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THE DESIGN AND CONSTRUCTION OF AN ABSOLUTE PERMEAMETER TO MEASURE THE
EFFECT OF ELEVATED T F E R A T U R E ON THE ABSOLUTE PERMEABILITY TO DISTILLED WATER OF UNCONSOLIDATED
SAND CORES
A R e p o r t S u b m i t t e d t o the D e p a r t m e n t of P e t r o l e u m E n g i n e e r i n g
of Stanford University in Pulf illment of the R e q u i r e m e n t f o r the
D e g r e e of Master of Science
BY A b r a h a m S a g e e v D e c e m b e r , 1980
To Michal
Acknowledgments
I would l i k e t o express s i n c e r e app rec i a t i on t o my research adv i so r ,
D r . Henry J . Ramey, Jr. , f o r h i s advis ing , guiding , and support ing m e
throughout t h i s work.
Many thanks are due t o my f r i e n d s and t h e department s t a f f who helped
m e f i n i s h t h i s work.
F inanc i a l support was provided through t h e Stanford Geothermal Pro-
gram by t h e Department of Energy, Grant No. DE-AT03-80SF11459.
i
Abstract
A new a b s o l u t e permeameter was designed and const ructed i n o rder t o
i n v e s t i g a t e t h e e f f e c t of temperature on a b s o l u t e permeabi l i ty . The main
g o a l of t h i s work was t o improve t h e c o n t r o l s of t h e permeameter and t o
i n v e s t i g a t e t h e f low of d i s t i l l e d water through unconsolidated s i l i ca
sand cores . No s i g n i f i c a n t change i n t h e abso lu te permeabi l i ty WLth
a change i n temperature was observed. This r e s u l t is d i f f e r e n t than
r e s u l t s r epor ted i n previous work done a t Stanford . It is be l i eved
t h a t system problems, such as converging f low i n t h e core p lugs ,
caused t h e observat ion of pe rmeab i l i ty reduc t ion wi th an i n c r e a s e i n
temperature.
This work w i l l be extended t o consol idated sandstones and w i l l a i d
i n t h e des ign of r e l a t i v e permeabi l i ty experiments.
ii
Table of Contents
Acknowledgements
Abstract
L i s t of I l l u s t r a t i o n s
L i s t of Tables
1. In t roduc t ion
2. Apparatus Descr ip t ion
2 .1 .
2.2
2.3
2.4
2.5
2.6
2.7
2.8
2.9-
2.10
2.11
2.12
2.13
2.14
A i r Bath Set-up
Water Pump and Accumulator
Excess Flow Loop
F i l t e r s
Confining P re s su re System
Core Holder
Temperature Recording
P re s su re Di f fe rences Recording and Ca l ib ra t i ng
Cooling System
Flowrate Measuring
In t ake Water System
Vacuum System
Gas System
Valve Manif o ld
3. Apparatus Improvements
3.1 Vibra t ions i n t h e A i r Bath
3.2 Accumulator
3.3 Excess Flow Loop
3.4 P re s su re Taps
3.5 Core Plugs
3.6 Sand Sieving and Cleaning
Page i
ii
v i
v i i l
1
3
3
6
6
8
8
10
10
10
15
17
18
18
18
19
21
21
21
23
23
25
26
iii
Table of Contents , cont.
4 . Procedure 29
29
29
31
31
31
33
33
33
34
35
35
36
36
37
37
38
38
39
39
, 4 2
42
42
4 3
4 3
4 3
44
4 . 1
4.2
4 . 3
4 . 4
4 .5
4.6
4.7
4 . 8
4.9
4 .10
4 . 1 1
4 .12
4 .13
4 .14
4 .15
4.16
4.17
4 .18
4.19
4 .20
4 .21
4.22
4 .23
4 .24
Sand P repa ra t ion
Sand Packing
Geometry Measuring
Core Holder Packing
Confining System Pre loading
P res su re Transducer Calibration
F i l t e r In spec t ion and I n s t a l l a t i o n
Charging t h e Accumulator
Washing t h e System (without t h e core)
S e t t i n g t h e Excess Loop P res su re
Vacuuming of t h e System (without t h e core)
I n s t a l l i n g t h e Core Holder i n t h e A i r Bath
Charging Confining Water and P res su r i z ing
Vacuuming t h e System
Flooding and P res su r i z ing t h e System
I n i t i a t i n g Flow, Temperature Recording, Ap Recor-
ding , and Cooling System Flow
Measurements a t Various Flowrates a t a Constant
Temperature (T, Ap, q)
Heating t h e System
Cooling t h e System
Stopping t h e Flow
Confining P r e s s u r e Bleed O f f
Removing. : t h e Core Holder
Taking t h e Core Holder Apart and Inspec t ing It
Problems
4 . 2 4 . 1 F i l t e r Plugging
4.24.2 Plugging of t h e Down Stream Needle Valve
i v
Table of Contents , cont .
5. Summary of Resu l t s
5 . 1 Permeabi l i ty Ca lcu la t ions
5 .2 Error Analysis
5.3 Resul ts of Runs 8 , 9 , 10, and 11
6. Conclusions
7 . References
8 . Tables of Data
V.
45
45
56
58
65
66
67
L i s t of I l l u s t r a t i o n s
1.
2.
3.
4.
5.
6.
7 .
8.
9.
10.
11.
1 2 .
13.
1 4 .
15.
16.
1 7 .
18.
19 .
20.
21 4
22 a
23,
General view of t h e appara tus
Schematic diagram of t h e apparatus - water f low
A schematic diagram of t h e water pump, t h e accumulatbr-and t h e overflow loop
A schematic of t h e conf in ing p re s su re system
Core ho lder body
Up stream core plug
Down stream core plug
A schematic of t h e core ho lder
A schematic of t h e cool ing system
Flow rate measuring system
Main va lve manifold
"Old" accumulator arrangement
II New" accumulator p ip ing
"Old" p re s su re t a p s
"Old" head l o s s on t h e core
End e f f e c t s p r e s su re l o s s e s
Up stream and down stream core plugs be fo re improvement
Working s h e e t of geometry measurements and weights
Pressure d i f f e r e n t i a l record ing a t k measurements and during hea t ing
Heating cyc le p r o f i l e : 150°F t o 250°F, run number 11
Viscos i ty of water vs . temperature at 200 p s i a
V i scos i t y of water vs. temperature at s a t u r a t i o n p re s su re
p p'p sat v s . temperature
Page
4
5.
7
9'
11
12
13.
14
16 '
17
20 I
22
' 2 2
24
24
26
28
32
40
41 ,
48
50
. 5 1
v i
Page
24. V i scos i ty vs. temperature a t 200 p s i a (improved range 70°F t o 100 F) 52
25. Permeabi l i ty vs. temperature f o r 150 mesh sand, run number 8 60
26. Permeabi l i ty vs. temperature f o r 150 mesh sand', run number 9 ,6 1
27. Permeabi l i ty vs. temperature f o r 200 mesh sand, run number 10 62
28. Permeabi l i ty vs. temperature f o r 260 mesh sand, run number 11 63
29. Permeabi l i ty vs. temperature f o r runs 8, 9 , 10, 11 64
0
vPi
L i s t of Tables
1. Water v i s c o s i t y
2. S p e c i f i c volume of water ( a t s a t u r a t i o n )
3. S p e c i f i c volume of water ( a t 200 p s i a )
4. Water v i s c o s i t y and s p e c i f i c volumes a t 200 p s i a (used i n t h e c a l c u l a t i o n s )
5. Au and Av f o r va r ious temperatures
6 . kT and ACT f o r runs 8 , 9 , 10, and 11 -
ab re1
7 . Data f o r run number 8
8. Data f o r run number 9
9. Data f o r run number 10
10. Data f o r run number 11
47
53
54
55
57
67
68
7 1
7 4
77
v iii
1. In t roduc t ion
Absolute pe rmeab i l i ty is an important parameter i n t h e eva lua t ion
and performance of geothermal o r hydrocarbon r e s e r v o i r s . Primary produc-
t i o n of o i l and gas r e s e r v o i r s does no t change t h e temperature of t h e
system. This i s not t h e case i n geothermal r e s e r v o i r s o r i n many of t h e
EOR* p r o j e c t s . I n t h e s e r e s e r v o i r s t h e temperatures of t h e formations
change and, along wi th t h i s , many of t h e formation p r o p e r t i e s change. Ab-
s o l u t e pe rmeab i l i ty is an e s s e n t i a l parameter and t h e r e is a g r e a t need
t o study t h e e f f e c t of temperature on a b s o l u t e permeabi l i ty .
A g r i d of experiments i n v e s t i g a t i n g t h e e f f e c t of temperature on
a b s o l u t e permeabi l i ty has been c a r r i e d out throughout t h e last decade.
These experiments covered a range of rock types , f l u i d s , conf ining pres-
s u r e s and s e v e r a l o t h e r system c h a r a c t e r i s t i c s . It i s evident t h a t n o t
a l l t h e r e s u l t s are i n agreement. I n some cases t h e observat ions i n t h e
l abora to ry y ie lded d i f f e r e n t i n t e r p r e t a t i o n s by t h e resea rchers . Casse' (1974)
i n t e r p r e t e d a decrease of a b s o l u t e pe rmeab i l i ty t o d i s t i l l e d water of
Berea sandstone wi th an i n c r e a s e i n temperature as a temperature e f fec t .
Other obse rvers , inc luding Sydansk (1980) claim a permeabi l i ty reduc t ion
is due t o f i n e s migra t ion and n o t temperature e f f e c t s .
Upon searching t h e l i t e r a t u r e , another disagreement s u r f a c e s t h a t i s
somewhat easier t o set t le. There are d i f f e r e n t l abora to ry obse rva t ions
f o r t h e same experiments. Most of t h e s e disagreements can be s e t t l e d
by t ak ing a c l o s e look at t h e " control" t h e experimenter has of t h e system.
Runs have t o be repeated wi th improved systems t h a t w i l l g i v e m a x i m u m
* EOR means "Enhanced O i l Recovery"
-1 -
3nformation about t h e parameters included ' in t h e experiment.
This is t h e p o i n t at which t h i s work is in t roduced. Out of t h e
g r i d of p o s s i b l e experiments, one conf igura t ion of rock, conf ining and
pore p r e s s u r e s , and f l u i d was chosen. This work s t u d i e d t h e e f f e c t of
temperature on t h e a b s o l u t e pe rmeab i l i ty t o d i s t i l l e d water of unconsoli-
dated sand cores . Work done a t Stanford Univers i ty , p r i m a r i l y by Casse'
and Aruna(1976), produced adecreaseinpermeabi l i tywith an i n c r e a s e i n teppera-
t u r e . This decrease i n pe rmeab i l i ty could no t be explained by thermal
expansion, p o r o s i t y changes, o r o t h e r explanat ions t h a t were suggested,
such as s i l i ca- wate r a t t r a c t i o n . This work w a s set up t o des ign and
cons t ruc t an a b s o l u t e permeameter wi th improved system c o n t r o l s i n o rder
t o t a k e a c l o s e look a t t h e change of pe rmeab i l i ty wi th temperature.
