G-DRIVE

QST1Curve Number:

FR-5160 (2P/ 2L)FR-5162 (Air-to-Air)

Data shown above represent gross engine performance capabilities obtained and corrected in accordance with ISO-3046 conditions of 100 kPa (29.53 in Hg)barometric pressure [110 m (361 ft) altitude], 25 °C (77 °F) air inlet temperature, and relative humidity of 30% with No. 2 diesel or a fuel corresponding to ASTM D2.

See reverse side for application rating guidelines.The fuel consumption data is based on No. 2 diesel fuel weight at 0.85 kg/litre (7.1 lbs/U.S. gal).Power output curves are based on the engine operating with fuel system, water pump and lubricating oil pump; not included are battery charging alternator, fan, optional equipment and driven components.

TECHNICAL DATA DEPT. CERTIFIED WITHIN 5% CHIEF ENGINEER

CONVERSIONS: (litres = U.S. Gal x 3.785) (Engine kWm = BHP x 0.746) (U.S. Gal = litres x 0.2642) (Engine BHP = Engine kWm x 1.34)

Displacement : 30.48 litre (1860 in3 ) Bore : 140 mm (5.51 in) Stroke : 165 mm (6.50 in)No. of Cylinders : 12 Aspiration : Turbocharged and Low Temperature Aftercooled

CUMMINS ENGINE COMPANY, INC

Columbus, Indiana 47201

ENGINE PERFORMANCE CURVE

Date:

8May00Basic Engine Model:

QST30-G4

Engine Speed Standby Power Prime Power Continuous Power

RPM kWm BHP kWm BHP kWm BHP

1500 970 1300 880 1180 683 915

1800 1112 1490 1007 1350 832 1115

OUTPUT POWER FUEL CONSUMPTION

% kWm BHPkg/

kWm·hlb/

BHP·hlitre/hour

U.S. Gal/hour

STANDBY POWER

100 970 1300 0.196 0.323 224 59.1

PRIME POWER

100 880 1180 0.195 0.320 202 53.2

75 660 885 0.194 0.319 151 39.8

50 440 590 0.197 0.324 102 26.9

25 220 295 0.207 0.341 54 14.2

CONTINUOUS POWER

100 683 915 0.194 0.319 156 41.1

These guidelines have been formulated to ensure proper application of generator drive engines in A.C. generator set installations. Generator drive engines are not designed for and shall not be used in variable speed D.C. generator set applications.

STANDBY POWER RATINGApplicable for supplying emergency power for the duration of the utility power outage. No overload capability is available for this rating. Under no condition is an engine allowedto operate in parallel with the public utility at the Standby Power rating. This rating should be applied where reliable utility power is available. A Standby rated engine should be sized for a maximum of an 80% average load factor and 200 hours of operation per year. This includes less than 25 hours per year at the Standby Power rating. Standby ratings should never be applied except in true emergency power outages. Negotiated power outages contracted with a utility company are not considered an emergency.

PRIME POWER RATINGApplicable for supplying electric power in lieu of commercially purchased power. Prime Power applications must be in the form of one of the following two categories:

UNLIMITED TIME RUNNING PRIME POWER

Prime Power is available for an unlimited number of hours per year in a variable load application. Variable load should not exceed a 70% average of the Prime Power rating during any operating period of 250 hours. The total operating time at 100% Prime Power shall not exceed 500 hours per year. A 10% overload capability is available for a period of 1 hour within a 12-hour period of operation. Total operating time at the 10% overload power shall not exceed 25 hours per year.

LIMITED TIME RUNNING PRIME POWER

Limited Time Prime Power is available for a limited number of hours in a non-variable load application. It is intended for use in situations where power outages are contracted, such as in utility power curtailment. Engines may be operated in parallel to the public utility up to 750 hours per year at power levels never to exceed the Prime Power rating. The customer should be aware, however, that the life of any engine will be reduced by this constant high load operation. Any operation exceeding 750 hours per year at the Prime Power rating should use the Continuous Power rating.

CONTINUOUS POWER RATINGApplicable for supplying utility power at a constant 100% load for an unlimited number of hours per year. No overload capability is available for this rating.

