10
Series 1 of 10 Publication No. TPD1919, April 2015. Copyright © 2015 Perkins Engines Company Limited, all rights reserved. No part of this document may be reproduced in any form or by any means, without prior written permission of Perkins Engines Company Limited. The information in this document is substantially correct at the time of printing and may be altered subsequently. Perkins Engines Company Limited Peterborough, PE1 5FQ, United Kingdom Tel: +44 (0)1733 583000 Fax: +44 (0)1733 582240 www.perkins.com 1106A-70TG1 155.8 kWm (Gross) @ 1800 rpm ElectropaK Basic technical data Number of cylinders 6 Cylinder arrangement In-line Cycle 4 stroke Induction system Turbocharged Combustion system Direct injection diesel Compression ratio 182:1 Bore 105 mm Stroke 135 mm Cubic capacity 701 litres Direction of rotation Anticlockwise when viewed from flywheel Firing order 1, 5, 3, 6, 2, 4 Estimated total weight (dry) 7387 kg Estimated total weight (wet) 7617 kg Overall dimensions, ElectropaK Height 1092 mm Length (air cleaner fitted) 1648 mm Width 760 mm Moments of inertia Engine rotational components 027 kgm² Flywheel 12 kgm² Centre of gravity, ElectropaK Forward from rear of block (wet) 426 mm Above crankshaft centre line (wet) 159 mm Offset to RHS of crankshaft centre line (wet) -14 mm Performance Speed variation at constant load ± 075% Cyclic irregularity at standby power 0028 All ratings within ± 5% Note: All data based on operation to ISO 3046-1:2002 standard reference conditions Sound level Average sound pressure level for prime power @ 1 m TBA dB(A) Test conditions Air temperature 25°C Barometric pressure 100 kPa Relative humidity 315% Air inlet restriction at maximum power 5 kPa (maximum) Exhaust back pressure at maximum power 6 kPa (maximum) Fuel temperature 40°C Note: If the engine is to operate in ambient conditions other than those of the test conditions, suitable adjustments must be made for these changes For full details, contact Perkins Technical Service Department 1100

1106A-70TG1 1100 - dinatek.ecdinatek.ec/wp-content/uploads/2016/07/FGV45-Ficha-técnica-Motor... · Maximum bending moment at rear of flywheel housing ..... .... .....

Embed Size (px)

Citation preview

Page 1: 1106A-70TG1 1100 - dinatek.ecdinatek.ec/wp-content/uploads/2016/07/FGV45-Ficha-técnica-Motor... · Maximum bending moment at rear of flywheel housing ..... .... .....

Series

1 of 10

Publication No. TPD1919, April 2015.

Copyright © 2015 Perkins Engines Company Limited, all rights reserved. No part of this document may be reproduced in any form or by any means, without prior written permission of Perkins Engines Company Limited. The information in this document is substantially correct at the time of printing and may be altered subsequently.

Perkins Engines Company LimitedPeterborough, PE1 5FQ, United Kingdom Tel: +44 (0)1733 583000 Fax: +44 (0)1733 582240 www.perkins.com

1106A-70TG1155.8 kWm (Gross) @ 1800 rpm

ElectropaK

Basic technical dataNumber of cylinders.. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ....6Cylinder arrangement .... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .. In-lineCycle .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .... 4 strokeInduction system .... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... TurbochargedCombustion system ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .... Direct injection dieselCompression ratio .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ..18..2:1Bore .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....105 mmStroke ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....135 mmCubic capacity .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... 7..01 litresDirection of rotation .. ...... .... ...... ....Anticlockwise when viewed from flywheelFiring order ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ..1, 5, 3, 6, 2, 4Estimated total weight (dry) .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .. 738..7 kgEstimated total weight (wet) .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .. 761..7 kg

Overall dimensions, ElectropaKHeight .. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... 1092 mmLength (air cleaner fitted) ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... 1648 mmWidth .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....760 mm

Moments of inertiaEngine rotational components ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .. 0..27 kgm²

Flywheel .. .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ..1..2 kgm²

Centre of gravity, ElectropaKForward from rear of block (wet) .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....426 mmAbove crankshaft centre line (wet) ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....159 mmOffset to RHS of crankshaft centre line (wet)...... .... ...... .... ...... .... ...... .... ......-14 mm

PerformanceSpeed variation at constant load .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....± 0..75%Cyclic irregularity at standby power...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ....0..028All ratings within ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ± 5%

Note: All data based on operation to ISO 3046-1:2002 standard reference conditions..

