M25C - Barloworld STET – Distribuidor Caterpillar em ... · PDF fileM25C Project Guide • Propulsion. m M 25 C Propulsion Introduction Caterpillar Motoren GmbH & Co. KG P. O. Box,

M 25 CProject Guide • Propulsion

m

M 25 C Propulsion

Introduction

Caterpillar Motoren GmbH & Co. KGP. O. Box, D-24157 KielGermanyPhone +49 431 3995-01Telefax +49 431 3995-2193

Issue Juli 2008

Information for the user of this project guide

The project information contained in the following is not binding, since technical data of products mayespecially change due to product development and customer requests. Caterpillar Motoren reservesthe right to modify and amend data at any time. Any liability for accuracy of information providedherein is excluded.

Binding determination of data is made by means of the Technical Specification and such other agree-ments as may be entered into in connection with the order. We will supply further binding data, draw-ings, diagrams, electrical drawings, etc. in connection with a corresponding order.

This edition supersedes the previous edition of this project guide.

All rights reserved. Reproduction or copying only with our prior written consent.

m

M 25 C Propulsion

Global Resource from One SourceWhen you select Cat Marine Power for yourvessel, look to Cat Financial for world-classfinancial support. With marine lending offices inEurope, Asia and the US supporting Caterpillar’sworldwide marine distribution network, CatFinancial is anchored in your homeport. We alsohave over 20 years of marine lending experience,so we understand your unique commercialmarine business needs. Whether you’re in theoffshore support, cargo, ship assist, towing, fish-ing or passenger vessel industry, you can counton Cat Financial for the same high standard youexpect from Caterpillar.

www.CAT.com/CatMarineFinanceVisit our web-site or see your local Cat dealerto learn how our marine financing plans and options can help your business succeed.

Marine Financing GuidelinesPower: Cat and MaK.Financial Products: Construction, term

and repower financing.Repayment: Loan terms up to

10 years, with longeramortizations available.

Financed Amount: Up to 80% of yourvessel cost.

Rates: Fixed or variable.Currency: US Dollars, Euros and

other widely tradedcurrencies.

Ocean-Going Vessels

Pleasure Craft

Commercial Vessels

m

M 25 C Propulsion

GlobalDealer Network Maintenance

Training

Commissioning

RemanufacturedParts

GenuineSpare Parts

DICAREDiagnostic Software

RepairsEngineUpgrades

Overhauls

Customer SupportAgreements

(CSAs)

Providing integrated solutions for your power system meansmuch more than just supplying your engines. Beyond completeauxiliary and propulsion power systems, we offer a broad port-folio of customer support solutions and financing options. Ourglobal dealer network takes care of you wherever you are –worldwide. Localized dealers offer on-site technical expertisethrough marine specialists and an extensive inventory of all thespare parts you might need.

To find your nearest dealer, simply go to:www.cat-marine.com or www.mak-global.com

m

M 25 C Propulsion

m

M 25 C Propulsion

Contents

Page

1. Engine description 1 - 2 2. General data and outputs 3 - 4 3. Restrictions for low load operation 5 4. Propeller operation 6 - 8 5. Technical data 9 - 10 6. Engine dimensions 11 - 18 7. Space requirement for dismantling of charge air cooler

and turbocharger cartridge 19 8. Maintenance platform 20 9. System connections 2110. Fuel oil system 22 - 3311. Lubricating oil system 34 - 4112. Cooling water system 42 - 4813. Flow velocities in pipes 4914. Starting air system 50 - 5115. Combustion air system 5216. Exhaust system 53 - 5917. Air borne sound power level 6018. Foundation 61 - 6719. Power transmission 68 - 7120. Data for torsional vibration calculation 7221. Control and monitoring system 73 - 9122. Diagnostic system DICARE 92 - 9323. Diesel engine management system DIMOS 9424. Standard acceptance test run 9525. EIAPP certificate 9626. Painting/Preservation 97 - 9827. Lifting of engines 9928. Engine parts 100

m

1M 25 C Propulsion

1. Engine description

The M 25 C is a four stroke diesel engine, non-reversible, turbocharged and intercooled with direct fuelinjection.

In-line engine M 25 C

Cylinder configuration: 6, 8, 9 in-lineBore: 255 mmStroke: 400 mmStroke/Bore-Ratio: 1.57Swept volume: 20.4 l/Cyl.Output/cyl.: 317 - 333 kWBMEP: 25.8 barRevolutions: 720/750 rpmMean piston speed: 9.6/10.0 m/sTurbocharging: pulse pressureDirection of rotation: clockwise, option: counter-clockwise

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2 M 25 C Propulsion

1. Engine description

Engine design

- Designed for heavy fuel operation up to 700 cSt/50 °C, fuel grade acc. to CIMAC H55 K55, ISO 8217,1996 (E), ISO-F-RMH55 RMK55.

- 1-piece dry engine block made of nodular cast iron. It incorporates the crankshaft bearing, cam-shaft bearing, charge air receiver, vibration damper housing and gear drive housing.

- Underslung crankshaft with corrosion resistant main and big end bearing shells.

- Natural hardened liners, centrifugally casted, with calibration insert.

- Composite type pistons with steel crown and nodular cast iron skirt.

- Piston ring set consisting of 2 chromium plated compression rings, first ring with chrom-ceramiclayer and 1 chromium plated oil scraper ring. All ring grooves are hardened and located in the steelcrown.

- 2-piece connecting rod, fully machined, obliquely split with serrated joint.

- Cylinder head made of nodular cast iron with 2 inlet and 2 exhaust valves with valve rotators.Direct cooled exhaust valve seats.

- Camshaft made of sections per cylinder allowing a removal of the pieces sideways.

- Turbocharger supplied with inboard plain bearings lubricated by engine lubricating oil.

- 2-stage fresh water cooling system with 2-stage charge air cooler.

- Nozzle cooling for heavy fuel operation with engine lubricating oil.

m

3M 25 C Propulsion

2. General data and outputs

Output definition

The maximum continuous rating (locked output) stated by Caterpillar Motoren refers to the followingreference conditions according to "IACS" (International Association of Classification Societies) formain and auxiliary engines:

Reference conditions according to IACS (tropical conditions):air pressure 100 kPa (1 bar)air temperature 318 K (45 °C)relative humidity 60 %seawater temperature 305 K (32 °C)

Fuel consumption

The fuel consumption data refer to the following reference conditions:intake temperature 298 K (25 °C)charge air temperature 318 K (45 °C)charge air coolant inlet temperature 298 K (25 °C)net heating value of the Diesel oil 42700 kJ/kgtolerance 5 %

Specification of the fuel consumption data without fitted-on pumps; for each pump fitted on an additio-nal consumption of 1 % has to be calculated.

Lubricating oil consumption

Actual data can be taken from the technical data.

Engine 720/750 rpm kW

6 M 25 C 1800/2000

8 M 25 C 2320/2640

9 M 25 C 2610/3000

The maximum fuel rack position is mechanicallylimited to 100 % output for CPP and FPP appli-cations. Limitation of 110 % for gensets and DEapplications.

m

4 M 25 C Propulsion

Nitrogen oxide emissions (NOx-values)

NOx-limit values according to MARPOL 73/78 Annex VI: 12.0 g/kWh (n = 750 rpm)

CPP and DE propulsion acc. to cycle E2: 9.9 g/kWh (n = 750 rpm)FPP propulsion acc. to cycle E3: 10.6 g/kWh (n = 750 rpm)

An engine version which keeps the requirements of "Blauer Engel" (20 % less NOx than MARPOL 73/78)is also available.

Emergency operation without turbocharger

Emergency operation is permissible only with MDO and up to approx. 20 % of the MCR.

General installation aspect:

Inclination angles of ships at which engine running must be possible:

Heel to each side: 15°Rolling to each side: + 22.5°Trim by head and stern: 5°Pitching: + 7.5°

2. General data and outputs

m

5M 25 C Propulsion

3. Restrictions for low load operation

The engine can be started, stopped and run on heavy fuel oil under all operating conditions.

The HFO system of the engine remains in operation and keeps the HFO at injection viscosity. The tem-perature of the engine injection system is maintained by circulating hot HFO and heat losses are com-pensated.

The lube oil treatment system (lube oil separator) remains in operation, the lube oil is separated con-tinuously.

The operating temperature of the engine cooling water is maintained by the cooling water preheater.

Below 25 % output heavy fuel operation is neither efficient nor economical.

A change-over to diesel oil is recommended to avoid disadvantages as e.g. increased wear and tear,contamination of the air and exhaust gas systems and increased contamination of lube oil.

Cleaning run of engine

1 h 2 3 4 5 6 8 10 15 20 24 h

PE %

100

70

5040

30

20

15

10

8

6

HFO-operation

3 h 2 1 h 30 min 15 min 0

Cleaning run after partial load operation

Load increase periodapprox. 15 min.

Restricted HFO-operation

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6 M 25 C Propulsion

4. Propeller operationRequired fixed pitch propeller layout

I. Speed range for continuous operationThis speed range must not be exceeded for long-term operating conditions.

II. Speed range for short-time operationPermitted for a short time only, e.g. during acceleration and manoeuvring (torque limitation)

Fixed-pitch propeller design Max. output at 100 % rated speed:Sea going vessel (fully loaded) max. 85 % for seaships

max. 100 % for towing ships at bollard pullInland waterway vessels (fully loaded) max. 95 % for inland waterway vessels

max. 90 % for push boatsSpeed increase (grey area) The speed is blocked always at 100 % of rated speed. If

required 103 % of rated speed is permissible at continuousoperation.During the yard trial trip the engine speed may be increasedto max. 106 % of the rated speed for max. 1 h, if required.

n/no [%]Speed

m

7M 25 C Propulsion

4. Propeller operationRecommendation for control pitch propeller

The design area for the combinator has to be on the right-hand side of the theoretical propeller curveand may coincide with the theoretical propeller curve in the upper speed range.

A load above the output limit curve is to be avoided by the use of the load control device or overloadprotection device.

Binding data (depending on the type of vessel, rated output, speed and the turbocharging system) willbe established upon order processing.

