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KTA19-G3A: Engine Model: Reference Information

This document provides specifications for an KTA19-G3A engine model including: - The engine produces 755 horsepower in standby mode and 680 horsepower in prime mode at 1800 rpm. - It is a 6-cylinder, turbocharged and aftercooled inline engine with a displacement of 1150 cubic inches. - Specifications are provided for the engine's dimensions, weight, cooling requirements, lubrication system, fuel system and electrical system.
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0% found this document useful (0 votes)
626 views3 pages

KTA19-G3A: Engine Model: Reference Information

This document provides specifications for an KTA19-G3A engine model including: - The engine produces 755 horsepower in standby mode and 680 horsepower in prime mode at 1800 rpm. - It is a 6-cylinder, turbocharged and aftercooled inline engine with a displacement of 1150 cubic inches. - Specifications are provided for the engine's dimensions, weight, cooling requirements, lubrication system, fuel system and electrical system.
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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ENGINE MODEL: KTA19-G3A

STAND_BY: 755 BHP REFERENCE INFORMATION:


@1800r/min
563 kW CONFIGURATION……………………………………D193091DX02
PRIME: 680 BHP CPL NUMBER ……………………………………… 4153
@1800r/min
507 kW PERFORMANCE CURVE NUMBER………………FR-4212

GENERALENGINE DATA
Type…………………………………………………………………………………………………4 Cycle , In-line , 6 Cylinder
Aspiration……………………………………………………………………………………………Turbocharged , Aftercooled
Bore—in.(mm)×stroke—in.(mm)…………………………………………………………………6.25×6.25 (159×159)
Displacement—in3(L)………………………………………………………………………………1150 (19)
Compression Ratio…………………………………………………………………………………13.9:1
Dry Weight
Fan Hub to Flywheel Engine —lb(kg)…………………………………………………………
3725 (1690)
Radiator Cooled Engine —lb(kg)………………………………………………………………
5900 (2676)
Wet Weight
Fan Hub to Flywheel Engine —lb(kg)…………………………………………………………
3880 (1760)
Radiator Cooled Engine —lb(kg)………………………………………………………………
6300 (2858)
Moment of Inertia of Rotating Components (Excluding Flywheel) —lb m.ft2(kg•m 2)…………43 (1.82)
2 2
·With FW 4001 Flywheel —kg•m (lbm.ft )………………………………………………
7.16 (170.0)
·With FW 4006 Flywheel —kg•m2(lbm.ft2)………………………………………………
8.39 (199.0)
C.G. Distance From Front Face of Block—in(mm)…………………………………………… 23.6 (598)
C.G. Distance Above Crank Centerline—in(mm)………………………………………………9 (229)
Maximum Allowable Bending Moment at Rear Face of Block —N•m(lb.ft)………………… 2000 (907)
Firing Order…………………………………………………………………………………………1-5-3-6-2-4

ENGINE MOUNTING
Moment of Inertia About Roll Axis —lb.ft 2(kg•m 2)………………………………………………1876 (79)
EXHAUST SYSTEM
Maximum Allowable Back Pressure (1500/1800 rpm) —in.Hg(kPa)…………………………2.3/3 (7.8/10.2)
Maximum Allowable Back Pressure —in.Hg(kPa)………………………………………………
3 (10)
Exhaust Pipe Size Normally Acceptable —in(mm)…………………………………………… 5 (127)
AIR INDUCTION SYSTEM
Maximum Allowable Intake Air Restriction With Heavy Duty Air Cleaner
Clean Element —in.H2O(kPa)…………………………………………………………………15 (3.73)
Clean Element —in.H2O(kPa)…………………………………………………………………15 (3.73)
— …………82 (180)
COOLING SYSTEM
Coolant Capacity
After-cooler Only —U.S.Gal(L)……………………………………………………………… 6 (23)
With heat exchanger HX 6076 ( With out explantion tank) —U.S.Gal(L)…………………
53 (199)
With explantion tank & LTA—U.S.Gal(L)……………………………………………………30 (112)

