control

of HC emissions from this type of engine and Fords success

in this regard is probably due in part to use of the already

highly developed PROCO-gasoline injection system Figure 4-3

is a cutaway view of Fords adaptation of a 400-CID V-8 engine

to the divided-chamber system 2 e

Volkswagen (VW) has recently published results of a program

aimed at development of a large volume precharnber engine 29

In the Volkswagen adaptation the primary chamber which comshy

prises about 30 of the total clearance volume is fueled by a

direct timed injection system and auxiliary fuel for high

power output conditions is supplied to the cylinder region by

a carburetor

Table 4-II presents emissions data for both air-cooled and

water-cooled versions of VW s dtvided-middotchamber engine 3 0

Emissions levels while quite low do not meet the ultimate

1978 statutory US standards

179

Table 4-II

Volkswagen Jarge Volume _Jrechamber Er[ Lne Emissions

Exhaust Emissions

_ _gMile 1

___E_n_gi_n_e__t--H_C___c_o__N_O_x____E_ng__i_n_e_S_p_e_c_i_f_i_c_a_tmiddot_1_middoto_n_s__

20 50 09 841 compression ratio Air-Cooled 16-Liter

prechamber volume 28 of total clearance volume conventional exhaust manishyfold direct prechamber fuel injection

20-Liter 10 40 10 91 compression ratio Water-Cooled prechamber volume 28 of

total clearance volume simple exhaust manifold reactor direct prechamber fuel injection

1cvs c-H

Toyota also has experimented wlth ___a large volume prechamber

engine using direct prechamber fuel injection and has

reported emissions levels comparable to those of Table 4-II 31

43 Problem Areas

A number of major problems inherent in the large volume

prechamber engine remain to be 3olved I~ These problems include the following II

Fuel injection spray characteristics are critically

important to achieving acceptable HC emissions

The feasibility of producing asatisfactory injecshy

tion system hasnot been estab1ished

180

Combustion noise due to high turbulence levels and

hence high rates of heat release and pres[-ure rise

in the prechamber can be excessive It has been

shown that the-noise level can be modified through

careful chamber design and combustion event timing

If the engine is operated with prechamber fuel

injection as the sole fuel source maximum engine

power output is limited This might be overcome

by a~xiliary carburetion of the air inlet for maximum

power demand or possibly by turbocharging Either

approach adds to system complexity

The engine is charmiddotaeter1zed by low exhaust temperatures

typical of most lean mixture engines

References

1 Ricardo H R Recent Research Work on the Internal Combustion Engine 11 SAE Journal Vol 10 p 305-336 (1922)

2 Bishop I N and Simko A Society of Automotive Engineers Paper 680041 (1968)

3 Simko A Choma M A and Repco L L Society of Automotive Engineers Paper 720052 (1972)

4 Mitchell E Cobb JM and Frost R A Society of Automotive Engineers Paper 680042 (1968)

5 Mitchell E Alperstein M and Cobb JM Society of Automotive Engineers Paper 720051 (1972)

6 1975-77 Emission Control Program Status Report submitted to EPA by Ford Motor Company November 26 1973

181

if

7 consultant Report on Emissions Control of Engine Systems National Academy of Sciences Committee on Motor Vehicle Emissions Washington DC September 1974

8 Austin T C and Hellman K H Society of Automotive Engineers Paper 730790 (1973)

9 See Ref 7

10 Alperstein M Schafer G H and Villforth F J Iiil SAE Paper 740563 (1974)

11 US Patent No 2615437 and No 2690741 Method of Operating Internal Combustion Engines Neil O Broderson Rochester New York

12 Conta L~ D and Pandeli American Society of Mechanical Engineers Paper 59-SA-25 (1959)

13 Canta L D and Pandeli American Society of Mechanical Engineers Paper 60-WA-314 (1960)

14 US Patent No 2884913 0 Internal Combustion Engine R Mi Heintz i

15 Nilov N A Automobilnaya Promyshlennost No 8 (1958)

l 16 Kerimov N A and Metehtiev R I Automobilnoya Promyshlennost No 1 p8-11 (1967)

17 Varshaoski I L Konev B F and Klatskin V B Automobilnaya Promyshlennost No 4 (1970)

18 An Evaluation of Three Honda Compound Vortex Controlled Combustion (CVCC) Powered Vehicles Report B-11 issued by Test and Evaluation Branch Environmental Protection Agency December 1972

19 Automotive Spark Ignition Engine Emission Control Systems to Meet Requirements of the 1970 Clean Air Amendments report of the Emissions Control Systems Panel to the Committee on Motor Vehicle Emissions National Academy of Sciences May 1973

20 An Evaluation of a 300-CID Compound Vortex Controlled Combustion (CVCC) Powered Chevrolet Impala Report 74-13 DWP issued by Test and Evaluation Branch Environmental Protection Agency October 1973

21 See Ref 7

22 See Ref 7

23 See Ref 7

24 See Ref 7

182

25 Newhall H K and El-Messiri I A Combustion and Flame 14 p 155-158 (1970)

26 Newhall H K and El-Messiri I A Society of Automotive Engineers Transaction Ford 78 Paper 700491 (1970)

27 El-Messiri I A and Newhall H K Proc Intersociety Energy Conversion Engineering Conference p 63 (1971)

28 See Ref 7

29 Decker G and Brandstetter W MTZ Motortechnische Zeitschrift Vol 34 No 10 p 317-322 (1973)

30 See Ref 7

31 See Ref 7

183

Fig 2-1 FORD PROCO ENGINE

l

Ford Proco Engine Fuel Economy and Emissions _ 15 _ f--1

00 +

I ~ x X gt( X _ x A 7- ~ X x~ ~c - l4catalyst Feed u NOx vs ruel Econ with 1 C0-71 CJ) 14 x x Ynn H( RP c tr ir-t irm vltgtZ G I HC - C0-127 _ A txcessve c

13 Approx W EG R

~ C~~r 351 CID 5000 Lb Inertia Weight

Q 21 A L 0 u w II _j

LJ =gt LL

10

35i CD 4500 Lb Inertia Weight

~ 1974 Production Average Fuel Economy

4 soo _b r-r-r-----z~lt_~~---7--_~--r--1r-7-r1--~-rz7-w~~

150 0 0 Lb PU221ufrac122-1 I

LO 20 30

NOx EMISSIONS-GMSMILE (CVS-CH) Revised216174

0

HKN 71074

Fig 2-2

l

~___-~ ~--=---~ ~=---__---~1 f-=-----1__middot-_~J ~-----------1 ~bull-=-=- (-~-~ LJii-ZJj ~ ~~-~ ~~ -__c~~ 1--~~ ~----~--1 ---------s___-c--1 ~~~-~~~bull r~~-~--middot1 ____c__ J~ p- ~

Texaco TCCS Engine

Shrouded Intake Valve

~ Intakemiddot r~ )p__-- Fuel Nozzle Fuel Nozzte Port ~ -- -yen -_~

X f -J J ( ~1 I --- ~ f middotmiddotj_Ja 1(~-~_ frff 1-Cylinderv~ v_ r--L~ I (~~)J ~- Intake 1 - ------L- middotmiddot - middotmiddot -1 H0 ad middot --- - -- 1 Po rt I 1 I ~~ ) ~ ~ ~~~ -A- I ------

- I _ ---_ ~ P1ston-mgt-lt_ffrac12 T_77~~~--1 i- r_-~J N

- ~- i~-L - _ _ - IExhaust - - I ~ - 1-_ r- bullsect ~ ----lt_ ~ I PortJ~bJ lt 7A--7~ ~1 ~j --~ ~ yl ind er

-__~lli- klmiddot ~ro v_t_gt11J1bull Bti Or K__ - middot ~

I t--tL pgt-- Ultmiddot middot- - Spark Plugr- -1 --U2middot- ~-~

LHorizont al Projections of Nozzle and Spark Plug Centerlines

Fig 2-3 i--1 00 U1

---~---~-~ -------c- --~--- 7middot-r---c-- ~- -~~~==---~~~~~- srsr RZIIEF7 11t111-~-----==-----=-~--~-~~---c=rmiddot=