- 2-
2. Apparatus Descr ip t ion
Figure 1 is a rough 60 axonometric view of t h e apparatus whi le 0
Figure 2 is a schematic of t h e system. Later i n t h i s chapter a l l t h e
components w i l l b e descr ibed i n d e t a i l . Most of t h e equipment ( a i r ba th ,
r ecorders , pumps) was used i n o t h e r experiments. The va lves , t h e tub ing ,
and t h e core ho lder are new.
2 . 1 A i r Bath Set-up
A i r Bath S p e c i f i c a t i o n s : "Blue M" by Blue M Electric Company, Blue
Is land , I L . Model #: POM - 1406C-1 Serial #: CD - 10690 Line Voltage: 240V/1 PH/60 Hz Temperature Range: To 343"C/650°F Line Currents: L1 - 40A, L2 - 40A
The a i r ba th houses t h e fo l lowing:
The hea t ing c o i l s b e f o r e t h e core The core ho lder Four (4) thermocouples Flow l i n e s Pressure recording l i n e s Confining p ressure l i n e
To minimize v i b r a t i o n t h e core holder hangs from t h e c e i l i n g of t h e
b a t h and s i ts on a rubber cushion. The tubing i n t h e ba th i s t i e d toge ther
i n va r ious p l a c e s w i t h thermal t a p e t o f u r t h e r dampen v i b r a t i o n .
The b a t h mainta ins a . cons tan t temperature. It has a v a r i a b l e '
hea t ing capac i ty and small temperature o s c i l l a t i o n s . The temperature
ba th w i l l h e a t up an increment of 100°F i n about f i f t e e n minutes. The
core hea t ing r e q u i r e s about two t o t h r e e hours.
The b a t h is equipped wi th a ven t which makes c o n t r o l l e d cool ing
p o s s i b l e . The b a t h had 100 hours of use when t h i s p r o j e c t began. The
p r o j e c t used another 370 hours.
- 3-
-4- . . .
n
J
. . I
W
I, - r4’
0
-5-
2 . 2 Water Pump and Accumulator
Water pump s p e c i f i c a t i o n s :
Lapp Pulsafeeder Model #LS. 20 Serial no. X-7704 Process Equipment Lapp I n d u s t r i e s Company, Inc . Leroy, NY
Accumulator s p e c i f i c a t i o n s :
Greero la to r Model f20-30 TMR 5 1/2 WS Serial #14008 30 cub ic inches A d i v i s i o n of Greer Hydraul ics , Inc. Los Angeles, CA
Figure 3 p r e s e n t s t h e pump and t h e accumulator. The
tubing and v a l v e s between "A" and I'D" are 1/4". (See s e c t i o n 3.2 f o r
o t h e r d e t a i l s ) . The gas l i n e c o i l and t h e f low l i n e c o i l s e p a r a t e t h e
pump from t h e recording elements. The c o i l s reduce v i b r a t i o n s t h a t
are caused by t h e pump and t r a n s f e r e d t o t h e t r ansducers . The pump i s
set d i r e c t l y on t h e f l o o r s o no v i b r a t i o n s are t r a n s f e r r e d t o t h e recording
t a b l e s . The pump can produce a maximum flow of about 1150 cc/hour a t
room condi t ions . This arrangement produced a good dampening of t h e p u l s e s ,
leaving them almost negligfble.2 I n o the r words, as can be seen i n Figure 18,
t h e th ickness of t h e l p s ' i p l a t e l i n e is p r a c t i c a l l y t h e th ickness t h e pen
produces.
2 .3 Excess Flow LOOD
F igure 3 p r e s e n t s t h e excess f low loop o r t h e overflow loop. This
f low system accep t s t h e d i f f e r e n c e of f low between t h e pump's output and
t h e f low i n t h e core.
The p ressure r e l i e f va lve i s a 1/4" "Nupro" va lve wi th swagelokk
f i t t i n g s . The opera t ing p ressure can be manually set a t a range of 150 psig
-6-
-7-
t o 350 ps ig . The v a l v e is set h o r i z o n t a l l y i n o rder t o g e t a constant
behavior of both t h e sp r ing and t h e t r a v e l l i n g seat. I n a d d i t i o n t o t h e
improvement i n t h e f low c o n t r o l descr ibed i n s e c t i o n 3 . 3 , t h e loop provides
a s a f e t y va lve f o r t h e whole system. Most important ly , i t p r o t e c t s t h e
accumulator f r m a 25% i n c r e a s e i n t h e l i n e p ressure . This high p r e s s u r e
would blow t h e diaphragm i n t h e accumulator.
2 .4 F i l t e r s
There are two p a r a l l e l up stream f i l t e r s and one down stream f i l t e r .
Seven micron f i l t e r s were used al though o t h e r types of f i l t e r elements ( 6 0 ~ )
can be used.
The up stream f i l t e r s cannot b e changed dur ing t h e run. Some a i r
would be d r iven i n t o t h e core . B u t ' t h e f low can be d i r e c t e d through e i t h e r
one of them. This doubles t h e time f o r plugging. The down stream f i l t e r
can be changed i n t h e middle of a run. Figure 2 shows t h e l o c a t i o n of t h e
f i l t e r s .
2.5 Confining Pressure System
Figure 4 p r e s e n t s a schematic diagram of t h e confining p ressure
system. Water .was used i n s t e a d of o i l i n t h e conf ining chamber
of t h e ' core holder . This e l imina tes contamination of t h e down .
stream if a f a i l u r e should happen. Furthermore, a s p i l l of o i l i n t h e b a t h
at 300°F can b e - dangerous . The p ressure is app l ied by an
"Enerpac" hand pump r a t e d a t 10,000 ps ig . The pump i s o i l opera ted. The
conver t ing v e r t i c a l v e s s e l (see Figure 4 ) is no t i n t h e bath . The o i l i n l e t
is on t h e t o p and t h e water o u t l e t is on t h e lower p a r t . The volume of t h e
v e s s e l is l a r g e r than t h e conf ining chamber i n t h e core ho lder so t h a t no
-8-
-L c
r' gJAiE2
Q
c
-9-
o i l can g e t i n t o t h e ba th .
The p ressure gauge is a "Helicoid" gage U.S .A. , 8 1 / 2 W, 10,000,
50 l i b s . , subd. f1 /4% accuracy.
2.6 Core Holder
The core ho lder . c o n s i s t s .' of t h r e e p a r t s : (1) The core ho lder body,
Figure 5; (2) The up stream core plug, Figure 6: and (3) The down stream
core plug, Figure 7 .
It is r a t e d a t about 4000 p s i g conf ining p ressure . The core plugs
are sea led by ''o" r i n g s a t both ends. The v i t o n s l e e v e suppor t ing t h e sand
i s he ld i n an aluminum per fo ra ted sleeve. The assembled core ho lder is
presented i n F igure 8. This core holder w a s redesigned by Mr. A. S u f i , and,
t o d a t e , has been performing very well.
2.7 Temperature Recording
Five (5) thermocouples are scanned about once i n t e n (10) seconds
by a Leeds and Northrup Speedomax Recorder. The recorder has twenty-four
channels and a range of 0°F t o 600°F. Figure 8 shows t h e l o c a t i o n of t h e
f i v e thermocouples: (1) i n stream, up stream of t h e core ; (2) i n stream,
down stream of t h e core ; (3) up stream core plug metal; ( 4 ) core holder
body s u r f a c e ; and (5) out f low temperature e n t e r i n g t h e f l o w r a t e metering
b u r e t t e . A l l thermocouples were checked and t h e recorder c a l i b r a t e d p r i o r
2.8 Pressure Differences Recording and Ca l ib ra t ing
The p ressure recording system inc ludes t h e fo l lowing: (1) p r e s s u r e
t a p s , 1/16" l i n e s open a t t h e sand f a c e s , Figure 8; (2) p ressure l i n e s
-10-
!
Figure 5 - CORE HOLDER BODY
-11-
z: Y w
-12-
I I
1 . 1 I I
. - I
I
’ . Figure 7 - DOWN STREAM CORE ’PLUG
-13-
Figure 8 - A SCHW3XC OF THE CORE HOLDER
-14- .
and va lve manifold, Figure 2; ( 3 ) t r ansducers , Figure 2 ; ( 4 ) pressure ind i-
c a t o r s , Figure 2; and (5) r e c o r d e r , Figure 2.
P ressure gauges read t h e p ressures up stream of t h e core and down stream
of t h e v iscometer , F igure 2 .
The s e n s i t i v i t y of t h e readings t o t h e l o c a t i o n of t h e p ressure t a p s i s
presented i n s e c t i o n 3.4. The core t ransducer has a 1 p s i p l a t e model KP 15.
The viscometer t r ansducer has a 5 p s i p l a t e . The p ressure i n d i c a t o r s (one
f o r each t r ansducer ) are model "CD 25" by Dynasciences Corporation. The
recorder i s a two (2) channel "Chessell BD9" Recorder.
The up stream p r e s s u r e gauge is a "Duragauge AIS1 3 / 6 tube and socke t ,
0-600 p s i , 5 p s i subd." The down Stream gauges are a "U.S. Gauge" make, 0-600
and 0-1000 p s i range. The accuracy of t h e t r ansducers is *l% of t h e p l a t e
value .
C a l i b r a t i o n is done by a manometer . A water manometer i s used
f o r t h e 1 p s i p l a t e and a mercury one is used f o r t h e 5 p s i p l a t e . The
mercury c a l i b r a t i o n is done wi th a n i t r o g e n cushion whi le t h e water ,columnl
i s appl ied d i r e c t l y t o t h e t ransducer .
The t ransducer p l a t e s can be changed dur ing a run. They are loca ted
high above t h e valve manifold and can be b led a f t e r r e i n s t a l l i n g .
They can b e r e c a l i b r a t e d dur ing a run as well.
2.9 Cooling system
Figure 9 p r e s e n t s t h e cool ing system. The f i r s t g o a l i s t o cool t h e
outflow from t h e b a t h t o room temperature. This i s done by running a c o i l
of t h e f low l i n e through a v e s s e l wi th t a p water c i r c u l a t i n g i n i t .
The second g o a l is t o keep t h e water flowing through t h e f i n e needle
-15-
c FI!.TER
J
-16-
va lve at a constant room temperature. The performance of t h e va lve
is very s e n s i t i v e t o changes i n room temperature. The temperature
is kept constant by surrounding t h e 1/8" f low l i n e s wi th a 1/4" flow
l i n e and l e t t i n g t a p water run i n t h e annular space. This cooling
exchanger is l o c a t e d be fore t h e needle va lve .
