Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-01-430-2158 A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 408629501, 4086295-01, 408629401, 4086294-01, 407122301, 4071223-01, 408163301, 4081633-01, 2840-01-430-2158, 01-430-2158, 2840014302158, 014302158
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 24, 1996 | 01-430-2158 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-430-2158
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4086295-01 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4086294-01 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4071223-01 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4081633-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-430-2158
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 15.500 INCHES NOMINAL |
| DIAMETER | 18.783 INCHES NOMINAL |
| SPECIAL FEATURES | ROTOR CONSISTS OF 3 STGS; DISK & HUB; 1STG O/A DIA ON/C 14.590; O/A LENGTH 9.000; 2ND STG O/A DIA ON/C 16.188; O/A LENGTH 7.970; INVOLUTE SPLINE DATA: NO OF TEETH 79; SPLINE PITCH 20/40; PRESSURE ANGLE 30 DEG.; PITCH DIA. 3.9500; 3RD STG O/A LENGTH 4.000; ALL STAGES RECIEVE DOVETAIL BLADES |
| END ITEM IDENTIFICATION | F100PW229 AIRCRAFT GAS TURBINE ENGINE |