OPEN CHAMBER TYPE STRATI Fl ED CHARGE ENGINE i-shyCj

DIRECTIONAl~Fsw7 Q

NOZZLE P

I

~J~treg lt-_(__(lt-(11

c_-- _7- -

SPARK PLUG_ l 1__- -_ - l --_ ~ ----__ lt_ lt_ -- --

ltlt_I_--- _

~ gt - _____- -- --~ ~-l_- 1_~ -~- ~ ------

~~~ r_I FUEL SPRAY 2 FUEL-AIR MIXING ZONE ~- _ -------

FLAME FRONT AREA 4 COMBUSTION PRODUCTS

TCCS COMBUSTION SYSTEM

Fig 2-4

3

----==-----~ l~~----bulli r-~ ~-----=-- 1 ~~ ~ -~ ~~ ___-_=gt---l p--- --=-=-_-__71-~-~~ 1-0-- --=---=-- 4 L--_-_-~ P--- ~

25

-c u

f

Cl) 24 gt u _

tgt 23a ~

I

gt-~ 220 2 0 u w 21 _J

lJJ gt LL

2

Texaco TCCS Powered Cricket Vehicle

Max Econ Setting gt A L07 HC

141 CID JQf CR 084 CO 2500 Lb Inertia Wgt

50-so Retard_ 0_73 HC

12 co 051 HC ~ 061 HC

085COA 064CO Retard+ ESPRetard+

EGR

036 HC ~ 115 co Retard +ESP+ EGR

04 06 08 10 12 14 16 18 20 NOx EMISSIONS-GMSMILE (CVS-CH) HtltN1110114

I- 00 -JFig 2-5

-~ ~=- ~ - -i______c_J ~-====c= wr=- ~-~ p--w~~~ rr w -

25

-c u

I

(f)

gt u-lt a_

2

gt-I 20

~ 0 z 0 u LLI

_J

w tJ_

15

I- CJ) CJ)

Turbocharged Texaco TCCS Ml51 Vehicle

Max Econ Adjustment_ HC-3J catalyst Feed C0-70

141 CID 10~1 CR 2750 Inertia Weight 8deg Retard ~

~bull HC-3middot2 catalyst Feed ~~ _ C0-64

_ 5deg Retard HC-0 30 8degRetard LowEGV bullco-11 ~bull HC-3middot6 catalyst Feed WIW21

Med EGR C0-67 1974 Production 33 Average Fuel Economy ~

COmiddoti05 (2750Lb)

I

bull HC-035 co- 141 13deg Retard High EGR

04 10 20 NOx EMISSIONS -GMSMILE (CVS-CH) ~~ts~b~~~74

Fig 2-6

189

Fig 3-1

PRECHAMBER TYPE STRATIFIED CHARGE ENGINE

r Inlet

(Fuel-lean Mixture )

I 0 I

Spark -Prechamber (Fuel-rich mixture)

-Main Chamber

1] HON DA CVCC ENGINE CONCEPT

190

Fig 3-2 Honda CVCC Engine

28 -l u

1

UJ 26 -gt u-(9 CL 24 2-

f

gtshy0gt

22 z ~ _)

u w

20 _J

w ~ LL

18

J= ---- 4 --~~-_----a ~~ _-_bull --~~ 1~~1 ltiil~I ~ ~-r~ ~ -~ ~-~ ~J~-iii-1 ~~1 s _-_ __-

Fuel Economy vs HC Emissions for 3-Valve Prechamber Engines

e NOx-14 15 Liter

bull Honda CVCC 2000 LbsNOx - 12 A Datsun NVCCbull15 Liter

bull ~JOx -09 A 2500 Lbs J LL 1ter NOv -15

2750 Lbs -NOx -17

- I AiJOx -12

0 02 04 06 08 LO 0HYDROCARBON EMiSSlmiddotONS - Glv1 I MILE (CVS-CH) I-

Fig 3-3

J--1

1--Fuel Economy vs NOx Emissions IO N

-- for Honda CVCC Powered Vehiclesr 26 u

l VHc-023 U1 gt umiddot 24_-__

(_IJ o_

~ 22 l

gt-5~-0 z 20 C0-200 u A HC-033w I co -3o_j

_A HC-029w 18 J I C0-27 LL

_ HC-025

HC-017 co -2-3

C0-22

0 -- 02 04 06middot 08 10 12 NOx Ef11SSIONS -GlviS MILE (CVS-CH)

Fig 3-4 middot

I

I

i93

J J

Fig 4-1 Divided Chamber Engine

middot(4) Fuel Injector

1

f J

f ff

f

~ Ii

I f

i

I f ] [

~~

0 0 0 0

i ~ I

1jl

194

E Cl 0

C QJ

CJl 0 _

-1-

z

0

Vl (lJ

-0

X 0

-t-J

V1 ro c X

LLI

Fig ~-2

COMPARISON OF CONVENTIONAL AND DIVIDED COMBUSTION CHAMBER NOx EMISSIONS

5000 MBT Ignition Timing Wide Open Ttl rattle

4000 Conventional Charnber

3000

J = fraction of Total Combustion 2000 Volume in Primary Ct1arnber

Divided Chamber 13 = 0 85

1000

Divided Chamber fo = 0 52

05 06 0 7 08 09 10 11

O~erall Fuel-Air Equivalence Ratio

195

196

AIRBORNE SURVEYS IN URBAN AIR BASINS IMPLICATIONS FOR MODEL DEVELOPMENT

by

Donald L Blumenthal Manager of Program Development

Meteorology Research Inc Altadena California 91001

middotI would like to make several points today First ozonemiddotis basically

a regional long-range problem There is a lot of long range ozone transshy

port and this transport is a normal occurrence The second point is that

ozone is stable in the absence of scavengers Junge mentions in his book

that the residence time of ozone in the troposphere is on the order of a

month Third vertical variations in concentration and ventilation rate are i very important in modeling atmospheres such as Los Angeles Layers aloft

are ventilated down to the surface on occasion and surface pollutants are

ventilated up mountain slopes as Jim Edinger has pointed out before and

often ventilated out of the basin in upper winds Fourth the day to day

carry over of pollutants from one day to the next is a very important considshy

eration in the Los Angeles Basin Finally there is a definite background

level of ozone The geophysical literature says its about O 02 to O 03 ppm (

in various parts of the world Weve seen data varying from 003 to 005 ppm

The difference may be due to calibration differences In any case numbers

like 005 are pretty substantial background levels for ozone

I am going to illustrate the points listed above with some data from

Los Angeles Basin The data were collected during a two-year study funded

by the Air Resources Board some of the analyses were funded by EPA The

study examined the three dimensional distribution of pollutants in the Los

Angeles Basin using airborne sampling systems Coinvestigators on the

project were Dr Ted Smith and Warren White of Meteorology Research Inc (MRI)

197

The first slide shows one of the aircraft we used Its a Cessna 205

which had sampling inlets on the side of the aircraft Figure 2 shows the

instrument system on the inside of the aircraft We were measuring nitrogen

oxides ozone scattering coefficient with a nephelometer condensation nuclei

carbon monoxide and meteorological parameters such as temperature humidity

turbulance Altitude and position were also measured

Figure 4 shows that the typical sampling pattern was a series of spirals

from the top of the mixing layer over an airport virtually to ground level

then we would climb up to the next point on the route and spiral down again

We had three routes (A B C Figure 3) that we would fly We had two airshy

craft and we would fly two of these three routes three times a day any

given day that we could The day I will be talking about September 25~ 1973

we flew what was called the Riverside route (C) and the Los Angeles route

(A) The 25th of July 1973 you might remember was the day before the

federal office buildings were closed in the area here because of smog

Figure 5 shows the surface streamlines at 0300 Pacific Standard Time

about 4 oclock in the morning daylight time on July 25 This streamline

analysis points out the morning stagnation conditions which are a very normal

occurrence in the Los Angeles Basin You start out with very light winds

quite variable maybe a slight off shore flow early in the morning On this

particular day this kind of situation extended well into midday The sea

breeze did not really pick up until up around noon When you have this kind

of a situation and a low radiation inversion at night you have a

long period of accumulation of pollutants all over the Basin espt~cialJy

in the prime source area the southwest portion of the Basin

198

I

Figure 6 shows the streamline pattern at 1600--400 cclock in the

afternoon same day sea breezes develop and with them a transport pattern

that carries pollutants up to the northeast and out toward the eastern por-

tion of the Basin This is a very regular pattern which we see day after l middot

day On July 25 1973 it was a little bit exaggerated The sea breeze was

held off for awhile started a bit late and so there was a very long period

of accumulation in the southwest area and then transport across the Basin

Figure 7 is an average streamline pattern at 1600 PacHic Daylight Time

on low inversion days for August 1970 It is included to show that the pattern

shown before is very typical Flow starts in the western portion of the

Basin and goes right across to the eastern portion This is using surface

data There is a very high average wind velocity in Ontario about 13 m iles

per hour and 23 mph in Riverside This is the average for the whole month

of August at 1600 PDT on low inversion days There is a considerable amount

of transport across the Basin starting relatively slowly in the morning and

accelerating in the afternoon

Figure 8 shows a verticle cross section of the scattering coefficient

The darker areas indicate higher levels of particulates Scattering coefficshy

ient is inversely proportional to visibility In the crosshatched area

visibility is less than about 3 miles In plotting altitude versus distance

inland from the coast you have Santa Monica (SMO) on the coast El Monte (EMT)

Pomona (BRA) Rialto (RIA) Redlands (RED) The lower broken line is surface

ground level The heavy dashed line is the base of the subsidence inversion

that occurred on the two days during this episode The middle line is the

base of the marine inversion There is a large area over in the western

portion of the Basin where emissions accumulate for much of the day At

199

midday the sea breeze has just started ventilating the Santa Monica area

The layer between the inversions is a layer aloft which is fairly well separshy

ated from the surface layer Ozone concentrations for instance in the

layer aloft were on the order of 04 05 ppm using the ARB calibration

method Down in the surface layer they were quite a bit lower in the mornshy

ing due to scavenging

Figure 9 shows that by afternoon the sea breeze starts and you get

kind of a clean air front Sea breeze starts ventilating the whole Basin

the stuff that was over in the west is transported eastward and at approxishy

mately Brackett (BRA) at 1700 PDT there is a clean air front The high conshy

centrations that were over Los Angeles earlier are now centered near Upland

(CAB) The numbers shown over CAB are data taken from a vertical profile

spiral over Upland at about 1600 That turns out to be the time when there

was the worst ozone concentration of the day in the Basin and it did occur

at Upland It could well be a result of the very polluted mass from the

western Basin being transported over the Upland area The layer aloft has

been a bit undercut by the sea breeze and some of the polluted mass has been

around possibly as long as the night before There has been very little

transport in the area aloft ozone concentrations are still very high

Figure 10 shows a trajectory analysis of the air arriving at Upland at

1600 since that was the worst time of the day at Upland We developed a

trajectory envelope using surface wind data and winds aloft so the air

arriving at Upland at 1600 started out somewhere back within this envelope

for example at 1130 PDT We did not go earlier than 1130 because the winds

were pretty much light and variable before that The air that arrives at

Upland at 1600 has been over the western portion of the Basin for much of

200

the morning and q~ite a bit of the evening before Thus there is

a very long period of accumulation and then a transport a pulsing effect

where you have pollutants moved across the Basin

Figure 11 is an isopleth map of surface ozone concentrations Again all

data are corrected to agree with the ARB calibration method Again you can

see that for the hours between 1600 and 1700 using surface data the Upland

area has the highest surface ozone concentrations about 063 ppm The western

area has been well ventilated by the sea breezes and it is cleaned out

The transport is actually pretty much perpendicular to the isopleth line

just about like that

Figure 12 is a vertical profile taken over Upland Cable Airportat

roughly the time of maximum ozone concentration 1636 PDT We are plotting

pollutant concentration on the x-axis versus altitude in meters (since it was

done for an EPA report) Surface leveJ at Upland is a little over 400 meters

the Z line is ozone Ozone concentration within the surface mixing layer

is pegged on the instrument at somewhat above 05 ppm Above the surface

mixing layer it drops off considerably and eventually get down to background

The T line is temperature and you ean see the subsidence inversion

on this day is very nicely documented here and provides a very strong trap

in that area The B line is the scattering coefficient inversely proporshy

tional to visibility Within the surface mixing layer visibility is on the

order of 3 miles or less while up above the surface mixing layer just a few

hundred feet difference visibilities get up to 60 or 80 miles The X is

condensation nuclei the measure of the very fine particles below about 010

micron It is a measure of quite fresh emissions If you have a high condenshy

sation nuclei count there are very fresh combustion emissions If you have

I

201

an aged air mass the condensation nuclei coagulate and the count decreases

considerably You can see that there are still some fresh emissions within

this surface layer as well But up above the surface mixing layer all the

pollutant indicators decrease considerably

Figure 13 is the same type of vertical profile taken over El Monte

which is on the western side of the sea breeze front The sea breeze front

has passed El Monte at this time almost 1700 PDT and again there are

distinct differences between the mass below the mixing layer within the sea

breeze front (below 400 meters) the marine inversion (400 to 800 meters) and

the subsidence inversion The subsidence inversion occurs at about 800 meters

and there is an old layer of very polluted stuff aloft The surface concenshy

trations are lower because of the ventilation by the sea breeze Condensashy

tion nuclei count (X line) within the surface layer is quite high There

are still fresh emissions in the El Monte area The 11 Z line is ozone

about 02 ppm within the surface layer (200 m) but it is 05 ppm up above

the surface mixing layer The scattering coefficient (B line) is very

similar it is lower at the surface and increases to a visibility equivalent

of less than 3 miles above the surface mixing layer The condensation nuclei

count is high in the lower portion of this (eg at 600 m) hut decreases conshy

siderably above This portion of the upper layer (600 m) has been around

at least all morning and condensation nuclei have been scattered from the

area The portion of the upper layer below 600 m has probably just recently

been undercut by the sea breeze and there are still some condensation nuclei

left in it

Figure 14 illustrates a different method of looking at the flushing

problems in the Basin We have tried to develop an objective criteria based

on ground level ozone to show the cleansing of the basin using the time of

202

arrival of clean air We determine the time when the ozone concentrations

drop by a factor of two at any given point The 1600 line means that between

1500 and 1700 the ozone concentration at that point dropped a factor of two

This sort of isopleth chart of when the clean air arrives agrees quite well

with the trajectory analyses although the numbers are a little bit behind

the trajectory analyses for the polluted air Figure 14 again shows the

transport process that takes place across the Basin which is ventilated from

west to east At 1900 some of the fresh ocean air finally gets out to

Redlands

In Figure 15 in order to put this whole flux problem into some perspecshy

tive we looked at the numbers the actual amount of ozone flux across the

basin We calculated the mean trajectory from Torrance towards Redlands

using the surface and upper air data We looked at the flux from the western

basin to the eastern basin basically from Los Angeles and Orange Counties to

Riverside and San Bernardino Counties This is a calculation made at 1700 PDT

We used the winds aloft from Chino as well as the vertical profiles taken at

Pomona and Corona Averaging the ozone concentration throughout the mixing

layer and multiplying by an average wind speed we arrive at a number of 185

metric tons per hour being transported directly from one side of the Basin

to the other If you look at this in terms of actual concentration in the

eastern Basin and assume that the flow was constant for about an hour it

is eno_ugh to fill up the box shown in Figure 15 to 025 ppm ozone which

exceeds the air quality standard by a factor of three (using the ARB calibrashy

tion method) Thus there is a very significant transport of ozone or ozone

precursors from one portion of the Basin to the other side of the Basin One

thing to mention though is that the concentration would not be kept up on a

203

steady state basis because the transport is a result of the pulsing effect

I Illentioned earlier There is a lot of accumulati6n in the western Basin

and these accumulated pollutants are then transported across the Basin This

kind of transport did take place in a couple hours because we also have

measurements from 1500 PDT which give us similar flux numbers

Figure 16 is a trajectory envelope similar to Figure 10 calculated for

Upland at 1600 for the air arriving at Redlands about 600 oclock in the

afternoon I wanted to include this trajectory envelope to show that the

problem is not really simple You cannot say that the air at Redlands came

from Long Beach per se The air at Redlands if you look at the whole

envelope of possible trajectories using upper air data as well as surface

data could have come from anywhere between Downtown Los Angeles and over

the Pacific Ocean south of Long Beach

Another thing to recognize is that the wind actually changes direction

slightly as you go up and down through the mixing layer and the mixing layer

is exactly what it implies There is mixing within the mixing layer so if

you begin with a parcel of air near the surface this parcel may move to the

top of the mixing layer and go one direction for awhile it then may go back

down to the bottom of the mixing layer and move in another direction for

awhile The ratio of the length scales indicata3mixing layer depths of 1500

or 2000 ft and distances on the order of 70 miles This makes it very

difficult for tetroons to follow an air trajectory because they do not go

up and down They stay at one altitude and in one wind regime and yet the

wind regimes are different at different altitudes and the air is continually

mixed up and down through this layer You can often see this on time lapse

photographs

204

The question is where does the pollutant mass go after Redlands Figure

17 is a repeat of Jim Pitts slide from yesterday and it is data for the

same day that we did our analysis It shows the ozone peaks starting at

Pomona and Riverside and on July 25 1973 eventually getting out to Palm

Springs so there is quite a bit of long-range transport The ozone is

stable at 8 00 or 9 00 oclock at night There still are ozone concenshy

trations of 02 ppm it hasnt dissipated even at the surface Ozone does

dilute as the mass moves Other calculations we did were integrations

through the mixing layer of various pollutants such as ozone and CO along

with trajectories that we measured Th~se integrations show just what the

ground data show in Figure 17 The concentrations increase through the western

portion of the Basin and then show a decrease through the eastern portion

of the Basin CO tends to decrease faster than the ozone indicating a

continued production of ozone further east

Figure 18 is a streamline chart on a larger area map for the 16th of

August 1973 It shows the typical streamline patterns that occur for

ventilation from the Basin By mid-afternoon there is flow out through the

major passes to the north and towards Palm Springs (PSP) On this particushy

lar day we had data from Arrowhead showing that the air mass from the Basin

does indeed get up there

Figure 19 shows a vertical profile over Arrowhead early in the morning

16 August 1973 at a time when there was a north wind Ozone level was

about 005 ppm the scattering coefficient was quite low on the order of

probably 60 miles visibility or so Figure 20 is a vertical profile again

over Arrowhead late that afternoon when the winds had switched There is a

flow from the Los Angeles Basin into the Arrowhead area thus one sees a

205

vertical profile that shows a distinct increase near the surface in both the

ozone and the scattering coefficient and in the condensation nuclei Ahove

that you have fairly clean air The top of the polluted level is just about

the top of the mixing level over the Basin

I want to leave the transport now and discuss the complicated vertical

structure that can occur If you want to try to model something try this

one for instance Figure 21 is a vertical profile over Brackett Airport

Pomona about 830 in the morning on 26 July 1973 which is the day after

the episode shown earlier A bit of interpretation shows how complicated

th is can be If one looks at the temperature profile it would be very

difficult to pick out a mixing layer theres a little inversion here another

inversion there several more up here After looking at hundreds of these

profiles though you can start interpreting them What is happening is that

there is a surface mixing layer at about 500 m In this layer there is a

high condensation nuclei (X line) count due to morning traffic The San

Bernardino freeway is quite close to Brackett there is a relatively high

nitrogen oxide count about 02 ppm and the b-scat is fairly high Ozone (Z)

within the surface layer however at this time is quite low The layer beshy

tween 500 m and 700 rn turns out to be the Fontana complex plume Note the

very high b-scat level it is below 3 miles visibility the plume is very

visible especially at this time of the morning when it is fairly stab]e

There is a high nitrogen oxide level (800 m) a high condensation nuclei

level and again a deficit of ozone Above this layer (800 m) you have stuff

that has been left all night very low condensation nuclei indicating a very

aged air mass ozone concentrations about 016 ppm b-scat of about 04 It

has been around all night and not yet had a chance to mix down within the

206

surface layer In fact one good way of determining the surface mixing layer

early in the morning and at night is to look for the ozone deficit Another

thing to mention is that wind reversals occurred for each of these three

layers The winds were fairly light and westerly at the surface slightly

easterly in the 500 m 700 m layer and westerly above 800 m There is a

complicated situation early in the morning but the main problem is that by

the middle of the day there is good surface heating and the pollutants have

all been entrained and mixed down to the ground so in order to modeI what

happens on the second or third day of an episode you must be able to look

at both old pollutants as well as fresh emissions And you need to account

r for ozone that is actually transported down to the surface from layers aloft l

The next slide is a photograph (not included) which is another e xample

of some layers aloft This is due to upslope flow as explained by Jim Edinger

in his publications The mountains are heated during the day in turn heating

the air and making it buoyant there is upslope flow to a point where the

heating cannot overcome the subsidence inversion and the stuff comes right

out from the mountains and spreads out over the Basin The pollutants can

stay up there if the winds aloft are very light and on the subsequent day

will he re-entrained to the surface On the other hand if there are winds

aloft different from those in the surface mixing layer or the wind velocity

aloft is high there can be a very substantial ventilation process for the

Basin Pollutants can be ventilated up the slope and blown away in the upper

winds In the case of the entire July 25th episode winds aloft were quite

light and these upper layers remained

Figure 22 is a vertical profile of one of those upslope flow conditions

in the same location shown in the photograph but on a different day Again

207

there is a relatively high surface concentration of about 03 ppm of ozone

(Z line) a layer of clean air between 900 to 1100 m and then high concenshy

trations of ozone again above 1100 m It has gone up the slopes of the

mountains and then come back out Concentrations in the 1100 to 1300 m area

are just slightly lower than they were at 600 to 800 m area Notice however

that the condensation nuclei count (X line) is quite a bit lower mainly

because the stuff is much more aged above the 1000 m level than it is down

below 900 m

Figure 23 shows the stability of ozone the fact that it can stay around

all night long This is a vertical profile taken over Riverside about 2200

PDT 1000 oclock at night Above the surface mixing layer (600 m) there

are ozone concentrations of about 0 15 ppm (Z line) Within the surface

mixing layer (below 500 m) ozone is completely scavenged decreasing to

zero The nitrogen oxides within this surface layer are being contained and

are around 01 ppm from fresh emissions that occurred during the evening

Condensation nuclei near the surface are very high The temperature profile

is very stable You have a surface based radiation inversion which is a

little strange looking for a radiation inversion~ nevertheless it is quite

stable There is a definite restriction of the mixing--a very difficult

time getting air from below 500 m to above 500 m The ozone that exists in

the 700 m range is in air where the reactions have virtually gone to compleshy

tion and is very stable All the profiles on this night changed very little

the ozone peak stays there High concentrations stay around

Figure 24 is a cross section across theurban plume of the City of St

Louis I wanted to show that this occurrence is not limited to Los Angeles

We have seen ozone formation and transport in other urban plumes These data

l

208

were taken during a project sponsored by EPA in conjunction with R Husar of

Washington University and William Wilson of EPA The dark line on this is

the ozone concentration across the urban plume perpendicular to plume The

dashed line is the scattering coefficient The power plant plume is parallel

to the urban plume The data on the left were taken 35 kilometers down wind

about 1100 oclock in the morning The ozone concentration increases slightly

to 005 ppm in the urban plume there is a deficit of o in the power plant plume3

In the same urban plume same conditions 1500 CDT two hours later further

downwind there has been substantial increase in the ozone in the urban plume

itself The b-scat is very similar to what it was before but the ozone is

now increased quite substantially except in the power plant plume where

there is a strong deficit of ozone due to scavenging by nitrogen oxides So

the formation and transport of ozone and ozone precursors in urban plumes is

a regular occurrence that happens in more places than Los Angeles and as Bob

Neligan showed this morning it can happen over quite a bit longer distances

than we are showing here

To summarize the conclusions as they affect model development first

once ozone is formed in the absence of scavengers ozone is a very stable

compound It remains for long periods of time It can he transported for

very long distances Ozone is a regional problem which cannot be controlled

on a local basis To have effective ozone control middotone must have a regional

control strategy and probably regional type air pollution districts

A second conclusion is that the vertical distribution of pollutants can

be highly complex and models have to include more than just a simple wellshy

mixed surface layer

209

A third conclusion is that layers aloft can persist over night and can

be re-entrained within the surface mixing layer on subsequent days models

should be able to account for old pollution as well as fresh emissions Also

pollutant accumulation and transport can have distinct diurnal patterns that

are strongly dependent on the meteorology Models should be time dependent

and should start at the beginning of the accumulation period In other words

models ought to be able to run for 24 or 48 hours if they have to In this

case in Los Angeles there is often an accumulation of pollutants which starts

in one portion of the Basin at midnight and continues through the next mornshy

ing even before it starts to be transported

As far as recommendations go in many areas a lot of ambient data has

been collected and in some cases the data are actually ahead of some of the

models so I think a research program is needed in developing models that

will account for this vertical structure and the day to day carry over and

the models need to be extended to cover longer distances In addition more

smog chamber work is going to be needed in looking at the effects of carry

over and mixing old pollutants with fresh emissions How people go about

this I leave to the modelers and the smog chamber people They know more

about that than I do

I

210

I

~ INVERTER

AUDIO TAPE

MONIT0R

MONITOR OBSERVER SEAT

MON ITOR

NEPHELOMETFR FLfCTRONICS

j DIGITAL DATA LOGGER

CONDENSATION

VOR DME NEPHELOMETER TUBE

JUNCTION middoteox ASSORTED POWER

AIRBORNE

TEMPERATURE TURBULENCE

middot HUMIDITY

ALTITUDE BOX

__

middotE=-middot RECORDER ----r----------

NUCLEI KJNITOR

CONVERTER

SUPPLIES

INSTRUMENT PACKAGE (

lCO

03

Ndeg

-

-----NEPHELOMETER

BLOWER

Figure 2 Instrumentation Layout for Cessna 205

211

bullubullbullbullbull

Figure 3 Airborne Sampling Routes in the Los Angeles Basin

Figure 4 Vertie al Profile Flight Path

~-~ r~i ~~1 -- ~ ~ ~2-1~ LJ-----~ r~~ ~~ t~~--l

~ ALM l

0 RIA

ec 8v

M

~ Afo

-o

M 0

~IV

ltgt

IN J--1 N

SCALE II fi M I j_ ES 0 3 4 5 =-JSEJ--J~ _middot ~middot- - =- =

I

~

M

N~J

Figure 5 SURFACE STREAMLINE ANALYSIS - 0300 PST 25 July 1973

