TAG1A TAG2A. Series kwm 1500 rpm kwm 1500 rpm ElectropaK. Basic technical data.

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1 TAG1A kwm 1500 rpm TAG2A kwm 1500 rpm ElectropaK 4000 Series Basic technical data Number of cylinders Cylinder arrangement Vee Cycle stroke, compression ignition Induction system Turbocharged Compression ratio :1 nominal Bore mm Stroke mm Cubic capacity litres Direction of rotation anti-clockwise viewed on flywheel Firing order A, 6 B, 5 A, 2 B, 3 A, 4 B, 6 A, 1 B, 2 A, 5 B, 4 A, 3 B Cylinder furthest from flywheel Note: Cylinders designated A are on the right hand side of the engine when viewed from the flywheel end Weight of ElectropaK Temperate Dry kg Wet + fuel cooler kg Wet - fuel cooler kg Tropical Dry kg Wet + fuel cooler kg Wet - fuel cooler kg Overall dimensions of Electropak Temperate Length mm Width mm Height mm Tropical Length mm Width mm Height mm Moment of inertia Engine kgm² Flywheel kgm² Cyclic irregularity, engine/flywheel Prime power TAG1A TAG2A Ratings Steady state speed stability at constant load ± 0.25% Electrical rating are based on average alternator efficiency and are for guidance only (0.8 power factor being used). Operating point Engine speed rpm Static injection timing See engine number plate Cooling water exit temperature < 98 C Fuel data To conform to BS2869 class A2 or BS EN590. Performance Sound pressure level 1500 rpm / 109 db(a) Note: All data based on operation to ISO 3046 / 1, BS 5514 and DIN 6271 standard reference conditions. For engines operating in ambient conditions other than the standard reference conditions stated below a suitable de-rate must be applied. De-rate tables for increased ambient temperature and/ or altitude are available, please contact Perkins Applications Department. Test conditions Air temperature C Barometric pressure kpa Relative humidity % Air inlet restriction at maximum power (nominal) kpa Exhaust back pressure (nominal) kpa Fuel temperature (inlet pump) C maximum ctm/sp.1500/ Limited, Peterborough. PE1 5NA. United Kingdom. Tel: +44 (0) Fax: +44 (0)

2 General installation TAG1A - Temperate TAG1A - Tropical Designation Units Baseload power Prime Power Standby power Gross engine power kwb Fan power kwm 42 Net engine power kwm BMEP gross bar Combustion air flow m³/min Exhaust gas temperature, after turbo C Exhaust gas flow (max) at atmospheric pressure m³/min 280 Boost pressure ratio Mechanical efficiency % Overall thermal efficiency % Friction power and pumping losses kwm 120 Mean piston speed m/s 9.5 Engine coolant flow (minimum) l/s 17 Typical Genset electrical output 0.8pf 25 C (100 kpa) kva kwe Assumed alternator efficiency % 95 Designation Units Baseload power Prime Power Standby power Gross engine power kwb Fan power kwm 64 Net engine power kwm BMEP gross bar Combustion air flow m³/min Exhaust gas temperature, after turbo C Exhaust gas flow (max) at atmospheric pressure m³/min 280 Boost pressure ratio Mechanical efficiency % Overall thermal efficiency % Friction power and pumping losses kwm 120 Mean piston speed m/s 9.5 Engine coolant flow (minimum) l/s 17 Typical Genset electrical output 0.8pf 25 C (100 kpa) kva kwe Assumed alternator efficiency % 95

