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National Stock Number:
2835-01-345-3402
Federal Supply Class:
2835
National Item Identification Number:
013453402
Description:
ENGINE,GAS TURBINE,NONAIRCRAFT
Detail:
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.
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Manufacturer Information:
| 161331-135 | 55820 | RAYTHEON TECHNOLOGIES CORPORATION |
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Techincal Specification:
| FUEL TYPE | JET FUEL | | OVERALL HEIGHT | 24.400 INCHES NOMINAL | | OVERALL LENGTH | 38.800 INCHES NOMINAL | | OVERALL WIDTH | 17.600 INCHES NOMINAL | | MOUNTING TYPE | AIRCRAFT | | SPECIAL FEATURES | 110 SHAFT HP @ 64643RPM. APU IS SIMILAR TO P/N 161331-121/-128 EXCEPT UPDGRADED BY ECP-007R1C1. TMD IS T-62T-40LC-2. WEIGHT 186LBS. | | POWER OUTPUT FOR WHICH DESIGNED | SHAFT | | REFERENCE DATA AND LITERATURE | AIR FORCE TO. 2G-T62T-44 | | TEST DATA DOCUMENT | 55820-ECPT-62T-40LC-2-007R1C1 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.). |
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