~~~ ~~-- cp1FJ=D -~~

~ 1

~ ~ 8c

8v

~25

PACIFIC OCEAN

diams Tt

0

9 I 4 5 10 I- m p H - -middotmiddot u 4H__8 middott_

D i6 J4 k W~D SPED llaquotl SNA NJ ~1

SCALE m ICtt84bullmh R v1s1a1L1n (mil 6 ~ CONTOURS REPRESENT

-- 10ml 16km (~() bull ~ ) ~ - 000 ft 3C5

Figure 6 S_cJRFACE WIND STREAMLINES - l 600 PDT JULY 2 S I 8 7 3

l - ~---i ~-=-___-----c---it~~-~~ r----=------1 ~-~~--cpc---_t__A --~ ---llil

~_ - ~-l-cL

34bull vi~-dff

bullbullbullbull bull ~ bull -1 bullbull - -_- L bull-J bull ~bull-bull-ii------~ bullmiddot r_ -~- ~ bullI ~_ bull bull bullbull bull I bull _ - bull -~-~ middotbullbullbull ~ ~ --middot -~- bullbullmiddot ~v ) ~ - -__rl v middotmiddot - 1- ~ -- middot middotmiddot - 1 91 frac12 - ~- lt( middot K i - middot bull - middot - bullmiddot~~-~lJ) obullmiddot~ ~-f- _J_~---Smiddot~middot-~----~~~---gt_middotfY-_middot-~middot --middot-~-~----fJ_middot- middotmiddotbullmiddot u-- bullmiddot ~ ~ -middot L~ bullbull

~bullbullbullbull bullbull l_bull bull bullbullbull EW bullbullbullbull-- ~ __bull f f - middotbull - J middot f bull S bull I ~ -r --

_ bullbull bull- _ bullbull-bull ~ ~ bull bull bull bull I bull bull bull bull bull bull gt - bull middotbulliJ -bull I bull bull _1 bullJ C-- ~-middot _ bull bullbull bullbull bull _____ ~ ~ l _ middot q bull 1 -middot middot ~~middot middot middotbull_ J ~gt - J bull-bullbullbullbull ) _ -middotmiddotbullmiddot J ~middotmiddotmiddot -bullmiddotbull fmiddot 7middot _middotmiddotmiddot bullmiddot(middot Ii~ middotmiddot~_--~middot 1middot__middotmiddotmiddotmiddot middot- gt_ -~ -~-- Imiddotbullmiddotbullbull_ -