3 TAG2A - Temperate TAG2A - Tropical Note: Not to be used for CHP design purposes. (Indicative figures only). Consult Perkins Engines Company Limited. Assumes complete combustion. Rating definitions Designation Units Baseload power Prime Power Standby power Gross engine power kwb Fan power kwm 42 Net engine power kwm BMEP gross bar Combustion air flow m³/min Exhaust gas temperature, after turbo C Exhaust gas flow (max) at atmospheric pressure m³/min 320 Boost pressure ratio Mechanical efficiency % Overall thermal efficiency % Friction power and pumping losses kwm 120 Mean piston speed m/s 9.5 Engine coolant flow (minimum) l/s 17 Typical Genset electrical output 0.8pf 25 C (100 kpa) kva kwe Assumed alternator efficiency % 95 Designation Units Baseload power Prime Power Standby power Gross engine power kwb Fan power kwm 64 Net engine power kwm BMEP gross bar Combustion air flow m³/min Exhaust gas temperature, after turbo C Exhaust gas flow (max) at atmospheric pressure m³/min 320 Boost pressure ratio Mechanical efficiency % Overall thermal efficiency % Friction power and pumping losses kwm 120 Mean piston speed m/s 9.5 Engine coolant flow (minimum) l/s 17 Typical Genset electrical output 0.8pf 25 C (100 kpa) kva kwe Assumed alternator efficiency % 95 Baseload power Unlimited hours usage with an average load factor of 100% of the published Baseload Power. No overload is permitted on Baseload Power. Prime power Unlimited hours usage with an average load factor of 80% of the published Prime Power over each 24 hours period. A 10% overload is available for 1 hour in every 12 hours operation. Standby power Limited to 500 hours annual usage with an average load factor of 80% 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. Emissions capability All TAG ratings are optimised to the best fuel consumption and do not comply to Harmonised International Regulation Emission Limits. More information on these statements can be obtained by contacting the Applications Department at Perkins Engines Company Limited.

4 Energy balance Note: Not to be used for CHP design purposes. (Indicative figures only). Consult Perkins Engines Company Limited. Assumes complete combustion TAG1A - Temperate TAG1A - Tropical TAG2A - Temperate TAG2A - Tropical Designation Units Baseload power Prime power Standby power Energy in fuel kw Energy in power output (gross) kw Energy to cooling fan kw 42 Energy in power output (nett) kw Energy to exhaust kw Energy to coolant and oil kw Energy to radiation kw Energy to charge coolers kw Designation Units Baseload power Prime power Standby power Energy in fuel kw Energy in power output (gross) kw Energy to cooling fan kw 64 Energy in power output (nett) kw Energy to exhaust kw Energy to coolant and oil kw Energy to radiation kw Energy to charge coolers kw Designation Units Baseload power Prime power Standby power Energy in fuel kw Energy in power output (gross) kw Energy to cooling fan kw 42 Energy in power output (nett) kw Energy to exhaust kw Energy to coolant and oil kw Energy to radiation kw Energy to charge coolers kw Designation Units Baseload power Prime power Standby power Energy in fuel kw Energy in power output (gross) kw Energy to cooling fan kw 64 Energy in power output (nett) kw Energy to exhaust kw Energy to coolant and oil kw Energy to radiation kw Energy to charge coolers kw Note: Not to be used for combined heat and power (CHP) purposes (indicative figures only). If necessary, please consult the Applications Department, Perkins Engines Company Limited, Stafford.