2.10 Flowrate Measuring
Figure 10 shows t h e simple system t h e a t was used t o measure f lowra te . --..---.--------- -_I.--I_____.___ __r __._. __cc.____, - -
l . 1
I
A very important po in t must be made h e r e and it w i l l be s t r e s s e d
i n o t h e r p laces throughout t h e r e p o r t . It is s a i d t h a t 10 cc are measured
f o r a l l f l o w r a t e s . Perhaps due t o a t h i n l a y e r of water, only 9.8 cc are
a c t u a l l y measured. This w i l l i n t roduce an e r r o r i n t h e a b s o l u t e v a l u e of
k, but as long as t h e measuring procedure is followed i n t h e same way
-17-
every time, an e r r o r i n t h e r e l a t i v e changes i n k is n o t . introduced.
The time needed t o produce t h e given volume i n t h e b u r e t t e is measured
by a "Precis ion S c i e n t i f i c Com." timer , which is good t o about 0.05 seconds,
cat. iI69230, 120V - 60 cyc l e s .
2.11 I n t a k e Water System
I n o rde r t o be a b l e t o change t h e i n t ake water r e s e r v o i r without
s h u t t i n g down t h e pump and without g e t t i n g a i r i n t o the s u c t i o n , a two
s t a g e feed ing system was b u i l t (Figure 1). The l a r g e r r e s e r v o i r , #15 , is
a f i v e ga l lon g l a s s b o t t l e t h a t can be replaced. Water is syphoned
t o t h e primary r e s e r v o i r , i h 7 , a 4000 cc glass b o t t l e . This lower primary
r e s e r v o i r i s n o t touched during t h e run and t h e pump's suc t ion end is never
above water l e v e l . An a d j u s t i n g va lve is loca ted on t h e syphon between
t h e two r e s e r v o i r s and it is set in such a way t h a t t h e l e v e l of water i n
t h e low r e s e r v o i r is cons tan t (around t h e 4000 cc mark).
2.12 Vacuum System
Vacuum is appl ied by t h e vacuum pump. A l i q u i d t r a p is loca t ed between
t h e pump and the flow lines. The vacuum is measured with a "Labconco"
mercury gauge which is good t o 5 mic ro to r r . The gauge is disconnected
be fo re flow is i n i t i a t e d t o p r o t e c t i t . . .
2.13 Gas System
A 2200 ps ig n i t rogen b o t t l e supp l i e s gas t o charge t h e gas chamber
i n t h e accumulator. It a l s o supp l i e s gas t o t h e up stream o r down stream
ends of t h e core i f gas f lood i s des i r ed (Figure 2) .
-18-
2.14 Valve Manif o ld
Figure 11 p r e s e n t s a schematic diagram of t h e va lve manifold. All t he
gas va lves and t h e t ransducer va lves are needle v a l v e s , i n s t a l l e d t o pre-
vent shocks. The down stream c o n t r o l valve' and , a u x i l i a r y valve ( 7 and 6 ~- ~
i n Figure 11) are f i n e needle va lves .
-19-
3
\a \. . @
1
"\ j \ 0
a 0
. .-
e. ...
1 I
i
3. Apparatus Improvements
Four major problems t h a t arose dur ing t h e f i r s t run were: (1) Noise
and pump p u l s a t i o n s a f f e c t i n g t h e t r ansducer ' s performance; (2) Control
of t h e average pore p ressure wi th varying f lowra tes ; (3) A c a l c u l a t e d
permeabi l i ty t h a t w a s f l o w r a t e dependent; and ( 4 ) Plugging of t h e down
stream need le valve . These problems were s t u d i e d i n order dur ing t h e
next seven runs. Actual ly , t h i s procedure y ie lded a s e n s i t i v i t y a n a l y s i s
of t h e behavior of t h e apparatus . The magnitude of t h e problems and t h e
ways f o r improving t h e apparatus are descr ibed i n t h e fo l lowing s e c t i o n s .
3 . 1 Vibra t ions i n t h e A i r Bath ~-
The flow was i n i t i a t e d a t room temperature. For a given accumulator
s e t t i n g and a constant f low t h e core t r ansducer (1 p s i p l a t e ) had a
c e r t a i n magnitude of o s c i l l a t i o n . When t h e b a t h w a s turned on, t h e o s c i l l a -
t i o n magnitude doubled. The main cause was t h e f a c t t h a t t h e core ho lder
sat on t h e b a t h f l o o r and t h e v e n t s ' v i b r a t i o n was picked up by t h e pres-
s u r e t a p s . The problem w a s solved by hanging t h e core from t h e main c e i l i n g
frame of t h e ba th . A rubber l i n i n g separa ted t h e core holder from t h e
frame t o f u r t h e r dampen t h e v i b r a t o n s .
3.2 Accumulator
The two following changes c u t t h e pump p u l s a t i o n e f f e c t on t h e core
t r ansducer by 50% each time.
The f i r s t accumulator p iping was t h e 1/8" tubing shown i n F igure 12.
-21-
Figure 1 2 - l'Old" Accumulator Arrangement
The connection t o t h e core a t poin t "A" was moved t o po in t "B" as is
shown in Figure 13. This put t h e accumulator i n t h e d i r e c t l i n e of t h e
pu l sa t ions and 'helped t h e accumulator absorb t h e pulses .
TO THE CORE 7"
Figure 13 - "New" Accumulator P ip ing
The second change was t h e replacement of t h e s e c t i o n of 1/811 tubing
-22-
3.3 Excess Flow Loop
A s e r i o u s problem arises when a p u l s a t i n g pump, an accumulator, and
a back p ressure need le valve are used. One must a d j u s t t h e o u t l e t flow t o
be e x a c t l y t h e same as the pump output . I f t h e flows are no t t h e same,
the accumulator e i t h e r loads o r unloads, hence varying t h e p ressure .
The problem was magnified when t h e accumulator unloaded i n t o t h e f lowing
system. Rust and gum (orange i n c o l o r ) would b u i l d i n t h e accumulator.
When unloading would occur , t h e r u s t and gum would plug t h e f i l t e r s
and accumulate i n t h e upper s e c t i o n of t h e core.
The two problems were solved by in t roducing t h e excess flow loop
presented i n Figure 3 . The p r e s s u r e r e g u l a t o r maintained a good average
up stream pressure , and as long as t h e output of t h e pump was l a r g e r than
t h e flow i n t h e core , t h e e x t r a flow e x i t e d through t h e excess loop.
The volume of t h e tubing between p o i n t "A" and po in t "B" (Figure 3 )
is l a r g e r than t h e maximum p u l s e of t h e pump. So no f l u i d t h a t went by
p o i n t "B" towards t h e accumulator could f i n d i t s way back t o t h e core .
T h r s c o m p l e t e l y i s o l a t e s contamination i n t h e accumulator from t h e core.
A l l up stream sand f a c e s of t h e cores were inspected and showed no evi-
dence of contamination a f t e r t h e excess loop was introduced.
3.4 Pressure Taps
Na tura l ly , i n t h e i n i t i a l cons t ruc t ion of t h e apparatus t h e p ressure
t a p s were as i n F igure 1 4 .
- 2 3-
FIGURE 1 4 - "Old" Pressure Taps
A t t h i s p o i n t a s e r i o u s f l o w r a t e dependency of t h e pe rmeab i l i ty was
experienced. By a l l means t h e flow i s laminar, as shown i n s e c t i o n 5 ,
hence t h e r e s h o u l d n o t be f low rate dependency. It is obvious t h a t
t h e Ap measured is n o t only t h e Ap of t h e core b u t inc ludes t h e Ap i n t h e
tubing s e c t i o n s A-B and C-D. S impl i f ied w e have t h e fo l lowing cond i t ion :
I I I CD
-c'
B C
"F igure 15 - l'O1d'' Head Loss on t h e Core
-2 4-
ApAB and ApCD are mostly a f u n c t i o n of V b u t some of t h e "T" and elbows
and o the r i r r e g u l a r i t i e s are a f u n c t i o n of V and hence are no t l i n e a r wi th
q as Darcy's l a w is . This y ie lded p a r t of t h e permeabi l i ty (k) dependence
upon t h e f l o w r a t e (9) . Varying t h e f lowrate (q) from 200 cc/hour t o
300 cc/hour caused a drop i n k of about 100 md from a l e v e l of 3500 md.
Figure 8 p r e s e n t s t h e s o l u t i o n t o t h i s problem. The p ressure t a p s
2
were made of 1/16" tubing and put i n t o t h e 1/8" f low l i n e s .
a t t h e sand face. This cu t t h e f low rate dependency of t h e pe rmeab i l i ty by
50%. This p r e s s u r e t a p . measures t h e k i n e t i c p o t e n t i a l of t h e flow:
A sample c a l c u l a t i o n shows t h a t t h e e x t r a Ap due t o t h e f low i s
negl ig ' ibae:
Ap = 14.7 y V 2
2g
Where : Ap Z p s i
y E kg/cm3 =
V E cm/sec E 0.3 (Maxhum flow)
so :
g cm/sec2 = 981
Ap = = 687, ir 10-9 psi 14 .7 x x 0. 32
2 x 981
3.5 Core plugs
As presented i n s e c t i o n 3 . 4 , t h e rate dependency remained.
It was reduced by h a l f b u t something was s t i l l wrong. A c l o s e r look a t t h e
core plugs is presented i n ' Figure 1 7 . As they were, t h e r e was a s e r i o u s
-25-
P W I T H O U T E N D EFFECTS
P WITH E N D EFFECTS
A B C D
I
FIGURE 1 6 - End E f f e c t s P ressure Losses
ApAB and ApCD are a f u n c t i o n of t h e flow. This was a
key f a c t o r once improved. The improved c o r e p lugs are presented i n
Figures 6 and 7 . Once improved, not only d i d t h e k dependency on q van ish ,
but k increased by as much as 30%. That is l o g i c a l s i n c e Ap decreased by
a l a r g e amount f o r t h e same flow.
3.6 Sand Sieving and Cleaning
F i n a l l y , t o complete t h i s s e c t i o n , one more problem was solved: t h e
plugging of t h e needle v a l v e t h a t sets t h e flow i n t h e core . The sand
w a s s i f t e d about f i v e times, and then washed wi th d i s t i l l e d water and d r i e d
a t 70°C. That improved t h e flowing s t a b i l i t y a g r e a t d e a l . The particles ~
plugging t h e needle v a l v e were sxaller than seven microns s i n c e a seven
micron f i l t e r is up stream of t h e valve . The sand sand sizes are about
-26-
130 t o 180 microns s o probably t h e flow of f i n e s d i d no t a f f e c t t h e
permeabi l i ty . 'Furthermore, a f t e r t h e f i r s t hea t ing cyc le t o 300°F , the
plugging e f f e c t p r a c t i c a l l y disappeared.