Sound levelAverage sound pressure level for prime power @ 1 m .... .... ...... ..TBA dB(A)

Test conditionsAir temperature.. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... 25°CBarometric pressure ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....100 kPaRelative humidity .... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ..31..5%Air inlet restriction at maximum power.... ...... .... ...... .... ...... .... ..5 kPa (maximum)Exhaust back pressure at maximum power.. ...... .... ...... .... ..6 kPa (maximum)Fuel temperature .... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... 40°C

Note: If the engine is to operate in ambient conditions other than those of the test conditions, suitable adjustments must be made for these changes.. For full details, contact Perkins Technical Service Department..

1100

Page 2: 1106A-70TG1 1100 - dinatek.ecdinatek.ec/wp-content/uploads/2016/07/FGV45-Ficha-técnica-Motor... · Maximum bending moment at rear of flywheel housing ..... .... .....

2 of 10

Publication No. TPD1919, April 2015.

Copyright © 2015 Perkins Engines Company Limited, all rights reserved. No part of this document may be reproduced in any form or by any means, without prior written permission of Perkins Engines Company Limited. The information in this document is substantially correct at the time of printing and may be altered subsequently.

Perkins Engines Company LimitedPeterborough, PE1 5FQ, United Kingdom Tel: +44 (0)1733 583000 Fax: +44 (0)1733 582240 www.perkins.com

General installationGeneral installation Units Prime Standby

Gross engine power kW 140..5 155..4

Gross BMEP kPa 1336..2 1477..9

Mean piston speed metre/s 8..1

ElectropaK nett engine power kW 133..5 148..4

Engine coolant flow (against 35 kPa restriction) litres/min 170

Combustion air flow (at STP) m³/min 11..28 11..86

Exhaust gas flow (maximum) m³/min 27..83 29..72

Exhaust gas temperature (maximum) in manifold (after turbocharger) °C 526

Nett engine thermal efficiency % 37..9 38..4

Typical generator set electrical output (0..8pf 25°C)kWe 121..5 135

kVA 151..9 168..8

Regenerative power (estimated) kW 7..0

Assumed alternator efficiency % 91

Rating definitionsPrime powerUnlimited hours usage, with an average load factor of 80 percent over each 24 hour period.. A 10 percent overload is available for 1 hour in every 12 hours operation..

Standby powerLimited to 500 hours annual usage, with an average load factor of 80 percent of the published Standby power rating over each 24 hour period.. Up to 300 hours of annual usage may be run continuously.. No overload is permitted on Standby power..

Energy balance

Designation Units Prime Standby

Heat in fuel kW 352 386..8

Power to cooling fan kW 7..0

Power to coolant and lubricating oil kW 84..2 92..0

Power to exhaust kW 113..6 124..5

Power to radiation kW 13..7 14..9

Note: Not to be used for CHP design purposes (indicative figures only).. Consult Perkins Engines Company Limited.. Assumes complete combustion..

Page 3: 1106A-70TG1 1100 - dinatek.ecdinatek.ec/wp-content/uploads/2016/07/FGV45-Ficha-técnica-Motor... · Maximum bending moment at rear of flywheel housing ..... .... .....

3 of 10

Publication No. TPD1919, April 2015.

Copyright © 2015 Perkins Engines Company Limited, all rights reserved. No part of this document may be reproduced in any form or by any means, without prior written permission of Perkins Engines Company Limited. The information in this document is substantially correct at the time of printing and may be altered subsequently.