A (sec) B (sec) C (sec) D (sec)

6, 8, 9 M 25 C 35 1 0 40 180

10 %

70 %

100 %MCR

10 %

70 %

100 %MCR

0%

10%

20%

30%

40%

50%

60%

70%

80%

90%

100%

110%

50% 60% 70% 80% 90% 100% 110%Engine speed [%]

Engi

ne o

utpu

t [%

]

Power limit curve for overload protection

Combinator curve

I : Normal operation

II: Short time operation allowed

103%

Droop

III

Normal acceleration time

n = const100 % rpm

A

10 %

70 %

100 %

B

MCR

t

n = const100 % rpm

A

10 %

70 %

100 %

B

MCR

t

n =combinator

10 %

70 %

100 %MCR

n = 70 % rpm

n =97 % rpm

C D

n = 100 % rpm

t

n =combinator

10 %

70 %

100 %MCR

n = 70 % rpm

n =97 % rpm

C D

n = 100 % rpm

t

8

m

8 M 25 C Propulsion

4. Propeller operationAcceleration time propulsion, standard engine

Min

imum

tim

e fo

r em

erge

ncy

oper

atio

n N

orm

al o

pera

tion

n m

in =

70

%

acce

lera

tion

from

10

% M

CR a

t 70

% s

peed

to

100

% M

CR a

t 10

0 %

spe

ed

n =

cons

tant

ac

cele

ratio

n fro

m

10 %

MCR

to

100

%

MCR

Smok

e Re

duct

ion

from

10

0 %

MCR

to

0 %

MCR

n min

= 7

0 %

ac

cele

ratio

n fro

m

10 %

MCR

at

70

% s

peed

to

70 %

MCR

at

97%

spe

ed

n min

= 7

0 %

ac

cele

ratio

n fro

m

70 %

MCR

at

97%

spe

ed to

10

0 %

MCR

at

100

% s

peed

n =

cons

tant

ac

cele

ratio

n fro

m

10 %

MCR

to

70

% M

CR

n =

cons

tant

ac

cele

ratio

n fro

m

70 %

MCR

to

100

%

MCR

Smok

e Re

duct

ion

from

10

0 %

MCR

to

0 %

MCR

Puls

e-Ch

argi

ng /

CPP

and

Gens

ets

for S

tand

ard

appl

icat

ion

(Tan

ker,

Cont

aine

r fee

der a

nd B

ulke

r)

6 M

25

C 25

s

20 s

vi

sibl

e 8

s 40

s

3 m

in

35 s

3

min

in

visi

ble

20 s

8 M

25

C 30

s

25 s

vi

sibl

e 8

s 40

s

3 m

in

35 s

3

min

in

visi

ble

20 s

9 M

25

C 30

s

25 s

vi

sibl

e 8

s 40

s

3 m

in

35 s

3

min

in

visi

ble

20 s

For T

ugs

and

Ferr

ies

M 2

5 C

for T

ug

See

abov

e vi

sibl

e 8

s 20

s

35 s

20

s

35 s

20 s

M 2

5 C

for F

erry

Se

e ab

ove

visi

ble

8 s

30 s

40

s

30 s

40

s

20

s

Puls

e-Ch

argi

ng /

FPP

and

Voith

10

% to

100

%

MCR

10 %

to 5

0 %

MCR

50

% to

100

%

MCR

M 2

5 C

40 s

n.

a.

visi

ble

8 s

30 s

40

s

n.a.

n.

a.

20

s

Rem

arks

: Ac

cele

ratio

n tim

e in

sec

onds

, Tol

.: ±5

sec

., en

gine

war

m in

ope

ratin

g co

nditi

ons

In e

mer

genc

y m

ode

smok

e w

ill b

e vi

sibl

e.

M

inim

um o

pera

ting

time

10 m

inut

es

For t

ugs

and

ferr

ies

a ha

rge

air p

ress

ure

cont

rolle

d fu

el li

mite

r

Lub.

Oil

> 50

°C

is re

com

men

ded.

Cool

ant >

65

°C

Star

t of a

ccel

erat

ion

at le

ast 1

0 %

MCR

, low

est o

pera

tion

poin

t with

CPP

Ba

sis

ratin

gs (M

CR):

6,

8, 9

M 2

5 C

-

290

/ 30

0 / 3

17 /

330

kW /

cyl.

Stan

dard

acc

eler

atio

n tim

e w

ill p

rovi

de lo

nges

t com

pone

nt li

fetim

es.

Emer

genc

y ac

cele

ratio

n po

ssib

le, b

ut n

ot re

com

men

ded,

due

to h

ighe

r the

rmal

stre

sses

of e

ngin

e co

mpo

nent

s.

c

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9M 25 C Propulsion

5. Technical data

Cylinder 6 8 9 Performance data Maximum continous rating acc. ISO 3046/1 kW 1900 2000 2534 2660 2850 3000

Speed 1/min 720 750 720 750 720 750 Minimum speed 1/min 240 250 240 250 240 250 Brake mean effektive pressure bar 25.8 26.1 25.8 26.1 25.8 26.1 Charge air pressure bar 3.1 3.2 3 3.2 3.2 3.2 Compression pressure bar 172 175 172 175 172 175 Firing pressure bar 204 208 204 208 200 204 Combustion air demand (ta = 20 °C) m3/h 11100 12850 14515 15665 16550 17020 Delivery/injection timing ° v. OT 11.0/8 11.0/8 11.0/8 Exhaust gas temperature after cylinder/turbine

°C 360/305 360/290 370/325 370/320 380/320

Specific fuel oil consumption Propeller/n = const 1) 100 % 85 % 75 % 50 %

g/kWh g/kWh g/kWh g/kWh

184182/183 180/185 187/193

184 182/183 180/185 187/193

184182/183 180/185 187/193

Lubricating oil consumption 2) g/kWh 0.6 0.6 0.6 Turbocharger type HPR6000 HPR6000 HPR6000 Fuel Engine driven booster pump m3/h/bar 1.5/5 1.5/5 1.5/5 Stand-by booster pump m3/h/bar 2.3/6 2.7/5 2.7/5 2.8/5 Mesh size MDO fine filter mm 0.025 0.025 0.025 Mesh size HFO automatic filter mm 0.010 0.010 0.010 Mesh size HFO fine filter mm 0.034 0.034 0.034 Nozzle cooling by lubricating oil system

Lubricating Oil Engine driven pump m3/h/bar 89/10 93/10 89/10 93/10 89/10 93/10 Independent pump m3/h/bar 40/10 55/10 60/10 Working pressure on engine inlet bar 4 - 5 4 - 5 4 - 5 Engine driven suction pump m3/h/bar 107/3 112/3 107/3 112/3 107/3 112/3 Independent suction pump m3/h/bar 57/3 70/3 70/3 Priming pump pressure m3/h/bar 6.6/8/5 10/13/5 10/13/5 Sump tank content m3 2.6 2.7 3.4 3.6 3.9 4.0 Temperature at engine inlet °C 60-65 60-65 60-65 Temperature controller NB mm 80 100 100 Double filter NB mm 80 80 80 Mesh size double filter mm 0.08 0.08 0.08 Mesh size automatic filter mm 0.03 0.03 0.03

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10 M 25 C Propulsion

5. Technical data

Cylinder 6 8 9 Fresh water cooling Engine content m3 0,4 0,5 0,6 Pressure at engine inlet min/max bar Header tank capacity m3

Temperature at engine outlet °C

2.5/6.0 0.2

80 - 90

2.5/6.0 0.25

80 - 90

2.5/6.0 0.3

80 - 90 Two circuit system Engine driven pump HT m3/h/bar 40/3.7 55/3.5 60/3.7 Independent pump HT m3/h/bar 40/3.0 55/3.0 60/3.0 HT-Controller NB mm 80 100 100 Water demand LT-charge air cooler m3/h 40 45 50 Temperature at LT-charge air cooler inlet

°C 38 38 38

Heat Dissipation Specific jacket water heat kJ/kWh 500 500 500 Specific lub. oil heat kJ/kWh 490 490 490 Lub. oil cooler MJ/h 931 970 1242 1294 1396 1455 Jacket water MJ/h 950 990 1267 1320 1425 1485 Charge air cooler (HT-Stage) 3) MJ/h 2160 2255 2808 2934 3096 3240 Charge air cooler (LT-Stage) 3) MJ/h 828 884 1116 1116 1260 1260 (HT-Stage after engine) Heat radiation engine MJ/h 306 408 460 Exhaust gas Silencer/spark arrester NB 25 dBA mm 500 600 600 NB 35 dBA mm 500 600 600 Pipe diameter NB after turbine mm 500 600 600 Maximum exhaust gas pressure drop

bar 0.03 0.03 0.03

Starting air Starting air pressure max. bar 30 30 30 Minimum starting air pressure bar 10 10 10 Air consumption per Start 4) Nm3 0.8 0.8 0.8 1) Reference conditions: LCV = 42700 kJ/kg, ambient temperature 25 °C charge air temperature 45 °C,

tolerance 5 %, + 1 % for each engine driven pump 2) Standard value, tolerance + 0,3 g/kWh, related on full load 3) Charge air heat based on 45 °C ambient temperature 4) Preheated engine

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11M 25 C Propulsion

6. Engine dimensions

Removal of:

Piston in transverse direction X1 = 2420 mmin longitudinal direction X2 = 3000 mm

Cylinder Liner in transverse direction Y1 = 2510 mmin longitudinal direction Y2 = 2735 mm

Reduced removal height Piston and Liner: 2300 mmSpecial tool for liner removal in transverse direction necessary and according to lifting device ar-rangement.

Engine centre distance 6, 8, 9 Cyl. 2500 mm(2 engines side by side)

Turbocharger at driving end

Dimensions [mm] Engine type A B C D E F G H

Weight with flywheel [t]

6 M 25 C 1191 5345 1151 672 2260 861 460 2906 21.0

8 M 25 C 1191 6289 1151 672 2315 861 460 3052 28.0

9 M 25 C 1191 6719 1151 672 2315 861 460 3052 29.6

m



Turbocharger at free end

Dimensions [mm] Enginetype B H

6 M 25 C 4917 2951

8 M 25 C 5777 3097

9 M 25 C 6207 3097

m

13M 25 C Propulsion


6 M 25 C, Turbocharger at driving end

Scal

e 1

: 50

m




Scal

e 1

: 50

m

15M 25 C Propulsion



Scal

e 1

: 50

m



6 M 25 C, Turbocharger at free end

Scal

e 1

: 50

m

17M 25 C Propulsion



Scal

e 1

: 50

m




Scal

e 1

: 50

m

19M 25 C Propulsion

7. Space requirement for dismantling of charge air cooler andturbocharger cartridge

Charge air cooler cleaning

Cleaning is carried out with charge air cooler dis-mantled. A container to receive the cooler and clean-ing liquid is to be supplied by the yard. Intensivecleaning is achieved by using ultra sonic vibrators.

Turbocharger Removal/Maintenance

Caterpillar Motoren recommends providing rightabove the center of the turbocharger a lifting rail witha travelling trolley to which a lifting gear can be at-tached in order to carry out the work on the turbo-charger according to the maintenance schedule.

Weights M 25 C Turbocharger

Turbo-charger, compl.

Si-lencer

Compres-sor

housing

Turbine inlet

housing

Exhaust-gas

elbow

Car-tridge

Bearing housing

Rotor

563 kg 63 kg 136 kg 125 kg 68 kg 150 kg 100 kg 32 kg

Dimensions [mm] Weight

X Y A B C kg

6 M 25 C 1900 1225 475 1155 552 270

8/9 M 25 C 2130 1225 475 1155 552 295

Not Caterpillar Motorensupply

Maintenance SpaceP = min. 1300R = min. 750

m


8. Maintenance platform

The platform, located at the control side of the engine including stairs and ladder, is normally designedand manufactured by the shipyard. As an option Caterpillar Motoren can supply a platform for rigidlymounted engines. For resiliently mounted engines a separate platform, that has to be adapted to localconditions, is strongly recommended.

m

21M 25 C Propulsion

9. System connections

C14 Charge Air Cooler LT, Inlet DN 65C15 Charge Air Cooler LT, Outlet DN 65C17 Charge Air Cooler HT, Outlet DN 65C21 Freshwater Pump HT, Inlet DN 80C22 Freshwater Pump LT, Inlet DN 80C23 Freshwater Stand-by Pump HT, DN 65

InletC28 Freshwater Pump LT, Outlet DN 65C46a Luboil Stand-by Pump, DN 125

Suction SideC51 Luboil Force Pump, Inlet DN 125

C55c Connection Flushing Pipe DN 50Automatic Filter

C58 Luboil Force Pump, Outlet DN 100C59 Luboil Inlet, Duplex Filter DN 80C60 Separator Connection, Suction Side G 1 1/2"C61 Separator Connection, Delivery Side G 1 1/2"C76 Inlet, Duplex Filter DN 32C78 Fuel, Outlet DN 32C86 Crankcase Ventilation DN 40C91 Crankcase Ventilation DN 80C91a Exhaust Gas Outlet 6 M 25 C DN 500

8/9 M 25 C DN 600

m


10. Fuel oil systemMarine gas oil / marine diesel oil operation

Two fuel product groups are permitted for MaK engines:

Pure distillates: Gas oil, marine gas oils, diesel fuel

Distillate/mixed fuels: Marine gas oil (MGO), marine diesel oil (MDO). The differ-ence between distillate/mixed fuels and pure distillates arehigher density, sulphur content and viscosity.