Engine Performance Data @ 1500 RPM

Engine Critical Parts List:CPL: 2499 (2 Pump / 2 Loop)

CPL: 2548 (Air-to-AIr)

0.0

50.0

100.0

150.0

200.0

250.0

0 100 200 300 400 500 600 700 800 900 1000

Gross Engine Output - kWm

1500 RPM

Litre/hour

G-DRIVE

QST2

0

5

10

15

20

25

30

0 500 1000 1500 2000 2500 3000Altitude (m)

Ambient Temp. (°C / °F)

50 / 122

40 / 104

25 / 77

0

5

10

15

20

25

30

0 500 1000 1500 2000 2500 3000

Altitude (m)

Ambient Temp. (°C / °F)

50 / 12240 / 104

CONTINUOUS

QST30-G4 Derate Curves @ 1500 RPM CURVE NO: FR-5160 (2 Pump 2 loop)FR5162 (Air-to-AIr)

DATE: 8May00

Note: Derates shown are based on 15 in H20 air intake restriction and 2 in Hg exhaust back pressure.

Reference Standards:

BS-5514 and DIN-6271 standards are based on ISO-3046.

Operation At Elevated Altitude and Temperature:

For sustained operation above these conditions, derate an additional 9% per 500 m (1640 ft) and 15% per 10°C (18°F)

STANDBY / PRIME

Per

cen

t D

erat

e o

f R

ated

Po

wer

(%

)P

erce

nt

Der

ate

of

Rat

ed P

ow

er (

%)

G-DRIVE

QST3Curve Number:

FR-5160 (2P / 2L)FR-5162 (Air-to-Air)

Engine Speed Standby Power Prime Power Continuous Power

RPM kWm BHP kWm BHP kWm BHP

1500 970 1300 880 1180 683 915

1800 1112 1490 1007 1350 832 1115

Displacement : 30.48 litre (1860 in3 ) Bore : 140 mm (5.51 in) Stroke : 165 mm (6.50 in)No. of Cylinders : 12 Aspiration : Turbocharged and Low Temperature Aftercooled

CUMMINS ENGINE COMPANY, INC

Columbus, Indiana 47201

ENGINE PERFORMANCE CURVE

CONVERSIONS: (litres = U.S. Gal x 3.785) (kWm = BHP x 0.746) (U.S. Gal = litres x 0.2642) (BHP = kWm x 1.34)

Basic Engine Model:

QST30-G4

OUTPUT POWER FUEL CONSUMPTION

% kWm BHPkg/

kWm·hlb/

BHP·hlitre/hour

U.S. Gal/hour

STANDBY POWER

100 1112 1490 0.204 0.336 267 70.5

PRIME POWER

100 1007 1350 0.203 0.333 240 63.3

75 756 1013 0.199 0.327 177 46.7

50 504 675 0.202 0.331 119 31.5

25 252 338 0.223 0.366 66 17.4

CONTINUOUS POWER

100 832 1115 0.199 0.327 194 51.4

These guidelines have been formulated to ensure proper application of generator drive engines in A.C. generator set installations. Generator drive engines are not designed for and shall not be used in variable speed D.C. generator set applications.

STANDBY POWER RATINGApplicable for supplying emergency power for the duration of the utility power outage. No overload capability is available for this rating. Under no condition is an engine allowedto operate in parallel with the public utility at the Standby Power rating. This rating should be applied where reliable utility power is available. A Standby rated engine should be sized for a maximum of an 80% average load factor and 200 hours of operation per year. This includes less than 25 hours per year at the Standby Power rating. Standby ratings should never be applied except in true emergency power outages. Negotiated power outages contracted with a utility company are not considered an emergency.

PRIME POWER RATINGApplicable for supplying electric power in lieu of commercially purchased power. Prime Power applications must be in the form of one of the following two categories:

UNLIMITED TIME RUNNING PRIME POWER

Prime Power is available for an unlimited number of hours per year in a variable load application. Variable load should not exceed a 70% average of the Prime Power rating during any operating period of 250 hours. The total operating time at 100% Prime Power shall not exceed 500 hours per year. A 10% overload capability is available for a period of 1 hour within a 12-hour period of operation. Total operating time at the 10% overload power shall not exceed 25 hours per year.

LIMITED TIME RUNNING PRIME POWER

Limited Time Prime Power is available for a limited number of hours in a non-variable load application. It is intended for use in situations where power outages are contracted, such as in utility power curtailment. Engines may be operated in parallel to the public utility up to 750 hours per year at power levels never to exceed the Prime Power rating. The customer should be aware, however, that the life of any engine will be reduced by this constant high load operation. Any operation exceeding 750 hours per year at the Prime Power rating should use the Continuous Power rating.