Perkins Engines Company LimitedPeterborough, PE1 5FQ, United Kingdom Tel: +44 (0)1733 583000 Fax: +44 (0)1733 582240 www.perkins.com

Cooling systemRadiatorOverall weight (wet) .. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... 35 kgFace area .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....464025 mm²Number of rows and materials ...... .... ...... .... ...... .... ...... .... ...... .... 2 rows, aluminiumMatrix density and material .. .... ...... .... ...... .... ...... ..12..7 fins per inch, aluminiumWidth of matrix .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ....672..5 mmHeight of matrix.. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....690 mmPressure cap setting (minimum) .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .... 110 kPa

FanDiameter .. .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ....558..8 mmDrive ratio .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ..1..25:1Number of blades.... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ....7Material...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ....NylonType.. .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... PusherAir flow, 1800 rpm @ 200 Pa air side restriction .. ...... .... ...... .... ...... 182 m3/minPower, 1800 rpm @ 200 Pa air side restriction .... ...... .... ...... .... ...... .... ...... 4..6 kW

CoolantTotal system capacity...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .... 21 litresSystem capacity ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ..10%Engine capacity ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .. 9..5 litresMaximum top tank temperature .. .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .. 110°CTemperature rise across engine (maximum rating dependent) .. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ..6°C - 12°CMaximum permissible external system resistance.. .... ...... .... ...... .... ...... 35 kPaThermostat operation range .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .. 82°C to 93°CShutdown switch setting .. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ..118°CCoolant pump method of drive ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... GearRecommended coolant immersion heater rating (minimum) .... ....0..75 kWRecommended coolant .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .. .... .... ...... .... ...... .... BS6580 - 1992, ASTM D3306 and ELC coolants to 1E1966

Duct allowanceMaximum additional restriction (duct allowance to cooling airflow and resultant minimum air flow) - standby power

Description rpm kPa m3/min

Duct allowance with inhibited coolant at 50°C

Minimum air flow 1800 0..120 252

Duct allowance with inhibited coolant at 46°C

Minimum air flow 1800 0..200 234

Electrical systemAlternator .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .... 8SIAlternator voltage.... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ......12 voltsAlternator output ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .. 65 ampsStarter.. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ..AZFStarter motor voltage ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ......12 voltsStarter motor power .. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... 4..2 kWNumber of teeth on the flywheel.. .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....126Pull-in and hold-in current of starter motor solenoid@ 25°C maximum (1) ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .. 68 amps at 12 voltshold-in current of starter motor solenoid@ 25°C maximum (1).. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .. 20 amps at 12 voltsEngine stop method.. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ..Solenoid1 All leads to rated at 10 amps minimum

Cold start recommendationsMinimum required cranking speed over TDC .... .... ...... .... ...... .... ...... .... ...... 60 rpm

5 to -10°C -10 to -20°C -20 to -25°C

Oil 15W40 10W40 5W40

Starter AZF

Battery 2x 1200 CCA

Cranking current 960

Aids None Glow plugs

Minimum mean cranking speed 130 rpm 100 rpm 100 rpm

Note: Battery capacity is defined by the 20 hour rate..

Note: If a change to a low viscosity oil is made, the cranking torque necessary at low ambient temperatures is much reduced.. The starting equipment has been selected to take advantage of this.. It is important to change to the appropriate multigrade oil in anticipation of operating in low ambient temperatures..

Exhaust systemMaximum back pressure - 1800 rpm.. .... ...... .... ...... .... ...... .... ...... .... ...... .... ......6..0 kPaExhaust outlet, internal diameter .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... 72 mm

Page 4: 1106A-70TG1 1100 - dinatek.ecdinatek.ec/wp-content/uploads/2016/07/FGV45-Ficha-técnica-Motor... · Maximum bending moment at rear of flywheel housing ..... .... .....

4 of 10

Publication No. TPD1919, April 2015.

Copyright © 2015 Perkins Engines Company Limited, all rights reserved. No part of this document may be reproduced in any form or by any means, without prior written permission of Perkins Engines Company Limited. The information in this document is substantially correct at the time of printing and may be altered subsequently.