-27-
t
-28-
4 . Procedure
The main g o a l of t h i s s e c t i o n i s t o advance an opera t ing desc r ip-
t i o n so t h a t t h e work can b e reproduced. Furthermore, t h e mechanical
behavior of t h e system is one of t h e sources f o r an eva lua t ion of t h e
system and what can be done wi th i t i n t h e f u t u r e . Several problems and
disagreements may o r g i n a t e from a d i f f e r e n t and i n c o n s i s t e n t procedure.
Many schematics and diagrams i n o the r s e c t i o n s w i l l be r e f e r r e d t o i n
t h e fo l lowing s e c t i o n .
4 . 1 Sand Prepara t ion
The Ottawa s i l ica sand was c a r e f u l l y s ieved. Two sands were used:
mesh 120-150 (what i s l e f t on t h e 150 Mesh screen) and mesh 170-200 (what
is l e f t on t h e 200 mesh sc reen) . An i n i t i a l q u a n t i t y of about 500 cc of
sand is put on t h e top s i e v e . Then only t h e des i red mesh is res ieved
four (4) more times. Sieving time is about 15-30 minutes f o r every cyc le .
After a l a r g e enough q u a n t i t y of t h e two g r a i n s i z e s was on hand,
washing commenced. The c o a r s e p o r t i o n (mesh 150-120) was washed under
t a p water through a mesh 270 sc reen t h r e e times, about 5 cc of sand a t
a time. Then a l l t h e sand was washed t h r e e times wi th d i s t i l l e d water.
The f i n e r sand (mesh 200-170) w a s washed t h r e e times wi th d i s t i l l e d water,
not through a screen. The sands were d r i e d i n an oven a t 60"-70°C . I n o rder t o achieve a good s iev ing of t h e sand, t h e q u a n t i t y on every
s i e v e should be small. A t h i n l a y e r of sand w i l l expose a b e t t e r f r a c t i o n
of t h e g r a i n s on a s i e v e t o t h e ho les . One c y c l e of s i ev ing produced
10-30 cc of t h e s i n g l e mesh sand.
4.2 Sand Packing
1. Wash t h e up stream c o r e plug wi th water and acetone, and dry. P r o t e c t
-29-
t h e "o" r i n g from t h e acetone.
2 . Cut a 1 1 / 2 " x 1 1 / 2 " mesh 270 sc reen and p l a c e i t on t h e c o r e
plug end. Put t h e sc reen r i n g on and t a p down g e n t l y wi th a
p l a s t i c hammer. Be s u r e t h a t t h e sc reen is n o t dammaged. Cut
t h e e x t r a p a r t s of t h e sc reen below t h e r i n g . Inspec t care-
f u l l y . 3. Repeat s t e p s 1 and 2 f o r t h e down stream c o r e plug.
4 . Cutyan 8" p i e c e of v i t o n tubing. Square one end .and
wash it wi th water. Wash t h e aluminum per fo ra ted s l e e v e and push
t h e v i t o n i n t o t h e s l eeve . Center t h e v i t o n . Then dry t h e i n s i d e
of t h e v i t o n and, as much as p o s s i b l e , t h e aluminum s leeve .
5. F i t t h e squared v i t o n end onto t h e up stream core plug so t h a t
two t h i n g s happen: (1) t h e rubber sleeve goes as f a r on t h e end plug
as p o s s i b l e and (2) t h e aluminum sleeve over laps t h e core plug __
by t h e width of t h e sc reen r i n g , about 3/16". Clamp w i t h
a clamp t h a t does not exceed t h e aluminum s l e e v e diameter. Put
t h e clamp as c l o s e as p o s s i b l e t o t h e aluminum s leeve . Make s u r e
t h a t t h e clamp does no t cu t t h e rubber . The c o r e plug and
s l e e v e are set v e r t i c a l l y wi th t h e open end of t h e s l e e v e po in t ing
upwards.
6. Take 100 cc of sand i n a 100 cc beaker and weigh i t .
7 . F i l l t h e s l e e v e wi th 30 cc ' of sand.
8 . Use a s t a i n l e s s s teel rod about 2 1 / 2 " long and 3/8" i n diameter
wi th a rounded end. L e t i t drop on t h e sand from a he igh t of
about 2"-3". Pound t h e sand 50 times. (30 cc were used t o p r o t e c t
t h e up stream screen) Then t a p t h e aluminum s l e e v e wi th t h e handle
-30-
of a medium screwdriver , 50 times, a t t h e sand f a c e level,
whi le tu rn ing t h e core 360' (on a c i r c l e ) .
9. Repeat s t e p s 7 and 8 w i t h a 20 cc increment u n t i l t h e level of
t h e sand is 3/16" below t h e aluminum s l e e v e end.
10. Weigh t h e sand l e f t i n t h e beaker. (Figure 17)
11. Put up stream core plug i n p lace . Tap i t very gen t ly . Make
s u r e i t is vertical. Clamp i t as c l o s e as p o s s i b l e t o t h e alumi-
num sleeve. Cut t h e v i t o n a t t h e upper l e v e l of t h e upstream
core plug.
4.3 Geometry Measuring
For each run, t h e core dimensions were recorded on a d a t a s h e e t l i k e
F igure 18. The upstream measurements are taken 90 a p a r t . The down stream
measurements are taken 120 a p a r t .
0
0
4 . 4 Core Holder Packing
1. S e t t h e core ho lder body i n a vise wi th t h e f l a n g e p o i n t i n g upwards.
2. Clean "o" r i n g s ' housing. O i l t h i n l y .
3. O i l 'lo" r i n g s t h i n l y .
4 . Clean f l a n g e s u r f a c e s .
5. O i l b o l t s .
6 . F i t co re i n t o core ho lder body and t i g h t e n b o l t s i n a 90' alter-
na t ing manner. Use spr ing washers. Do n o t over t igh ten . Tighten
t o t h e same torque.
4.5 Confining System Preloading
Two th ings are done here : (1) Charge water i n t h e high p ressure v e s s e l
-31-
r -
v3 E-c
. o X. H
5 sq
... L
r
J
J
-32-
and (2)
1.
2.
3 .
4 .
5 .
I 6.
7 .
8 .
9.
charge o i l i n t h e hand pump.
Close v a l v e 3 4 .
Open v a l v e 32.
Open v a l v e 3 3 .
Connect a d i s t i l l e d water r e s e r v o i r t o p o r t B .
Connect a vacuum t r a p t o p o r t A.
P u l l a l i g h t vacuum u n t i l t h e water g e t s t o t h e vacuum t r a p .
Close v a l v e 3 3 .
Disconnect vacuum system.
F i l l o i l (vacuum o i l ) i n p o r t C of t h e hand pump.
4.6 Pressure Transducer C a l i b r a t i o n
C a l i b r a t i o n i s done w i t h a mercury manometer f o r t h e 5 p s i viscometer
and a water manometer f o r t h e 1 p s i p l a t e . For t h e c a l i b r a t i o n , t h e
t r ansducers are disconeected from t h e main system and once t h e i n d i c a t o r
and t h e recorder are c a l i b r a t e d , t h e t r ansducers are pu t back i n p lace .
4.7 Fi l te r Inspec t ion and I n s t a l l a t i o n
The p rev ious ly used up Stream f i l t e r s and t h e down stream f i l t e r are
disconnected and inspected. Usually, t h e f i l t e r elements have t o be changed
every other run. A f t e r j p u t t i n e f n anew f i l ter element (of t h e des i red spe-
c i f i c a t i o n s ) , t h e f i l t e r s are r e i n s t a l l e d .
4.8 Charging t h e Accumulator
Figure 3 . desc r ibes . t h i s s e c t i o n .
1. Take accumulator o f f , inc luding v a l v e 27.
2 . Wash l i q u i d p o r t .
3 . F i l l up l i q u i d p o r t w i t h d i s t i l l e d water wi th t h e p o r t f ac ing upwards.
-33-
4 .
5.
6 .
7.
8.
9.
10.
11.
1 2 .
13.
1 4 .
15.
Apply p res su re t o t h e gas p o r t u n t i l water f lows through v a l v e
27 (va lve f ac ing up) . A s water i s flowing through v a l v e 2 7 , c l o s e i t .
I n s t a l l t h e accumulator.
Charge t h e gas manifold wi th 300 ps ig .
Open va lve 20.
Close va lve 26.
Open va lve 1 6 u n t i l p re s su re i n t h e gas gauge is 195 ps ig .
Close v a l v e 1 6 .
The accumulator i s ready f o r use a t an average pore p re s su re
of 200 p s i g .
Close t h e main gas v a l v e on t h e b o t t l e .
Open va lve 1 9 t o bleed off t h e gas manifold.
Close va lve 1 9 .
4.9 Washing t h e System (without t h e core)
1.
2 .
3.
4 .
5.
6 .
7 .
a .
9.
10.
11.
Connect t h e by-pass in s t ead of t h e core.
I n s t a l l t h e by-pass f o r t h e down stream pres su re t a p .
Plug t h e upstream p r e s s u r e t a p ; c l o s e va lve 10.
Open v a l v e 8.
Open v a l v e 7.
Valve 5 p o i n t s a t va lve 7 .
Choose an upstream f i l t e r .
Open v a l v e 31.
Open va lve 28; make s u r e t h e r e i s water .
Close v a l v e 10.
Close va lve 1 2 .
-34-
1 2 . open va lve s 11, 13 , 14 .
13. S e t t h e pump a t 500 and t u r n it on.
14. Wash wi th 250 t o 500 cc.
4.10 S e t t i n g t h e Excess Loop Pressure
1.
2.
3 .
4 .
5 .
6.
7 .
8 .
Take t h e hose off t h e p r e s su re r egu l a to r (Figure 3 ) .
Open t h e ad ju s t i ng screws on t h e p r e s su re r e g u l a t o r .
Close va lve 7 .
Look a t t h e upstream gauge. It w i l l o s c i l l a t e *lO p s i around
150 ps ig .
Close t h e ad ju s t i ng screws on t h e p r e s su re r egu l a to r u n t i l t h e
p r e s su re on t h e upstream gauge o s c i l l a t e s around 250 p s ig .
Connect t h e excess flow hose.
Open va lve 7 and bleed.
S top t h e pump.
4 .11 Vacuuming of t h e System (without t h e core)
1.
2 .
3 .
4 .
5.
6.
7 .
8 .
9.
10.
11.
Close va lve s 1, 7 , 8 , and 9.
Connect t h e vacuum pump t r a p . S t a r t t h e pump.
Valves 2 3 , 22 remain c losed .
Open va lve 21.
Open va lve 15 t o d r a i n the t ransducer l i n e .