Max. injection viscosity 12 cSt (2 °E)

Day tank DT 1: To be layed out for heat dissipation from injection pumps,approx. 1.5 kW/cylinder.

Strainer (separate) DF 2: Mesh size 0.32 mm, dimensions see HFO-system

Preheater (separate) DH 1: Heating capacity

Not required with:- MGO < 7 cSt/40 °C- Heated day tank

Q [kW] =Peng. [kW]

166

MGO MDO

Designation Max. viscosity[cSt/40 °C]

Designation Max. viscosity[cSt/40 °C]

ISO 8217: 1996 ISO-F-DMA 1.5 - 6.0 ISO-F-DMB ISO-F-DMC

1114

ASTM D 975-78 No. 1 D No. 2 D

2.44.1

No. 2 D No. 4 D

4.124.0

DIN DIN EN 590 8

m

23M 25 C Propulsion

Feed pump (fitted) DP 1: Capacity see technical data

Feed pump (separate) DP 2: Capacity see technical dataScrew type pump with mechanical seal.Installation vertical or horizontal.Delivery head 5 bar.

Pressure regulating valve (fitted) DR 2

Fine filter (fitted) DF 1: Duplex filter, mesh size see technical data.

Separator DS 1: Recommended for MGORequired for MDO

Capacity

V [l/h] = 0.22 · Peng. [kW]


m



General notes:For location, dimensions and design (e. g. flexible connection) of the connecting points see engine installation drawing.DH1 not required with: - MGO < 7 cSt/40°

- heated diesel oil day tank DT1

Accessories and fittings:DF1 Fuel fine filter (duplex filter) KP1 Fuel injection pumpDF2 Fuel primary filter (duplex filter) KT1 Drip fuel tankDF3 Fuel coarse filter FQI Flow quantity indicatorDH1 Diesel oil preheater LI Level indicatorDH2 Electrical preheater for diesel oil (separator) LSH Level switch highDP1 Diesel oil feed pump LSL Level switch lowDP2 Diesel oil stand-by feed pump PDI Diff. pressure indicatorDP3 Diesel oil transfer pump (to day tank) PDSH Diff. pressure switch highDP5 Diesel oil transfer pump (separator) PI Pressure indicatorDR2 Fuel pressure regulating valve PSL Pressure switch lowDS1 Diesel oil separator PT Pressure transmitterDT1 Diesel oil day tank TI Temperature indicatorDT4 Diesel oil storage tank TT Temperature transmitter (PT 100)

Connecting points:C73 Fuel inlet, to engine fitted pump C80 Drip fuelC75 Connection, stand-by pump C81b Drip fuelC78 Fuel outlet

Notes:p Free outlet requireds Please refer to the measuring

point list regarding design ofthe monitoring devices

m

25M 25 C Propulsion

10. Fuel oil systemHeavy fuel operation

1)An

indi

catio

n of

the

appr

oxim

ate

equi

vale

nts

inki

nem

atic

vis

cosi

ty a

t 50

°C a

nd R

edw

. I s

ec.

100

°F is

giv

en b

elow

:

Kine

mat

ic v

isco

sity

at

100

°C m

m2 /s

(cSt

)Ki

nem

atic

vis

cosi

ty a

t 5

0 °C

mm

2 /s (c

St)

Kine

mat

ic v

isco

sity

at

100

°F R

edw

. I s

ec.

Fuel

sha

ll be

free

of u

sed

lubr

icat

ing

oil (

ulo)

2)IS

O: 9

753)

ISO:

981

4)IS

O: 9

855)

ISO:

not

lim

ited

6)IS

O: C

arbo

n Re

sidu

e 10

7)IS

O: 0

.20

7

10

15

2

5

35

4

5

55

30

40

80

180

380

500

700

200

300

600

1500

3000

5000

7000

Requ

irem

ents

for r

esid

ual f

uels

for d

iese

l eng

ines

(as

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ered

)

De

sign

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n:

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AC

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CI

MAC

B

10

CIM

AC

C 10

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MAC

D

15

CIM

AC

E 25

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MAC

F

25

CIM

AC

G 35

CI

MAC

H

35

CIM

AC

K 35

CI

MAC

H

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AC

K 45

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MAC

H

55

CIM

AC

K 55

Re

late

d to

ISO8

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- RM

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RMB3

0 RM

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0 RM

E180

RM

F180

RM

G380

RM

H380

RM

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RM

H500

RM

K500

RM

H700

RM

K700

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ristic

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m.

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20

18

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max

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er

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max

0.

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dium

m

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m

ax

150

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0 35

0 20

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0 60

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0 60

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80

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m

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15

15

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15

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m

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15

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30

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30

30

30

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m



Visc

osity

/tem

pera

ture

dia

gram

m

27M 25 C Propulsion


Minimum requirements for storage, treatment and supply systems

Bunker tanks: In order to avoid severe operational problems due to incom-patibility, each bunkering must be made in a separate stor-age tank.

Settling tanks: In order to ensure a sufficient settling effect, the followingsettling tank designs are permissible:

- 2 settling tanks, each with a capacity sufficient for24 hours full load operation of all consumers

- 1 settling tank with a capacity sufficient for 36 hours fullload operation of all consumers and automatic filling

- Settling tank temperature 70 - 80 °C

Day tank: Two day tanks are required. The day tank capacity mustcover at least 4 hours/max. 24 hours full load operation of allconsumers. An overflow system into the settling tanks andsufficient insulation are required.

Guide values for temperatures

Fuel viscosity cSt/50 °C

Tank temperature [°C]

30 - 80 70 - 80

80 - 180 80 - 90

> 180 - 700 max. 98

Separators: Caterpillar Motoren recommends to install two self-clean-ing separators. Design parameters as per supplier recom-mendation. Separation temperature 98 °C! Maker and typeare to be advised to Caterpillar Motoren.

m


Booster pumps HP 1/HP 2: Screw type pump with mechanical seal.Installation vertical or horizontal. Delivery head 5 bar.

Capacity

V [m3/h] = 0.4 .. Peng. [kW]

1000


DN H1 H2 W D Output [kW ] m m

< 5000 32 249 220 206 180

< 10000 40 330 300 250 210

< 20000 65 523 480 260 355

> 20000 80 690 700 370 430

Supply system (Separate components): A closed pressurized system between daytank and engineis required as well as the installation of an automatic back-flushing filter with a mesh size of 10 μm (absolute).

Strainer HF 2: Mesh size 0.32 mm

m

29M 25 C Propulsion

Self cleaning filter HF 4: Mesh size 10 μm sphere passing mesh, type 6.60, make Boll& Kirch*, DN 50, without by-pass filter.

* In case of Caterpillar Motoren supply.


Dismantling of sieve300 mm

Pressure regulating valve HR 1: Controls the pressure at the engine inlet, approx. 4 bar.

Engine outputs

= 3000 kW > 3000 kW<

m


Final preheater HH 1/HH 2: Heating media:

- Electric current (max. surface power density 1.1 W/cm2)- Steam- Thermal oil

Temperature at engine inlet max 150 °C.

Viscosimeter HR 2: Controls the injection viscosity to 10 - 12 cSt.

Fine filter (fitted) HF 1: - Mesh size 34 μm- Without heating- Differential pressure indication and alarm contact fitted

Fuel Cooler DH 3: Required for heat dissipation with MGO/MDO operation.

V [m3/h] = 0.7 ...... Peng. [kW]

1000

Circulating pumps HP 3/HP 4: Design see pressure pumps.

Capacity


Mixing tank (without insulation) HT 2:

Engine output Volume Dimensions [mm] Weight

[kW] [l] A D E [kg]

< 4000 50 950 323 750 70

< 10000 100 1700 323 1500 120

> 10000 200 1700 406 1500 175

Vent

Inletfrompressurepump

Fromengine

Outletto engine

m

31M 25 C Propulsion


Notes:ff Flow verlocity in circuit system

< 0.5 m/sp Free outlet requireds Please refer to the measuring

point list regarding design of themonitoring devices

u From diesel oil separator or dieseloil transfer pump

All heavy fuel pipes have to be insu-lated.---- heated pipe

Connecting points:C76 Inlet duplex filterC78 Fuel outletC81 Drip fuelC81b Drip fuel

Accessories and fittings:DH3 MGO/MDO cooler HT1 Heavy fuel day tankDT1 Diesel oil day tank HT2 Mixing tankHF1 Fuel fine filter (duplex filter) HT5 Settling tank IHF2 Fuel primary filter HT6 Settling tank IIHF3 Fuel coarse filter KP1 Fuel injection pumpHF4 Self cleaning fuel filter KT2 Sludge tankHH1 Heavy fuel final preheater FQI Flow quantity indicatorHH2 Stand-by final preheater LI Level indicatorHH3 Heavy fuel preheater LSH Level switch highHH4 Heating coil LSL Level switch lowHP1 Fuel pressure pump PDI Diff. pressure indicatorHP2 Fuel stand-by pressure pump PDSH Diff. pressure switch highHP3 Fuel circulating Pump PDSL Diff. pressure switch lowHP4 Fuel stand-by circulating Pump PI Pressure indicatorHP5 Heavy fuel transfer pump (separator) PT Pressure transmitterHP6 Stand-by transfer pump (separator) TI Temperature indicatorHR1 Fuel pressure regulating valve TT Temperature transmitter (PT 100)HR2 Viscometer VI Viscosity indicatorHS1 Heavy fuel separator I VSH Viscosity Control switch highHS2 Heavy fuel separator II VSL Viscosity Control switch low

General notes:For location, dimensions and design (e. g. flexible connection) of the connectingpoints see engine installation drawing. Valve fittings with loose cone are not ac-cepted in the admission and return lines.

- Peak pressures max. 16 bar

m



Heavy fuel oil supply- and booster standard module

(Pressurized System), up to IFO 700 for steam and thermaloil heating, up to IFO 180 for electr. heating

Technical specification of the main components:

1. Primary filter

1 pc. Duplex strainer 540 microns

2. Fuel pressure pumps, vertical installation

2 pcs. Screw pumps with mechanical seal

3. Pressure regulating system

1 pc. Pressure regulating valve

4. Self cleaning fine filter

1 pc. Automatic self cleaning fine filter 10 microns absolut (without by-pass filter)

5. Consumption measuring system

1 pc. Flowmeter with local totalizer

6. Mixing tank with accessories

1 pc. Pressure mixing tank approx. 49 l volume up to 4000 kWapprox. 99 l volume from 4001 - 20000 kW

(with quick-closing valve)

7. Circulating pumps, vertical installation

2 pcs. Screw pumps with mechanical seal

8. Final preheater

2 pcs. Shell and tube heat exchangers each 100 % (saturated 7 bar or thermal oil 180 °C)each 100 % electrical

m

33M 25 C Propulsion

9. a) Heating medium control valve (steam/thermaloil)b) Control cabinet (electrical)

1 pc. control valve with built-on positioning drive 1 pc. control cabinet for electr. preheater

10. Viscosity control system

1 pc. automatic viscosity measure and control system VAF

Module controlled automatically with alarms and startersPressure pump starters with stand-by automaticCirculating pump starters with stand-by automaticPI-controller for viscosity controllingStarter for the viscosimeterAnalog output signal 4 - 20 mA for viscosity

AlarmsPressure pump stand-by startLow level in the mixing tankCirculating pump stand-by startSelf cleaning fine filter pollutionViscosity alarm high/lowThe alarms with potential free contacts

Alarm cabinet with alarms to engine control room and connection possibility for remote start/stop andindicating lamp of fuel pressure and circulating pumps

Performance and materials:The whole module is tubed and cabled up to the terminal strips in the electric switch boxes which areinstalled on the module. All necessary components like valves, pressure switches, thermometers,gauges etc. are included. The fuel oil pipes are equipped with trace heating (steam, thermaloil orelectrical) where necessary.The module will be tested hydrostatical and functional in the workshop without heating.