Perkins Engines Company LimitedPeterborough, PE1 5FQ, United Kingdom Tel: +44 (0)1733 583000 Fax: +44 (0)1733 582240 www.perkins.com

Fuel systemInjection componentsInjector ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... Mechanical Fuel pump.... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ..DP310G

Fuel primingPriming pump type .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ......Manual Maximum priming time.. .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... 90 seconds

Fuel feedMaximum fuel flow .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ..3 litres/min Maximum suction head at engine fuel pump inlet...... .... ...... .... ...... .... ...... 50 kPa Maximum static pressure head .. .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... 50 kPa Fuel temperature at engine fuel pump inlet .. ...... .... ...... .... ...... .... ...... .... ...... .... 85°C Tolerance on fuel consumption .... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ± 5%

Fuel specificationFuel standard.. .... ...... .... ......Various (contact Perkins Technical Department)

Fuel consumption

LoadType of operation and application

g/kWh litres/hr

110% Prime power 209..7 38..8

Prime power 210..9 35..2

75% Prime power 210..8 26..5

50% Prime power 209..3 18..0

25% Prime power 243..1 10..5

Induction systemMaximum air intake restrictionClean filter .. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ....3 kPa Dirty filter.. .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ....5 kPa Air filter type...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ....Paper element

Lubrication systemMaximum total system oil capacity ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... 18..0 litres Minimum oil capacity in sump ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... 12..5 litres Maximum oil capacity in sump ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... 16..1 litres Maximum engine operating angles - Front up, front down, right side, left side...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .... 25° Sump drain plug tapping size.. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....3/4 - 16 UNF Shutdown switch setting (where fitted)

Lubricating oilRelief valve opening pressure ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....460 kPa Pressure at maximum speed .. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ....520 kPa Maximum continuous oil temperature (in rail).... .... ...... .... ...... .... ...... .... ...... ..125°C Oil consumption at full load (% of fuel) .. ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... < 0..1

Recommended SAE viscosityA multigrade oil must be used which conforms to API CH4 or CI4 ACEA E5 must be used, see illustration below:

Viscosity grade (Perkins)

Ambient Temperature Deg °C

-50 -40 -30 -20 -10 0 10 20 30 40 50 60

15W-40

10W-40

10W-30

5W-40

5W-30

0W-40

0W-30

MountingsMaximum static bending moment at rear face of block .... .... ...... .... ..1130 Nm Maximum permissible overhung load on the flywheel .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... .. Calculated on request Maximum bending moment at rear of flywheel housing.. .... ...... .... ...... .... ...... .... .. .... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... .... ...... ..± 3000 in shock Nm

Load acceptanceThe data below complies with the requirements of classification 3 and 4 of ISO 8528-12 and G2 operating limits stated in ISO 8528-5..

Initial load application: When engine reaches rated speed (15 seconds maximum after engine starts to crank)..

Description Units Cold Condition

% of Prime power % 100

Load kWe 121..5

Transient frequency deviation % < 10

Frequency recovery time Seconds 1..8

Page 5: 1106A-70TG1 1100 - dinatek.ecdinatek.ec/wp-content/uploads/2016/07/FGV45-Ficha-técnica-Motor... · Maximum bending moment at rear of flywheel housing ..... .... .....

5 of 10

Publication No. TPD1919, April 2015.

Copyright © 2015 Perkins Engines Company Limited, all rights reserved. No part of this document may be reproduced in any form or by any means, without prior written permission of Perkins Engines Company Limited. The information in this document is substantially correct at the time of printing and may be altered subsequently.

Perkins Engines Company LimitedPeterborough, PE1 5FQ, United Kingdom Tel: +44 (0)1733 583000 Fax: +44 (0)1733 582240 www.perkins.com

Noise dataNoise levels

Noise level dB(A)

Position Prime power Standby

1 100..1 100..3

2 97..3 97..2

3 97..8 97..6

4 101..3 101..3

5 102..6 102..5

6 99..0 99..0

Engine AlternatorRadiator

45

6

12

3

¹/³ Octave analysis: TBC Engine AlternatorRadiator

45

6

12

3

Noise reference level 65 dB(A)

Page 6: 1106A-70TG1 1100 - dinatek.ecdinatek.ec/wp-content/uploads/2016/07/FGV45-Ficha-técnica-Motor... · Maximum bending moment at rear of flywheel housing ..... .... .....

6 of 10

Publication No. TPD1919, April 2015.