Open v a l v e 1 2 .
Close va lve 11; al low a few minutes t o pass .
Close v a l v e 1 2 .
Open va lve 11.
Close va lve 15.
Open va lve 10; a l low a few minutes t o pass .
-35-
1 2 .
1 3 .
1 4 .
15.
1 6 .
17 . 18.
Close va lve 10.
Open va lve 23 .
Open va lve 2 2 ; al low a few minutes t o pass .
Close v a l v e 22 .
Close va lve 23 .
Connect t h e vacuum gauge t o t h e va lve 23 p o r t .
Open va lve 23 and vacuum t o 2 t o r r o r less.
4.12 I n s t a l l i n g t h e Core Holder i n t h e A i r Bath
1.
2 .
3 .
4 .
5 .
6 .
7.
Close va lve 2 1 .
Open va lve 15.
Stop - the vacuum pump ;' ' allow a few minutes t o pass .
Disconnect t h e by-passes i n t h e ba th (two of than ) .
P l ace t h e co re holder i n t h e mounting device.
Connect t h e conf in ing p o r t , down stream p o r t , upstream p o r t ,
upstream thermocouple, upstream p res su re t a p , and down stream
pres s u r e t a p . Tape t h e s u r f a c e thermocouple t o t h e co re holder su r face .
4.13 Charging Confining Water and P res su r i z ing
1.
2 .
3 .
4 .
5 .
6 .
Remove t h e confining p res su re plug, loca ted a t t h e top cen te r of
t h e coreholder .
Open v a l v e 3 4 .
Pump u n t i l water comes out of t h e po r t .
Stop t h e above p o r t .
Pump confining prkssure t o 500 ps ig .
Bleed water from va lve 33 u n t i l o i l appears. .
-36-
7 . Close va lve 33.
8. P r e s s u r i z e t o 500 p s i g .
4.14 Vacuuming t h e system
1. Close va lve 15.
2 . Turn t h e vacuum pump on a f t e r emptying t h e t r a p .
3. Inc rease conf in ing p res su re by increments of 500 p s i p e r 10 minutes.
4 . Monitor vacuum q u a l i t y .
5. For a t least t h r e e t o fou r hours , reduce t h e vacuum t o 1 t o r r
o r less.
6. Check f o r confining p r e s s u r e l eaks and f o r movements of t h e down
stream plug.
7 . Be s u r e t o p r o t e c t t h e vacuum t r a p .
4.15 Flooding and P res su r k i n g t h e System
1.
2 .
3 .
4 .
5.
6.
7 .
8.
9 .
10.
Close v a l v e 23.
Disconnect t h e vacuum gauge.
Open v a l v e 1.
Turn on t h e pump and set i t a t 150 cclmin.
Allow time t o pas s u n t i l water e n t e r s t h e ' t r a p . . . 1 .
Close va lve 21 .
Stop t h e vacuum pump and disconnect t h e t r a p .
L e t p re s su re bu i ld up u n t i l t h e excess flow loop is flowing.
Open va lve 27 t o connect t h e accumulator.
Allow a few minutes f o r t h e p r e s s u r e t o s t a b i l i z e .
-37-
4.16 I n i t i a t i n g Flow, Temperature Recording, Ap Recording, and Cooling
System Flow
1.
2 .
3 .
4 .
5 .
6 .
7.
8 .
9 .
SFbitbh on t h e i n d i c a t o r s .
Turn on t h e cool ing water a t about 200-500 cc/min.
Turn on t h e temperature r eco rde r .
Open va lves 10 and 1 2 .
Close va lves 13 and 1 4 .
Open needle va lve -7 s l i g h t l y whi le watching t h e 1 p s i i n d i c a t o r .
Stop when t h e i n d i c a t o r shows 0.5 p s i .
S e t t h e pump a t 600 cc/min.
Allow 15 minutes t o one hour t o s t a b i l i z e .
B e s u r e t h e r e is always a f l o w through t h e excess loop.
4.17 Measurements a t Various Flowrates at a Constant Temperature (T, Ap, q)
To c a l i b r a t e t h e ' recorder (Ap reco rde r ) do t h e fol lowing:
For t h e viscometer:
1. Close v a l v e 1 2 .
2. Open v a l v e 1 4 .
3 . Adjust t h e recorder needle t o zero . Do not touch t h e i n d i c a t o r .
4 . Close v a l v e 1 4 .
5. Open v a l v e 1 2 .
Operate t h e va lves g e n t l y t o prevent shocks.
For t h e c o r e t r ansduce r :
6 . Close va lve 10.
7 . Open va lve 13.
8 . S e t t h e r eco rde r needle t o zero .
9. Close v a l v e 13.
10.' Open v a l v e 10.
-38-
The Ap on t h e core , Apc, can be read on t h e corresponding pen on t h e
recorder . F igure 19 shows an example of t h e Ap record,
Figure 20 shows an example of t h e temperature record,
When t h e four ba th thermocouple . r e c o r d s agree, t h e temperature
can be read on t h e s c a l e . (The recorder was preca l ib ra ted) ' .
Flow ra te measurements are made wi th a b u r e t t e . See F igure 10. The
f low rate is changed by c l o s i n g o r opening v a l v e 7 . Always b e s u r e t h a t
100-200 cc/hour flows through t h e excess loop.
4.18 Heating t h e System
The b a t h was p reca l ib ra ted ; The t a r g e t temperature was set
and hea t ing s t a r t e d ; Figure 20 shows t h e hea t ing p r o f i l e f o r run $111.
Heating of 50°F increments t akes 2 t o 2-1/2hours.While hea t ing , t h e conf ining
l i q u i d expands,-and is b led by v a l v e 3 3 . Valve 33 i s a need le v a l v e
and t h e bleeding should b e done g e n t l y t o prevent surges . Surges
can b e seen i n F igure 1 9 . Usually, when t h e conf ining p r e s s u r e reads
2050-2100 p s i g , it' is b led t o 2000 ps ig . Make s u r e that v a l v e 34 (Figure 4 )
is c losed . The only time it is opened is when t h e hand pump is used.
4.19 Cooling t h e System
The ba th has both an i n l e $ and an o u t l e t . Generally a t temperatures
exceeding 1 5 0 ° F , t h e s e v e n t s are c losed. To coo l t h e system, open t h e v e n t s
and t u r n t h e temperature knob t o t h e minimum s e t t i n g . Watch t h e f l u i d
temperature upstream from t h e core . When i t g e t s t o x h e d e s i r e d temperature,
set t h e knob t o t h a t temperature.
The cool ing is a t least as long a process as t h e hea t ing . Cooling
t o room temperature may t a k e s i x hours. During t h e cool ing c y c l e ,
-39-
Figure 1 9 - PRESSURE DIFFEJ@JJ'TIAL RECORDING AT k MEASUREMENTS AND DURING HEATING
-40-
.Figure 20 HEATING CYCLE PROF IEE : 150 OF to 250°F,
b
t h e conf ining p r e s s u r e r e q u i r e s con t ro l . Open v a l v e 3 4 and pump t h e p ressure
back t o 2000 psig . ' Close v a l v e 3 4 . The gauge w i l l read 2200 p s i g .
Sub t rac t ing 200 ps ig f o r t h e average pore p ressure w i l l y i e l d a conf ining
p r e s s u r e of 2000 ps ig .
4.20 Stopping t h e Flow
1.
2 .
3 .
4 .
5 .
6 .
7 .
8 .
Close v a l v e 7 .
Close v a l v e 1.
Close v a l v e 2 7 .
Stop t h e pump.
Close v a l v e 29 .
Open v a l v e 7 and bleed t h e p r e s s u r e t o 0.
Shut down t h e recorders and t h e i n d i c a t o r s .
Shut down t h e cool ing water.
4 . 2 1 Conf ininp, P r e s s u r e Bleed Off
Open v a l v e 3 3 and bleed t h e conf ining p r e s s u r e slowly. Make s u r e t h e
c o r e p r e s s u r e has ,dropped t o zero b e f o r e I bleeding t h e conf ining
p ressure .
4.22 Removing t h e Core Holder
1.
2 .
3 .
4 .
5.
6 .
7 .
Disconnect t h e down stream p r e s s u r e t a p .
Remove t h e upstream p r e s s u r e t ap .
Disconnect the upstream.meta1 and s u r f a c e thermocouples.
Disconnect t h e upstream and down stream p o r t s .
Close v a l v e 3 3 .
Disconnect t h e conf ining p o r t .
Remove t h e c o r e holder .
-42-
4.23 Taking t h e Core Holder Apart and Inspec t ing It
1. Put p r o t e c t o r s on a l l s i x Swagelock f i t t i n g s .
2 . S e t t h e co re holder i n v i s e , f l anges up. Take t h e b o l t s a p a r t .
3. Work t h e co re plugs and core out wi th two screwdrivers .
4 . Take t h e core plugs o f f .
5. Inspec t : Sand Face
0 r i n g s Screens
Viton tubing
11 1 1
4.24 Problems
The main problems were f i l t e r and va lve plugging.
4 .24 .1 F i l t e r plugging
When t h e upstream f i l t e r p lugs , swi teh t o t h e o the r as fo l lows:
Close va lve 7
Switch va lve 2 t o t h e o t h e r f i l t e r
Open v a l v e 7 ( s t a r t t h e f low).
This procedure w i l l no t shock t h e system. Keep va lves 3 and
4 always open.
When t h e downstream f i l t e r p lugs , do t h e fol lowing:
Close va lve 7
Close va lve 31
Remove f i l t e r and change t h e element
R e i n s t a l l t h e f i l t e r
Open va lve 31 u n t i l t h e flow i s zero
Open va lve 31 completely
Open va lve 7 t o start t h e flow.
-43-
4.24.2 Plugging of t h e down stream needle valve
This problem is common. P a r t i c l e s of 61.1 and smaller w i l l pass
through t h e f i l t e r s , bu t w i l l no t pass t h e va lve . Tapping t h e va lve
cas ing w i l l u s u a l l y c lean it. Sometimes it i s necessary t o open
t h e valve completely. To do t h a t , d i v e r t t h e flow t o va lve 6 , then
work va lve 7 a few times, and d i r e c t t h e flow back t o valve 7 .
I n most of t h e runs t h i s problem disappeared a f t e r t h e f i r s t
hea t ing cyc le .
-44-
5. Summary of Resu l t s
I n t h i s s e c t i o n , t h e c a l c u l a t i o n of pe rmeab i l i ty i s shown and a
sample c a l c u l a t i o n i s presented. F i n a l l y , t h e r e s u l t s of t h e runs and a
d i s c u s s i o n are presented.