5 Cooling system For details of recommended coolant specifications, refer to the Operation and Maintenance Manual for this engine model. Nominal jacket water pressure in crankcase kpa Maximum top tank temperature (standby) C Maximum static pressure head on pump m Total coolant capacity: Engine only litres ElectropaK (engine/radiator): Temperate litres Tropical litres Maximum permissible restriction to coolant pump flow kpa Thermostat operating range C Ambient cooling clearance (standby power) based on air temperature at fan 6 C above ambient. Temperature rise across the engines (standby power) with inhibited coolant C Coolant temperature shutdown switch setting C rising Coolant immersion heater capacity (2 off) kwe each Radiator temperate Radiator face area m² Material and number of rows: -charge air and water jacket Copper, 4 rows Fins per inch and material: -charge air and water jacket Brass, 12 rows Width of matrix m Height of matrix m Weight of radiator kg Pressure cap setting (min) kpa Radiator tropical Radiator face area m² Material and number of rows: -charge air and water jacket Copper, 4 rows Fins per inch and material: -charge air and water jacket Brass, 12 rows Width of matrix m Height of matrix m Weight of radiator kg Pressure cap setting (min) kpa Water jacket cooling data Temperate and Tropical Coolant exit temperature (max) C Coolant inlet temperature (min) Thermostatic control Coolant inlet temperature (max) C Coolant pump Speed x e rev/min Method of drive Gear Fan Type Axial flow Diameter Temperate mm Tropical mm Number of blades Material Aluminium Drive ratio :1 Maximum additional restriction (duct allowance) to cooling airflow (Stand-by power applications) and resultant minimum airflow TAG1A - Temperate TAG1A - Tropical TAG2A - Temperate TAG2A - Tropical Ambient clearance 50% glycol Duct allowance (Pa) Min airflow m³/sec 35 C C C C Lubrication system Recommended SAE viscosity: A multigrade oil conforming to the following must be used: API CH4 15W/40. Note: For additional notes on lubricating oil specifications, please refer to the Operation and Maintenance Manual (OMM). Lubricating oil capacity Total system capacity litres Sump maximum litres Sump minimum litres Oil temperature at normal operating conditions to bearings 105 C Lubricating oil pressure At rated speed kpa Minimum at 80 C kpa Oil relief values open kpa Oil filter spacing microns Sump drain plug tapping size g1 Oil pump speed rpm Method of drive Gear Shutdown switch pressure setting (where fitted) kpa falling Oil pump flow ,0 litres/sec Normal operating angles Front and rear Side tilt Oil consumption Prime power Units After running in (typically after 250 hours) g/kwhr 0,52 Oil flow rate from pump litres/sec 6 Induction system Maximum air intake restriction of engine Maximum air intake restriction of engine: -clean filter kpa -dirty filter kpa -air filter type Medium duty axial flow Exhaust system Maximum back pressure for total system Exhaust outlet size (internal) x 254 mm Table D flanges Exhaust outlet flange size x 254 mm Table D flanges Back pressure for total system at standby power kpa For recommended pipe sizes, please refer to the Installation Manual.

6 Fuel system Recommended fuel to conform to: BS Class A2 or BS EN590 Injection system direct Fuel injection pump and injector type combined unit injector Injector pressure MPa Lift pump type Tuthill TCH Delivery TAG1A/ TAG2A litres/hour Heat retained in fuel to tank kw Fuel inlet temperature to be less than C Delivery pressure kpa Maximum suction head at pump inlet m Maximum static pressure head..see installation manual for details Fuel filter spacing microns Governor type electronic Governing to ISO CLASS 3 and 4; ISO CLASS G2 Tolerance on fuel consumption % Note: All figures in the tables below are based on gross mechanical output, for fuel consumption based on electrical output of the generating set contact your OEM. Fuel consumption Ratings g/kw/hr litres/hr TAG1A, Temperate & Tropical Standby Prime Baseload % Prime % Prime TAG2A, Temperate & Tropical Standby Prime Baseload % Prime % Prime Electrical system Type Insulated return Alternator volts with integral regulator Alternator output amps, 28 volts at 20 C ambient Starter motor volts Starter motor type axial Starter motor power kw Number of teeth on flywheel Number of teeth on starter motor Minimum cranking speed (0 C) rpm Pull in current of starter motor -25 C max (1). 30 amps Hold in current of starter motor -25 C max (1)..9 amps Engine stop solenoid volts Hold-in current of stop solenoid amps (1) All leads rated to 10 amps minimum. Engine mounting Maximum static bending moment at rear face of block Nm Maximum additional load applied to flywheel due to all rotating components kg Centre of gravity Bare engine, dry Forward of the rear face of the cylinder block mm Above the crankshaft centre line mm ElectropaK, dry Forward of the rear face of the cylinder block mm Above the crankshaft centre line mm Cold start recommendations Temperature range down to -10 C (14 F) Oil W/40 CH4 Starter x 24V Battery x 12 volts x 286 Ah Max breakaway current amps Cranking current amps Aids Block heaters Min mean cranking speed rpm Battery capacity is defined by the 20 hour rate at 0 C The oil specification should be for the minimum ambient temperature as the oil will not be warmed by the immersion heater Breakaway current is dependant on battery capacity available. Cables should be capable of handling transient current which may be up to double the steady cranking current.