- ()_I (w--_ bullbull__(i- bullOmiddotbull bull middotbull -bull-_jlJ middot bull lt 1(middot t gt bull - ~ rbull I bull middot middot- bull41-bull l~r v-middot~- middot middot middot bull_ - middotmiddot ~Jtj (middot~ ~middoti middot middot middot middot middot ~- ~ -tmiddot~ I - middot middot_- ~ - -~ middot_ _- ~bull - _ ~) i bull bullbull bull- middot_ bull middotbull __ ( bull 11bull bull ~ampmiddot ~ l bull bullQ bull - -1 bull JY1 bullbull ~ or bullbullbullbullbull bullbull-bullbull _ ~ - bull bull-bullbullbull middotimiddot middot 91 bull t bull - - tfaw lJ--r- bull bull _ bull middot- - l

f ~~middot--~ middotmiddott ~ltrgtmiddotmiddotJmiddot_bull - ~ - __ middot- LOS ANGELES BASIN - LOW LEVEL -__ jmiddot l-gt bull - bull J iI bullbull bull bull bull _ bullbull _ Jmiddot middotL~_1 middot middot bullbullmiddot ( C middot INVERSION MEAN WIND FLOW _ J

lmiddot - f bullbullbull~ - f 1bullbullbull _ ~)- bull middot- _---_- 7f-~bull~ REGIME _F_~ AUG_UST_~ ~600 P~--- l

-__L-~bull --ncmiddotbull~~-j--bullmiddot~bullmiddot_-bull _fJibullmiddot Imiddotmiddotmiddot-bullmiddot- bullbull ~ bullbullbullbullmiddotmiddotmiddot~middotbull ___ bullJ_ _middot~0))deg bullt t1yensmiddotmiddot ( middot middotmiddot middot middot ~ middot lbullbull1 t_c0 bull -middot---l lt ~middot~- deg bullbull --= bull bull bull I bull bull bull bull bull bull bull bull bullbull _~bull b ---) bullbull-bull ) bulll middotbull middot1middot ) bullT --f bull I bullr ~bullbullbull bullbullbull( - -bull-- ( -o-----_i bull-~-l- i l l J l~-- c middotmiddot _--1 ---I middotmiddot ---- ~bull-bull bulli_ ALT Elmiddot_ bullbullbullbull _- ~~middot bull middot bullbull _ bull middotbull bull~ ~bull middot bull -middot bull--ua_-- bullbull bull

-- 01--- middot_ -middotmiddot hmiddotmiddot __1 ~-- ~ fi~~- ___ - ____ _ -middotmiddotmiddotmiddot~ ) -~-J bull bullbull bull bull 0 uc- -l ~- ~ IT ~~ll ~ bull -middot -middotmiddotmiddotmiddotbullCCAmiddotmiddotmiddot-middot middot bullbullbullbullbull

) i- 5 ~-==-- __ __ - bullbullbull _ bull~ bullbull _ bull bull l T[h4 ------ - 0

i17- o~-lt -(i-_~ 11t~bull-omiddot ~- -- 13 0l~~~bull bull Jbullbull~bull ~ ~bullbullbull bull bull x- middot~---=-~~ -=aJlll8 bull Ibull bull ~~ middotbull rbull~---bull1-~middot-middot _ middotmiddotmiddot-middot 1 0 ~vrbullmiddot ~middot ~ (J~-middot _-_~) ) ~ bull middot

l middot _ POMA_ middot =~~~----ti~ jmiddotmiddotmiddot - middot bull [j

~A ii J0 Vfli middot bullHud __=bt_ bull

CImiddot ~-- ~- middot)middot PACIFIC OCEAN I middot ---- middotmiddot ~

__ middot__ ~ - _ 23~1 middotbull 8 4 1 middot middot ~ middot middot gt ~~- l ~ u middot

bull - bull- I ~------ --1~ i middotmiddotmiddot - n _c-118 1130

~ n r -t ~~gt25) cmiddotbullmiddot

~--lt- ~~- 1-~__( i - t ~ _ middot 0 igt(_J

11bull bull11 ~~ -~[ ~i~gt----gtmiddotmiddotmiddotmiddot--~l_ ~~ ELEVATION

IN FEET bullbull (_- middot bullbullbull -middot middotbull middot ~~ middotmiddot bulltbullbull _ffmiddotmiddot-middot v I )tylt~ -~bullbull1bullbullrbullbull ~-lt -~ ( I~

600~ A0 Cv(A (1829 m AND OVER) deg )_ rJ__~7 middot middot ~--middot L==1 _J bullbullbull - bull -middot~-- rgt ~ middot(Zmiddot- middotbullmiddot middot

Z~C)-tGOO (762 middot 1829 m) 9-N4 __J (r -- lf _ bull bullgt-~~~ ~ _ w _ _ I (1 bullmiddot( middot1 middot -----~~~- middot L-bullmiddotbullW bullbullbull3 STA r I0-4 lODEL

100i -2soo (305~762m) -- Ow - -~1_- i ~~--- bull v~rvt ~~ -middot )) ~--

II gt J (-_bullmiddot middot~ l bull bull tr 1 )~ gt ) bullbull-_bullI-middot -middot bull~0 3 Mor nuq1ENr Wlbull~O JIAtCTIO-bull bull - lbull C---gt bullbull )t bullbull -( I bullf I - 20-00 (61 bull 305 ml J( Jloa xxE- -bullbull00 - -- middot1

0-200 (0middot61m) Wl)7 AVBt~gpound ) bullmiddot-iiNL~ middotntmiddot_ 1 iJJlt( _1J- ~ VAq IA9 IL ITY 0 ~ 10 15 ltS lHPtl

~--_ bull bull I bullbullbullbull 1 ~) J)J ~ bull Is bullmiddot bullbullbullbullbull ~ 3 V IS A VAqlABLE OIR~CTIO- 0 8 16 2-4 km

(SPEEDS SHOWN IN mph 10 mphbull 16 h1llr) -- middot ktr~~~ lt~ ) -middot-SCALE

Figure 7 LOS ANGELES BASIN MEAN WIND FLOW FOR DAYS WITH LOW LEVEL INVERSIONS DURING AUGUST I 970 AT 1600 PDT

-~~~~-=======~middot~-~======~middot--=-==-===gt=---==____________=== ~--=-J~==-- -=-ee----=-------

500

N f-- V

- - - SUBSIDENCE INVERSION

----MARINE INVERSION

bullbull-bull-bullbullGROUND LEVEL

x WINOS ALOFT (kmht)

WESTERN middoteASIN EASTERN BASIN

LAX WINOS EMT IHOS I I

CNO WIHOS

s_ 04 13 1500- 05 02 08

I 06 069 middot

11-1--

04 04 i ~4

06 ~ 4--

I 2

1000 n1 1005 -_E

lll --1 lJ -----------~----

~11

--=i-+- c -- 9 _____ - ~ C

lt I

I 6 4 _r 31

I 6 5 ~~ ~_ bull ---middot- 64 ~li- - middot- bullc - middot-----------

10

SMO (1347 PDT)

EMT (1246 PDT)

BRA CAB (1459 PDT) (1335 PDT

RIA (1349 PDT)

RED (1406PDT)

Figure 8 VERTICAL CROSS-SECTION OF bscat FOR lvflDDAY

T t 10-4 -1)(l n1 s are m

JULY 25 1973

- c - -~

~--~ JC_-_1- ~1pi~ oamp----~JilliiiM~f~-U~ -~--- --~~~ ~~~

-=--~

-E-- O

_ lt

1500 05

06 15

09 __~

1000 --

~- ~---middotmiddot 29

500

oJ11

__a

07

I 07 I

I I

I

09

I

I

I

I 7 ---

11 -----

~ ----- 6

---------------lt- -~middot4 --------

20

29

-

10 10

11 07 08 08

10

08

~8 _____ Y-

N

- - bull SUBSIDENCE INVERSION

----MARINE INVERSION

-bull-bull-bull GROUND LEVEL

WES TERN BASIN EASTERN BASIN x WINOS ALOFT (kmhr)

t t

CNO WINOSILA WllltOS poundMT WINOS

SMO LA EMT BRA CAB RIA RED O (1736 PDT) (1655 PDT) (1707 PDT) (163 PDT) (1823PDT) 1805 PDT)

Figure 9 VERTICAL CROSS-SECTION OF b FOR AFTERlOON OF JULY 25 1973 scat

T bull 1o- 4 - l )(units are m

__~~---iii~~- ~- ~~______ ~~- --~~J---=-~ ~

N ~ -J

PACIFiC OCEAN

0 5 10 15 1111

E 8 4 I 0 8 6 2 ~ bull

SCALE

dh Mes

CONTOURS REPRESENT - 000 ft 305 m

0 SNA

c8s

ec 8v

amp R~b

Figure 10 TRAJECTORY ENVELOPE FOR AIR ARRI1G AT CABLE AIRPORT (CPLAD) 1600 PDT JULY 25 1973

~-~

q_- ~ ------1 H~~~ -~~--~ ___---___--i- __r-=-1--===12---1 ~ ___r~ _==---_ - ~- f~~ ~-- - -5plusmn-at -~middot~