5 . 1 Permeabi l i ty Ca lcu la t ions
The c o r e used i n t h i s experiment has a c y l i n d r i c a l shape. The f l u i d
f lows i n t h e a x i a l d i r e c t i o n through a c i r c u l a r c r o s s s e c t i o n . The f low
is considered l i n e a r and laminar. Laminar f low is guaranteed i f t h e Reynolds
number is less than uni ty :
where: p = d e n s i t y , g /cc v = v e l o c i t y , cm/sec d = average g r a i n d iameter , cm p = v i s c o s i t y of t h e f lowing l i q u i d , g/cm-sec
For t h e h ighes t f low ra te of about 1000 cc/hour a t 300'F and wi th t h e
unconsolidated sand used i n t h i s s tudy:
p = 0.918 g/cc v = 0.0525 cm/sec d = 1601.1 = 0.016 c m p = 0.1829 c p = 0.001829 g/cm-sec
And t h e corresponding Reynolds number is:
R = (0.918) (0.0525) (0.016) = o.42 < l.o e (0.001829)
For a l i n e a r lamifiar flow, Darcy's law a p p l i e s :
-45-
where: q = cc / sec a t f low cond i t ions A = cm Ap = a t (1.0333 kg/cm2) L = cm IJ = CP k = Darcies
2
Rearranging f o r k:
L and A are measured w i t h a micrometer. is measured a t room Qsc
cond i t ions and must be converted t o q * res *
where : v = s p e c i f i c volume, cf / l b
%c = measured i n t h e b u r e t t e , u s u a l l y 10 cc
t = time totsflow YSCYLsec.
Ap is measured i n p s i , and is converted t o atmospheres by:
14.696 Ap , . p s i = 1 atm
This y i e l d s :
Assuming tha t V = 10 cc, and A = 5.292 e m 2 , equat ion ( 5- 5 ) becomes: sc
Any u n i t s may b e used f o r t h e s p e c i f i c volume terms as long as both
terms are c o n s i s t e n t . The v i s c o s i t y , 1-1 , a t run temperature is obtained
from published d a t a . Table 1 p r e s e n t s l i q u i d water v i s c o s i t y , and F igure 2 1
-46-
Table 1 - Water Viscos i ty
Vi scos i ty a t * Sa tu ra t ion Temp.
1. I
Viscos i ty a t *** 200 p s i
I I
T, "F
32
40
50
60
7 0
80
90
100
150
200
250
300
3 50
400
450
500
550
600
5 'sat
1 . 2 0 1 1.786 0.9810 366 .0 1 .752
271.3 1.299
1 .04 1 1.548
0.9916 0.88 1 .310
0 .76 1 .131
0.658 0.9792
0.578 0.8602
11.128 0.9927
0.9939
E 0.8561 0.9952
I 0.7621 0.9964 0.514 0.7649
0.458 0.6816 0.9975 142 .O 0.6799
0.4266 0.9818 O . 292 0.4345
0.205 0 .3051 62.7 0.3002
47 .6 0.2279
38.2 0.1829
31.8 0.1523
0.9839
0.9694 0.158 0 .2351
0.126 0.1875
0.105 0.1563
0 . 0 9 1 0.1354
0.080 0 .1191
0 .071 0.1057
0.064 0.0952
0.058 0.0863
* PrincipLes of Heat Transfer , K r e i t h ( 1 9 7 3 ) . **Completed Using F igure 23 ***ASME Steam Tables , p. 280 , t a b l e 10
-47-
1 .o .
508
TEMPERATUR , ‘F
Figure 2 1 - VISCOSITY OF WATER vs TDfPERATUPZ AT 200 PSIA
-48-
is a g r a p h i c a l p re sen ta t ion . The e f f e c t of v i s c o s i t y on permeabi l i ty
,determinat ion i s given i n t h e e r r o r ana lys i s . , s e c t i o n 5 .2 .
A sample c a l c u l a t i o n of t h e permeabi l i ty a t a g iven cons tant temperature
fo l lows . This example w i l l e s t a b l i s h t h e permeabi l i ty f o r a case i n
run 11:
T = 250°F Second cool ing c y c l e Record of measurements: 889-896
Measurement 889 w i l l fol low:
Date: September 26, 1980
'Pcor e = 0.664 p s i
v = 1 0 cc t = 60.75 sec T = 74OF sc
From Table 4 : % o V = 0.016990 f t 3 / l b
= 0.2279 cp
2 5 0
7 4 v = 0.016048 f t 3 / l b
L = 15.9906 cm A = 5.2924 c m 2
Hence, equat ion (5-6) y i e l d s :
k = 27.7677 (0.016990) (0.2279) (15.9906) = 2.656 Darcy 2 5 0 (0.664) (60.75) (0.016048)
This c a l c u l a t i o n w a s done f o r e i g h t measurements at t h i s temperature
and t h e average of t h e e i g h t is:
k,,, = 2.673 Darcy
The e i g h t v a l u e s of k250 are presented i n F igu re 28. The average v a l u e - k is presented i n F igu re 2 9 ,
2 5 0
-49-
-50-
1.01
0 Fz 1.00 a OL:
M !z 0.99
0.98 0
t 1 I '7- REG ION OF
50 100 150
T E M P E R A T U R E
F i g u r e 23 - pp/psat vs TDPERATURE
-51-
200
OF
1.C
+- f Qf
8 s
30 50 TEMPERATURE , 'F
Figure 24 .- VISCOSITY vs TEMPERATURE AT 200 PSIA
(Improved Range - 70°F to 100°F)
-52-
110.1 111.1 1U. I
lIIJ l1i.I
11D.l 1121 1M.I 1 l i . l l1IJ
1OO.l 104 J 101.1 711J 1lI.l
131.1 114 J 111.1 111J I J i J
24D.b 1UJ 141.1
I 5 i J 15ZJ
1iD.l 1U.I 1CIJ 11lJ l7iJ
11D.I IUJ 111.1 111.1 71IJ
118 J J U J
112.1 IIIJ
IIiJ
111.1
11IJ 114.1
131J I J I J
nu M4.I n1.1 111.1 1SCJ
1Cl.l 3U.I 161.1 111J 1lIJ
111.1 IUJ
112J 111.1
11iJ
410.1 404 J 40IJ 412J 4 l i J
4 l l J 414 J 41IJ 4 l l J UIJ
441.1 U 4 J 44JJ WJ uu
75110
8 203 7.850
a 56a
0.016510 0016522 0016534 0016517 0.016553
0016572 0.016585 0016598 0016611 0.01 6624
48.172 5021
46.232 44.313 42.621
40.941 39.337 37.808 36.348 34.954
33 622 31.135 28 862
24.878 26.782
23.131 21.529 20 056 18.701 17.454
16.304 15.243 14.264 13.358 12.520
11.745 11.025 10 358 9.738 9.162
8.1180 8.627
7.6634 72301 6.8259
6 4483 6 0955 5.7655 5 4566 5.1673
4.8961 4 6418 4 4030
3.9681
3.7699 3.5834
32423 3 0863
2.9392 2.8W2 2 6691 2.5451 2.4279
2.2120 2.3170
2.1116 2.0184 1.9291
1 8 4 4 4 1.7640
1.6152 1.6877
1.540
1.48G3 14184 1.3591
l302bS 124887
1.19761 1.14874 1.10212 ID5764 ID1511
4.1 7118
3407a
18.189 5022
46.249 44 400 42.638
40.957 39.354 3p.824 36.364 34.970
33.639 31.151 28.878 26.799 24894
23.148 21.545 20.073 18.718 17.471
16.321 15.260 14.281 13.375 12.538
11.762 11.042 10.375 9.755 9.180
8 1453 8 644
7.6807 72475 6 11133
6 4658 6.1 130 5.7830 54742 5.1849
4.9138 4.6595 4.4208 4.1 966 3.9859
3.7878 3 6013 3.4251 3.2603 3 . l M
2.9573 2.81114 2 6873 2.5633 2 4462
23353 2.2304 2.1311 2 0369 1.9477
1 8630 1.7827 1.7064 1.6340 1.5651
1.4997 1.4374 13782
132179 m a m 121687 1.16806 1.12152 107711 I DM72
990.2 989.0
986.5 9 u . 3
984.1
9m.4 981.6
979.1
977.9 975 4
970.3
987.8
982.a
972.a
967.1
965.2 962.6 960 0 957.4 954.8
952.1 949.5 946 8
94 1.4 944.1
938.6 935.9 933.1 930.3 927.5
924.6 921.7 918.8 915.9 913.0
* 910.0 907.0 9M.0 901 .o 897.9
8w.a 891.6 888.5 8853 882.1
875.5 878.8
868 9 w . 5
862.1 858 6 855.1 851.6 848.1
u 4 . 5 B40.8 a372 a33 4 829.7
825.9
8182 822.0
8142 8102
a062 802 2 798 0 793.9 789.7
785.4 781.1 776.7 7723 167)
a722
0.701 02662 0.1691 02725 02756
0.2787 02818
0.2879 0.2848
02910
02940 03001 03061 03121 03181
0324 1 03300 0.3359 0.341 7 03476
0.3533 03591 0.3649 03706 03763
0.3819 0.3876 03932 0.3987 OJM3
o 4098
0 4208 0.4 154
0 4163 04317
I5480 1.5411 1.5346 15279 1.5213
15148 1.5082 I 9 1 1 1.4952 1.411118
14024 I4697 1.4571 14447 1.4323
I 4101 1.4081 1.3961 I3842 13725
13609 13494 13379 13266 13154
13043 13933 12823 12715 12607
12301 12395 12190 12186 12082
.a1 I I 4075 4040
,7969 .8w4
,7334 .7 900 ,7865 .7U1 ,7798
.7 x4
.7698 , 7 0 2 .7568 . 7 9 5
,7442 ,7380 .7320 ,7260 ,7101
.7142
.7085 ,7028 A972 ,6917
.6862 I 6808 ,6755 1.6702 6650
1.6568 .6599
1.6498 1.6449 €44
-
I I IJ 111j 1 U J 111.1 111j
l¶DJ 111j 1 M J 191j 111.1
1d0.1 1UJ 101.1
m . 1 111.1
114J 1n.1
111.1 11zj 111.1
14d.1 1U J 141.1 151J 751j
1 C D J 1UJ 111.1 171J llIJ
111.1 184 J 711.1
291j 112.1
150.01 148 00
152.01 154.02 I56 03
158.04 . 160.05 162 05 164 06 166.08
168 09 172.11 176.14 180.17 18420
118.23 19227 196.31 70035 204.40
208 45 212.50 21636 220.62 224.69
228.76 232.83 236.91 240.99 245.08
249.17
257.4 253.3
765.6 261.5
269.7 273.8 278.0 262.1 2a63
2 W 4 294.6 298.7
. 307.1 302.9
315.5 3113
319.7 313 9 328 1
332.3 336.5 340 8 345.0 349.3
353.6 357.9 3622 366.5 370.8
375.1 379 4 383.8 388.1 3923
396.9 4013 405.7
414.6 410.1
419.0 4235 428 0 4325 437D
1138.2 1 139.0 11 39.8 1140.5 11413
1142.1 1142.9 1143.7 11 44.4 11452
1146.0 I1475 1149.0 1 I 5 0 3 1 152.0
1153.4 11 54.9 11 56.3
11592
11 60.6 11 62.0 11 63.4 1164.7 1166.1
1167.4 1168.7 I 1 70.0 1171.3 11 725
I 1 73.8 I 1 75.0 11762 I 1 77.4 11786
I I 57.11
11 79.7 11809 11 82.0 1183.1 1184.1
11852 11 862 11872 1 188.2 11 89.1
11 90.1 1191.0 1191.1 11 92.7 1193.6
11944 11952 11 95.9 11 %.7 1197.4
11 98.0 11 98.7 1199.3 1199.9 n m 4
1201.0 1201.5 12013 1202.4 1202.8
I2rn.l 1203.5 1203.7 1204.0 12042
1m.4 1104.6 1204.7 12Md 12Md
8.947
9 340 9.747
10.161
11.M8 10.605
11.526 0 01 6637 D O I h L M 12.5ii
13.568 14 696 15.901
17.186 18 556
21.567 20.015
23.216
- _.__. 0 01 6691 0016719 0 01 6747
0.016775 0016805 00161u4 00168M 0.016895
0.016926 D O 1 6958
14.968 26 826 28.796 30.11113 33.041
35.427 37.1194 40.500 43.249 46.147
0.016990 0.017022 0 O17MS
. . . . . . .
