|
|
|
National Stock Number:
2840-01-431-7924
Federal Supply Class:
2840
National Item Identification Number:
014317924
Description:
ROTOR,TURBINE,AIRCRAFT GAS TURBI
Detail:
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.
|
Manufacturer Information:
| 9545M18 | 07482 | GENERAL ELECTRIC COMPANY | | 9545M18G16 | 07482 | GENERAL ELECTRIC COMPANY |
|
Techincal Specification:
| DESIGN TYPE | AXIAL COMPRESSOR | | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE | | MATERIAL DOCUMENT AND CLASSIFICATION | INCONEL 718 MFR REF SINGLE MATERIAL RESPONSE OVERALL | | III MATERIAL | NICKEL ALLOY OVERALL | | PROPRIETARY CHARACTERISTICS | PACS | | SPECIAL FEATURES | 6HPT ROTOR AFT SHAFT DAMPER REDESIGN ECP FH165; HPT AFT SHAFT P/N 1385M24P01; SLEEVE DAMPER P/N 1864M56P01; ECP FH133C1 HPT AFT BLADE RETAINER P/N 1476M95P03; SUPERSEDES P/NS 9545M18G01, G02, G03 AND G13; SUPERSEDED BY 9545M18G15, G16 AND THEN G21 | | REFERENCE DATA AND LITERATURE | T.O. 2J-F118-4, FIG 1, IND 13, FIG 68 & 69 BREAKOUTS |
|
|