Maximum Coolant Friction Heat External to Engine @1800 rpm —PSI(kPa)………………10 (68.9)
@1500 rpm —PSI(kPa)……… 10 (68.9)
Maximum Allowable Air Friction Across radator —in.H2O(kPa)………………………………0.5 (0.1)
Minimum Raw Water Flow @ 90°F(32 ) to Heat Exchanger With HX 6076 —GPM(L/mi 108 (408.8)
Maximum Raw Water Inlet Pressure @ Heat Exchanger HX 6076 —PSI(kPa)……………50 (344.7)
Maximum Allowable Top Tank Temperature (Stand_by/Prime) —°F( )……………………220/212 (104/100)
Standard Thermostat (modulating) Range— °F( )……………………………………………180-200 (82-93)
Maximum Allowable Coolant Temperature —°F( )……………………………………………
205 (96.1)
Minimum Coolant Makeup Capacity —U.S.Gal(L)………………………………………………
1.6 (6.1)
Maximum Raw water Inlet Friction —PSI(kPa)…………………………………………………10 (254.0)
Minimum Allowable Fill Rate —U.S.GPM(L/min)………………………………………………5 (18.9)
Maximum Allowable Initial Fill Time —min………………………………………………………5
Minimum Allowable Coolant Expansion Space —% of System Capacity……………………5
Maximum Allowable Inlet Coolant Temperature at Limited situation (Stand_by/Prime) —° (71/66)
LUBRICATION SYSTEM
Oil Pressure
@ Idle —PSI(kPa)………………………………………………………………………………20 (138)
@ Rated Speed —PSI(kPa)………………………………………………………………… 50-70 (345-483)
Oil Flow at Rated Speed —U.S.GPM(L/min)……………………………………………………40 (151.4)
Maximum Allowable Oil Temperature —°F( )…………………………………………………250 (121.0)
By-Pass Filter Capacity
Spin-on Cartridge Type —U.S.Gal(L)…………………………………………………………
0.7 (2.6)
Replaceable Element Type —U.S.Gal(L) ……………………………………………………
2.9 (11.0)
Oil Pan Capacity (Option OP4019)
High —U.S.Gal(L)………………………………………………………………………………10.0 (37.9)
Total System Capacity (Excluding By-Pass Filter) —U.S.Gal(L)………………………………
22.3 (84.4)
Total System Capacity (Excluding By-Pass Filter) —U.S.Gal(L)………………………………
13.2 (50.0)
Angularty of Standard Oil Pan ( Option OP4
Front Down………………………………………………………………………………………30°
FUEL SYSTEM
Fuel Injection System………………………………………………………………………………Cummins PT
Maximum Fuel Consumption at Maximum Rated Output and Speed —lb/h(kg/h)…………
Maximum allowable Restriction to PT Fuel Pump
With Clean Fuel Filter —in.Hg(kPa)………………………………………………………… 4 (13.55)
With Dirty Fuel Filter —in.Hg(kPa)……………………………………………………………9 (30.48)
Maximum Fuel Supply at Rated Power and Speed —lb/h(kg/h)………………………………
Maximum Allowable Injector Return Line Restriction
With Check Valves —in.Hg(kPa)………………………………………………………………
7 (22)
Less Check Valves —in.Hg(kPa)…………………………………………………………… 3 (8)
Minimum Allowable Fuel Tank Vent Capability —ft 3/h L/h ……………………………… 15 (425)
(With 2.5 in. Hg (63 mm Hg) or Less Back Pressure)
Starter (Heavy, Anode) Volt…………………………………………………………………… 24
Battary Recharge System,Negative ground—A………………………………………………… 35
Maximum Allowable Resistance of Starting Circuit— ……………………………………… 0.002
Minimum Recommended Battary Capacity
·Cold Soak at 50°F(10 ) or Above—0°F CCA……………………………………………… 600
·Cold Soak at 32~50°F(0~10 ) or Above—0°F CCA……………………………………… 640
·Cold Soak at 0~32°F(-18~0 ) or Above—0°F CCA……………………………………… 900
PERFORMANCE DATA
All data is based on the engine operating with fuel system, water pump, lubricating oil pump, air cleaner, and
muffler, not included are altemator, compressor, fan, optional equipment and driven components. Data repressents
gross engine performance capabilities obtained and corrected in accordance with SAE J1349 conditions fo 29.61 in
Hg(100 kPa) barometric pressure[300ft. (90 m) altitude], 77°F (25 ) inlet air temperature, and 0.30 in. Hg (1kPa)
water vapor pressure with No. 2 diesel fuel or a fuel corresponding to ASTM D2. All data is subject to change without
notice

Engine Speed r/min…………………………………………… 1800 1500 1800 1500


Idle Speed r/min……………………………………………… 675-775 675-775 675-775 675-775
Gross Power Output BHP(kW)……………………………… 755(563) 675(504) 680(507) 600(448)
Brake Mean Effective Pressure PSI(kPa)…………………… 287(1978) 308(2125) 258(1781) 274(1889)
Piston Speed ft/min(m/s)……………………………………… 1870(9.5) 1555(7.9) 1870(9.5) 1555(7.9)
Friction Horsepower BHP(kW)……………………………… 83(62) 54(40) 83(62) 54(40)
Intake Air FlowCFM( L/s)……………………………………… 1517(716) 1226(579) 1455(687) 1126(531)
Exhaust Gas Flow CFM( L/s)………………………………… 3945(1862) 3398(1604) 3673(1734) 3039(1434)
Exhaust Gas Temperature °F( )…………………………… 939(504) 1034(557) 898(481) 1000(538)
Heat Rejection to Ambient BTU/min(kW)…………………… 4522(80) 4108(72) 4050(0) 3645(64)
Heat Rejection to Coolant BTU/min(kW)…………………… 22830(401) 20530(361) 20824(366) 18125(319)
Engine Water Flow L/s(U.S.GPM) @ 3psi………………… 196(12.4) 162(10.2) 196(12.4) 162(10.2)

Chanvge Log
Date Author Change Description
2013/6/25 Jiang Li Release

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