0.017089 0.017123 0.017157 0017193 0.017228
49.200 52.414 55.795 59.350
0.017264 0.01730 001734
001711 0 01 738
'' 71.119 67.005
79.953 75.433
84.688
0 01145 0 01 749 0 01 753 0.01757 0.01761
: : :3 0 01774 0 01779 0 01 783
0 01 787 0 01 792 0.01797 001801 001aO6
O O l 8 l l 001816 001821
0.0111l1 0 01826
001836 0.01842 001847 OOl8U OOI858
0.0111E4 0.01870 0.01 875 001881 0.01887
0019w 001894
0.01906 0.01913 0.01919
0.01 926 0 01933 0 . 0 1 ~ 0.01947 omn
04372 0 4426 04479 04533 0 4%
04640 0 4692 04745 0.4798 0 4BSO
1.1979 1.1877 1.1776 1.1616 I .1576
1.6109 111.1 1.6162 Ilil
111.1 114J 111.1 1121 131j
MI I Y J YIJ 112J 155J
ISOJ IUJ
1711 I I IJ
111j
110.1 IUJ J I I J 112J 1161
4 0 H 4MJ 481.1 41zj 415j
420.b 411j 421j 411J 4j1j
UI J 4441 441 J 4UJ 4561
1.6116 16071 16025 13981 15936
13m2 13849 13806 15763 15721
15678 1 3 0 7 15595 13554 15513
15473 15432 I 5 3 9 2 1.5352 1.5313
1.5274 1.5234 13195 15157 15118
MOM 1 9 4 2 1 .m 1.4966 1.4928
14890 1 .MU 1.4815 1.4778 1.4741
119.643 94.826
lW.245 laS.W7 111.820
1.1477 1.1378 1.1280 1.1113 1.1086
117.992
131.142 174.430
138.138 145.424
lYOl0 160 933
0 4W2 0 4954 0 5006 0.5058 0.5110
1.0990 1.0894 1.0799 1.0705 1.0611
03161 0.5212 03163 03314 05365
1.051 7 1.0424 1.0332 1.0240 1.0148
169 i i j 177.648 186.517
205294 195.729
215220 225516 236193
247259 258.725 270.600 282.894 295.617
308.780 322391 336463
366.03 351.00
%In 33756 414.09 431.14 -73
0.5416
0.5516 0.5567 0.5617
0.5667 0.5717 0 5766 - 0.5816 0.5866
o 5166 0.9466 1 . m 7
0.9876 0.9786 0 9696
03607 osiia 0.9429 0334 I 0.9253
0.5915
0 6014 06063 0.6112
0.6161 0.6210
0.6308 0 . 0 5 6
a5964
oun
0.9165 0.9077 Od990 0.8903 0.8816
0.8729 08643 04557 0.8471 Ol.385
T a b l e 2: SPECIFIC VOLmE OF WATER AT SATUFUiTION
From: Steam T a b l e s by C-E Power S y s t e m s
-53-
1 , O F
.XU.
274.
IWU.
;2cu.
?O* 3 0 .
210. 2*D.
210. 223.
500. 29u. 280. 270. 2bO.
250. 2*0. 21u. 220. 210.
zuo. 19u. 1co. 17U. IbO.
150. I*U.
- 150.
110. 120.
ioo. “I. 56.
7u. 60.
50.
32. 40.
v, Ib f13
T a b l e 3 : SPECIFIC VOLUME OF WATER AT 200 PSIA
From: ASME .Steam T a b l e s , p. 1 5 9 , T a b l e 3
-54-
Table 4 - Water Viscos i ty and S p e c i f i c Volumes a t - 200 ps ig (used i n t h e
c a l c u l a t i o n s )
T
(OF)
69 7 0 70 .5 7 1 71 .5 7 2 72.5 73 7 4 7 5 7 6 77 78 7 9 8 0 82
148 1 4 9 150 1 5 1 152 153 155
248 249 250 251 252
298 299 300 3 01
1-I (CP)
0.992 0.9732 0.970 0.964 0.960 0.953 0.945 0.940 0.925 0.915 0.903 0.890 0.880 0.870 0 .8561 0.837
0 .4316 0.4291 0.4266 0 .4241 0.4216 0 .4191 0.4141
0.2303 0 .2291 0.2279 0.2267 0.2255
0.1853 0 .1841 0.1829 0.1817
V
f t 3/11,
0.016038 0.016040 0 .016041 0.016042 0.016043 0.016044 0.016045 0.016046 0.016048 0.016050 0.016052 0.016054 0.016056 0.016058 0.016060 0.016066
0.016320 0.016325 0.016330 0.016335 0.016340 0.016345 0.016355
0.016960 0.01697 5 0.016990 0.017005 0.017020
0.017420 0.017430 0.017440 0.017450
-55-
5.2 Error Analysis
The u s u a l approximation f o r t h e e r r o r , AG, of a f u n c t i o n G(x) is:
The bas i c equat ion f o r permeabi l i ty is:
S u b s t i t u t i n g A = 7rD2/4 and Ap i n p s i , equat ion (5-8) y i e l d s :
k = 18.71277 'TF-( T 'SC
ApT t vsc D 2 ( 5 -9 )
The a b s o l u t e e r r o r i n the permeabi l i ty , Akabs, can be est imated by
equat ion (5-7) , y ie ld ing :
AV AvT AI, All 2AD A(Ap) A t AVsc
A kab s = k -++- 1 ' 'T
+ - + - + --- + - L UT D AP + - t + -1 (5-10)
L vsc
The r e l a t i v e e r r o r i n t h e permeabi l i ty , Akrel, r e f e r s only t o t h e
v a r i a b l e s measured i n each c a l c u l a t i o n . Hence 2AD/ D and AL/L cance l
from equat ion (5-10) leav ing :
ApT A(Ap) A t AvSc Akrel V T l lT AP
+-+ - + - + - sc t V
(5-11)
-5 6-
The A v a l u e s are:
AV = 0.025 cc AL = 0.00254 cm AD = 0.00254 cm A(Ap) = 0.01 p s i A t = 0.05 sec AT = 1°F
v and 1.1 are func t ions of T("F). Table 5 presen t s Av and Ap f o r
va r ious temperatures .
Table 5 - Ap, Av For Various Temperatures
T (OF) Room'L7 5 OF 150" 250 O 300 O
AP (cp) 0.01 0.0025 0.0012 0.0012
Av ( s3) 0.000001 0.000003 0.000008 0.000010
I I I I I I
A sample c a l c u l a t i o n f o r Ak and Akrel fo l lows: abs
Measurement
Run 11 T = 250°F Second Cooling Cycle Numbers of measurements: 889-896
88 9 fo l lows :
k = 2.656 d V = 10 cm v = 0.016990 ft 3 / l b
1 . 1 ~ = 0.2279 (cp)
L = 15.9906 cm Ap = 0.664 p s i V = 0.016048 f t 3 / lb
t = 60.75 sec. D = 2.59588 cm.
3
T
sc
-57-
AV = 0.0025 c m AL = 0.00254 cm AD = 0.00254 cm A(Ap) = 0.01 p s i A t = 0.05 sec AvT = 0.000008 f t 3 / lb
AV = 0.000001 f t 3 / l b
All = 0.0012 cp s c
Akabs = 2.656 - 0.01 +
0.025 0.000008 0.00254 +
0.0012 +
2 x 0.00254 1 10 + 0.016990 + 15.9906 0.2279 2.59588 +- 0.665
0.05 0.665 0.016048 !
o'oooool + = 2.656 = 0.098 darcy = 98 md
1
1 Akabs is about -3.7%
Akrel = 2.656 - 0.025 0.000008 0.0012 0 .01 .0.05 -0.000001 - [ 10 +
0.016990 0.2279 0.665 60.75 0.016048 + +- +- I -
2.656 0.02399 = 0.064 d = 64 md
1 Akrel is about 2.4%
For t h e . a b o v e set of k , a t 250" e i g h t d i f f e r e n t Ak f o ~ v a r i o u s re1
f lowrates were c a l c u l a t e d . The average e r r o r was found, Akrel. Akrel is -
ind ica ted by v e r t i c a l b a r s bn F igure 29.
The o b j e c t i v e is t h e r e l a t i v e change i n t h e pe rmeab i l i ty as a func t ion
of t h e temperature and n o t t h e v a r i a t i o n in t h e i n i t i a l permeabi l i ty of
every core . A cons tan t measuring procedure was used f o r a l l , t h e
repor ted runs . For a more d e t a i l e d d e s c r i p t i o n , see Sec t ion 4.
5.3 Resu l t s of Runs 8 , 9 , 10, and 11
Table 6 p r e s e n t s t h e 'i; and xrel f o r a l l t h e runs , Figures 2 5 , 2 6 ,
2 7 , and 28 present t h e c a l c u l a t e d k f o r all runs. . .
-58-
The l i n e s go through t h e k va lues . Table 6 summarizes a l l t h e runs
and F igure 29 p r e s e n t s them i n a g r a p h i c a l way. All d a t a is t a b u l a t e d
i n Tables 7 - 10.
-59-
5.1
5s
. 4.7
Y
4.6
4.5
4.4
4 3
START-
END- -
-60-
5.
5.
5 .