CONTINUOUS POWER RATINGApplicable for supplying utility power at a constant 100% load for an unlimited number of hours per year. No overload capability is available for this rating.

Engine Performance Data @ 1800 RPM

Data shown above represent gross engine performance capabilities obtained and corrected in accordance with ISO-3046 conditions of 100 kPa (29.53 in Hg)barometric pressure [110 m (361 ft) altitude], 25 °C (77 °F) air inlet temperature, and relative humidity of 30% with No. 2 diesel or a fuel corresponding to ASTM D2.

See reverse side for application rating guidelines.The fuel consumption data is based on No. 2 diesel fuel weight at 0.85 kg/litre (7.1 lbs/U.S. gal).Power output curves are based on the engine operating with fuel system, water pump and lubricating oil pump; not included are battery charging alternator, fan, optional equipment and driven components.

TECHNICAL DATA DEPT. CERTIFIED WITHIN 5% CHIEF ENGINEER

Engine Critical Parts List:CPL: 2499 (2 Pump / 2 Loop)

CPL: 2548 (Air-to-AIr)

Date:

8May00

0.0

10.0

20.0

30.0

40.0

50.0

60.0

70.0

80.0

0 200 400 600 800 1000 1200 1400

Gross Engine Output - BHP

1800 RPM

U.S. Gallons/hour

G-DRIVE

QST4

0

5

10

15

20

25

30

0 500 1000 1500 2000 2500 3000

Altitude (m)

Ambient Temp. (°C / °F)

50 / 122

40 / 104

0

5

10

15

20

25

30

0 500 1000 1500 2000 2500 3000

Altitude (m)

Ambient Temp. (°C / °F)

50 / 122

40 / 10425 / 77

QST30-G4 Derate Curves @ 1800 RPM

Reference Standards:

BS-5514 and DIN-6271 standards are based on ISO-3046.

Operation At Elevated Altitude and Temperature:

For sustained operation above these conditions, derate an additional 9% per 1000 ft (300 m) and 15% per 10°C (18°F).

Note: Derates shown are based on 15 in H20 air intake restrictions and 2 in Hg exhaust back pressure.

CURVE NO: FR-5160 (2 Pump 2 loop)FR5162 (Air-to-AIr)

DATE: 8May00

STANDBY / PRIME

CONTINUOUS

Per

cen

t D

erat

e o

f R

ated

Po

wer

(%

)P

erce

nt

Der

ate

of

Rat

ed P

ow

er (

%)

G-DRIVE

QST5

Cummins Engine Company, Inc.Engine Data Sheet

DATA SHEET : DS-5160ENGINE MODEL : QST30-G4 CONFIGURATION NUMBER : D573001GX03 DATE : 8May00

PERFORMANCE CURVE : FR-5160 (2P / 2L)FR-5162 (A - A)

INSTALLATION DIAGRAM CPL NUMBER• Fan to Flywheel (2 Pump / 2 Loop): 3170314 • Engine Critical Parts List (2 Pump / 2 Loop) :2499• Fan to Flywheel (Air-to-Air): 3170341 • Engine Critical Parts List (Air-to-Air) :2548

GENERAL ENGINE DATAType................................................................................................................................................................ 4-Cycle; 50° Vee; 12-Cylinder DieselAspiration ....................................................................................................................................................... Turbocharged and Low Temperature

Aftercooled Bore x Stroke..............................................................................................................— mm x mm (in x in) 140 x165 (5.51 x 6.50)Displacement..............................................................................................................................— (litre) in3 30.48 (1860)Compression Ratio........................................................................................................................................ 14.0 : 1Dry Weight,Fan to Flywheel Engine............................................................................................. — kg (lb) 3012 (6640)Wet Weight,Fan to Flywheel Engine............................................................................................ — kg (lb) 3112 (6860)Moment of Inertia of Rotating Components • with FW 5050 Flywheel ........................................................................................... — kg • m2 (lbm • ft

2) 8.7 (206)Center of Gravity from Rear Face of Flywheel Housing (FH 5031) ........................................ — mm (in) 845 (33.3)Center of Gravity Above Crankshaft Centerline ....................................................................... — mm (in) 195 (7.7)Maximum Static Loading at Rear Main Bearing.......................................................................... — kg (lb) 950 (2100)

ENGINE MOUNTINGMaximum Bending Moment at Rear Face of Block..................................................... — N • m (lb • ft) 3100 (2286)