Steam Thermal oil

Electric Steam Thermal oil

Electric Steam Thermal oil

Electric

For power in kW up to (50/60 Hz) 2400/2900 2400/2900 4000/4800 4000/4800 8000/9600 8000/9600 Length in mm 2200 2300 2200 2700 3200 3500 Width in mm 1000 1000 1200 1200 1200 1200 Height in mm 2100 2100 2000 2000 2000 2000 Weight (approx.) in kg 1700 2500 2300 2400 2500 2700

m


11. Lubricating oil system

Lube oil quality

The viscosity class SAE 40 is required.

Wear and tear and thus the service life of the engine depend on the lube oil quality. Therefore highrequirements are made for lubricants:

Constant uniform distribution of the additives at all operating conditions. Perfect cleaning (detergenteffect) and dispersing power, prevention of deposits from the combustion process in the engine. Suffi-cient alkalinity in order to neutralize acid combustion residues. The TBN (total base number) must bebetween 30 and 40 KOH/g at HFO operation. For MDO operation the TBN is 12 - 20 depending on sulphurcontent.

I Approved in operationII Permitted for controlled use

When these lube oils are used, Caterpillar Motoren must be informed because at the moment there is insufficient experience availablefor MaK-engines. Otherwise the warranty is invalid.

1) Synthetic oil with a high viscosity index (SAE 15 W/40). Only permitted if the oil inlet temperatures can be decreased by 5 - 10 °C.

Manufacturer Diesel oil/Marine-diesel oil operation

I II HFO operation I II

AGIP DIESEL SIGMA S CLADIUM 120

X X

CLADIUM 300 S CLADIUM 400 S

XX

BP ENERGOL DS 3-154 VANELLUS C 3

XX

ENERGOL IC-HFX 304 ENERGOL IC-HFX 404

XX

CALTEX DELO 1000 MARINE DELO 2000 MARINE

XX

DELO 3000 MARINE DELO 3400 MARINE

XX

CASTROL MARINE MLC MXD 154 TLX PLUS 204

X

XX

TLX PLUS 304 TLX PLUS 404

XX

CEPSA KORAL 1540 X CHEVRON DELO 1000 MARINE OIL

DELO 2000 MARINE OIL XX

DELO 3000 MARINE OIL DELO 3400 MARINE OIL

XX

TOTAL LUBMARINE DISOLA M 4015 AURELIA 4030

XX

AURELIA XL 4030 AURELIA XT 4040

XX

ESSO EXXMAR 12 TP EXXMAR CM+ ESSOLUBE X 301

XXX

EXXMAR 30 TP EXXMAR 40 TP EXXMAR 30 TP PLUS EXXMAR 40 TP PLUS

X

XX

X

MOBIL MOBILGARD 412 MOBILGARD ADL MOBILGARD M 430 MOBILGARD 1-SHC 1)

XXX

X

MOBILGARD M 430 MOBILGARD M 440

XX

SHELL GADINIA GADINIA AL ARGINA S ARGINA T

XXXX

ARGINA T ARGINA X

XX

TEXACO TARO 16 XD TARO 12 XD TARO 20 DP

XXX

TARO 30 DP TARO 40 XL

XX

m

35M 25 C Propulsion


Lube oil quantities/- change intervals: Circulating quantity:approx. 0.8 l/kW output with wet sump designapprox. 1.3 l/kW output with separate tank

The change intervals depend on:- the quantity- fuel quality- quality of lube oil treatment (filter, separator)- engine load

By continuous checks of lube oil samples (decisive arethe limit values as per "MaK Operating Media") an opti-mum condition can be reached.

Force pump (fitted) LP 1: Gear type pump

Lub oil stand-by force pump (separate) LP 2: - principle per engine- in case of Caterpillar Motoren supply vertical design

only- Prelubrication pressure pump only for inland water

way vessel and multi engines plants

Suction pump (fitted) LP 3: Option for the operation with high level tank

Lub oil stand by suction pump (separate)LP 4: - Option for the operation with high level tank

- principle per engine- in case of Caterpillar Motoren supply vertical design

only- Prelubrication suction pump only for inland water way

vessel and multi engine plants

Strainer LF 4: Mesh size 2 - 3 mm - to be supplied by the yard

m


Self cleaning filter LF 2: Mesh size 30 μm sphere passing mesh, type 6.46, make Boll& Kirch*. Without by-pass filter. Without flushing oil treat-ment.

* In case of Caterpillar Motoren supply.


Dismantling of sieve 300 mm

Engine Type6.46

Amm

Bmm

Cmm

Emm

Fmm

Smm

Xmm

Ymm

Weight kg

6 M 25 C DN 80 435 170 615 205 255 400 160 160 77

8/9 M 25 C DN 100 485 200 615 245 295 400 180 180 112

Self cleaning filter (fitted) LF 2: (Option)

Duplex filter (fitted) LF 1: Mesh size 80 μmDifferential pressure indication and alarm contact fitted.Omitted if LF 2 is fitted

m

37M 25 C Propulsion


Cooler (separate) LH 1: Plate type (plates made of stainless steel)

Temperature controller (separate) LR 1: P-controller with manual emergency adjustment


DN D F G H [kg]

6 M 25 C 80 200 171 267 151 27

8/9 M 25 C 100 220 217 400 167 47

Discharge to circulating tank: DN 200 at flywheel or counter flywheel side. Compensator tobe supplied by the yard.

Circulation tank: Volume

In case of a high level tank max. 2.5 m height above crank-shaft.Oil filling approx. 80 % of tank volume.

V [m3] =1.7 · Peng. [kW]

1000

m



Recommendation of pipe location in the circulating tank

Option (for MGO and MDO only): Deep oil pan (wet sump)

Crankcase ventilation: The location of the ventilation is on top of the engine blocknear to the turbocharger (see system connections C 91).

The vent pipe DN 80 must be equipped with a condensatetrap and drain. It has to be arranged separately for each en-gine. Crankcase pressure max. 150 Pa (15 mm WC).

Discharge from engine

Separator suction pipeFlushing oil from automatic filter

Separator return pipe

Suction pipe force pumpSuction pipe stand-by force pump

m

39M 25 C Propulsion

Treatment at MGO/MDO operation

The service life of the lube oil will be extended by by-passtreatment.

Centrifuge (Option, fitted on the engine)LS 2: Minimum requirement

Separator LS 1: RecommendedDesign:- Separating temperature 85 - 95 °C- Quantity to be cleaned three times/day- Self cleaning type

Separation capacity

Veff [l/h] = 0.18 · Peng [kW]

Treatment at heavy fuel operation

Separator LS 1: Required with the following design:- Separating temperature 95 °C- Quantity to be cleaned five times/day- Self cleaning type

Separation capacity

Veff [l/h] = 0.29 · Peng [kW]


m


11. Lubricating oil systemMGO/MDO operation (wet sump)

Connecting points:C46a Stand-by force pump, suction sideC55c Connection flushing pipe automatic

filterC58 Force pump, delivery sideC59 Luboil inlet, luboil coolerC60 Separator connection, suction side or

drain or filling pipeC61 Separator connection, delivery side

or from bypass filterC61b Inlet luboil centrifugeC62 Drip oil, duplex filterC91 Crankcase ventilation to stack

Accessories and fittings:LF1 Duplex luboil filter LI Level indicatorLF2 Self cleaning luboil filter LSL Level switch lowLF4 Suction strainer PDI Diff. pressure indicatorLH1 Luboil cooler PDSH Diff. pressure switch highLH2 Luboil preheater PI Pressure indicatorLP1 Luboil force pump PSL Pressure switch lowLP2 Luboil stand-by force pump PSLL Pressure switch lowLP9 Transfer pump (separator) PT Pressure transmitterLR1 Luboil temperature control valve TI Temperature indicatorLR2 Oil pressure regulating valve TSHH Temperature switch highLS1 Luboil separator TT Temperature transmitter (PT 100)LS2 Luboil centrifugeLT2 Oil pan

General notes:For location, dimensions anddesign (e. g. flexible connec-tion) of the connecting pointssee engine installation draw-ing.The separator (LS1) can beomitted for engine with fittedcentrifuge (LS2).

Notes:f Drainh Please refer to the meas-

uring point list regardingdesign of the monitoringdevices

o See "crankcase ventila-tion installation instruc-tions" 4-A-9570

p Free outlet required* Option

m

41M 25 C Propulsion


Connecting points:C51 Force pump, suction sideC53 Luboil dischargeC58 Force pump, delivery sideC59 Luboil inlet, luboil coolerC62 Dripoil, duplex filterC91 Crankcase ventilation to stack

Accessories and fittings:LF1 Duplex luboil filterLF2 Self cleaning luboil filterLF4 Suction strainerLH1 Luboil coolerLH2 Luboil preheaterLP1 Luboil force pumpLP2 Luboil stand-by force pumpLP5 Prelubrication pumpLP9 Transfer pump (separator)LR1 Luboil temperature control valveLR2 Oil pressure regulating valveLS1 Luboil separatorLT1 Luboil sump tank

Notes:h Please refer to the measuring point list

regarding design of the monitoringdevices

l A separator is required for heavy fueloperation

o See "crankcase ventilation installationinstructions" 4-A-9570

p Free outlet requiredy Provide an expansation jointz Max. suction pressure 0.4 bar

LI Level indicatorLSL Level switch lowLSH Level switch highPDI Diff. pressure indicatorPDSH Diff. pressure switch highPI Pressure indicatorPSL Pressure switch lowPSLL Pressure switch lowPT Pressure transmitterTI Temperature indicatorTSHH Temperature switch highTT Temperature transmitter (PT 100)

General notes:For location, dimensions and design (e. g.flexible connection) of the connectingpoints see engine installation drawing.

m


12. Cooling water system

The heat generated by the engine (cylinder, turbocharger, charge air and lube oil) is to be eliminated bymeans of treated freshwater acc. to the MaK coolant regulations.

The inlet temperature in the LT-circuit is max. 38 °C.

Two-circuit cooling: with two-stage charge air cooler.

HT-fresh water pump (fitted) FP 1: Capacity: acc. to heat balanceHT-fresh water pump (stand-by) FP 5

LT-fresh water pump (fitted) FP 2: Capacity: acc. to heat balanceLT-fresh water pump (stand-by) FP 6

HT-temperature controller (separate) FR 1: P-controller with manual emergency adjustment (basis).

LT-temperature controller (separate) FR 2: P-controller with manual emergency adjustment (basis).Option: PI-controller with electric drive.

* Minimum, depending on total cooling water flow


DN D F G H [kg]

6/8/9 M 25 C HT 6 M 25 C LT*

80 200 171 267 151 27

8/9 M 25 C LT* 100 220 217 403 167 47

m

43M 25 C Propulsion


Preheater (separate) FH 5/FP 7: Consisting of circulating pump (5 m3/h), electricheater (18 kW) and switch cabinet. Voltage 400 - 480,frequency 50/60 Hz. Weight 95 kg.

