Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-041-0198 A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 6891588, 6887113, 2840-01-041-0198, 01-041-0198, 2840010410198, 010410198
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 19, 1977 | 01-041-0198 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-041-0198
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6891588 | 73342 | ALLISON TRANSMISSION, INC. |
| 6887113 | 73342 | ALLISON TRANSMISSION, INC. |
Technical Data | NSN 2840-01-041-0198
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | 30 BLADES EQUALLY SPACED ON OUTER PERIPHERY; TAPERED OD, 7.51 MIN 7.512 MAX IN. LARGEST OD; 10 SLOTS EQUALLY SPACED ON OUTER PERIPHERY; 1.159 MIN 1.1595 MAX IN. ID |