ll~~r1 ri

40

ec 8v

-1 I

amp

0 HQ_

7 0

CAP LAAR) O

VER

PACIFIC OCEAN ~ 0

RLA

4

WHqR d

diams

H ~I

I l

0 COMA

3

L~

LAH

Fa_ f ~~

S ~ LA APCD VALUES ADJUSTED TO AGREE ~

lt

0

5 10 15 mi0 WITH ARB CALIBRATIONE-j I I CONTOURS REPRESENT NZJ ~ 0 a SCALE 6 24 km - 1000 ft 305m COS v~J

______ J 10 ro ( igtf t-i

coFigure 11 SURFACE OZONE CONCENTRATIONS (pphm) I 600- I 700 PDT JULY 25 1973 ~

~~~~~C-~ ------=--~-__-~--~~~=--- ----=--~

N

-E

D1600----------------------------- 1--

14001-------------------------------

1200

I Ground Elevation

1000 middot 445 m ] lampJ

sect ~~ 7 ) SURFACE i6~ 800 MIXED LAYER

~

~ [ J ~ ~ I OZONE CONCENTRATIONS~ 600 E E GREATER THAN

( 50 pohm

400 I C H T Z GROUND LEVEL

200

I PUUloCETER UNIT SnbullBOL

NOc N0 0 ppm01 02 03 04 05 03 z

40 --~45~~ 50 co pm C0 5 10 15 20 25 30 35 I I I I I I I I I I TEIIPERATURE oc T-5 b 5 10 15 20 25 30 35 40 45

I-- 100 RELATIVE HUlillOITY H0 10 20 30 40 50 60 70 60 90 b1eot IOmiddotm- 1 8

CN cmmiddot3 1 IO X0 I 2 3 4 ~ 6 7 8 9 10 URBJLENC-C cm213ue- E

Figure 12 VERTICAL PROFILE OVER CABLE (CAB) J CLY 2 5 l C)7 3 l 63 6 PDT

~ _~ ~--- -

--

1400 I bull bull

1200

1000-5 LampJ 0 ~ I- 800 ~ c(

sooLl

-1-=-1-~--t j --=~c-o-----i-bull 1-~~~ ilt~~ -~-1 lta-abull--~ -c-~---=---r F--- ---- I n_--middot- =~~ ai~IHJ

(~-It

1600 ___________________________________

C r 11 s Ground Elevation t~C E H I~lcc

- ~ 1 90 m

4001 bullc C H

C UNDrnCUTTNG svC ~ Ic- H

SEA BREEZEC II 200

C C

[C -PARAMETER ---UNIT SYMBOL

NOx N0 0 ppm01 02 03 04 05 03 z co ppm C0 5 10 15 20 25 30 35 40 45 50

-5 middot- -~20~----25 TEMPERATURE oc T0 5 10 15 30 35 40 45

100 RELATIVE HUIOITY H0 JO 20 30 40 50 60 70 80 90 bcot 10-4m-1 8

CN crrr3 10 0 I 2 3 4 5 6 7 8 9 10 X TURBULENCE cmZ-13 sec-1 E

N N

_-----=-G--~---

Figure 13 VER TICAL PROFILE AT EL MONTE (EMT) JULY 25 1971 1656 PDT SHOWING UNDERCUTTING BY THE SEA BREEZE

0

middot~_lt ~middotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotbullbull

-~

LACA

0 - )

i r=

-v2v

~

_middot~middot)( I bullbull

bullJ

K~Ji~middot

~~ 61iAS 0

EMT J~J---6~-11 ~orr

PACIFIC OCEAN

WEST 0

SMC

0RLA

14

L~8

R~A

~BL

16 ~ ~

0 5s Pcfrac14A c1i ~ )

wFJfo~J_) ltI~~~

_ff-Clf1ito J )

HILL~

~J U

~ _~~~

~

I o middot

1 1$ ~ 11yen ~middot ~I N

I

N I- I

t

0 --pomiddotmiddot bullmiddot i- 1LO middot Joomiddotmiddotmiddot -- middot middotmiddot -middotmiddot

_middotmiddot 0 middot middotbull MWS r

L4 ( 1 T bull bull __-- -A bullbullbullbull middot

0 i __ bullbull

17 t-J~ N7 a S I ~r ~ 1 rtd ~lt A-~ v- middot ~ - cXa 0

RIA 19

CLO

ltJ~

bull ~ 0

(

--

1

_ _

-2Wl

~s~o -- _)~J0JgtJ~ ___ Q

15 l1JI

0 15 r(A0

CAP

CLARR)~R 1900 1-shyPDT

II (_-L~X L2X I 0~ R[V

0 CCtwA

I

I18=00 POT~ l4 r1

fj

-11J - ----- 11=oomiddotmiddotpor

l~i middotmiddot- o

i

5 10 5 Tl o~1 middot--middotmiddotmiddot middotmiddot

_q it==i--__F-3 9 I I CONTOURS REPRESENT SNA NZJ ~1 o

_- I 0 8 16 24 km I - 1000 ft 305 m middot ~

7 14~CALE --- 2500 ft o2m V lr1 ) middot I i0 _ il o5

16QQ pol(middot v( ____________ _L

I i

Figure 14 APPROXIMATE TIME (PDT) OF ARRIVAL OF SEA BREEZE Jl-LY 25 1973 (Ogt_iective criterion based on ground level ozone concentrations)

~ -___~==~ ~~ - ~ =-~ f7r=~1 _j~-~ --c_~~

u-middot - middot middotmiddotmiddotmiddotmiddot

~- middotmiddot~ ~1 WESTERN BASIN r Joa_middotmiddotmiddotmiddot_ NOxEMISSION RATE ~- 95 METRIC TONShr

-----bull_ ~ ~middot~ I -OUR -----middot )omiddotmiddotmiddot - middot~ l21 (fTI

~ AT middot ~ middotbullmiddot- ~- ~ middot 4bull-middot

I EASTERN BASIN NOx EMISSION RATE 10 METRIC TONS hr

ri r bullbull

t10 Joa

) __ 8v -a_ -- -bull-I O ~AGA -_ ~S ___ _ middotmiddotmiddot -

~ ~v ai- omiddot-middot~-- - ) r -middotmiddotmiddot f middot( ---~ -l A ~ _ (- bull ___

it~ ~~~ middot-middot -- ~-~ ~~~ 0 0 AZU~

AVERAGE CONCEN7RCTi)N iN BOX (IF STEADY STATE)

IS 25 pphm

1 r f--Ji 7 ~Sv PAS ou )V~(~- ~ t i -~ Li_) 03 FLUX THROUGH f~

~ ~JI_~ - amp_ JiM O SHADED BOUNOA~middot~-~ ~~-s-- EMT 185 t 60 METRI~ bull ~ ~ TONShr 0 (m)

c~~~ 1t~CS A~JFP

1000 _29

-i32

_~o tUA

_

1

O~ ~

0 -__rJ( (r- J PACIFIC OCEAN LAX _ C-middotJbull _

l o M R No _

550m

r

A frac14

HAR O HJ LAH

_ o camptA REDLANDS 18QO POT ~ r

I bull ~

RB MEAN TRAJECT~~~y

0

TOA L~S

0 AN

I - ~ 8 OUNOARY ~ ~middotltdeg ~ ~ BETWEEN middot __ WES~ERN ANO- middot middot - ~

I gt I lt bullmiddot bull (EASTERN ~ i middotmiddot middot - - ~

S ~ ~~ ~ - middot-

rt1~1_--t------l

middot1-- BASIN ~-~

1-)~~--middot ~ ~l

~~ ~-bull bull J --

-is-eo -_

0 5 10

j=i r-i C

0 8 ltl

SCALE

5 mi

2~ un

CONTOURS REPRESENT - 1000 ft 3gt5 m

--middotmiddot 2500 ft 1 762 m

~

0SNA

cos 0

_ --~ ----- --- ( bullmiddotmiddotgt

- middotlt- ltgtmiddot t__ Q ~

1 1 rmiddot bullbullbullbullmiddot ~9

NZJ ~ middotmiddot - middot- Alr ---middotmiddot- middot middot( middotmiddotmiddotmiddotv ~ bullbullbullw bullbullbull bullmiddot 1 bullbullr~ ~-- -middot ~--v ~- - I -~

ESTIMATED OZONE FLUX FROM VESTER~ TO EASTER-J BASIN JULY 25 1973 I 700 PDT

C ~IV

N N N

I

l ~

-~~

I

iI

i I

I t

t

~ ---~ --

Figure 15

~Qa llfJD fl(~middot ~ 11f ~I I

l

Lfb ec~s0 CPK v2v 0

ALT 8v Ld~_----1

I

HO-

0 CA

middotLARRv O VE~

1330

ol(Di

A~U

0ENT

~lt

s~e ~ 1530

F8f 1730

~

rbull-~

oc (WljT) -_-~(~~c lt-rw---_

~~ ~-_i~cB~~~

2-~) - ~ ~ l~w-~~ p~- pound)_

0 ojI middot tl-1CfUp I ~ ) 1 ~ J~I i bull middotbull middot~-Li 1)- ) I

DiI ~- 0

i ) 0 l I I

t

A RALc~o JI

C

-~

0 r-iR

~IV 1230 1~

RE PO ~- I - Ftl

) 0 ---~gt- __L8s ~Zi diams ( T~ _middot_ ~~ ~

I AN ~~-~ j t bi 0

~ I

~ I L i

-_gt ji o 5 c 5 Tl middot 0 0 ~-i p__i=r 2=f I_ I 1 NZJSNA 1

1 8 2 4 km )

SCALE I 00 J_(1 CONTOURS REPRESENT cos f

1 0 I --- I - ))) 35

PACIFIC OCEAN

Figure 16 TRAJECTORY E~VELOPE FOR AIR ARRI1gtJG OVER REDL_)DS AT 1800 PDT JULY 23 l =i73

224

JULY 25 1973

LA DOWNTOWN

0sect040 a

~

~ 020 0 X z0 ~ LJ 0 ~ z

~5 040 330POMONA 0 ~ en~ 020 w z _J

w w 0 (9 z O----u-~~-__~_-~~~-------L-~-0--0-0~----- z

ltt~ 040 56 (I)z

0 0o _ RIVERSIDE _J0 20 t6 ~

0~ Qt---0-0--ltrO-ltgt-C~------~~~~ a

LL ~

Rate ~ IO mph___ (I) w

_J~ ~ ~

et~ lt(

3 040 PALM SPRINGS ~

j 020 ~

0------____-----L--___---------L---~--~

105

12 4 8 12 4 8 12 l~-s----am _ pm----1

HOUR OF DAY PST

Figure 17 Diurnal variation July 25 1973 of oxidant concentrations at air monitoring stations at Los Angeles Downtown Pomona Riverside and Palm Springs California Values are corrected data Los Angeles Downtown and Pomona x 11 and Riverside and Palm Springs X 08

CONO S t 1 fRESEIS7

~

~~ 0

ciffmiddotdK ~ ~v~~o

( ~s ~

bull ~r ~ bull 1--~~----Soootl ~ ~ ~ ~ lj i1 d t CJ ~ ampfrsmiddotflt- frac12 ~ middotL~Js _-- ~

_gtgt middot~ ~rroltf~-) ~ 0 s- r

middot-middot- r_~ ~~JtbO ~~bull~Jt ~~~ L r - bull _ ~ I= J 1 ~ ~ ~-~~bullJC ___ -_ middot ~ laquo -poundJ~ ~- middot1~ r-- - V--_1_ ~ I 1 S I

V ~ bullf-uv~ fi -~zumiddot -~middot~ LS gt -tmiddot-F Q~ ~-tv I_~ --- ONT p(_ s ~S ~~~-[ ( 0 c-_ --~ ~~~___d_) lt- ~ I -i-C - -

~----1-1 bull~~POMA ~V BN ) middot-~ f -- s - ~

~VA -middot- ~p AAL a 2~~ ~~middot01 r r ~ middot middot 0-- V

i LAX bull1

~ -~poundJ-i- ltllll _(__1-0~ ~t- degQ-0- ~~ _ _-__~~-qlK ( a_ II ~ ~p-~ ~J

N bull - - 0 r o_ _I ~ -~ ~middot ~ ~amp ~--= ~ ) s ~

- -~- - middotO _a - Tl --0- ov I lHOIO J I bull J -- ~ 6 ~ -__ 2 ~

(__ ~~ _- ~-~ middot8---fl~ -- ~ bull~-abullbull _~ ~-cgt ~ bull bull middot e bull bull l ~ 0

I 1A_ HZJ middoto~J

middot0 (~ ~ S TAA

- ~ - - - --0 () _-j J middotO=c==c-c==cc~~~ l ~~ ~ ~ bull-~---~ ~ bullbull -~ al1 ~ bull __ ~--middotmiddotmiddot

diams Skyforest _ Strawberry Mt Lookout

Figure 18 STRE ~[Ll)ES FOR 1600 PDT on 8 1673

~ ~--

vO 0

N N V1

au

91 V7

-1 ~ -=1 ~~ ~~~~l r=--~d- ---1 _J-_

~E1 ~L1-~f~

3100 ---------------------------------

2900r-----------------------------

T

e w 0

~ 5 Cl Ground Elevation

1560 m

T PARAMETER UNIT SnbullBOL

NOx N 01 02 03 04 05 03

ppm z co ppm C

10 15 20 25 30 35 40 --

45 50

170

I I I z

0 5

-5 - -0~ 5 10 15 20 25 30 35 40 45 TEMPERATURE oc T

0

0

10

I

20

2

30

3

40

4

50

5

60

6

70

7

80

8

90

9

100

o

RELATIVE HUMIDITY

bcot CN

TUR8ULENC~

110-4m-

cm-3 tobull 213 1 cm sec-

H

8 X E N

N OI

Figure 19 VER TI CAL PROFILE OVER ARROWHEAD u-RR_l A CG CST I 6 1973 939 PDT

3100----------------------------------

N2900r----------------------------- -i

N

2700i-------------------------------

2500

e 0 uJ 2300 gt ~ ct

2100

1900i---------------------+--------------

~le 1iation 1360 m) 17001 ~

- -PARA1jETER UNIT SYMBOL

T NOx N1500 o ppm01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50

TEWERATJRE oc T-5 middot --~o--- 5 10 15 20 25 30 35 40 45

IOO RELATIVE HUWIOIT Y H0 10 20 30 40 50 60 70 80 90 bcat 10-~- 1 8

CN cm- 3 104 X0 I 2 3 4 5 6 7 8 9 10 213 1 tURBliiENCE cm sec- E

Figure 20 VERTICAL PROFILE OVER ARROWHEA D -RR 1 --- -AUGlJST 16 I) 16--1S PDT

1-~i w--~i_f l-=--bullC- ---~-4

1600 bull t c- N 8 ff Tbull C[ 8 H 1 bull H z H T ~ C f N 1 H T bull C rn 1 C NE bull-~z Hi400 bull bull tf T bull N ~r --middot _P H -ybull EC N z__e H T i 8 z H Tbull C E HD Z H T POLLUTANTS REMAINING FROM bullt C Hbull L T PREVIOUS DAY1200 Et HO I II -middot-- bull Ct H 9 - H T

___ Hbull( E N 1 a tC N i--_ -1 H

C N Tbull Z HP poundIC C H z_ 1111 1

- bull C H Z l _H_ _J1000 )( cc H -z emiddot ksect bull C N ~ T

)( iz H 8 H TIAI -t XC z 7-- T0 bull pound N t H_8

t-gt

YCpound N 1800 l I-gtltbull - H (Jet

N i -r~Bltt t bull gt- t C X N H T

[ BUOYANT POINT SOURCE PLUMEH 1

N ~z-- -

C H

-bull SUPERIMPOSED ON POLLUTANTSC JZ X H T 600 -~ E c REMAINING FROM PREVIOUS OtY Cl JC t H H f bull cmiddot t HT -fl

C- X t fl _ REMNANT OF NOCTURNAL RADIATION INVERSION(I-----e-C f N K I T H

C Z [ T H x-8 400 _Zc r -H -K SURFACE MIXING LAYERz C II H K 8

C N T pound H M 8 _ I -t ff H E N -9 l

Ground Elevation 305 rn200

PARAMETER UNIT SYMBOL

_ I - I I I NOx N00 ppm01 02 03 04 05 03 z

co ppm C 0 5 IO 15 20 25 30 35 40 45 50

L middot1 TEMPERATURE oc T-5 0 5 IO 15 20 25 30 35 40 45

100 RELATIVE HUPAIDIT y H0 10 20 30 40 50 60 70 80 90 bscot o-4m- 1 B

CN cm-3 x 104 X0 2 3 4 5 6 7 8 9 10 TURBULENC~ cm213sec-1 E N

N co

Figure 21 VERTICAL PROFILE OVER BRACKETT (BRA) JULY 26 1973 0825 PDT SHOWING BUOYANT PLUME AND UNDERCUTTING BY RADIATION INVERSION

N N 01600

___bull C M C

C

1400~~~ t C [ middot H LAYER CAUSED BY

C C H C [ H UPSLOPE FLOWl

1200

1000 ] w

SURFACE MIXING LAYER 0 --= ~ -~~ 6 800~ er

C C

600t-i C C t C

I ~00

Ground Elevation 436 m 2001-------------------------------

PAIUWETU UNIT SYWBOL

NOx N ppm0 0 01 02 03 04 05 03 z co ppm C

0 5 10 15 20 25 30 35 40 45 50 I I I I I I I I TEWPERAT1JftE degC T-o b 5 10 15 20 25 30 35 40 45

100 ~EIATIVE HUWIOITY H0 10 20 30 40 50 60 70 80 90 b1tt1 10-m- 8

CN enr3 110 X0 2 3 4 5 6 7 8 9 10 Tu RUL Erct cm23sec- E

Figt1re 22 VERTICAl PROFILE AT RIALTO (RIA) JlJL Y 19 1973 1738 PDT SHOWI=JG LAYER CAUSED BY UPSLOPE FLOW

~~-7 ~ ~- 1 ~iri ~~- ~~-~ ~t ~~ ~ =~middot-1

1200 I t 1 If J-

1000

I C ltTl a_ ~l- t

800

600

L gE __r H

H

400 j (~ c pound N C E I~

t EH -

1-1 M

H H

H M H H

H

H H

11 bull H M H

M H If

H H

H

- C t H ~ C poundmiddot H

I C E I(

200

1600--------------------------- t

T t t T l

l T t

T t_

t 1

l] w ) g f

Tt t

ltt ~ T

t J t T

t J

f 1

t

Klt

H M Cro1nd Elevation 250 m HT X

5Yl80LPAllAlETER ~

NOx N0 0 ppm01 02 03 04 05 03 z

co ppm C0 5 10 io 20 25 30 35 40 45 50

25~--- ---35~~-40 TEMPERATU~E oc T-5 0 5 lO 15 20 30 45

100 RELATIVE HUMIDITY H0 iO 20 30 40 50 60 70 80 90 bact 10--ltllm-1 B

CN cmmiddot3 11 04 X0 I 2 3 4 5 6 7 8 9 10 IURBULENCE cm2hioC-1 E

Figure 23 VERTICAL PROFILE OVER RIVERSIDE (RAL) N

JULY 26 1973 2239 PDT I)

middot==-=-=

0

bull

N w 1--

ii -s~~ l-obull

CJ ~

obull -obull obull

5 02~

bscat

Oa

4l o2J

-I 3 e I 0

--)(

~

Abullu 2

ll

ol

Traverse at 750 m msl 35 km Downwind (SW) of Arch - St Louis Mo 1117 - 1137 CDT

( Power Plant Plume -01 Ibull-[ ~ e

11 bull E I -)(I

I0bull I 1r~ l -

0

I I Io 1 u I

I r- l A bull I i I 1I

H1I I 4 t I II I I

11 I I

I I r I I I

I I qo 01 I I

I I bullJ~viI I middot ~

I

I I

~

Urban Plume

ood 0 10 20 30 40 50

kilometers

o~

02

01

