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National Stock Number: 2840-01-431-7917
Federal Supply Class: 2840
National Item Identification Number: 014317917
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.
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Manufacturer Information:
9545M18 | 07482 | GENERAL ELECTRIC COMPANY | 9545M18G15 | 07482 | GENERAL ELECTRIC COMPANY |
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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 | REFERENCE DATA AND LITERATURE | T.O. 2J-F118-4, FIG 1 IND 13, FIG 68 & 69 BREAKOUTS | SPECIAL FEATURES | HPT ROTOR AFT SHAFT DAMPER REDESIGN ECP FH165; HPT AFT SHAFT P/N 1385M24P01; SLEEVE DAMPER P/N 1864M56P01; ECP FH1351C1 HPT ROTATING AIR SEAL (REWKD ROTATING AIR SEAL) P/N 1498M90P01; ECP FH133C1 HPT AFT BLADE RETAINER P/N 1476M95P03; SUPERSES P/N 9545M18G01, G02, G03, G13 AND G14; SUPERSEDED BY 9545M18G16 AND THEN G21 |
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