Charge air heating CR 4:: Control unit for charge air heating in part load con-dition with electric/pneumatic 2 position flap.

Option:

Charge-air thermostat (separate) CR 1: PI-controller with electric drive

m


ρ · H · VP = [kW]

367 · η

.

P - Power [kW]PM - Power of electr. motor [kW]V - Flow rate [m3/h]H - Delivery head [m]ρ - Density [kg/dm3]η - Pump efficiency

0.70 for centrifugal pumps

< 1.5 kW1.5 - 4 kW4 - 7.5 kW

> 7.5 - 40 kW> 40 kW

PM = 1.5 · PPM = 1.25 · PPM = 1.2 · PPM = 1.15 · PPM = 1.1 · P

.

HT-cooler (separate) FH 1: Plate type (plates made of titanium), size depending on thetotal heat to be dissipated.

LT-cooler (separate) FH 2: Plate type (plates made of titanium), size depending on thetotal heat to be dissipated.

Header tank FT 1/FT 2: - Arrangement: min. 4 m above crankshaft centre line.- Size acc. to technical engine data.- All continuous vents from engine are to be connected.

Drain tank with filling pump: Is recommended to collect the treated water when carryingout maintenance work (to be installed by the yard).

Electric motor driven pumps: Option for fresh and seawater, vertical design.Rough calculation of power demand for the electric bal-ance.


m

45M 25 C Propulsion


Heat balance 6 M 25 C

m




m

47M 25 C Propulsion



m



Notes:b Measurement min 2.0 m dis-

tance to C17e Bypass DN 12f Drainh Please refer to the measuring

point list regarding design ofthe monitoring devices

m Air supply 2 - 10 bar

For temp. control valve P-typeFR1, FR2, FR3 alternative PI-typepossible

Connecting points:C14 Charge air cooler LT, inletC15 Charge air cooler LT, outletC17 Charge air cooler HT, outletC21 Freshwater pump HT, inletC22 Freshwater pump LT, inletC23 Stand-by pump HT, inletC28 Freshwater pump, LT, outletC37 Vent

Accessories and fittings:CH1 Charge air cooler HTCH2 Charge air cooler LTCR4 Flap for charge preheatingDH3 Fuel oil cooler for MDO operationFH1 Freshwater cooler HT *FH2 Freshwater cooler LT *FH3 Heat ConsumerFH5 Freshwater preheaterFP1 Freshwater pump (fitted on engine) HTFP2 Freshwater pump (fitted on engine) LTFP5 Freshwater stand-by pump HTFP6 Freshwater stand-by pump LTFP7 Preheating pumpFR1 Temperature control valve HTFR2 Temperature control valve LTFR3 Flow. temperature control valve HT

* Classification society requirements have to be taken into account

General notes:For location, dimensions and design (e. g. flexible connection) of the connecting points see engineinstallation drawing. With skin cooler not required: - Seawater system (SP1, SP2, SF1, ST1)Temp. control valve FR3 required, if heat recovery installed.

FT1 Compensation tank HTFT2 Compensation tank LTLH1 Luboil coolerLH3 Gear luboil coolerSF1 Seawater filterSP1 Seawater pumpSP2 Seawater stand-by pumpST1 Sea chestLI Level indicatorLSL Level switch lowPI Pressure indicatorPSL Pressure switch lowPSLL Pressure switch lowPT Pressure transmitterTI Temperature indicatorTSHH Temperature switch highTT Temperature transmitter (PT 100)

m

49M 25 C Propulsion

13. Flow velocities in pipes

Example: di = 100 mm, V = 60 m3/hVelocity in the pipe 2,1 m/s

m


14. Starting air system

Requirement of Classification Societies (regarding design)

- No. of starts: 6- No. of receivers: min. 2

Receiver capacity acc. to GL recommendation AT 1/AT 2

When CO2 fire extinguishing plants are arranged in the engine room, the blow-off connection of thesafety valve is to be piped to the outside.

1 Filling valve DN 182 Pressure gauge G 1/43* Relief valve DN 74 Drain valve DN 85 Drain valve DN 8 (for vertical position)6 Connection aux. air valve G1/27 To starting valve at engine8 Typhon valve DN 16

Option:* with pipe connection G 1/2

6/8/9 Cyl.

Single-engine plant 2 x 250 l

Twin-engine plant 2 x 500 l

Receiver capacity [l]

Lmm

D Ø mm

Valve head Weight

approx. kg

250 2960 480 DN 38 230

500 3470 480 DN 50 320

m

51M 25 C Propulsion

14. Starting air system

Compressor AC 1/AC 2: 2 compressors with a total output of 50 % each are required.

The filling time from 0 to 30 bar must not exceed 1 hour.

Capacity

V [m3/h] = Σ VRec. · 30.

VRec. = Total receiver volume [m³]

General notes:For location, dimensions and design (e. g. flexible connection) ofthe connecting points see engine installation drawing.

Clean and dry starting air is required. A starting air filter has tobe installed before engine, if required.

The air receivers are to be drained sufficiently at least once perday.

Notes:a Control aird Water drain (to be mounted at the lowest point)e To engine no. 2h Please refer to the measuring point list regarding design of

the monitoring devices* Automatic drain required

Connecting points:C86 Connection, starting air

Accessories and fittings:AC1 CompressorAC2 Stand-by compressorAR1 Starting valveAR4 Pressure reducing valveAR5 Oil and water separatorAT1 Starting air receiver (air bottle)AT2 Starting air receiver (air bottle)PI Pressure indicatorPSL Pressure switch low, only for main enginePT Pressure transmitter

AT1/AT2 Option:- Typhon valve- Relief valve with pipe connection

m


15. Combustion air system

General: To obtain good working conditions in the engine room and toensure trouble free operation of all equipment attentionshall be paid to the engine room ventilation and the supply ofcombustion air.

The combustion air required and the heat radiation of allconsumers/heat producers must be taken into account.

Air intake from engine room (standard): - Fans are to be designed for a slight overpressure in theengine room.

- On system side the penetration of water, sand, dust, andexhaust gas must be avoided.

- When operating under tropical conditions the air flowmust be conveyed directly to the turbocharger.

- The temperature at turbocharger filter should not fall be-low + 10 °C.

- In cold areas warming up of the air in the engine roommust be ensured.

Air intake from outside: - The intake air duct is to be provided with a filter. Penetra-tion of water, sand, dust and exhaust gas must beavoided.

- Connection to the turbocharger is to be established via anexpansion joint (to be supplied by the yard). For this pur-pose the turbocharger will be equipped with a connectionsocket.

- At temperatures below + 10 °C the Caterpillar Motoren/Application Engineering must be consulted.

- The max pressure loss (incl. silencer and exhaust gasboiler) of 30 mbar is applicable as value for the total flowresistance of plants with separate intake air filter!

Radiated heat: see technical dataTo dissipate the radiated heat a slight and evenly distributedair current is to be led along the engine exhaust gas mani-fold starting from the turbocharger.

m

53M 25 C Propulsion

16. Exhaust system

Position of exhaust gas nozzle: A nozzle position of 0, 30, 45, 60 and 90° is possible.The exhaust outlet of the turbocharger has a fixed positionof 45°.Transition pieces for outlets of 0, 30, 60 and 90° areavailable.

Exhaust compensator:

Design of the pipe cross-section: The pressure loss is to be minimized in order to optimize fuelconsumption and thermal load of the engine.

Max. flow velocity: 40 m/s (guide value).

Max pressure loss (incl. silencer and exhaust gas boiler):30 mbar(lower values will reduce thermal load of the engine).

The aforesaid value is also applicable as value for the totalflow resistance of plants with separate intake air filter!

Notes regarding installation: - Arrangement of the first expansion joint directly on theexhaust gas nozzle

- Arrangement of the first fixed point in the conduit directlyafter the expansion joint

- Drain opening to be provided (protection of turbochargerand engine against water)

- Each engine requires an exhaust gas pipe (one commonpipe for several engines is not permissible).

If it should be impossible to use the standard transitionpiece supplied by Caterpillar Motoren, the weight of thetransition piece manufactured by the shipyard must not ex-ceed the weight of the standard transition piece. A drawingincluding the weight will then have to be submitted ap-proval.

Diameter DN Length [mm] Weight [kg]

6 M 25 C 500 360 42

8/9 M 25 C 600 450 76

m


16. Exhaust system

t = Exhaust gas temperature (°C)G = Exhaust gas massflow (kg/h)Δp = Resistance/m pipe length (mm WC/m)d = Inner pipe diameter (mm)w = Gas velocity (m/s)l = Straight pipe length (m)L' = Spare pipe length of 90° bent pipe (m)L = Effective substitute pipe length (m)ΔPg = Total resistance (mm WC)

Example (based on diagram data A to E):t = 335 °C, G = 25000 kg/hl = 15 m straight pipelength, d = 700 mm3 off 90° bend R/d = 1.51 off 45° bend R/d = 1.5ΔPg = ?

Δp = 0.83 mm WC/mL' = 3 · 11 m + 5.5 mL = l + L' = 15 m + 38.5 m = 53.5 mΔPg = Δp · L = 0.83 mm WC/m · 53.5 m = 44.4 mm WC

Resistance in exhaust gas piping

m

55M 25 C Propulsion

16. Exhaust system

0.031 0.063 0.125 0.25 0.5 1 2 4 8 f [kHz]

160

150

140

130

120

110

100

140 140 139135

133 132 131126

123

0.031 0.063 0.125 0.25 0.5 1 2 4 8 f [kHz]

160

150

140

130

120

110

100

140 139 139134

133 132 130125

122

Exhaust sound power level not attenuated [1 x 1 m]

Tolerance + 2 dB

LwOct [dB](reference 10-12 W)



6 M 25 C (1900 kW/720 rpm, 1980 kW/750 rpm)

9 M 25 C (2850 kW/720 rpm, 2970 kW/750 rpm)

8 M 25 C (2540 kW/720 rpm, 2640 kW/750 rpm)

0.031 0.063 0.125 0.25 0.5 1 2 4 8 f [kHz]

160

150

140

130

120

110

100

139137 138

132 132 130 129

122 119

m


16. Exhaust system

Exhaust data: Tolerance: 5 %Atmospheric pressure: 1 barRelative humidity: 60 %Constant speed

Intake air temperature: 25 °C• Output % • Output [kW] • [kg/h] • [°C]

Output [kW]

100 90 80 70 60 50

19001900

14845312

171013570

313

152012385

313

133011200

315

1140 10100

319

9507686339

6 M 25 C

19801980

16120290

178213540

285

158412500

285

138610833

285

1188 9375 305

9907850318

25402540

19100335

228617940

323

203216560

320

177815000

315

1524 13415

315

127010100

3358 M 25 C

26402640

20070316

237617710

312

211216050

309

184814270

303

1584 12500

308

132010800

313

28502850

22030338

256520442

324

228018650

320

199516850

315

1710 15825

318

142511925

3299 M 25 C

29702970

22000320

267319375

317

237617920

309

207916460

309

1782 14060

312

148512170

316

• Output % • Output [kW] • [kg/h] • [°C]

Output [kW]

100 90 80 70 60 50

19001900

14250331

171013027

332

152011890

332

133010750

334

11409700338

9507380359

6 M 25 C

19801980

14146306

178212920

302

158411355

302

138610312

302

11888960323

9907590337

25402540

18335355

228617222

342

203215900

339

177814400

334

152412900

336

12709700355

8 M 25 C

26402640

18044335

237616666

331

211215210

321

184813545

322

158411875

327

132010171

332

28502850

21150358

256519624

343

228017905

339

199516175

334

171015192

337

142511448

3499 M 25 C

29702970

19600339

267318230

336

237616980

328

207915375

328

178213333

332

148511480

335

Intake air temperature: 45 °C

m

57M 25 C Propulsion

16. Exhaust system

Silencer: Design according to the absorbtion principle with wide-band attenuation over a great frequency range and lowpressure loss due to straight direction of flow. Sound ab-sorbing filling consisting of resistant mineral wool.

