NSN 2835-01-341-5955
Part Details | NONAIRCRAFT GAS TURBINE ENGINE
2835-01-341-5955 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: 378798110, 378798-1-10, GTCP85106A, GTCP85-106A, 2835-01-341-5955, 01-341-5955, 2835013415955, 013415955
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 01, 1991 | 01-341-5955 | 50489 ( ENGINE, GAS TURBINE, NONAIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-341-5955
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 378798-1-10 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| GTCP85-106A | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2835-01-341-5955
| Characteristic | Specifications |
|---|---|
| FUEL TYPE | JET FUEL |
| POWER OUTPUT FOR WHICH DESIGNED | SHAFT |
| MOUNTING TYPE | AIRCRAFT |
| REFERENCE DATA AND LITERATURE | MODEL GTCP85-106A |