s 1

P

0bull 01

00S~J1 I ti middotmiddot1 middotvmiddotmiddot~ J

Urban Plume

I y

oo 0 10 20 30 40 so

kilometers

Traverse at 750 m msl 46 km Downwind (SVV) of Arch - St Louis Mo 153 0 - J 549 CDT

---- bscat

o-

Power Plant Plume

1l~ 11I 1 t

ill~t fl Ibull I ii

I

lmiddotmiddotrI

I I I I t II

l vrI V

JV-f Jl bull

bull t I bull I

Figure 24

l

232 RELATIVE CONTRIBUTIONS OF STATIONARY ANDMOilILE

SOURCES TO OXIDANT FORMATION IN LOS ANGELES COUN1Y IMPLICATIONS FOR CONTROL STRATEGIES

by Robert G Lunche Air Pollution Control Officer

Los Angeles County Air Pollution Control District Los Angeles California

Introduction

The type of air pollution problem characteristic of the west coast of the

United States and particularly of Southern California has come to be known

as photochemical smog because it is the result of sunlight-energized atmospheric

reations involving oxides of nitrogen and reactive hydrocarbons Its manifesta-

tions- -eye irritation reduced visibility damage to vegetation and accumula-

tion of abnormally high concentrations of ozone or oxidant - -are by now well

known In fact the occurrence of high levels of oxidant which consists almost

entirely of ozone has become the primary indicator for the presence and relative

severity of photochemical smog

During the 25 years since photochemical smog in Los Angeles County was

first identified an extensive program has been underway for control of the responshy

sible contaminant emissions Initially during the 1950 s these programs concenshy

trated on controlling emissions of hydrocarbons from the stationary sources of this

contaminant In the early 60 s programs for the control of hydrocarbon emissions

from motor vehicles in California were begun An exhaust emission control proshy

gram for hydrocarbons and carbon monoxide from new vehicles was begun in 1966

C011trol of oxides of nitrogen emissions from motor vehicles began in 1971

As a result of the overall control program by 1974 emissions of reactive

hydrocarbons from stationary sources have been reduced 70fo from uncontrolled

levels and about the same percentage from mobile sources Oxides of nitrcgen emissions

233

from statjonary sources have been reduced about 53 while emissions from moshy

bile sources are still about 7 above uncontrolled levels due to the increase

in NOx from 1966-1970 models Additional controls already planned for the future

will by 1980 achieve reductions of reactive hydrocarbons from stationary sources

of about 87 from uncontrolled levels and from mobile sources about 93 By

1980 emissions of oxides of nitrogen from stationary sources will have been reshy

duced 53 and from mobile sources 63 from uncontrolled levels The past

present and projected emissions of these contaminants are shown in Figure 1

A I though compliance with the air quality standards has not yet been achieved-shy

and is not likely before 1980- -the results of these programs have been reflected rather

predictably in changes in certain of the manifestations of photochemical smog For

example eye irritation is less frequent and less severe and in some areas js

rarely felt at all any more and damage to vegetation has been markedly reduced

Ozone (or oxidant) concentrations have been decreasing in Southern California

coastal areas since _1964 in areas 10-15 miles from the coast since 1966 and in

inland areas 40-60 miles from the coast since 1970 or 1971 as shown on Figures

2 arrl 3- All of these positive effects have occurred despite the continuing growth

of the area indicating that themiddot control programs are gradually achieving their purpos

a return to clean air

This improvement is al~o refutation of the so-called Big Box -concept which

assumes that the total daily emissions in a given area are somehow uniformly disshy

tributed throughout that area--regardless of its size or of known facts about the

meteorology of the area or the spatial and temporal distribution of its emissions- -

234

and of control strategies based on that concept And since the improvement in

air quality refutes the control strategies based on reductions in total emissions

it thus confirms the value of more recent control strategies which emphasize conshy

trol of motor vehicle emissions and use of a source-effect area concept

Following is a brief listing of the evidence we intend to present as supporting

our views on just what control strategy is appropriate

Examination of relative contributions of HC and NOx from stationarybull and mobile sources demonstrates that motor vehicles are the overwhelming

f source of both contaminants~

I bull Observation of air monitoring data shows that the effects of photochem -

ical smog are not uniformly distributed t_hroughout the county

bull Study of the meteorology of LA County shows consistent paths of trans -

port for various air parcels and consistent relationships between the

areas most seriously affected by photochemical smog and high oxidant

concentrations and certain other areas

bull The upwind areas are found to be source areas--the downwind areas-shy

effect areas

bull Central L A is found to be the predominant source area for the effectI area in which the highest oxidant levels in the SCAB consistently occur

bull The predominant source of emissions in this source area is found to

be motor vehicles

bull Central LA has the highest traffic density I

ij bull Both pr~mary and secondary contaminant concentrations reflect the effects

of the new motor vehicle control program in a predictable fashion 11 I

A strategy based upon these findings is gradually being verified by atmosshybull pheric oxidant data~

235

The Evidence that Motor Vehicle Emissions Are the Principal Source of Oxidant

As seen from Figure 1 at the present time the total daily emissions of I-IC

and_ NOx from all sources in Los Angeles middotcounty are primarily due to the motor

vehicle The problem now is to find the spatial and temporal representation of

emissions which when examined in the light of the known meteorology and geogra -

phy of the Los Angeles region best describes the source of emissions responsible

for the highest observed oxidant readings

In the rollback models used by EPA and others the basin is treated as a

big box with uniformly distributed emissions and peak oxidant is considered to

be proportional to total basinwide hydrocarbon emissions

The fact is that the middotemitted contaminants from which the smog is formed

and the effects which characterize that smog are not evenly distributed throughout

the Los Angeles Basin in other words the basin area under the inversion is not one

large box filled to all corners with homogeneously distributed air contaminants and

photochemical smog

Refutation of Big Box Myth

Examination of atmospheric contaminant concentrations refutes the big box

concept It is found for example that concentrations of djrectly emitted contam -

inants measured at a particular sampling site reflect the emissions within a rather

limited area around that site For this reason contaminant concentration levels

vary from one location to another and each has a characteristic daily pattern which

reflects the daily pattern of emissions in that area

middot 236

The big box concept is further refuted by the fact that peak concentrations

of carbon monoxide and oxides of nitrogen in areas of high traffic density were

fairly static prior to 1966 Thus they did not reflect the 45-50 per cent growth

in motor vehicle registrations and gasoline consumption which occurred in Los

Angeles County between 1955 and 1965 and which caused comparable increases in

total daily emissions of such vehicle-related contaminants This demonstrates

that growth was outward rather than upward so that a larger area of the County

began to be affected by photochemical smog but no area experienced smog ofJ

greater severity than that originally affected by smog formed from the vehicular

emissions which accumulated each weekday in central Los Angeles and were trans-

1 I

ported later that day to the San Gabriel Valley

1 Meteorological Evidence

To verify the geographical dependence of emissions and resulting atmospheric

concentrations let us examine the meteorology of these large areas of Southern

California Both the County and the Basin have many meteorological sub-regions

in which the patterns of wind speed and direction may be similar but within

which the patterns of air transport are parallel with those of adjacent sub-regions

and the respective air parcels do not ever meet or join

The characteristic patterns of inversion height and wind speed and direction

in these sub-regions and their patterns of vehicular emissions together have

created a network of source areas- -those in which the reactant contaminants accu -1T

i ~ mulate in the morning and begin to react--and related receptor areas--those to which

~ the products and associated effects of the photochemical reactions of the contamshy)

inants originally emitted in the source areas are carried by the late morning and

237 middot

afternoon winds ( sea breeze)

Wind-flow patterns show that characteristic patterns of transport for related

source area-effect area combinations are separate and parallel not mixing or

joining Each source area has its own reactor pipeline to its own effect area

or areas

To illustrate this source area-effect area relationship the typical flow of

polluted air from downtown Los Angeles to Pasadena was selected as a worst

case situation for in-depth examination Figure 4 shows that the air in downtown

Los Angeles on the morning of smoggy days moves directly from the central area

to Pasadena

Vehicular traffic is the predominant emission source in both downtown Los

Angeles and Pasadena Thus the air in each locality should contain CO Also

since oxidant would form in the air parcel moving from Los Angeles to Pasadena

oxidant levels would be expected to be higher in Pasadena than in downtown Los

Angeles

Figure 5 shows these relationships for the period 1960-1972 The atmosshy

pheric CO level is similar for the two areas while oxidant levels were higher in

Pasadena than in Los Angeles throughout this time period This demonstrates

that a significant amount of oxidant formed in the air as it moved to Pasadena

containing both the unreactive CO and the photochemical reactants for producing

oxidant Both CO and oxidant show a marked downward trend in each locality since

1965 which emphasizes the effect of vehicle exhaust controls and the correlation

between the localities

238

On a day which is favorable to the formation and accumulation of photoshy

chemical smog a contaminated air parcel normally originates during the

6-9 a m period on a weekday from an area of dense traffic centered just

south and west of Downtown Los Angeles It is oxidant generated within that air

parcel which usually affects Central Los Angeles and the West San Gabriel

middotK IJ l J

Valley area around Pasadena

The traffic area in which this smog had its origin is about the most dense

in Los Angeles County and has been so for the past 25-30 years No area

has a higher effective density thampn-this Using carbon monoxide which

1

is almost entirely attributable to motor vehicles as an indicator of such emis-

sions it is found that the concentrations of emitted vehicular contaminants

middotr i

measured in Central Los Angeles during the past 15 years confirms both this lack

of change in effective density and the absence of any area of any greater effective

density when local differences in inversion are acknowledged

This area the Central Source Area is depicted in Figure 4 The size

and shape of the Central Source Area was ch~sen to be large enough to reduce to

an insignificant level any diffusion or transport into this area from any externally

l generated reactants This conclusion is based in part on the trajectory studies

previously referenced as well as an analysis of the diffusion and transport parashy

meters for the area

239

The Central Source Area has been identified as that geographical region