Sound level reduction 25 dB(A), alternatively 35 dB(A).Max. permissible flow velocity 40 m/s.

Silencer with spark arrester: Soot separation by means of a swirl device (particles arespun towards the outside and separated in the collectingchamber). Sound level reduction 25 dB(A) or 35 dB(A). Max.permissible flow velocity 40 m/s.

Silencers are to be insulated by the yard. Foundation brack-ets are provided as an option.

m


16. Exhaust system

Silencer/Spark arrestor and silencer: Installation: vertical/horizontalFlange according to DIN 86044Counterflanges, screws and gaskets are included, withoutsupports and insulation

Silencer

Spark arrestor and silencer

Attenuation 25 dB (A) 35 dB (A)

DN D B L kg L kg

6 M 25 C 500 950 588 3185 710 3940 750

8/9 M 25 C 600 1100 659 3760 1100 4760 1300

Exhaust gas boiler: Each engine should have a separate exhaust gas boiler. Al-ternatively, a common boiler with separate gas sections foreach engine is acceptable.

Particularly when exhaust gas boilers are installed attentionmust be paid not to exceed the maximum recommendedback pressure.

m

59M 25 C Propulsion

16. Exhaust system

Cleaning the turbocharger compressor: The components for cleaning (dosing vessel, pipes, shut-offvalve) are engine mounted.

Water is fed before compressor wheel via injection pipesduring full load operation every 24 to 48 hours.

Cleaning the turbine blade andnozzle ring: The cleaning is carried out with clean fresh water "wet

cleaning" during low load operation at regular intervals, de-pending on the fuel quality, 250 to 500 hours.

Duration of the cleaning period is approx. 20 minutes. Freshwater of 1.5 bar is required.

During cleaning the water drain should be checked. There-fore the shipyard has to install a funnel after connectionpoint C36.

Water flow[l/min]

Injection time[min]

6/8/9 M 25 C 6 - 18 15 - 20

C42 Fresh water supply, Ø 16C36 Drain, Ø 25

Connection of C42 with quick coupling device

Dirty water tank

m


17. Air borne sound power level

The airborne noise of the engines is measured as a sound power level according to EN ISO 9614-2/Accuracy class 3.

Tolerance + 2 dB




6 M 25 C (1900 kW/720 rpm, 1980 kW/750 rpm)

9 M 25 C (2850 kW/720 rpm, 2970 kW/750 rpm)

8 M 25 C (2540 kW/720 rpm, 2640 kW/750 rpm)

111

105108

111112

117

111

95

100

105

110

115

120

125

0.063 0.125 0.25 0.5 1 2 4 [kHz]

115 110112

113113

117

116

95

100

105

110

115

120

125

0.063 0.125 0.25 0.5 1 2 4 [kHz]

116 111113

114

113

118120

95

100

105

110

115

120

125

0.063 0.125 0.25 0.5 1 2 4 [kHz]

m

61M 25 C Propulsion

18. Foundation

Support distance a = 1210 mmF = TN / a

2. Dynamic load: The dynamic forces and moments are superimposed on thestatic forces. They result on the one hand from the firingforces causing a pulsating torque and on the other handfrom the external mass forces and mass moments.

The tables indicate the dynamic forces and moments aswell as the related frequencies.

External foundation forces and frequencies:

The following information is relevant to the foundation design and the aftship structure.

The engine foundation is subjected to both static and dynamic loads.

1. Static load: The static load results from the engine weight which is dis-tributed approximately evenly over the engine’s foundationsupports and the mean working torque TN resting on thefoundation via the vertical reaction forces. TN increases theweight on one side and reduces it on the other side by thesame amount.

Output[kW]

Speed[1/min]

TN

[kNm]

1900 720 25.3 6 M 25 C

1980 750 25.2

2540 720 33.7 8 M 25 C

2640 750 33.6

2850 720 38.0 9 M 25 C

2970 750 37.8

m


All forces and moments not indicated are irrelevant or do not occur. The effect of these forces andmoments on the ship’s foundations depends on the type of engine mounting.

18. Foundation

Output [kW]

Speed [rpm] Order-No.

Frequency [Hz]

Mx [kNm]

1900 720 3 6

36 72

20.7 10.4

6 M 25 C 1980 750 3

6 37.5 75

20.6 10.4

2540 720 4 8

48 96

36.1 4.7

8 M 25 C 2640 750 4

8 50

100 36.0 4.6

2850 720 4.5 9

54 108

33.9 3.0

9 M 25 C 2970 750 4.5

9 56.25 112.5

33.8 3.0

Output [kW]

Speed [rpm]

Order-No.

Frequency [Hz]

My [kNm]

Mz [kNm]

1900 720 — — 6 M 25 C

1980 750 — —

2540 720 — — 8 M 25 C

2640 750 — —

2850 720 1 2

12 24

8.6 7.2

— 9 M 25 C

2970 750 1 2

12.5 25

9.3 7.8

—

m

63M 25 C Propulsion

18. Foundation

2.1 Rigid mounting: The vertical reaction forces resulting from the torque varia-tion Mx are the most important disturbances to which theengine foundation is subjected. As regards dynamic load,the indicated moments Mx only represent the exciting val-ues and can only be compared among each other. The ac-tual forces to which the foundation is subjected depend onthe mounting arrangement and the rigidity of the foundationitself.

In order to make sure that there are no local resonant vibra-tions in the ship’s structure, the natural frequencies of im-portant components and partial structures must be suffi-ciently far away (+ 30%) from the indicated main excitingfrequencies.

2.2 Resilient mounting: The dynamic foundation forces can be considerably re-duced by means of resilient engine mounting.

General note: The shipyard is solely responsible for the adequate designand quality of the foundation.

Information on foundation bolts (required pretightening tor-ques, elongation, yield point), steel chocks, side stoppersand alignment bolts is to be gathered from the foundationplans.

Examples "for information only" for the design of the screwconnections will be made available as required.

If pourable resin is used it is recommendable to employ au-thorized workshops of resin manufacturers approved by theclassification societies for design and execution.

It has to be taken into account that the permissible surfacepressure for resin is lower than for steel chocks and there-fore the tightening torques for the bolts are reduced corre-spondingly.

m


18. FoundationRigid mounting

Side stopper to be with 1 wedge (see sketch). Wedge to be placed at operating temperature and se-cured by welding.

Dimensioning according to classification society and cast resin suppliers requirements.

Number of Bolts

Jacking Bolts - To be protected against contact/bond with resin- After setting of resin dismantle the jacking screws completely

To be supplied by yard: Foundation bolts, fitted bolts, nuts and tension sleeves, side stoppers,steel chocks, cast resin

The shipyard is solely responsible for adequate design and quality of the foundation.

Fitted bolts Foundation bolts

6 M 25 C 4 24

8 M 25 C 4 32

9 M 25 C 4 36

6 M 25 C 8/9 M 25 C

1 Pair 1) 2 Pairs 2)

Side stoppers 1) 1 pair at end of bed plate2) 1 pair at end of cylinder housing and

1 pair between cyl. 4 and 5.

m

65M 25 C Propulsion

18. FoundationRigid mounting

Proposal for rigid mounting

Pre-tightening force

Cast resin Steel

Through bolts M 24 [N]

Fitted bolts M 24 [N]

Through bolts M 24 [N]

Fitted bolts M 24 [N]

100000 100000 170000 170000

Bolts and chocks are yard supply. Design responsibility is with the yard.

m


18. FoundationResilient mounting

Conical elements

6 M 25 C 6

8 M 25 C 8

9 M 25 C 8

Major components:- Conical rubber elements for active isolation of dynamic engine forces and structure born noise are

combined horizontal, lateral and vertical stoppers to limit the engine movements.- Dynamically balanced highly flexible coupling.- Flexible connections for all media.- Special designed exhaust gas below.

Details are shown on binding installation drawings.

No. of elements:

Important note:- The resilient mounting alone does not provide garant for a quiet ship. Other sources of noise like

propeller, gearbox and aux. engines have to be considered as well.- Radial restoring forces of the flexible coupling (due to seaway) may be of importance for the layout

of the reduction gear.

m

67M 25 C Propulsion

Structure borne sound level Lv, expected (measured in the test cell)

Lv Oct [dB](reference5*10-8 m/s)

20

30

40

50

60

70

80

90

100

110

0.031 0.063 0.125 0.25 0.5 1 2 4 8

Frequency [kHz]

above

below

18. FoundationStructure borne

m


19. Power transmission

Coupling between engine and gearbox

For all types of plants the engines will be equipped with flexible flange couplings.

The guards for the flexible couplings should be of perforated plate or gratings to ensure an optimumheat dissipation (yard supply).

Mass moments of inertia

* Running gear with balance weights and vibration damper

Selection of flexible couplings

The calculation of the coupling torque for main couplings is carried out acc. to the following formula.

T KN [kNm] > · · 9.55Po [kW]no [min-1]

Po Engine outputno Engine speedTKN Nominal torque of the coupling in the catalog

For installations with a gearbox PTO it is recommended to oversize the PTO coupling by the factor 1.5in order to have sufficient safety margin in the event of misfiring.

Speed[rpm]

Engine * [kgm2]

Flywheel [kgm2]

Total[kgm2]

6 M 25 C 135 355

8 M 25 C 205 425

9 M 25 C

720/750

215

220

435

m

69M 25 C Propulsion


Fly wheel and flexible coupling

Space for OD-Box to be considered!

Couplings for twin rudder propeller have to be designed with a supplementary torque of 50 %.

Power Speed Nominal torque of coupling

Type Vulkan Rato-R Weight

Size d L1 4) L2 3) 1) 2)

[kW] [rpm] [kNm] Rato-R [mm] [mm] [mm] [kg] [kg]

6 M 25 C 2000 750 31.5 G 262 ZR

8 M 25 C 2640 750 40.0 G 262 TR

9 M 25 C 3000 750 45.0 G 262 YR

800 594 309 333 352

1) without torsional limit device2) with torsional limit device3) length of hub4) Alignment control (recess depth 5 mm)

m



Power take-off

The PTO output 6, 8 and 9 M 25 C in equal to the engine output.

The connection requires a highly flexible coupling, type Vulkan (if supplied by Caterpillar Motoren).

A combination (highly flexible coupling/clutch) will not be supplied by Caterpillar Motoren. The weightforce of the clutch cannot be absorbed by the engine and must be borne by the succeeding machine.

The coupling hub is to be adapted to suit the PTO shaft journal.

The definite coupling type is subject to confirmation by the torsional vibration calculation.

X Y Z

< 1000 kW 100 170 1320

< 2700 kW 157 240 1320

m

71M 25 C Propulsion


Voith propeller drive, rudder-propeller-drive

All components after flex. coupling are not suppliedby Caterpillar Motoren!

All components after flex. coupling are not suppliedby Caterpillar Motoren!

