NSN 2835-01-032-7140

Part Details | NONAIRCRAFT GAS TURBINE ENGINE

2835-01-032-7140 A continuous combustion type engine. Consists primarily of a COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE; CHAMBER, COMBUSTION, NONAIRCRAFT GAS TURBINE ENGINE and a TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. It may have a fan section. Air is compressed and heated by a combustible fuel and expanded through the turbine. It is designed to furnish a source of rotary shaft and/or pneumatic power. The pneumatic power is obtained by a bleedoff of the engine compressor. For a complete operating power unit, mounted on a base, see POWER UNIT, GAS TURBINE ENGINE.

Alternate Parts: 13217E4331, 3802781 AND 130010488, 380278-1 AND 1300-1048-8, 2835-01-032-7140, 01-032-7140, 2835010327140, 010327140

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
28DEC 18, 197601-032-714050489 ( ENGINE, GAS TURBINE, NONAIRCRAFT )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-032-7140
Part Number Cage Code Manufacturer
13217E433197403CECOM LR CENTER
380278-1 AND 1300-1048-899193HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
Technical Data | NSN 2835-01-032-7140
Characteristic Specifications
SPECIAL FEATURESPNEUMATIC SHAFT POWER OUTPUT,190.0 SHAFT HORSEPOWER RATING,6000.0 RPM SHAFT HORSEPOWER SPEED RATING,40700.0 AIR HORSEPOWER RATING,460.0 LB PER MINUTE AIR FLOW,80.0 PSI DISCHARGE PRESSURE,0.0 ALTITUTE AT WHICH HORSEPOWER IS RATED,130.0 DEG FAHRENHEIT HORSEPOWER RATED,7500 HR OF OPERATION BETWEEN OVERHAULS,JET FUEL,AC,120.0/208.0 V,CENTRIFUGAL SWITCH,DUAL PAD DRIVE,FUEL CONTROL,IGNITER,OIL COOLER,OIL PUMP,STARTER,LOAD CONTROL VALVE,INCLOSURE,BASE FRAME MOUNTING,STEEL CONTAINER ACCOMMODATES ENGINE,42.630 IN. MAX O/A LG,27.810 IN. NOM O/A HEIGHT,29.460 IN. NOM O/A WIDTH
REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICSAS DIFFERENTIATED BY SOURCE CONTROL DWG NO.,STEEL CONTAINER