Copyright © 2015 Perkins Engines Company Limited, all rights reserved. No part of this document may be reproduced in any form or by any means, without prior written permission of Perkins Engines Company Limited. The information in this document is substantially correct at the time of printing and may be altered subsequently.

Perkins Engines Company LimitedPeterborough, PE1 5FQ, United Kingdom Tel: +44 (0)1733 583000 Fax: +44 (0)1733 582240 www.perkins.com

12

34

56

78

ACDEF

12

34

56

78

ABCDEF

B

1647

.9

98

263.

523

4.9

99.4

250.

4

361.

7

240.

9

525.

2

828.

7

511.

754

7.1

454.

345

7.7

195

528.

9

272.

6

755

791.

4

818.

7

1186

.8

1204

.8

274

499.

657

4.4

614

708.

2 O

IL F

ILLE

R

162

134.

1

701.

6 C

US

TOM

ER

MO

UN

TIN

G H

OLE

207.

6

67.9

FUE

L IN

27 L

IFTI

NG

EY

E

76.2

165.

1

55.6 10

3.2

22.2

284.

7

372.

7

341

19.2

156.

4

67.9

OIL

FIL

LER

1E27

22B

DR

AW

ING

1E

0198

PLE

TTE

RS

1E

0013

YC

ON

FID

EN

TIA

LITY

M A T L HT

TR

PA

RTS

LIS

TED

OP

TIO

NS

PR

_A85

04

PR

_B00

00

PR

_C00

01

PR

_D00

04

PR

_E04

21

PR

_EL0

01

PR

_F43

72

PR

_G01

01

PR

_H02

10

PR

_HD

000

PR

_J02

11

PR

_JD

001

PR

_K00

60

PR

_L00

56

PR

_M44

17

PR

_N05

10

PR

_NL0

01

PR

_Q11

00

PR

_R00

00

PR

_S11

14

PR

_SD

003

PR

_V00

02

PR

_VD

001

PR

_W00

00

PR

_X00

01

PR

_Y00

00

PR

_ZA

000

PR

_ZB

000

PR

_ZC

000

PR

_ZE

000

PR

_ZG

000

PR

_ZJ0

06

PR

_ZL0

02

PR

_ZM

025

PR

_ZN

000

PR

_ZV

051

PR

_ZY

402

PR

_ZZ0

00

GA

_P

P8

30

36

TH

IRD

AN

GLE

PR

OJE

CT

ION

SH

EE

T 1

O

F 5

DW

G C

ON

TR

OL W

169

TH

E I

NF

OR

MA

TIO

N H

ER

EO

N I

S T

HE

PR

OP

ER

TY

OF

CA

TE

RP

ILL

AR

IN

C.

AN

D/O

R I

TS

SU

BS

IDIA

RIE

S.

WIT

HO

UT

WR

ITT

EN

PE

RM

ISS

ION

, A

NY

CO

PY

ING

, T

RA

NS

MIT

TA

L T

O

OT

HE

RS

, A

ND

AN

Y U

SE

EX

CE

PT

TH

AT

FO

R W

HIC

H I

T I

S L

OA

NE

D,

IS P

RO

HIB

ITE

D

EN

GIN

E A

R_C

OM

PLE

TE

(1106A

-70T

G1 6

0H

Z)

GA

_P

P8

30

36

VE

RC

HG

ED

X00

N O T E

1E00

11IN

TPR

& T

OL

Cat

erpi

llar:

Con

fiden

tial Y

ello

w

PR

OD

.

OT

HE

RR

EC

OR

DS

UN

LE

SS

OT

HE

RW

ISE

SP

EC

IFIE

D D

IME

NS

ION

S A

RE

IN

mm

DIM

EN

SIO

NS

W/O

TO

L A

RE

BA

SIC

VE

RS

ION

TY

PE

PR

IMA

RY

XS

EC

ON

DA

RY

X

YY

SE

E R

ELE

VA

NT

ES

M F

OR

ALL

OTH

ER

DIM

EN

SIO

NS

X-X

CY

LIN

DE

R B

LOC

K R

EA

R F

AC

E(V

ER

TIC

AL-

SID

E V

IEW

S)