which contributes essentially all of the primary contaminant emissions giving

rise to the highatmospheric oxidant levels in the West San Gabriel Valley

The proportion of emissions in the CSA due to motor vehicles and that due to

stationary sources is shown in Table 1 For the County as a whole about 80 per

cent of _(6-9) AM reactive hydrocarbons are due to motor vehicle emissions and this

figure rises to 90 per cent for the CSA The same conclusion a pp lies to NOx

emissions The Central Source Area contains the greatest density of vehicle traffic

in the County and thus the greatest density of source emissions Thus it appears

that the source area with the highest density of emissions during the critical (6-9)

AM period is responsible for the highest afternoon oxidant levels observed in Los

A i1geles County and in the South Coast Air Basin These highest oxidant levels

are consistently observed to occur in the San Gabriel Valley This is true whether

the LAAPCD or the ARB oxidant calibration procedure is used

Further the atmospheric concentrations of the primary pollutants can be

identified as originating primarily from the motor vehicle and they reflect the

effects of the motor vehicle emission control program A vehtcular source area

can be identified by its atmospheric levels of CO and NOx Figure 6 compares

measured atmospheric levels with calculated atmospheric levels for CO NOx

and the CONOx ratio in the downtown area

TABLE 1 240

REACTIVE HYDROCARBON EMISSIONS

(6-9) AM

1970

LOS ANGELES COUN1Y middot CENTRAL SOURCE AREA middot SOURCE TONS PER CENT TONS PER CENT

Mobile 1260 81 3 135 91 2

Stationary 290 187 1 3 88

Total 1s~o 1000 148 1000

By 7 -Mode Gallonage

241

The calculated values shown in Figure 6 were derived from a baseline

survey of 1100 vehicles and continued surveillance tests both using the Calishy

fornia 7-Mode test cycle The baseline survey showed that motor vehicles withshy

out exhaust control systems had average exhaust emissions concentrations of 3 4

per cent CO and 1000 parts per million of NOx Baseline emissions data apply

to 1965 and earlier model vehicleg and surveillance data to 1966 and later modelsmiddot

Since it can be concluded from calculations and observations that the dilushy

tion of auto exhaust emissions in the atmosphere on a smoggy day in Los Angeles

is approximately 1000 to 1 the calculated values for CO and NOx prior to 1965 are

34 ppm CO and 1 ppm NOxo After 1965 the changing effect of controlled vehicles

in the total vehicle population is reflected in the calculated values

CO and NOx values measured in the atmosphere are also shown in Figure

6 and confirm the values calculated entirely as diluted vehicular emissions NOx

concentrations measured in the atmosphere tend to be consistently a little lower

than the calculated values probably because photochemical reactions remove some

NOx from the system

The data for CO and NOx calculated and measured show that emissions in

downtown Los Angeles originate almost exclusively from motor vehicles and that

atmospheric concentrations there reflect the average emissions from a representashy

tive vehicle population

The ARB has recently published a report entitled A Trend Study of Two

Indicator Hydrocarbons in the South Coast Air Basin Acetylene was used as a

242

specific indicator of automobile exhaust emissions and it was found to have de-

clined in concentration in the Los Angeles atmosphere at an annual rate of 12 5

per cent since 1970 To quote from this report The California implementation

plan requires an annual average reduction in these emissions (reactive organic

compounds) of 166 tons per day or 11 1 of the 1970 tonnage per year The per cent

reductions in the_ acetylene levels at Los Angeles and Azusa are greater than reshy

quired by the implementation plan Since acetylene is almost entirely associated

J with auto exhaust this demonstrates that the motor vehicle emission control

program is achieving its purpose

To summarize at this point it has been deomonstrated that high oxidant values

are due to motor vehicular emissions of NOx and HC because

NOx and HC are the principal reactants in the oxidant formation process

and they originate primarily from motor vehicle emissions and

The highest oxidant values are recorded in_ effect areas that receive air

from source areas where motor vehicles are clearly identified as the

dominant source of NOx and HC

243

Future Control Strategy

The APCD strategy for achieving and maintaining the oxidant air quality

standard is based upon the fact that high oxidant values are due to motor ve-

hicle emissions of hydrocarlxms arrl nitrogen oxides This strategy is as follows

1 Both Hydrocarbon and Nitrogen Oxides Emissions Must Be Considered To Achieve the Federal Oxidant Standard

There is wide agreement that NOx and HC are the principal reactants in

the oxidant formation process and that vehicular emissions are a major source

of NOx HC and CO

2 Effective Regulation of Atmospheric Concentrations of Both HC and NOx and of the Ratio Between Them is necessary for Attainment of the Federal Air Quality Standard for Oxidant

Basmiddoted on the abundance middotof available experimental evidence it is our firm

position that the most rational approach to solving the photochemical oxidant smog

problem in the South Coast Air Basin (SCAB) is to control the quantities of emissions

from motor vehicles of both smog precursors--Hcmiddot and NOx--their resulting atmosshy

pheric concentrations and the ratios between both contaminants which will result

from these controls

We arc also convinced that the oxidant and nitrogen dioxide air quality stanshy

dards can and will be met not by 1975 or 1977 but by the early 1980 s if the emisshy

sion control program as originally outlined by Ca~ifornia or a slight modification

of it proposed by the District is followed and enforced This should also provide

for continued compliance with these air quality standards at least through 1990

244

It will also allow time for a reappraisal in about 1978 of the whole situation relative

to the ultimate emission standards required and the best approach to their impleshy

mentation

Calculation of the degree of control necessary to attain the air quality

~ standards for oxidant and nitrogen dioxide involves indirect complex methods 1

aimed at determ_ining the degree of control of the primary contaminants directly

emitted by automobiles

The following evidence supports our proposed solution to the problem in

terms of both the atmospheric concentrations of the oxidant precursors NOx

and HC the ratio between them as reflected in their exhaust emission standards

and the resulting atmospheric concentrations of oxidant which comply with the air

quality standards

Chamber Results and Projections to the Atmosphere

The importance of environmental chamberwork cannot be minimized the

j need for and direction of the whole emission control program was based initially

j on the results of chamber experiments In order to understand the importance to

air quality of achieving both the correct low quantities of emissions and the right

ratio we can present several graphic portrayals of analyses of experimental labshy

oratory work together with their relationship to past present and future air quality

in terms of both morning primary reactant concentrations during the morning

traffic peak and the equivalent emissions which would produce them

245

Figure 7 shows maximum ozone levels that were obtained by irradiating

varying amounts of auto exhaust hydrocarbons and oxides of nitrogen in an environshy

mental chamber The corresponding ozone levels then can be found for any comshy

bination of BC and NOx concentrations Thus high ozone is produced with high

emissions of both hydrocarbons and oxides of nitrogen and low oxidant is formed with

low emissions However either low NOx or low HC emissions11 can also produce

low oxidant--graphic and clear evidence of the importance of the NOxHC ratio in

ozone formation Furthermore each and every possible combination of values for

NOx and HC has then a corresponding characteristic maximum chamber ozone

concentration

Using this graph we can estimate what ozone levels would result if certain

atmospheric mixtures of NOx and HC could be injected into the chamber and

irradiated Such estimates were made for 1960 and 1965 using atmospheric data

rlThe points labeles 1960 and 65 show the location of the highest levels of both

HC and NOx found in the air in those years in Downtown Los Angeles (OOLA) area

during the 6-9 AM traffic peak

It has been demonstrated by use of CO and NOx data and CONOx ratios

hnw well the characteristics of vehicle emissions are reflected in the atmosphere

We know what emissions from the average vehicle were then in 1960-1965 both

for HC and NOx so that we can mathematically relate emissions to atmospheric

concentrations for those years and so for future years also knowing or calculating

only what the characteristic emissions will be from the average vehicle

246

The NOx concentrations stayed about the same from 1960 through 1965 because

average vehicle emissions of that contaminant did not change during that time

Mobile source emissions can be shown to have contributed essentially all of this obshy

served result However blow by controls did reduce emissions of HC and the

concentrations dropped accordingly In 1965 the last year before exhaust controls

the point 65 indicates where we were then in terms of maximum ozone formation

to be expected in a chamber with the highest HC and NO concentrations found in the X

air that year Levels of ozone actually measured in the atmosphere however

are higher than those shown on the graph for high NOx and I-IC concentrations for

those years up to the present

The strategy to meet the oxidant standard is obvious--get atmospheric NOx

and HC concentrations out of the area on the chart that produces high ozone levels

and put them in tie areas with the lowest levels This can only be done by implementshy

ing appropriate emission standards

As can be seen that did not happen between 1965 and 1970 because manufacshy

turers used controls on new cars in California which while causing a decrease in

BC (and CO) allowed a large increase in NOx emissions Thus the path line of

the atmosphere on the chart goes up from 65 and diagonally to the left passing

through an area of higher ozone levels The atmospheric concentrations of oxidant

predictably increased during the years 1967 and 1968 By 1970 they dropped to lower

levels - -back to about the same as in 1965- -exactly as predicted by the model The

app14oximate location of the point for 1970 (70) was both predicted on the basis of

247

the mathematical model and confirmed by atm-ospheric measurements of

[)owntown Los Angeles morning summertime NOx and calculated HC values

Again it should be pointed out that those points show the highest possible

concentrations of NOx and HC Years with less restrictive weather conditions

(for accumulating high primary contaminant levels) would cause lower measured

maximum NOx and HC levels but the calculations would still yield the points

shown Thus we are taking the most pessimistic view

Future Projections

In 1973 we were at about the point labeled 73 and ozone levels were beginshy

ning to drop as expected middot It should be emphasized that ozone values plotted on

thi$ graph are for the chamber only- -not the atmosphere The future path the

points 7 4 and on to 90 represents our estimate of future atmospheric levels of

NO and BC expected if the exhaust emission standards are just met While that X -

is optimistic it is all we really can do since performance of future vehicle models

is unknown We will achieve maximum ozone levels at or below the standard by

about 1980-1985 This will only be true however if cars in compliance with the

California interim standards for HC and NOx continue to be added to the vehicle

population at the normal rate These standards provide the optimum ratio of NO X

