Part Details | NONAIRCRAFT GAS TURBINE ENGINE
2835-01-328-7477 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: T62T40C7D, T-62T-40C7D, 2835-01-328-7477, 01-328-7477, 2835013287477, 013287477
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 06, 1990 | 01-328-7477 | 50489 ( ENGINE, GAS TURBINE, NONAIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-328-7477
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| T-62T-40C7D | 55820 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
Technical Data | NSN 2835-01-328-7477
| Characteristic | Specifications |
|---|---|
| FUEL TYPE | GASOLINE |
| POWER OUTPUT FOR WHICH DESIGNED | SHAFT |
| SPECIAL FEATURES | SHAFT HORSEPOWER RATING IN RPM 61565.0; ALTITUDE AT WHICH HORSEPOWER IS RATED 20000.0 FEET; INLET AIR TEMP AT WHICH HORSEPOWER IS RATED 400.0 DEG FAHRENHEIT |