5.t - - n
t' i2 y" 4.8
4.5
'' D
I
P
Y 4.1
4.6
I I I I I I I
HEATING
COOLING
CYCLE
CYCLE - - -
T , TEMPERATURE ( P )
Figure 26: PERMEABILITY vs TEMPERATURE FOR 150 MESH SAND
. RUN /I9
-61-
2.9
2.8
' 2.7 h
P u
> k 2.61 -I - m w I w U n . ' 2.s Y
2.4(
I I I I I I r
HEATING
COOLING- - - -
T TEMPERATURE ('F)
-62-
t
2.70
2.60
I I I I I I I
HEATING
COOLING - - - -
* c d m 2 5 .2.40
- W n
x 2.30 -
2.20 -
2.10 -
I I I I 1 . o 60
I I 100 160 200 250 300 360 ’
-63-
- 6.C
5.f
5.0
4.5
4.0
3.5
3.0
2.5
2 .o
1.5
. 1.0
0.5
0.0 0
I I I I I I I I . .
WATER FLOW
PI - 2000 psig 200 psig
I- K
. ..-
RUN N0.8
n z w
RUN NO.10
L
MESH 150-120
w
RUN N0.9
-v) I-
n MESH 200-170
z W
RUN NO. I!
I I I I I I I I
100 200 300 T (OF)
0 100 m 300 400
T (OF)
Figure 29 - PERMEABILITY VS TEMPERATURE FOR RUNS 8, 9 , '10, and 11
-64-
6. Conclusions
The a b s o l u t e permeabi l i ty t o d i s t i l l e d water of Ottawa s i l i c a sand
was n o t dependent upon t h e temperature l e v e l from 70°F t o 300°F. This
r e s u l t does not agree wi th much of t h e d a t a i n t h e l i t e r a t u r e . It is
bel ieved t h a t some of t h e work done a t Stanford Univers i ty i n recen t
yea rs experienced mechanical problems t h a t r e s u l t e d i n flow rate dependent
permeabi l i ty measurements which were i n t e r p r e t e d as temperature dependent
r e s u l t s . A s e n s i t i v i t y a n a l y s i s of t h e apparatus helped i n i d e n t i f y i n g
sources of t roub le . These problems were addressed and t h e performance
of t h e apparatus improved.
I n o r d e r t o expand t h e s e conclus ions it is recommended t h a t f u t u r e
experiments be conducted, These experiments could s tudy a range of consol i-
dated sandstones , f l u i d s , and conf ining and pore p ressures . Then a s tudy
of t h e e f f e c t of temperature l e v e l on r e l a t i v e permeabi l i ty should be
resumed.
-65-
7. References
Amyx, J. W . , Bass, D. M . , J r . , and Whiting, R. L. Petroleum Reservoir Engi- nee r ing , McGraw-Hill Book Company, Inc . , New York, 1960.
Aruna, M. "The Ef fec t of Temperature and P res su re on Absolute Permeabil i ty of Sandstones," Ph.D. D i s s e r t a t i o n , S tanford Un ive r s i ty , 1976.
Cass6, F. J. "The E f f e c t of Temperature and Confining P res su re on F lu id Flow P r o p e r t i e s of Consolidated Rocks," Ph.D. D i s s e r t a t i o n , S tanford Un ive r s i ty , 1974.
Danesh, A. , Ehlig-Economides, C . , and Ramey; H. J . , Jr., "The Effect of Temperature Level on Absolute Permeabi l i ty of Unconsolidated S i l ica
Gobran, B. D . , S u f i , S. H . , Sanyal , S. K . , and Brigham, W. E. "Effec ts of Temperature on Permeabi l i ty ," F o s s i l Energy, 1980 Annual Heavy O i l / E O R Cont rac tor Presentat ions- Proc. , J u l y 22-24, 1980.
Keenan, J. H . , Keyes, G . F . , H i l l , G. P . , and Moore, G. J. Steam Tables, English U n i t s , Wiley and Sons, New York, 1969.
Kre i th , F. P r i n c i p l e s of Heat Trans fe r , Third Ed i t ion , Harper and Row Pub l i she r s , New York, 1973.
Muskat, M. Flow of Homogeneous F l u i d s Through Porous Media, McGraw-Hill Book Company, Inc . , 1937.
Sanyal , S . K . , Marsden, S. S . , Jr . , and Ramey, H. J . , Jr. "Effect of Temper- a t u r e on Pe t rophys ica l P r o p e r t i e s of Reservoir Rocks," 49th Annual F a l l Meeting, Houston, Texas, Socie ty of Petroleum Engineers No. 4898, October 1974.
Sydansk, R. D. "Aqueous Permeabi l i ty Var i a t ion w i t h Temperature i n Sandstone," Jour . P e t . Tech. August 1980, 1329-1330.
Thermodynamics and Transport P r o p e r t i e s of Steam, American Socie ty of Mechanical Engineers , New York, 1967.
Weinbrandt, R. M . , Ramey, H. J . , Jr. , and Cass6, F. J. "Relative and Absolute Permeabi l i ty of Sandstones , I ' Socie ty of Petroleum Engineering Jou rna l , (October, 1975), 376-384.
-66-
8. Tables of Data
- Table 6 - k, and ET f o r Runs 8 , 9, LO, and 11. (Darcies)
Run
8
9
10
11
Room 70°F-72"F
5.033/0.134
4.869/0.133
4.835/0.124
5.201/0.144
5.032/0.131
5.086/0.145
2.764/0.073
2.642/0.066
2.666/0.067
2.671/0.067
2.653/0.067
2.612/0.067
150
4.947/0.188
4.851/0.119
4.828/0.115
4.841/0.129
5.180/0.133
5.112/0.128
5.034/0.127
5.089/0.136
2.702/0.059
2.695/0.063
2.658/0.059
2.680/0.059
2.652/0.055
2.649/0.054
2.610/0.054
2.634/0.054
250
4.906/0.148
4.868/0.151
4.883/0.152
4.866/0.147
5.094/0.160
5.101/0.166
5.081/0.163
5.058/0.163
2.691/0.059
2.699/0.059
2.739/0.060
2.769/0.063
2.652/0.060
2.647/0.058
2.635/0.061
2.646/0.062
3 50
+ 4.889/0.175
=4 5.094/0.199
--i 5.113/0.193
-4 2.694/0.066
2.700/0.074 1 2.663/0.068
_7 2.666/0.071
-67-
Table 7
Run no. 8 : L = 16.350 cm; A = 5.293 cm2; Mesh = 120-150; p = 2000 p s i g ; C
- p = 200 ps ig
529 I 53 0 53 1 53 2 533 53 4
53 6 537 538
I 1
I t
II
I t
0.517 0.544 0.4155 0.493 0.487 0.349 0.378 0.432 0.435 0.394
I1
11
I 1
11
11
t l
I I
11
11
I t
43.80 4839 40.90 4925 54.10 4874 37.70 300 7 5 4855 37.85 , 4896 52 .70 4906 49.05 42.60 4903 42.40 4893 57.05 250 73 4849
I 1 I t
II I 1
I t t l
I t
I 1
I t
I t
t l 11
I 1 11
535 ; II I I 4867-2 I 1 I 1
t I I t I 1
1 1
-68-
T a b l e 7,
Run no. 8 : L = 16 .350 cm; A = 5 .293 em2 ; Mesh = 120- 150 , pc = 2000 p s i g ;
6 = 200 p s i g
I 5 7 1 I I t 10 .485 i I 46 .20 I i 4888 I L
57 2 57 3 57 4 57 5 57 6 57 7 57 8 57 9 58 0
I 1 11
11 I 1
I 1 I 1
I 1 11
I 1 11 11 11
I 1 11 11 I 1
1 1 ' 11 11 I 1
1 1 11 11 1 1
I I 1 1 I 1
0.485 0 ,547 0.547 0 .400 0.399 0.528 0 .522 0.307 0.306
46.10 I 4899 41 .10 1 4872 40 .90 i 4896 46 .15 3 00 77 4887 4 6 . 2 0 4894 35 .10 48 68 35.40 4882 60.10 48 90 60.00 4914
11 I 1
I 1 11
11 11
1
I 1
-63-
Table 7
Run no. 8: L = 16.350; A = 5.293 cm2 ; Mesh = 120-150; = 2000 p s i g ; PC - p = 200 p s i g
-70-
Table 8
Run no. 9: L = 16.118 cm; A = 5.293 cm2 ; Mesh = 120-150; p = 2000 p s i g C
- D = 200 D s i l r
-
-71-
Table 8
Run no 9 : L = 16.118 cm; A = 5.293 cm2 ; Mesh = 120-150; p = 2000 p s i g ; C
- p = 200 p s i g
-72-
Table 8
~
Number of
69 0 6 9 1 692 693 694 695 696 697 9 / 2 0 / 8 1 698 699 700 701
II
11
1 1
1 1
II
11
1 1
11
II
I 1
-7 3-
Table 9
-74-
Table '9
Run no. l o : L = 16.303 cm; A = 5.293 a n 2 ; Mesh = 170-200 ; p, = p s i g ;
, ' 783 0.510 7 8 2698 65 .00 65.50 2700 48.20 2702 48.45 2686 58.95 2698
1 1
1 1
1 1
11
1 1
11
1 1 11
I t 1 1
1 1 11
I 1 1 1
784 785 786 787
11
11
I t
11
0.509 0.691 0.687 0 .568
c
-75-
Table 9
Run no. 10: L = 16.303 cm; A = 5.293 a n 2 ; Mesh = 170-200; p, = 2000 p s i g
p = 200 p s i g
-76-
Table 10
Run no. 11: L = 15 .991 cm; A = 5.293 cm2; Mesh = 170-200; = 2000 p s i g PC - p = 200 p s i g
Number of' measure- Date ''core Temp. V t Run
813 I 1 0.955 814 0.953 815
I 1
11
1 1 11
I 1 I 1
I 1 1 1
V I . O J 2646 2648
8 9 - 9 5 2656
1 1
I 1 1 90.10
I 1 I 1
11 I 1
2653 2648
48.50 250 7 4 2656 48.75 2659
1 1
11
II
1 76.70
I 1 I 1
1 1 11 1 2648 t I
I 1 11
II I 1 I 2666 I 2656 11 61.60 I
1 1
1 1
1 1
II
I 1
I 61.60 I 1 11
1 1
2643 51.80 73 2643 45.50 300 7 6 2666
2664 49 - 70 2654
1 46.25 11 I 1
1 1 II
11
13 I 45.60
1 1 1 1
I 1
2638 2654 74 .70 152
-77-
Table 10
-7 8-
Table 10
Run no. 11: L = 15.991 cm ; A = 5.293 cm2 ; Mesh = 170-200; = 2000 p s i g ; PC
- p = 200 p s i g .
-79-