P/n [kW/rpm]

A[mm]

B[mm]

6 M 25 C 2.7 1823 1261

8 M 25 C 3.5 1823 1261

9 M 25 C 4.0 1823 1261

B Is valid for Vulkan Rato-couplings

m


20. Data for torsional vibration calculation

Details to be submitted for the torsional vibration calculation

A torsional vibration calculation is made for each installation. For this purpose exact data of all compo-nents are required. See table below:

1. Main propulsion

Clutch existing ? yes no

Moments of Inertia: Engaged ............. kgm² Disengaged: .............. kgm²

Flexible Coupling: Make .................. Type: ....... Size

Gearbox: Make ................... Type: ....... Gear ratio .........

Moments of Inertia and dyn. torsional rigidity (Mass elastic system)

Shaft drawings with all dimensions

CPP D = ............ mm Blade No. ........

Moments of Inertia: in air ............. kgm² / in water = ............. kgm²

Exciting moment in percent of nominal moment = ............. %

Operation mode CPP: const. speed Combinator:

Speed range from: ................. – rpm

Normal speed range: CPP = 0.6 Nominal speed

2. PTO from gearbox: yes no

If yes, we need the following information:

Clutch existing? yes no

Moments of Inertia: Engaged: ............ kgm2 Disengaged: .............. kgm²

Flexible coupling: Make: .............. type .................... Size ..............

Gearbox: .................. Make: .............. type .................... Gear ratio: .............

Moments of Inertia and dyn. torsional rigidity (Mass diagram)

Kind of PTO driven machine: ............................ Rated output .............. kW

Power characteristics, operation speed range .............. rpm

3. PTO from free shaft end: yes no

If yes, we need the following information:

Clutch existing? yes no

Moments of Inertia: Engaged: ............ kgm2 Disengaged: .............. kgm²

Flexible coupling: Make ............. type .................... Size ..............

Gearbox: .................. Make ............. type .................... Gear ratio .............

Moments of Inertia and dyn. torsional rigidity (Mass diagram)

Kind of PTO driven machine: ........................... Rated output .............. kW

Power characteristics, operating speed range .............. rpm

4. Explanation:

Moments of Inertia and dyn. torsional rigidity in absolut dimensions, i. e. not reduced.

m

73M 25 C Propulsion

21. Control and monitoring system

Engine control panel

m



Remote control for reversing gear plant

m

75M 25 C Propulsion

21. Control and monitoring systemRemote control for reversing gear plant

m


21. Control and monitoring systemRemote control for CP propeller plant

m

77M 25 C Propulsion

21. Control and monitoring systemRemote control for twin engine plant with one propeller

m


21. Control and monitoring systemElectric remote control/Fixed rudder propeller

m

79M 25 C Propulsion

21. Control and monitoring systemElectric remote control/Voith-propeller propulsion

m



Speed control

Main engines are equipped with a mech./hydr. speed governor (milliampere speed setting). With thefollowing equipment:

- Stepper motor in the top part of the governor for remote speed control- Separate stepper motor control with adjustable speed range and speed ramp. Voltage supply =

24 V DC

The control is fitted easily accessible on the engine in the terminal board box (X3) especially providedfor control components.

The set speed value of

nmin = 4 mAnmax = 20 mA

is converted into a current required by the stepper motor.

- Speed setting knob (emergency speed setting)- Shut-down solenoid (24 V DC/100 % duty cycle) for remote stop (not for automatic engine stop).- Steplessly adjustable droop on the governor from 0 - 10 %- Standard setting: 0 %- Device for optimization of the governor characteristic- Serrated drive shaft (for easy service)

m

81M 25 C Propulsion


Speed control

Twin engine plant with one CPP: The engines are equipped with an actuator (optional with mech.back-up). Electronic governors are installed in a separate con-trol cabinet.

The governor comprises the following functions:

- Speed setting range to be entered via parameters- Adjustable acceleration and deceleration times- Starting fuel limiter- Input for stop (not emergency stop)- 18 - 32 V DC voltage supply- Alarm output- Droop operation (primary shaft generator)- Isochronous load distribution by master/slave princip for twin

engine propulsion plants via double-reduction gear

Twin engine plant with one CPP Single engine plant with CPP

Control cabinets electronic governor Woodward 723+ (standard)Regulateurs Europa Viking 35 (option)

Cabinets with different dimentions

m



Engine monitoring

m

83M 25 C Propulsion


List of measuring point: Main engine M 25 C all classes

Sensor Measur.-point

Monitoring point Abbrev. Action

Fitted Separate

Remarks

1104 Luboil pressure PAL OA B Starting stand-by pump from pump control

1105 Luboil pressure PAL OA A1

1106 Luboil pressure PALL OAMS

B1

1111 Luboil differential pressure duplex filter

PDAH OA B1 Only if 1112 separate

1112 Luboil differential pressure selfcleaning filter

PDAH OA B1 B1

1202 Lubricating oil temperature engine inlet

TAH OA A1

1203 Lubricating oil temperature engine inlet

TAHHOAAD

B1

1251 Smoke concentration crankcase

QAH OA B1 Above 2200 kW 1 device f. 1251+1253

1253 Smoke concentration crankcase

QAH OAMS

B1 Above 2200 kW 1 device f. 1251+1253

1301 Luboil level wet sump plan LAL OA B1 Not provided with dry sump

1315 Niveau dry sump LAH OA B1 Only at high tank Starting stand-by luboil suction pump

2101 FW pressure high temp. circuit engine inlet

PAL OA B Starting stand-by pump from pump control


PAL OA A1


PALL OAMS

B1

2111 FW pressure low temp. circuit cooler inlet

PAL OA B Starting stand-by pump from pump control

2112 FW pressure low temp. circuit cooler inlet

PAL OA A

2211 FW temp. high temp. circuit engine outlet

TAH OA A1

2212 Fresh water temp. high temp. circuit engine outlet

TAHHOAAD

B1

m




* located in the fuel pressure system

Sensor Measur.-point


Fitted Separate

Remarks

2229 Fresh water temp. low temp. circuit

TI A

2321 Oil ingress in fresh water cooler outlet

QAH OA B Option

5101 Fuel oil pressure engine inlet

PAL OA B Not provided with HFO Starting stand-by pump from pump control

5102 Fuel oil pressure engine inlet

PAL OA A

5105 Fuel oil pressure pressure pump

PAL OA B* Starting stand-by pump from pump control

5111 Fuel oil differential pressure before and after filter

PDAH OA B1

5112 Fuel oil differential pressure before and after autom. filter

PDAH OA B*

5115 Fuel oil differential pressure circulating pump

PDAL OA B* Starting stand-by pump from pump control

5116 Fuel oil differential pressure before and after circulating pump

PDAL OA B*

5201 Fuel oil temperature engine inlet

TAL OA A1 1 Sensor f. 5201+5202

5202 Fuel oil temperature engine inlet

TAH OA A 1 Sensor f. 5201+5202

5251 Fuel oil viscosity engine inlet

VAH OA A* 1 Sensor f. 5251, 5252 + (5253 DICARE if available)

5252 Fuel oil viscosity engine inlet

VAL OA A* 1 Sensor f. 5251, 5252 + (5253 DICARE if available)

5301 Level of leak fuel LAH OA B1

5333 Fuel level mixing tank LAL OA B*

6101 Starting air pressure engine inlet

PAL OA A1

6105 Shut down air pressure on engine

PAL OA B1

7201 Charge air temperature engine inlet

TAH OA A

m

85M 25 C Propulsion



SensorMeasur.-point


Fitted Separate

Remarks

7301 Water in charge air manifold QAH OA B

8211 Exhaust gas temp. deviation from average each cylinder

TAHTAHH

OAAD

A

8221 Exhaust temperature after turbocharger

TAHTAHH

OAAD

A1

8231 Exhaust temperature before turbocharger

TAHTAHH

OA A1

9401 Engine speed S B1 Alarm suppression

9402 Engine speed S B1 Start/stop luboil stand-by pump

9403 Engine speed n < 0,7 n nom

S B1 Alarm suppression

9404 Engine overspeed S OAMS

B1

9411 Engine speed S B Start/stop of luboil gear box stand-by pump from pump control

9419 Engine speed NI A1

9531 Load/>=Engine limit curve speed governor

GI B1 Overload indication (CP-propeller)

9532 Load/>=Engine limit curve speed governor

GI A1 Load control (CP-propeller)

9561 Barring gear engaged S B1 Start interlock

9601 Electronic units/terminal point X1/voltage failure

S OA B1

9611 RPM switch/voltage failure/ wire break

S OA B1

9615 Failure electronic governor S OA B only with electronic governor

9616 Failure electronic governor S OAMS

B only with electronic governor

9622 Exhaust gas temp. average equipment, voltage failure

S OA B1

9631 Crankcase oil mist detector voltage, lens/lamp

QA OA B If provided

9671 Safety system failure OA B1

9717 Electrical start/stop equipment/voltage failure

OA B1

m




SensorMeasur.-point


Fitted Separate

Remarks

9751 Temperature controller voltage failure

OA B1 Dependent from system

9761 Viscosity control, voltage failure

OA B Dependent from system

9771 Freshwater preheater, voltage failure


9775 Fuel oil preheater, voltage failure


Abbreviations

1 = Min. requirements for inland vessel MDO OA = Visual and audible alarmB = Binary sensor AD = Autom. speed/load reductionA = Analogue sensor MS = Autom. engine stopGI = Position indication QA = Measurement alarmLAH = Level alarm high QAH = Measurement alarm highLAL = Level alarm low S = SpeedNI = Speed indication TAH = Temperature alarm highP = Pressure TAHH = Temperature alarm high highPAL = Pressure alarm low TAL = Temperature alarm lowPALL = Pressure alarm low low TI = Temperature indicationPDAH = Pressure difference alarm high VAH = Viscosity alarm highPDAL = Pressure difference alarm low VAL = Viscosity alarm lowPI = Pressure indication

Sensors for DICARE see chapter 22

Option: Modbus connection to alarm system

m

87M 25 C Propulsion


Local and remote indicatorsRemote indication interfacing

* no

t Cat

erpi

llar M

otor

en s

uppl

y

mA

VΩ

mV

mA

V

Sens

or S

igna

ls fr

om th

een

gine

RPM

sw

itch

unit

Anal

og-m

onito

ring

equi

pmen

t *

Disp

lay

(mA)

Rem

ote

indi

cato

rop

tion

Turb

ocha

rger

spee

dop

tion

Rem

ote

indi

cato

ren

gine

spe

edop

tion

Mon

itor

*

Sign

al ty

pe4-

20 m

A

0 - 10 V

0 - 10 V

Indi

cato

rs

DIC

AR

E "O

FF"

Line

A

t the

eng

ine

Rem

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96 x

96

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Protection system Version = unattended engine room seagoing vessel

Operating voltage: 24 V DCType of protection: IP 55 for wall-mounting type housing

IP 20 for 19" subrack type

Protection against false polarity and transient protection provided.

Designed for: 6 starting interlock inputs6 automatic stop inputs4 automatic reduction inputs4 manual stop inputs

The input and output devices are monitored for wire break.

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89M 25 C Propulsion

21. Control and monitoring systemProtection system

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Rpm switch system Operating voltage: 24 V DCType of protection:IP 55 for wall-mounting type housingIP 20 for 19" subrack type

Designed for:8 rpm switching pointsAnalogue outputs for speed:2 x 0-10 V, 2 x 4-20 mA, 2 x frequencyAnalogue outputs for fuel rack position:0 - 10 V, 2 x 4-20 mA plus 2 binary outputs

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91M 25 C Propulsion

21. Control and monitoring systemRpm switch system

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22. Diagnostic system DICARE

DICARE is an efficient expert system which collects permanently the actual operating data of the en-gine, scales them to ISO condition, compares them with the nominal values and evaluates all detecteddeviations from these nominal values. Out of this comparison a printable diagnosis results which easecondition based maintenace considerably.