EXHAUST SYSTEMMaximum Back Pressure............................................................................................... — mm Hg (in Hg) 51 (2)

AIR INDUCTION SYSTEMMaximum Intake Air Restriction • with Dirty Filter Element ......................................................................................... — mm H2O (in H2O) 635 (25) • with Clean Filter Element....................................................................................... — mm H2O (in H2O) 381 (15)

COOLING SYSTEM (Low Temperature Aftercooling Required)Coolant Capacity — Engine Only.......................................................................... — litre (US gal) 79 (21)

— Aftercoolers (2 Pump / 2 Loop) ............................................ — litre (US gal) 12 (3.2)Minimum Pressure Cap ........................................................................................................... — kPa (psi) 69 (10)

Jacket Water Circuit RequirementsMaximum Coolant Friction Head External to Engine — 1500 / 1800 rpm..................... — kPa (psi) 48 / 69 (7 / 10)Maximum Static Head of Coolant Above Engine Crank Centerline............................................ — m (ft) 14 (46)Standard Thermostat (Modulating) Range................................................................................. — °C (°F) 82 - 95 (180 - 203)Maximum Top Tank Temperature for Standby / Prime Power...................................................— °C (°F) 104 / 100 (220 / 212)

Aftercooler Circuit Requirements (2 Pump / 2 Loop Aftercooling)Maximum Inlet Water Temperature to Aftercooler @ 77 °F.......................................................— °C (°F) 49 (120)Maximum Inlet Water Temperature to Aftercooler ......................................................................— °C (°F) 65 (150)Maximum Coolant Friction Head External to Engine — 1500 / 1800 rpm ..................... — kPa (psi) 35 / 48 (5 / 7)

Air-to-Air Core RequirementsMaximum Temp. Rise Between Engine Air Inlet and Intake Manifold — 1500 / 1800 rpm — °C (°F) 33 / 39 (60 / 70)Maximum Air Press. Drop from Turbo AIr Outlet to Intake Manifold — 1500 / 1800 rpm — mm (in Hg) 102 / 127 (4 / 5)

LUBRICATION SYSTEMOil Pressure @ Idle Speed .................................................................................................... — kPa (psi) 166 (24)

@ Governed Speed.......................................................................................... — kPa (psi) 310 - 386 (45 - 56)Maximum Oil Temperature.......................................................................................................... — °C (°F) 121 (250)Oil Capacity with OP 5133 Oil Pan : High - Low............................................................... — litre (US gal) 133 - 114 (35 - 30)Total System Capacity (Including Bypass Filter).............................................................. — litre (US gal) 154 (40.7)

FUEL SYSTEMType Injection System................................................................................................Bosch P8500 LLA Direct InjectionMaximum Restriction at Lift Pump — with Clean Fuel Pre-Filter......................................................— mm Hg (in Hg) 102 (4.0)

— with Dirty Fuel Pre-Filter ........................................................— mm Hg (in Hg) 203 (8.0)Maximum Allowable Head on Injector Return Line (Consisting of Friction and Static Head)...........— mm Hg (in Hg) 508 (20)Maximum Fuel Flow to Injection Pumps (Left and Right Banks Combined) 1500 / 1800 rpm.....— litre / hr (US gph) 550 / 570 (145 / 150)Maximum Fuel Inlet Temperature .....................................................................................................................— °C (°F) 71 (150)Maximum Return Flow..................................................................................... 1500 / 1800 rpm ....— litre / hr (US gph) 530 / 550 (140 / 145)

G-DRIVE

QST6

ELECTRICAL SYSTEMCranking Motor (Heavy Duty, Positive Engagement)......................................................................................................... — volt 24Battery Charging System, Negative Ground................................................................................................................ — ampere 35Maximum Allowable Resistance of Cranking Circuit ........................................................................................................ — ohm 0.002Minimum Recommended Battery Capacity

• Cold Soak @ 10 °C (50 °F) and Above............................................................................................................. — 0°F CCA 1200• Cold Soak @ 0 °C to 10 °C (32 °F to 50 °F)...................................................................................................... — 0°F CCA 1280• Cold Soak @ -18 °C to 0 °C (0 °F to 32 °F)....................................................................................................... — 0°F CCA 1800