7 Typical load acceptance (cold) Engine type Prime power% Load kwe nett Initial load acceptance when engine reaches rated speed (15 seconds maximum after engine starts to crank) Transient frequency deviation % Frequency recovery time seconds 2nd load application immediately after engine has recovered to rated speed (5 seconds after initial load application) Prime power% Load kwe nett Transient frequency deviation % Frequency recovery time seconds TAG1A TAG2A The above figures were obtained under test conditions as follows: Engine block temperature C Ambient temperature C Governing mode Isochronous Alternator inertia kgm² Under frequency roll off (UFRO) point set to ,5 UFRO rate set to v/hz LAM on / off on All tests were conducted using an engine installed and serviced to Perkins Engines Company Limited recommendations. Applied load is a percentage of generator electrical output efficiency as published in the general installation section of this data sheet. The information given on this Technical Data Sheet is for standard engines, and for guidance only. For ratings other than those shown contact Perkins Engines Company Limited, Stafford.

8 Noise data Octave analysis performed at the position of maximum noise Fan RPM POWER 1/ 3 (1/ 1 bandwidth) octave analasis SITE POSN. DBA HZ DB AT POSN k k k k k 9 8 POSN. DBA HZ DB AT POSN k 10 6 Noise Levels The figures for total noise levels are typical for an engine running at Standby Power rating in a semi-reverberant environment and measured at a distance of one metre from the periphery of the engine. Total Noise Level Sound pressure level re: -20x10 Pa Ambient noise level 79 dba Octave analysis performed at the position of maximum noise k k k k 9 8 POSN. DBA HZ DB AT POSN k k k k k 9 8 AMBIENT NOISE 79.DBA

9 TAG1A / TAG2A Temperate - Left hand side view FUEL LEAK-OFF CON, NO FUEL COOLER FITTED. 73, OVERALL LENGTH A A FRONT FACE C/CASE FAN PULLEY 5 GROOVE FOR SPB & B SECTION BELTS TO BS3790:1995 FRONT GROOVE IN PULLEY 19 GROOVE CRS 533 LUB.OIL FILLER LUB.OIL DIPSTICK LUB.OIL PRESS CONN. CRANKCASE INSPECTION COVERS OIL COOLER DRAIN TAP LUB.OIL TEMP.CONN. REAR FACE C/CASE REAR FACE FLYWHEEL HSG LOW OIL PRESSURE SWITCH. FUEL LEAK-OFF CONNECTOR AIR FILTER INLET REAR LIFTING BRACKET ENGINE ONLY BOTH SIDES EXHAUST OUTLET ELBOW. SEE FLANGE DETAIL. SYSTEM PIPEWORK MUST BE ADEQUARTELY SUPPORTED TO ENSURE THAT NO LOAD IS EXERTED ON TURBOCHARGERS LUB.OIL COOLER

10 TAG1A / TAG2A Temperate - Front view FUEL COOLER CONN , PITCHES OF OVER MATRIX IN THERMOSTAT HOUSING THERMOSTAT HOUSING THERMOSTAT HOUSING ELECTRONIC ACTUATOR FUEL INLET CONNECTION 15 (OUTSIDE) STEEL PIPE. MAXIMUM FUEL LIFT 2.5 METRES WHEN FUEL TANK OUTLET IS LOWER THAN LIFT PUMP INLET A NON-RETURN VALVE MUST BE FITTED AT FUEL TANK. IF MAX FUEL LIFT FIGURE IS EXCEEDED CONSULT PERKINS TECHNICAL DEPT. FUEL FILTER/ WATER SEPERATOR TORSIONAL VIBRATION DAMPERS RADIATOR DRAIN PLUG G1/2 CONDENSATE DRAIN PLUG (WITH 3mm HOLE THRO) IN BOTTOM OF AIR TANK. 75 CLEARANCE REQUIRED TO REMOVE SUMP. RADIATOR FILLER 0.7 BAR RELIEF VALVE 18 SLOTS 19 WIDE x 19 HIGH (FOR DUCTING PURPOSES) FUEL LEAK-OFF CONN TO SUIT 15mm O/D PIPE. `BITE` TYPE NON RETURN VALVE SUPLIED (NO FUEL COOLER) 20 HOLE FRONT LIFTING BRACKET (ENGINE ONLY).