X2-

X2

CY

LIN

DE

R B

LOC

K R

EA

R F

AC

E(V

ER

TIC

AL-

SID

E V

IEW

S)-

STR

ES

SE

D

BLO

CK

6 C

YLI

ND

ER

110

0 S

ER

IES

AN

D D

ER

IVA

TIV

ES

ON

LYY

-Y C

RA

NK

SH

AFT

CE

NTR

E L

INE

(HO

RIZ

ON

TAL-

SID

E A

ND

EN

D V

IEW

S)

Z-Z

CR

AN

KS

HA

FT C

EN

TRE

LIN

E(V

ER

TIC

AL-

EN

D V

IEW

S)

W-W

CR

AN

KS

HA

FT C

EN

TRE

LIN

E-P

LAN

VIE

W O

NLY

Figu

re 1

- P

arts

Lis

ted

Opt

ions

Dra

win

g N

o.

Vie

wG

A_P

P83

036

LE

FT

XLU

B O

IL D

RA

IN P

LUG

ON

SU

MP

3/4

-16

70 O

IL F

ILLE

R C

AP

17 R

EM

OV

AL

17 R

EM

OV

AL

4-M

12X

1.75

X24

1106A-70TG1 - Left side view

Page 7: 1106A-70TG1 1100 - dinatek.ecdinatek.ec/wp-content/uploads/2016/07/FGV45-Ficha-técnica-Motor... · Maximum bending moment at rear of flywheel housing ..... .... .....

7 of 10

Publication No. TPD1919, April 2015.

Copyright © 2015 Perkins Engines Company Limited, all rights reserved. No part of this document may be reproduced in any form or by any means, without prior written permission of Perkins Engines Company Limited. The information in this document is substantially correct at the time of printing and may be altered subsequently.

Perkins Engines Company LimitedPeterborough, PE1 5FQ, United Kingdom Tel: +44 (0)1733 583000 Fax: +44 (0)1733 582240 www.perkins.com

1106A-70TG1 - Front view

12345678

A

C

D

E

F

12345678

A

B

C

D

E

F

B759.8

130LIFTING EYE

109LIFTING EYE

359.1 370

232 TO FRONT 21.0CUSTOMER MOUNTING HOLE

232 TO FRONT 21.0CUSTOMER MOUNTING HOLE

491.3REAR LIFTING EYE

491.3FRONT LIFTING EYE

751.8

828.7778.4

1092.3

1E2722B DRAWING 1E0198P LETTERS 1E0013Y CONFIDENTIALITY

MATL

HTTR

GA_PP83036

THIRD ANGLE

PROJECTION

SHEET 4 OF 5

DWG CONTROL W169

THE INFORMATION HEREON IS THE PROPERTY OF CATERPILLAR INC. AND/OR ITS

SUBSIDIARIES. WITHOUT WRITTEN PERMISSION, ANY COPYING, TRANSMITTAL TO

OTHERS, AND ANY USE EXCEPT THAT FOR WHICH IT IS LOANED, IS PROHIBITED

ENGINE AR_COMPLETE(1106A-70TG1 60HZ)

GA_PP83036VER CHG

EDX 00

NOTE

1E0011 INTPR & TOLCaterpillar: Confidential Yellow

PROD.

OTHER RECORDSUNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN mm

DIMENSIONS W/O TOL ARE BASIC

VERSION

TYPE

PRIMARY XSECONDARY

Z

Y Y

Figure 4 - Parts Listed OptionsDrawing No. ViewGA_PP83036 Front

Z

Page 8: 1106A-70TG1 1100 - dinatek.ecdinatek.ec/wp-content/uploads/2016/07/FGV45-Ficha-técnica-Motor... · Maximum bending moment at rear of flywheel housing ..... .... .....

8 of 10

Publication No. TPD1919, April 2015.

Copyright © 2015 Perkins Engines Company Limited, all rights reserved. No part of this document may be reproduced in any form or by any means, without prior written permission of Perkins Engines Company Limited. The information in this document is substantially correct at the time of printing and may be altered subsequently.