COLD START CAPABILITYMinimum Ambient Temperature for Cold Start with 8000 watt Coolant Heater to Rated Speed................................— °C (°F) -7 (20)Minimum Ambient Temperature for Unaided Cold Start to Idle Speed............................................... .......................— °C (°F) 7 (45)Minimum Ambient Temperature for NFPA110 Cold Start (90°F Minimum Coolant Temperature)............................— °C (°F) 0 (32)

PERFORMANCE DATAAll data is based on: • Engine operating with fuel system, water pump, lubricating oil pump, air cleaner and exhaust

silencer; not included are battery charging alternator, fan, and optional driven components.• Engine operating with fuel corresponding to grade No. 2-D per ASTM D975.• ISO 3046, Part 1, Standard Reference Conditions of:

Barometric Pressure : 100 kPa (29.53 in Hg) Air Temperature : 25 °C (77 °F)Altitude : 110 m (361 ft) Relative Humidity : 30%Air Intake Restriction : 254 mm H2O (10 in H2O) Exhaust Restriction : 51 mm Hg (2 in Hg)

Steady State Stability Band at any Constant Load .............................................................................................................. — % +/- 0.25Estimated Free Field Sound Pressure Level of a Typical Generator Set;

Excludes Exhaust Noise; at Rated Load and 7.5 m (24.6 ft); @1500 / 1800 rpm ................................................. — dBA 91 / 93Exhaust Noise at 1 m Horizontally from Centerline of Exhaust Pipe Outlet Upwards at 45° @1500 / 1800 rpm......... — dBA 128 / 131

STANDBY POWER PRIME POWER60 hz 50 hz 60 hz 50 hz

Governed Engine Speed .............................................................— rpm 1800 1500 1800 1500Engine Idle Speed....................................................................... — rpm 700 - 900 700 - 900 700 - 900 700 - 900Gross Engine Power Output...........................................— kWm (BHP) 1112 (1490) 970 (1300) 1007 (1350) 880 (1180)Brake Mean Effective Pressure...........................................— kPa (psi) 2427 (352) 2544 (369) 2199 (319) 2310 (335)Piston Speed ................................................................— m / s (ft / min) 9.9 (1949) 8.3 (1634) 9.9 (1949) 8.3 (1634)Friction Horsepower....................................................... — kWm (BHP) 82 (110) 58 (78) 82 (110) 58 (78)Engine Jacket Water Flow at Stated Friction Head External to Engine:

• 5 psi Friction Head.......................................... — litre / s (US gpm) 17.0 (270) 14.2 (225) 17.0 (270) 14.2 (225)• Maximum Friction Head.................................. — litre / s (US gpm) 16.5 (262) 13.7 (217) 16.5 (262) 13.7 (217)

Engine Data with Dry Type Exhaust ManifoldIntake Air Flow................................................................— litre / s (cfm) 1340 (2840) 1005 (2130) 1250 (2650) 945 (2005)Exhaust Gas Temperature .....................................................— °C (°F) 525 (975) 575 (1070) 495 (920) 565 (1050)Exhaust Gas Flow..........................................................— litre / s (cfm) 3670 (7775) 2980 (6310) 3285 (6960) 2750 (5820)Air to Fuel Ratio..................................................................... — air : fuel 25 : 1 22 : 1 26.5 : 1 22.6 : 1Radiated Heat to Ambient .....................................— kWm (BTU / min) 130 (7460) 115 (6410) 115 (6650) 105 (5860)Heat Rejection to Jacket Water Coolant...............— kWm (BTU / min) 365 (20880) 335 (18940) 340 (19350) 320 (18150)Heat Rejection to Exhaust.....................................— kWm (BTU / min) 740 (42130) 670 (38050) 660 (37640) 600 (33990)

Engine Aftercooler DataHeat Rejection to Aftercooler................................— kWm (BTU / min) 270 (15420) 170 (9560) 215 (12120) 145 (8240)Aftercooler Water Flow at Stated Friction Head External to Engine:

• 2 psi Friction Head....................................... — litre / s (US gpm) 5.4 (85) 4.5 (71) 5.4 (85) 4.5 (71)• Maximum Friction Head.............................. — litre / s (US gpm) 5.0 (80) 4.4 (68) 5.0 (80) 4.4 (68)

Charge Air Flow.......................................................— kg/ min (lb / min) 93 (205) 70 (154) 87 (192) 66 (145)Turbocharger Compressor Outlet Pressure ...........— mm Hg (in / Hg) 1859 (73) 1534 (60) 1666 (66) 1374 (54)Turbocharger Compressor Outlet Temperature................... — °C (°F) 202 (395) 177 (350) 183 (360) 165 (330)

ENGINE MODEL : QST30-G4DATA SHEET : DS-5160

DATE : 8May00

N.A. - Data is Not AvailableN/A - Not Applicable to this EngineTBD - To Be Determined

HCI634J - Technical Data Sheet

HCI634JSPECIFICATIONS & OPTIONS

STANDARDS

Newage Stamford industrial generators meet therequirements of BS EN 60034 and the relevantsection of other international standards such asBS5000, VDE 0530, NEMA MG1-32, IEC34, CSAC22.2-100, AS1359.Other standards and certifications can be consideredon request.

