NSN 2835-01-323-0762
Part Details | NONAIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER
2835-01-323-0762 The portion of a ENGINE, GAS TURBINE, NONAIRCRAFT in which fuel is burned. It may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case.
Alternate Parts: TG200861, 2835-01-323-0762, 01-323-0762, 2835013230762, 013230762
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 19, 1990 | 01-323-0762 | 50338 ( CHAMBER, COMBUSTION, NONAIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-323-0762
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| TG200861 | 28839 | TELEDYNE INDUSTRIES INCTELEDYNE POWER SYSTEMS DIV |
Technical Data | NSN 2835-01-323-0762
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 15.750 INCHES NOMINAL |
| OVERALL HEIGHT | 3.280 INCHES NOMINAL |
| SPECIAL FEATURES | COMBUSTOR COVER ASSY,A ONE AND ONE HALF (1 1/2) HOLE IN DOME RECEIVES COMBUSTOR CAN NECK,SECURED BY A SNAP RING; FUEL/AIR NOZZLE AND IGNITOR ARE BOLTED TO COVER; A TEMPERATURE SENSINGELEMENT IS MOUNTED BEHIND FUEL NOZZLE |
| END ITEM IDENTIFICATION | GROUND POWER GENERATOR SYSTEM; NEXT HIGHER ASSEMBLY IS TG200878 |