Perkins Engines Company LimitedPeterborough, PE1 5FQ, United Kingdom Tel: +44 (0)1733 583000 Fax: +44 (0)1733 582240 www.perkins.com

1106A-70TG1 - Right side view

12

34

56

78

ACDEF

12

34

56

78

ABCDEF

B

234.

9

786.

7

219.

1

691.

3745.

7786.

7

76.9

52.3

29

591

234.

925

0.4

573.

7

513.

1

205

179

269.

3

701.

6 C

US

TOM

ER

MO

UN

TIN

G H

OLE

560.

7

76.2

165.

1

55.6 10

3.2

437.

344

1.7

1E27

22B

DR

AW

ING

1E

0198

PLE

TTE

RS

1E

0013

YC

ON

FID

EN

TIA

LITY

M A T L HT

TR

GA

_P

P8

30

36

TH

IRD

AN

GL

E

PR

OJE

CT

ION

SH

EE

T 2

O

F 5

DW

G C

ON

TR

OL W

16

9

TH

E IN

FO

RM

AT

ION

HE

RE

ON

IS

TH

E P

RO

PE

RT

Y O

F C

AT

ER

PIL

LA

R IN

C. A

ND

/OR

IT

S

SU

BS

IDIA

RIE

S. W

ITH

OU

T W

RIT

TE

N P

ER

MIS

SIO

N, A

NY

CO

PY

ING

, T

RA

NS

MIT

TA

L T

O

OT

HE

RS

, A

ND

AN

Y U

SE

EX

CE

PT

TH

AT

FO

R W

HIC

H IT

IS

LO

AN

ED

, IS

PR

OH

IBIT

ED

EN

GIN

E A

R_

CO

MP

LE

TE

(11

06

A-7

0T

G1

60

HZ

)

GA

_P

P8

30

36

VE

RC

HG

ED

X0

0

N O T E

1E00

11IN

TPR

& T

OL

Cat

erpi

llar:

Con

fiden

tial Y

ello

w

PR

OD

.

OT

HE

RR

EC

OR

DS

UN

LE

SS

OT

HE

RW

ISE

SP

EC

IFIE

D D

IME

NS

ION

S A

RE

IN

mm

DIM

EN

SIO

NS

W/O

TO

L A

RE

BA

SIC

VE

RS

ION

TY

PE

PR

IMA

RY

XS

EC

ON

DA

RY

X X

YY

Figu

re 2

- P

arts

Lis

ted

Opt

ions

Dra

win

g N

o.

Vie

wG

A_P

P83

036

Rig

ht

LUB

OIL

DR

AIN

PLU

GO

N S

UM

P 3

/4-1

6

4-M

12 X

1.7

5 24

M10

X 1

.5

M6

X 1

GR

OU

ND

TE

RM

INA

L

M10

X 1

.5

2-21

MO

UN

TIN

G H

OLE

S

Page 9: 1106A-70TG1 1100 - dinatek.ecdinatek.ec/wp-content/uploads/2016/07/FGV45-Ficha-técnica-Motor... · Maximum bending moment at rear of flywheel housing ..... .... .....

9 of 10

Publication No. TPD1919, April 2015.

Copyright © 2015 Perkins Engines Company Limited, all rights reserved. No part of this document may be reproduced in any form or by any means, without prior written permission of Perkins Engines Company Limited. The information in this document is substantially correct at the time of printing and may be altered subsequently.

Perkins Engines Company LimitedPeterborough, PE1 5FQ, United Kingdom Tel: +44 (0)1733 583000 Fax: +44 (0)1733 582240 www.perkins.com

1106A-70TG1 - Rear view12345678

A

C

D

E

F

12345678

A

B

C

D

E

F

B

295.3

334

41.5

143.9 143.9

240.7

247.1

238.1 238.1

1E2722B DRAWING 1E0198P LETTERS 1E0013Y CONFIDENTIALITY

MATL

HTTR

GA_PP83036

THIRD ANGLE

PROJECTION

SHEET 3 OF 5

DWG CONTROL W169

THE INFORMATION HEREON IS THE PROPERTY OF CATERPILLAR INC. AND/OR ITS

SUBSIDIARIES. WITHOUT WRITTEN PERMISSION, ANY COPYING, TRANSMITTAL TO

OTHERS, AND ANY USE EXCEPT THAT FOR WHICH IT IS LOANED, IS PROHIBITED

ENGINE AR_COMPLETE(1106A-70TG1 60HZ)

GA_PP83036VER CHG

EDX 00

NOTE

1E0011 INTPR & TOLCaterpillar: Confidential Yellow

PROD.