VOLTAGE REGULATORS

MX321 AVR - STANDARD

This sophisticated Automatic Voltage Regulator(AVR) is incorporated into the Stamford PermanentMagnet Generator (PMG) system and is fitted asstandard to generators of this type.The PMG provides power via the AVR to the mainexciter, giving a source of constant excitation powerindependent of generator output. The main exciteroutput is then fed to the main rotor, through a fullwave bridge, protected by a surge suppressor. TheAVR has in-built protection against sustained over-excitation, caused by internal or external faults. Thisde-excites the machine after a minimum of 5seconds.Over voltage protection is built-in and short circuitcurrent level adjustments is an optional facility.

WINDINGS & ELECTRICAL PERFORMANCE

All generator stators are wound to 2/3 pitch. Thiseliminates triplen (3rd, 9th, 15th …) harmonics on thevoltage waveform and is found to be the optimumdesign for trouble-free supply of non-linear loads.The 2/3 pitch design avoids excessive neutralcurrents sometimes seen with higher windingpitches, when in parallel with the mains. A fullyconnected damper winding reduces oscillationsduring paralleling. This winding, with the 2/3 pitchand carefully selected pole and tooth designs,ensures very low waveform distortion.

TERMINALS & TERMINAL BOX

Standard generators feature a main stator with 6ends brought out to the terminals, which are mountedon the frame at the non-drive end of the generator.A sheet steel terminal box contains the AVR andprovides ample space for the customers' wiring andgland arrangements. It has removable panels foreasy access.

SHAFT & KEYS

All generator rotors are dynamically balanced tobetter than BS6861:Part 1 Grade 2.5 for minimumvibration in operation. Two bearing generators arebalanced with a half key.

INSULATION/IMPREGNATION

The insulation system is class 'H'.All wound components are impregnated withmaterials and processes designed specifically toprovide the high build required for static windingsand the high mechanical strength required forrotating components.

QUALITY ASSURANCE

Generators are manufactured using productionprocedures having a quality assurance level to BSEN ISO 9001.

The stated voltage regulation may not be maintainedin the presence of certain radio transmitted signals.Any change in performance will fall within the limits ofCriteria 'B' of EN 61000-6-2:2001. At no time will thesteady-state voltage regulation exceed 2%.

NB Continuous development of our products entitlesus to change specification details without notice,therefore they must not be regarded as binding.

Front cover drawing typical of product range.

2

CONTROL SYSTEM SEPARATELY EXCITED BY P.M.G.

A.V.R. MX321

VOLTAGE REGULATION ± 0.5 %

SUSTAINED SHORT CIRCUIT

INSULATION SYSTEM

PROTECTION

RATED POWER FACTOR

STATOR WINDING

WINDING PITCH

WINDING LEADS

STATOR WDG. RESISTANCE

ROTOR WDG. RESISTANCE

R.F.I. SUPPRESSION BS EN 61000-6-2 & BS EN 61000-6-4,VDE 0875G, VDE 0875N. refer to factory for others