The sensor equipment of the engine laid out for the "on-line operation" with analogue transmitters viaa data converter feeds the PC with measured data on-line for evaluation and storing. Due to the auto-matically established history files trends can be made visible.

Benefits of DICARE:

• Early detection of wear.• Optimum operating condition due to clearly laid out display of deviating engines parameters.• Reduction of maintenance cost due to recognition of trends.• Longer service life of components due to display of comparison of actual vs. desired values.• Information about the engine condition by means of remote access possibilities.• Allows personnel and material planning by early, condition-based recognition of contamination or

wear.

Option:Installed in junction box

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93M 25 C Propulsion

22. Diagnostic system DICARE

Transmitter for DICARE ON-LINE M 25 C

= Transmitter from engine monitoring

LocationL = SeparateM = EngineDS = RPM switch system

Designation Transmitter Signal Meas. point no. CM

Location

Fuel viscosity 4 - 20 mA 5253 L

Fuel temperature after viscomat PT 100 5206 L

Fuel temperature at engine inlet PT 100 5201 M

Injection pump rack position 4 - 20 mA 9509 DS

Lube oil pressure 4 - 20 mA 1105 M

Lube oil temperature at engine inlet PT 100 1202 M

Freshwater pressure HT 4 - 20 mA 2102 M

Freshwater temperature at engine inlet HT PT 100 2201 M

Freshwater temperature at engine outlet HT PT 100 2211 M

Differential pressure charge air cooler 4 - 20 mA 7307 M

Intake air pressure 4 - 20 mA 6181 M

Intake air temperature before turbocharger PT 100 7206 M

Charge air pressure after intercooler 4 - 20 mA 7109 M

Charge air temperature before intercooler NiCrNi mV 7309 M

Charge air temperature at engine inlet PT 100 7201 M

Exhaust gas temperature for each cylinder and after turbocharger

NiCrNi mV 8211/8221 M

Exhaust gas temperature before turbocharger NiCrNi mV 8231 M

Engine speed 4 - 20 mA 9419 DS

Turbocharger speed 4 - 20 mA 9429 M

Service hour counter (manual input) Counter binary 9409 DS

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23. Diesel engine management system DIMOS

DIMOS is a computer aided maintenance and spare part management system for Caterpillar Motorendiesel engines. The DIMOS-system will include a data base which is filled with information derivedfrom the operating instructions and the spares catalogue of your respective engine type. This systemenables to administration and check the following four major subjects:1. Maintenance2. Material management3. Statistics4. Budget control.

These four major subjects are provided with many internal connections, so that no double inputs arerequired. All you need for running the DIMOS-system is commercial PC hardware.

The advantages are evident:• Precise follow-up regarding the maintenance intervals as specified by Caterpillar Motoren. No

scheduled date will be forgotten and no history file will be missed.• Immediate access to maintenance and component information.• Quick and simple modification of data is possible at any time.• Extensive and permanently up-to-date decision documents for maintenance with precise updating

of terms.• A lot of paper work can be omitted, and this means a considerable saving of time.• This can be taken from the DIMOS databank as well as from the CD-Rom and the standard docu-

mentation.From various single information to an integrated system

DIMOS

Engine operatinginstructions

Engine spare partscatalogues

Maintenanceschedule

Maintenancejob cards

Maintenanceplanning

Work ordercreation

History andstatistics

Inventory andpurchase

O U T P U T

I N P U TDIMOS

Engine operatinginstructions

Engine spare partscatalogues

Maintenanceschedule

Maintenancejob cards

Maintenanceplanning

Work ordercreation

History andstatistics

Inventory andpurchase

O U T P U T

I N P U T

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95M 25 C Propulsion

24. Standard acceptance test run

In addition to that the following functional tests will be carried out:

- governor test- overspeed test- emergency shut-down via minimum oil pressure- start/stop via central engine control- starting trials up to a minimum air pressure of 10 bar- measurement of crank web deflection (cold/warm condition)

After the acceptance main running gear, camshaft drive and timing gear train will be inspectedthrough the opened covers. Individual inspection of special engine components such as piston orbearings is not intended, because such inspections are carried out by the classification societies atintervals on series engines.

Engine movement due to vibration referred to the global vibration characteristics of the engine:

The basis for assessing vibration severity are the guidelines ISO 10816-6.

According to these guidline the MaK engine will be assigned to vibration severity grade 28, class 5. Onthe engine block the following values will not be exceeded:

Displacement Seff < 0,448 mm f > 2 Hz < 10 HzVibration velocity Veff < 28,2 mm/s f > 10 Hz < 250 HzVibration acceleration aeff < 44,2 m/s2 f > 250 Hz < 1000 Hz

The acceptance test run is carried out on the testbed with customary equipment and auxiliaries usingexclusively MDO and under the respective ambient conditions of the testbed. During this test run thefuel rack will be blocked at the contractual output value. In case of deviations from the contractualambient conditions the fuel consumption will be converted to standard reference conditions.

The engine will be run at the following load stages acc. to the rules of the classification societies. Afterreaching steady state condition of pressures and temperatures these will be recorded and registeredacc. to the form sheet of the acceptance test certificate:

Load [%] Duration [min]

50 30

85 30

100 60

110 30

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25. Engine International Air Pollution Prevention Certificate

The MARPOL Diplomatic Conference has agreed about a limitation of NOx emissions, referred to asAnnex VI to Marpol 73/78.

When testing the engine for NOx emissions, the reference fuel is Marine Diesel Oil (Distillate) and thetest is performed according to ISO 8178 test cycles:

Subsequently, the NOx value has to be calculated using different weighting factors for different loadsthat have been corrected to ISO 8178 conditions.

An EIAPP (Engine International Air Pollution Prevention) certificate will be issued for each engineshowing that the engine complies with the regulation. At the time of writing, only an interimcertificate can be issued due to the regulation not yet in force.

According to the IMO regulations, a Technical File shall be made for each engine. This Technical Filecontains information about the components affecting NOx emissions, and each critical component ismarked with a special IMO number. Such critical components are injection nozzle, injection pump,camshaft, cylinder head, piston, connecting rod, charge air cooler and turbocharger. The allowablesetting values and parameters for running the engine are also specified in the Technical File.

The marked components can later, on-board the ship, be easily identified by the surveyor and thus anIAPP (International Air Pollution Prevention) certificate for the ship can be issued on basis of theEIAPP and the on-board inspection.

E2: Diesel-electric propulsion, controllable pitch propeller

Speed [%] 100 100 100 100

Power [%] 100 75 50 25

Weighting factor 0.2 0.5 0.15 0.15

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97M 25 C Propulsion

26. Painting/Preservation

Inside preservation

N 576-3.3Up to 1 year, engine protected from moisture.- Main running gear and internal mechanics

Outside preservation

N 576-3.1 - Tectyl lightEuropeStorage in the open, protected from moisture, up to 1 year

Appearance of the engine:- Castings with red oxide antirust paint- Pipes and machined surfaces left as bare metal- Attached components with colours of the makers

N 576-3.2 - Tectyl heavy-dutyOverseasStorage in the open, protected from moisture, up to 1 year

Appearance of the engine:- Castings with red oxide antirust paint- Pipes and machined surfaces left as bare metal- Attached components with colours of the makers

N 576-4.1 - Clear VarnishClear varnish painting is applicable within Europe for land transportation with protection frommoisture. It is furthermore applicable for storage in a dry and tempered atmosphere.

Clear varnish painting is not permissible for:- Sea transportation of engines- Storage of engines in the open, even if they are covered with tarpaulin

VCI packaging as per N 576-5.2 is always required!Durability and effectiveness are dependent on proper packing, transportation, and storage, i.e. theengine must be protected from moisture, the VCI foil must not be torn or destroyed.Checks are to be carried out at regular intervals.If the above requirements are not met, all warranty claims in connection with corrosion damagesshall be excluded.

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26. Painting/Preservation

Appearance of the engine:- Castings with red oxide antirust paint- Pipes and machined surfaces left as bare metal- Attached components with colours of the makers- Surfaces sealed with clear varnish- Bare metal surfaces with light preservation

N 576-4.3 - Painting- No VCI packaging:

Short-term storage in the open, protected from moisture, max. 4 weeks- With VCI packaging:

Storage in the open, protected from moisture, up to 1 year

Appearance of the engine:- Surfaces mostly painted with varnish- Bare metal surfaces provided with light or heavy-duty preservation

N 576-5.2 - VCI packagingStorage in the open, protected from moisture, up to 1 year.Applies for engines with painting as per application groups N 576-4.1 to -4.4Does not apply for engines with Tectyl outside preservation as per application groups N 576-3.1 and -3.2.

Description:- Engine completely wrapped in VCI air cushion foil, with inserted VCI-impregnated flexible

PU-foam mats.

N 576-5.2 Suppl. 1 - Information panel for VCI preservation and inspectionApplies for all engines with VCI packaging as per application group N 576-5.2

Description:- This panel provides information on the kind of initial preservation and instructions for inspection.- Arranged on the transport frame on each side so as to be easily visible.

N 576-6.1 - Corrosion Protection Period, Check, and RepreservationApplies to all engines with inside and outside storage

Description:- Definitions of corrosion protection period, check, and represervation

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99M 25 C Propulsion

27. Lifting of engines

For the purpose of transport the engine is equipped with a lifting device which shall remain the prop-erty of Caterpillar Motoren. It has to be returned in a useable condition free of charge.

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28. Engine parts

Cylinder head, Weight 240 kg

Connecting rod, Weight 79 kg Piston, Weight 46 kg

Cylinder liner, Weight 162 kg

Subject to change without notice.Leaflet No. 229 · 07.08 · e · L+S · VM3

© 2008 Caterpillar All Rights Reserved. CAT, CATERPILLAR, their respective logos,„Caterpillar Yellow“ and the POWER EDGE trade dress, as well as corporate identityused herein, are trademarks of Caterpillar and may not be used without permission

Europe, Africa, Middle East

Caterpillar MarinePower SystemsNeumühlen 922763 Hamburg/Germany

Phone: +49 40 2380-3000Telefax: +49 40 2380-3535

Caterpillar Marine Asia Pacific Pte Ltd14 Tractor RoadSingapore 627973/SingaporePhone: +65 68287-600Telefax: +65 68287-624

Americas

MaK Americas Inc.

3450 Executive WayMiramar Park of CommerceMiramar, FL. 33025/USAPhone: +1 954 447 71 00Telefax: +1 954 447 71 15

Caterpillar Marine Trading(Shanghai) Co., Ltd.25/F, Caterpillar Marine Center1319, Yan’an West Road200050 Shanghai/P. R.ChinaPhone: +86 21 6226 2200Telefax: +86 21 6226 4500

Asia PacificHeadquarters

Caterpillar MarinePower SystemsNeumühlen 922763 Hamburg/Germany

Phone: +49 40 2380-3000Telefax: +49 40 2380-3535

For more information please visit our website:www.cat-marine.com or www.mak-global.com

Caterpillar Marine Power Systems

Documents

M25C - Barloworld STET – Distribuidor Caterpillar em ... · PDF fileM25C Project Guide • Propulsion. m M 25 C Propulsion Introduction Caterpillar Motoren GmbH & Co. KG P. O. Box,