OTHER RECORDSUNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN mm

DIMENSIONS W/O TOL ARE BASIC

VERSION

TYPE

PRIMARY XSECONDARY

Z

Z

Y Y

Figure 3 - Parts Listed OptionsDrawing No. ViewGA_PP83036 Rear

12-M10 X 1.5 X 20EQUISPACED ON428.6 P.C.D.

8-3/8-24 UNF X 25.4EQUISPACED ON295.3 P.C.D.

8-3/8-24 UNF X 25.4EQUISPACED ON333.4 P.C.D.

8-M8 X 1.25 X 14.3EQUISPACED ON203.2 P.C.D.

Page 10: 1106A-70TG1 1100 - dinatek.ecdinatek.ec/wp-content/uploads/2016/07/FGV45-Ficha-técnica-Motor... · Maximum bending moment at rear of flywheel housing ..... .... .....

10 of 10

Publication No. TPD1919, April 2015.

Copyright © 2015 Perkins Engines Company Limited, all rights reserved. No part of this document may be reproduced in any form or by any means, without prior written permission of Perkins Engines Company Limited. The information in this document is substantially correct at the time of printing and may be altered subsequently.

Perkins Engines Company LimitedPeterborough, PE1 5FQ, United Kingdom Tel: +44 (0)1733 583000 Fax: +44 (0)1733 582240 www.perkins.com

1106A-70TG1 - Plan view

12

34

56

78

ACDEF

12

34

56

78

ABCDEF

B

182.

654

7.9

EX

HA

US

T

119.

521

4.5

273

287.

2

235.

4

295.

624

8.6

41.5

50.3

405

341

1E27

22B

DR

AW

ING

1E

0198

PLE

TTE

RS

1E

0013

YC

ON

FID

EN

TIA

LITY

M A T L HT

TR

GA

_P

P83036

TH

IRD

AN

GLE

PR

OJE

CT

ION

SH

EE

T 5

O

F 5

DW

G C

ON

TR

OL W

169

TH

E I

NF

OR

MA

TIO

N H

ER

EO

N I

S T

HE

PR

OP

ER

TY

OF

CA

TE

RP

ILL

AR

IN

C.

AN

D/O

R I

TS

SU

BS

IDIA

RIE

S.

WIT

HO

UT

WR

ITT

EN

PE

RM

ISS

ION

, A

NY

CO

PY

ING

, T

RA

NS

MIT

TA

L T

O

OT

HE

RS

, A

ND

AN

Y U

SE

EX

CE

PT

TH

AT

FO

R W

HIC

H I

T I

S L

OA

NE

D,

IS P

RO

HIB

ITE

D

EN

GIN

E A

R_C

OM

PLE

TE

(1106A

-70T

G1 6

0H

Z)

GA

_P

P83036

VE

RC

HG

ED

X00

N O T E

1E00

11IN

TPR

& T

OL

Cat

erpi

llar:

Con

fiden

tial Y

ello

w

PR

OD

.

OT

HE

RR

EC

OR

DS

UN

LE

SS

OT

HE

RW

ISE

SP

EC

IFIE

D D

IME

NS

ION

S A

RE

IN

mm

DIM

EN

SIO

NS

W/O

TO

L A

RE

BA

SIC

VE

RS

ION

TY

PE

PR

IMA

RY

XS

EC

ON

DA

RY

X X

WW

Figu

re 5

- P

arts

Lis

ted

Opt

ions

Dra

win

g N

o.

Vie

wG

A_P

P83

036

Top

3-M

10 X

1.5

TH

RU

EQ

UIS

PA

CE

D O

N10

4.8

P.C

.D.