WAVEFORM DISTORTION NO LOAD < 1.5% NON-DISTORTING BALANCED LINEAR LOAD < 5.0%

MAXIMUM OVERSPEED 2250 Rev/Min

BEARING DRIVE END

BEARING NON-DRIVE END

1 BEARING 2 BEARING

WEIGHT COMP. GENERATOR

WEIGHT WOUND STATOR

WEIGHT WOUND ROTOR

WR² INERTIA

SHIPPING WEIGHTS in a crate

PACKING CRATE SIZE

TELEPHONE INTERFERENCE

COOLING AIR

VOLTAGE STAR 380/220 400/231 415/240 440/254 416/240 440/254 460/266 480/277

VOLTAGE DELTA 220 230 240 254 240 254 266 277

kVA BASE RATING FOR REACTANCE VALUES 1000 1000 1000 1000 1150 1200 1250 1300

Xd DIR. AXIS SYNCHRONOUS 3.02 2.73 2.54 2.26 3.49 3.25 3.10 2.96X'd DIR. AXIS TRANSIENT 0.24 0.22 0.20 0.18 0.28 0.26 0.25 0.24X''d DIR. AXIS SUBTRANSIENT 0.17 0.15 0.14 0.12 0.19 0.18 0.17 0.16Xq QUAD. AXIS REACTANCE 1.78 1.61 1.50 1.33 2.05 1.91 1.82 1.74X''q QUAD. AXIS SUBTRANSIENT 0.21 0.19 0.18 0.16 0.25 0.23 0.22 0.21XL LEAKAGE REACTANCE 0.09 0.08 0.08 0.07 0.10 0.10 0.09 0.09X2 NEGATIVE SEQUENCE 0.21 0.19 0.18 0.16 0.25 0.23 0.22 0.21X0 ZERO SEQUENCE 0.03 0.02 0.02 0.02 0.03 0.03 0.03 0.03

REACTANCES ARE SATURATED VALUES ARE PER UNIT AT RATING AND VOLTAGE INDICATED

T'd TRANSIENT TIME CONST.T''d SUB-TRANSTIME CONST.T'do O.C. FIELD TIME CONST.Ta ARMATURE TIME CONST.SHORT CIRCUIT RATIO

0.1850.0253.030.046

HCI634J

1.614 m³/sec 3420 cfm 1.961 m³/sec 4156 cfm

50 Hz

THF

Winding 312HCI634J

THREE PHASE EFFICIENCY CURVES

50Hz

4

Winding 312HCI634J

THREE PHASE EFFICIENCY CURVES

60Hz

5

HCI634JWinding 312

Locked Rotor Motor Starting Curve

0

5

10

15

20

25

30

0 200 400 600 800 1000 1200 1400 1600 1800 2000 2200 2400 2600 2800LOCKED ROTOR kVA

PER

CEN

T TR

AN

SIEN

T VO

LTA

GE

DIP

.

346V 380V 400V 415V 440V

50Hz

0

5

10

15

20

25

30

0 200 400 600 800 1000 1200 1400 1600 1800 2000 2200 2400 2600 2800 3000 3200LOCKED ROTOR kVA

PER

CEN

T TR

AN

SIEN

T VO

LTA

GE

DIP

.

380V 416V 440V 460V 480V

60Hz

6

3-phase 2-phase L-L 1-phase L-NVoltage Factor Voltage Factor x 1.00 x 0.87 x 1.30

380v X 1.00 416v x 1.00 x 1.00 x 1.80 x 3.20400v X 1.07 440v x 1.06 x 1.00 x 1.50 x 2.50415v X 1.12 460v x 1.12 10 sec. 5 sec. 2 sec.440v X 1.18 480v x 1.17

Minimum

HCI634J

50Hz 60Hz

The sustained current value is constant irrespectiveof voltage level

Three-phase Short Circuit Decrement Curve. No-load Excitation at Rated SpeedBased on star (wye) connection.

Max. sustained durationAll other times are unchanged

Instantaneous

Sustained

Sustained Short Circuit = 3,600 Amps

Sustained Short Circuit = 4,900 AmpsNote 1The following multiplication factors should beused to adjust the values from curve betweentime 0.001 seconds and the minimum currentpoint in respect of nominal operating voltage :

Note 2The following multiplication factor should be used to convert thevalues calculated in accordance with NOTE 1 to those applicableto the various types of short circuit :

Note 3Curves are drawn for Star (Wye) connected machines. For Delta connection multiply the Curve current value by 1.732

50Hz

60Hz

1000

10000

100000

0.001 0.01 0.1 1 10TIME (secs)

CUR

RENT

(Am

ps) SYMMETRICAL

ASYMMETRICAL

1000

10000

100000

0.001 0.01 0.1 1 10TIME (secs)

CU

RR

EN

T (A

mps

)