to HC necessary to provide the nitric oxide (NO) needed for the reaction that re-

moves from the air both oxidant formed photochemically and oxidant which occurs

as natural background which alone may cause the standard to be exceeded This

ratio is about 112 or 2 parts NOx to 1 part HC

248

The optimum NOxHC ratio is a key element in the APCD strategy but will

require a finite time for its attainment Replacement of older cars by newer ones

equipped to meet the most stringent standards is the only reasonable mechanism

which can change it VMT reduction proposed as a prime strategy by EPA cannot

change this crl(ical ratio which is a basic characteristic of the population at any

given time

Validation of the Districts Control Strategy

Figure 8 compares (1) future chamber oxidant levels based upon the

future maximum concentrations of HC and NOx we expect each year with the

California control program (2) calculated atmospheric concentrations using ~ I

our chamber-to-atmasphere empirical translation and (3) actual measured atmos-f 1l pheric oxidant maxima This clearly sets forth the relationship among these three

factors

The chamber concentrations (lower curve) middotare the lowest values shown

The actual atmospheric data (points connected by heavy dotted and solid lines)

vary considerably from year to year partly because of the vagaries of the weather

In all cases the atmospheric oxidant values are higher than the chamber values

because of the addition of vehicle emissions as the air parcel travels from source

to receptor areas The calculated atmospheric data (thin dashed and solid curves)

are shown to be the highest generally exceeding or equalling the actual measured

data and of course always exceeding the chamber data Thus the model paints

the most pessimistic picture possible It can be seen that by about 19801 1985 atmos -

pheric levels should be at or below the Federal air quality standard of 0 08 ppm oxidant

249

3 Motor Vehicle Exhaust Control is the Only Requirement for Achieving the Oxidant Standard by 1980

We can show that the existing motor vehicle control program has resulted

in a significant reduction of oxidant concentrations in the air

The foregoing material explained the relationship between vehicula~ emis -

sions in source areas and the high oxidant levels measured in effect areas This

relationship is exemplified by the downward trend of oxidant levels in the atmosshy

phere and by the similar year-by-year trends of NO and HC emissions from the X

average motor vehicle A projection of these vehicle emissions factors shows that

the associated maximum oxidant level in the atmosphere will meet the oxidant standard

by about 1980-1985

Figure 9 compares by year the number of days that the oxidant air quality

standard was exceeded in three separate areas with the average NO and HC emissions X

per vehicle mile To comply with the air quality regulations the number of days that

this standard is exceeded must be reduced to one per year

The lines plotted on Figure 9 show that a definite relationship exists between

the emissions from the average motor vehicle and the number of days each year that

the oxidant concentration in the air exceeds the clean air standard

The oxidant trendlines for downtown Los Angeles Pasadena arrl Azusa are

all downward and the slopes are about the same This similarity is logical because

the process that results in the suppression of oxidant accumulation simply has been

displaced from one area to another This was a unique one time situation because

of the increase in NOx between 1966 and 1971 After 1971 all areas are down Thus

l

250

the same conclusion is reached that the oxidantstandard will be met in the 1980s

I whether air quality data or vehicle emissions trends are projected middot~ Ul-

This outlook is based on the APCD s belief that future growth in both the

Los Angeles area and SCAB will not create any locality with a traffic density greater

than any traffic density in the area to date For the past 25 years the area around

downtown Los Angeles has been the area of maximum traffic density and therefore

the emissions source area responsible for the maximum effect area measurements

It is assumed that the traffic density in any future source area will be no

greater than the traffic density in downtown Los Angeles Thus since the

vehicular emissions control program will achieve and maintain the air quality

standards in areas affected by vehicular emissions from downtown Los Angeles it

will also achieve and maintain them for any area of SCAB

Summary Conclusions and Recommendations

In conclusion we have shown that a source and effect area analysis of emisshy

sions and resulting oxidant is a more reasonable and accurate representation of

the Los Angeles area for air quality analysis than gross integration metho9s such

as the big box technique It has been shown that motor vehicles are the major and

almost sole contributor to the primary HC and NOx emissions in the downtown source

area which results in the high oxidant levels in the San Gabriel Valley in fact the

highest in SCAB An air quality model and vehicle emissions control strategy has

been suggested to meet the oxidant standard by mid-1980 s

251

We have shown that

bull Only by adjusting the ratio of NOxHC in the motor vehicle emissions to

permit accumulation of sufficient atmospheric NO to sea venge the normal

atmospheric background oxidant can the standard be attained

bull The APCD strategy which provides for implementation of the present

California interim emissions standards for NOx HC and CO for new

motor vehicles in California beginning with the 1975 model vehicles will

result in compliance with the CO N02 and oxidant air quality standards

by the mid 1980 s and will maintain this compliance until 1990 and

possibly longer

bull The effectiveness of the present California motor vehicle control program

is easily demonstrable using air quality data from several areas in Los

Angeles County 1960-1973

bull To assure achievement and maintenance of the air quality goals as now preshy

dicted there must be periodic assessments of the effectiveness of the

motor vehicle control program followed by corrective actions if necessary

What has been accomplished thus far is significant but much more remains

to be done so that the best possible representation of emissions and resulting air

quality may be available for use in this air basin A much better emission inventory

defining the spatial and temporal distribution of both mobile and stationary sources

is needed Better statbnary source information is needed to evaluate the local

effects of these emissions Further detailed studies are needed to establish the

252

true relationship between emissions data from vehicle test cycles and the actual

operation of vehicles neither the 7-mode nor the CVS procedure provides a true

representation of actual vehicle operation Further tracer studies to assess the

transport and dilution of mobile and stationary source emissions from selected

source areas are also needed

253

1111

IUD

a CC I w gt-

1111

1UO

IUD

I 990

IDJO

1180

1111

IUO

FIGURE I

HYDROCARBONS

STATIONARY SOURCES MOTOR VEHICLES

- --

8 12 II 20 742 2l IS 12 I 4

HUNDREDS

HYDROCARBON EMISSIONS STATIONARY SOURCES IN

OXIDES OF

0

OF TONSDAY

FROM MOTOO VEHICLES AND LOS ANGELES COUNTY

NITROGEN

STATIONARY SOURCES

MOTOR VEHICLES

011111111111111111110111bull1111111

IIIIIIHIIIIIIIIIHIUII

llillL Its rd

l1uu~111111u1111111

2 I O 1 J 3

HUND REDS OF TONSDAY

OXIDES OF NITROGEN EMISSIONS FROM MOTOR VEHICLES ANO STATIONARY SOURCES IN LOS ANGELES COUNTY

illl~ -~--~ i~-=i _J~l ~--~ bull_~L- I ~~~-~~--Z ~

6

6S-66 ox

ICS ~A~1 M

i ssmuwmmgt

bullI

e COROyent_

64 ~ IDB RIVERS~

ORAJfD

-

t t 10 miles

bullmiddotsame Avg Cone Both Years

Pigare 2

YEAR OP HIGHEST OXlDANI CONCENTRATIONS

Highest Average of Daily -Maiimum One-Hour Concentrations

During July August amp September 1963-1972

bullLj

I

64

70 s11 3RlU)U0

70

--__ 69bull

N V +=

middot Source Air Resources Board

-200o

t t 10 adlea

tDS ampIJtsect

-1~

-1611ASampXllmiddot bull - bull -z----~------

I ldmmprwJ

IIVERSIDI

~ - 70

OampY -1 U 70 bull L

I

N V1 V

middot-i___

-----------------------------------------------------------i----------------------------

Figure 3

CHANGE OP OXIDANT CONCENTRATIONS

Percent Change from the Highest Three-Year Average to the 1970-72 Average

Of Daily Maximum One-Hour Con~entrationa for JulY August amp September

Source Air Resources Board

256

FIGURE 4 TYPICAL FLOW OF POLLUTED Am PARCEIS CIUGINATING AT DIFFERENT LOCATIONS IN THE LOS ARE~S BASIN - STARTIOO 0900 PST

l I

OAT

TRAJECTORY SUWMATIOl4

----- SMOG ~AVS

I

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullNONbullSlfOG DAYS

ISTARTING Tl~ cgxpsy

~ HAW

(CA

257

FiGURE 5 ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AND OXIDANT IN DOWlflC1N LOS AIDELES (SOURCE AREA) AND PASADENA (EFFECT AREA) 1

1960-1972

LO CARBON MONOXIDE

30

Pasadena

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotbullbullbullbullbull Downtown Los Angeles

20

10

o_______________________________

OXIDANT

)

2 Down~ Los Angeles

1

o________________________ 1960 1962 196L 1966 1968 1970 1972

YEAR

bullbullbullbullbull

bullbullbullbullbullbullbull

258

FIGURE 6 COMPARISON 01 CALCULATED AND MEASURED ATMOSPHERIC CONCENTRATIONS OF CARBON MONOXIDE AN1) OXIDES OF NITROOEN IN DCMNTOWN IDS AIJELES

196o-1972

CARBON MONOXIDE

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ~ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot _-- ---_ middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~ ----middotmiddot-bullw-_~ ---bullbullbull

10

o_______________1111111_____

OXIDES OF NITROGEN25

20

15 bullbullbullbullbullmiddotmiddotmiddotmiddotbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ~

1-i 10 middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot ---

oS o_______________________

RATIO CONOx

40

50

0 +raquo Cd

p 30

~ 20

middotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot bullbullbullbullbull middotmiddotmiddotmiddotmiddot-shybullbullbullbullbull 0 u

bullbullbullbullmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddotmiddot 10

0 j

ilI 196o 1964 1968 1970 1972 I

YEAR

Measured~D-owntown Los Angeles (90th percentile ofmiddot daily] instantaneous maxima)

Calculated - Aver~ge vehicle emissions - Present control program

259

FIGURE 7

25

t i5

flJ

~ on ~ ~ Q) bO 100 Jo

+gt on z

o5

EFFECT OF CALIFORNIA 1 s AUTO EXHAUST CONTROL ffiOORA M ON MAXIMUM CHAMBER OZONE CONCENTRATION

- PPM

357bullbull

r 76 bull

11 l

30

20

CHAMBER OZONE MAXIMUM

50

10

o___________111111111111______111111111111_____________

0 05 10 15 20 25

Hydrocarbons m-2 (LB-15) - PPM (as Hexane)middot

--

bull bull bull

r--=--~1 ~a==-~ - _~l ~ y--===-- ~~--~-- ~ r---~~

o

o8

~ I

~ 0 H 8 o6 I

c~ ~ 0 z 0 0

8

~ o+ A H gtlto-

02

middoto

Figure 8 Calculated t1ax1mum Levels Instantaneous and Hourly Average

of Atmospheric Oxidant Compared to Measured Los Angeles County Maxima-with Projections to 1990

(California Standards)

~ -Calculated Inst ax ~

f Calculate Max Hr Avg 03

_ bullbull _ _ - i bull

0 bullbull -l bullbull a0Ieasured Inst Lax o3 bull middotmiddotmiddot~bull 0bull _ ____ V ~ ea~ured ~ Hr Avr o3

~~ r---

~ ~ NB r~ima for 197 4 amiddots of 121074--- -_ Chamber Ozone F ~_ _~

- 1L_

~ Federal Primarfo Air ~uality Standard ~6- -UaximumT- our Avera~elr~ppm-------------- --~ ------- -~- -~-- ~

I I I I I I I I I I I I I I I I I N1 O

1960 6i 64 66 ~i middot-o 72 74 76 79 middotso middot92 84 bullg s9 9o

TBAR (end)

0

261 FIGURE -OMPARISON OF ATMOSPHERIC OXIDANT TRENDS WITH AVERAGE NCJx AND

HC EMISSIONS (Grams per Mile from Average Vehicle)

JOO Number of days state oxidant standara wds equalled or exceeded

--- Azusa __ Pasadena ________ Downtown Los Angeles

20

15 u

___ Hydroc_arbons Oxides of Nitrogenbullmiddotmiddotmiddotmiddotmiddotbullbullmiddot 1975 and later-assume middotcalifornia ARB standards

o_ ___________________________11111____

1965 1970 1975middot 198omiddot 198S 1990