11 TAG1A / TAG2A Temperate - Right hand side view AIR FILTER A A LUB OIL FILTERS 3 EACH SIDE FRONT LIFTING BRACKET 36 LEAK OFF CONNECTION NO FUEL COOLER FITTED FUEL INLET CONNECTION C OF G WET WITH FUEL COOLER 1911 C OF G WET NO FUEL COOLER CRANKCASE BREATHER SUPPLIED WITH FLEXIBLE PIPE 51 INSIDE x 865 LG FRONT FACE C/CASE EXHAUST GAS HIGH TEMP PROTECTION MODULE DUAL 24V STARTERS STARTER RELAY LUB.OIL PRESS CONN. ELECTRONIC CONTROL UNIT FOR ACTUATOR FUEL HAND PRIMING PUMP FUEL LIFT PUMP LUB. OIL TEMP.CONN. H.W.PROTECTION SWITCH G 3/4 FUEL COOLER CONNECTIONS 24 V ALTERNATOR LUB.OIL PUMP G 3/4 FUEL COOLER CONNECTIONS RADIATOR LIFTING HOLES RADIATOR WATER LEVEL SWITCH AIR FLOW

12 TAG1A / TAG2A Temperate - Rear view B BANK AIR FILTER ,3 ENGINE FEET 25 A 1775 OVERALL WIDTH ,25 A BANK OVERALL HEIGHT AIR FILTER RESTRICTION INDICATOR.. 24V AIR SHUT-OFF VALVE ENERGISED TO CLOSE. 16 HOLES M12 x 21 DEEP EQUALLY SPACED AS SHOWN 6 HOLES M16 x 30 DEEP EQUALLY SPACED ON 543 (33.5) PC ROTATION SUMP DRAIN PLUG REAR LIFTING BRACKET CLEARANCE REQUIRED TO REMOVE FUEL FILTER

13 TAG1A / TAG2A Temperate - Plan view of support pads, exhaust outlet flange and flywheel 22,5 8 HOLES 22 EQUALLY SPACED ON 356 PC , ,5 787, , DETAIL OF EXHAUST OUTLET FLANGE (B.S.10 TABLE D) SCALE 1:5 DETAIL OF SAE 518 FLYWHEEL AND SAE 00 FLYWHEEL HOUSING (METRIC TAPPINGS) SCALE 1: ,7 70, REAR FACE FLYWHEEL HSG LC 8 HOLES 22 FRONT FACE C/CASE PLAN VIEW OF SUPPORT PADS 6-HOLES

14 TAG1A / TAG2A Tropical - Left hand side view PULLEY 5 GROOVE FOR SPB & B SECTION BELTS TO BS 3790 : 1995 FUEL LEAK-OFF CONNECTION. 19 PULLEY GROOVE CRS 3915 OVERALL LENGTH ,5 FUEL LEAK-OFF CONN. NO FUEL COOLER FITTED 2236 LUB.OIL FILLER LUB.OIL DIPSTICK (BOTH SIDES) REAR LIFTING BRACKET (ENGINE ONLY) 25 EXHAUST OUTLET ELBOW -SEE FLANGE DETAIL. SYSTEM PIPEWORK MUST BE ADEQUATELY SUPPORTED TO ENSURE THAT NO LOAD IS EXERTED ON TURBOCHARGERS CRANKCASE INSPECTION COVERS OIL COOLER DRAIN TAP LUB.OIL COOLER LUB.OIL TEMP CONNECTION FRONT FACE C/CASE REAR FACE C/CASE REAR FACE FLYWHEEL HSG. LOW OIL PRESSURE SWITCH FAN FRONT GROOVE IN PULLEY AIR FILTER INLET. LUB.OIL PRESS CONNECTION....