SYMMETRICAL

ASYMMETRICAL

7

Class - Temp Rise

Star (V) 380 400 415 440 380 400 415 440 380 400 415 440 380 400 415 440

Delta (V) 220 230 240 254 220 230 240 254 220 230 240 254 220 230 240 254

kVA 900 927 900 900 1000 1030 1000 1000 1060 1070 1060 1060 1100 1110 1100 1100

kW 720 742 720 720 800 824 800 800 848 856 848 848 880 888 880 880

Efficiency (%) 95.3 95.4 95.5 95.6 95.0 95.1 95.3 95.4 94.7 94.9 95.1 95.3 94.6 94.8 95.0 95.2

kW Input 756 777 754 753 842 866 839 839 895 902 892 890 930 937 926 924

Star (V) 416 440 460 480 416 440 460 480 416 440 460 480 416 440 460 480

Delta (V) 240 254 266 277 240 254 266 277 240 254 266 277 240 254 266 277

kVA 1063 1100 1150 1188 1150 1200 1250 1300 1206 1250 1300 1350 1250 1300 1350 1400

kW 850 880 920 950 920 960 1000 1040 965 1000 1040 1080 1000 1040 1080 1120

Efficiency (%) 95.2 95.3 95.3 95.4 95.0 95.1 95.1 95.2 94.8 95.0 95.0 95.1 94.7 94.8 94.9 94.9

kW Input 893 923 965 996 968 1009 1052 1092 1018 1053 1095 1136 1056 1097 1138 1180

14 18 21 24

25.4 15.87 0 0

HCI634J

Cont. F - 105/40°C Cont. H - 125/40°C Standby - 150/40°C Standby - 163/27°C

Winding 312 0.8 Power Factor

RATINGS

TD_HCI634J.GB_08.02_01_GB

SAE

AN

DIMENSIONS

50Hz

60Hz

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© 2002 Newage International Limited.Reprinted with permission of N.I. only.Printed in England.

60Hz

50Hz

N.A. - Data is Not AvailableN/A - Not Applicable to this EngineTBD - To Be DeterminedCONVERSIONS: (litres = U.S. Gal x 3.785) (kWm = BHP x 0.746) (U.S. Gal = litres x 0.2642) (BHP = ...Percent Derate of Rated Power (%)CONVERSIONS: (litres = U.S. Gal x 3.785) (Engine kWm = BHP x 0.746) (U.S. Gal = litres x 0.2642) ...STANDBY / PRIME1500 RPMPRIME POWER RATINGApplicable for supplying electric power in lieu of commercially purchased power. Prime Power appl...Limited Time Prime Power is available for a limited number of hours in a non-variable load applic...such as in utility power curtailment. Engines may be operated in parallel to the public utility u...The customer should be aware, however, that the life of any engine will be reduced by this consta...Prime Power rating should use the Continuous Power rating.CONTINUOUS POWER RATINGApplicable for supplying utility power at a constant 100% load for an unlimited number of hours p...Engine Performance Data @ 1500 RPMLitre/hourCONTINUOUSCURVE NO: FR-5160 (2 Pump 2 loop)FR5162 (Air-to-AIr)DATE: 8May00Percent Derate of Rated Power (%) (1)Reference Standards:BS-5514 and DIN-6271 standards are based on ISO-3046.Operation At Elevated Altitude and Temperature:For sustained operation above these conditions, derate an additional 9% per 1000 ft (300 m) and 1...Note: Derates shown are based on 15 in H20 air intake restrictions and 2 in Hg exhaust back press...Engine Performance Data @ 1800 RPM1800 RPMU.S. Gallons/hourPercent Derate of Rated Power (%) (2)CONTINUOUS (1)Percent Derate of Rated Power (%) (3)PRIME POWER RATING (1)Applicable for supplying electric power in lieu of commercially purchased power. Prime Power appl... (1)Limited Time Prime Power is available for a limited number of hours in a non-variable load applic... (1)such as in utility power curtailment. Engines may be operated in parallel to the public utility u... (1)The customer should be aware, however, that the life of any engine will be reduced by this consta... (1)Prime Power rating should use the Continuous Power rating. (1)CONTINUOUS POWER RATING (1)Applicable for supplying utility power at a constant 100% load for an unlimited number of hours p... (1)QST30-G4 Derate Curves @ 1500 RPMQST30-G4 Derate Curves @ 1800 RPMCURVE NO: FR-5160 (2 Pump 2 loop) (1)FR5162 (Air-to-AIr) (1)DATE: 8May00 (1)Reference Standards: (1)BS-5514 and DIN-6271 standards are based on ISO-3046. (1)Operation At Elevated Altitude and Temperature: (1)For sustained operation above these conditions, derate an additional 9% per 500 m (1640 ft) and 1...STANDBY / PRIME (1)