15 TAG1A / TAG2A Tropical - Front view 2160 CRS 2112 OVER MATRIX 522 FUEL COOLER CONNECTION RADIATOR FILLER 0.7 BAR RELIEF VALVE FUEL COOLER WHEN FITTED THERMOSTAT HOUSING. THERMOSTAT HOUSING. 14 SLOTS 19 WIDE x 11 HIGH (FOR DUCTING PURPOSES) THERMOSTAT HOUSING. ELECTRONIC ACTUATOR FUEL INLET CONNECTION 15 (OUTSIDE STEEL PIPE) MAXIMUM FUEL LIFT 2.5 METRES WHEN FUEL TANK OUTLET IS LOWER THAN LIFT PUMP INLET A NON RETURN VALVE MUST BE FITTED AT FUEL TANK. IF MAX FUEL FIGURE IS EXCEEDED CONSULT PERKINS TECHNICAL DEPT. FUEL LEAK -OFF CONNECTION TO SUIT 15mm O/D PIPE BITE TYPE-NON RETURN VALVE SUPPLIED - NO FUEL COOLER. 20 HOLE FRONT LIFTING BRACKET (ENGINE ONLY) PITCHES OF FUEL FILTER/WATER SEPARATOR 70 CLEARANCE REQUIRED TO REMOVE SUMP OVER MATRIX RADIATOR DRAIN TORSIONAL VIBRATION DAMPERS CONDENSAGE DRAIN PLUG WITH 3mm HOLE THRO.IN BOTTOM OF AIR TANK.

16 TAG1A / TAG2A Tropical - Right hand side view FRONT FACE C/CASE AIR FILTER EXHAUST GAS HIGH TEMP PROTECTION MODULE A DUAL 24V STARTERS LUB OIL FILTERS 3 EACH SIDE STARTER RELAY G1/4 TAPPING FOR LUB OIL PRESSURS CONECTION LUB-OIL TEMPERATURE CONNECTION FRONT LIFTING BRACKET. H.W.T PROTECTION SWITCH ELECTRONIC CONTROL UNIT FOR ACTUATOR FUEL HAND PRIMING PUMP CRANKCASE BREATHER SUPPLIED WITH FLEXIBLE PIPE 51 INSIDE x 865 LONG. G3/4 FUEL COOLER CONNECTIONS RADIATOR WATER LEVEL SWITCH. AIR FLOW V ALTERNATOR LUBE OIL PUMP FUEL LIFT PUMP 1854 CENTRE OF GRAVITY WET NO FUEL COOLER 1851 CENTRE OF GRAVITY WET WITH FUEL COOLER...

17 TAG1A / TAG2A Tropical - Rear view AIR FILTER RESTRICTION INDICATOR - 24V AIR SHUT-OFF VALVE ENERGISED TO CLOSE ,4 (ENGINE FEET) 6 HOLES M16 X 30 DEEP EQUALLY SPACED ON 16 HOLES M12 X 21 DEEP EQUALLY SPACED AS SHOWN ON , ,5 REAR LIFTING BRACKET 39 CLEARANCE REQUIRED TO REMOVE FUEL FILTER SUMP DRAIN PLUG OVERALL HEIGHT 646.

18 TAG1A / TAG2A Tropical - Plan view of support pads, exhaust outlet flange and flywheel 22, HOLES 22 EQUALLY SPACED ON 356 PC , , , ,40 DETAIL OF EXHAUST OUTLET FLANGE (B.S.10 TABLE D) SCALE 1:5 6.5 DETAIL OF SAE 518 FLYWHEEL AND SAE 00 FLYWHEEL HOUSING (METRIC TAPPINGS) SCALE 1: REAR FACE FLYWHEEL HSG 435 LC 8 HOLES 22 FRONT FACE C/CASE HOLES