|
|
|
National Stock Number:
2840-01-447-2504
Federal Supply Class:
2840
National Item Identification Number:
014472504
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:
| 9547M19 | 07482 | GENERAL ELECTRIC COMPANY | | 9547M19G07 | 07482 | GENERAL ELECTRIC COMPANY | | 9547M19G08 | 07482 | GENERAL ELECTRIC COMPANY |
|
Techincal Specification:
| CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ | | DESIGN TYPE | AXIAL COMPRESSOR | | ENGINE SECTION LOCATION | LOW PRESSURE TURBINE | | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME ROTOR ASSEMBLY,LOW PRESSURE TURBINE | | SPECIAL FEATURES | MATERIAL IS A CRYSTAL RENE N6, A PRECIPITATION STRENGTHENED ALLOY; ROTOR HAS A NEW REDESIGNED STG 1 BLADE WITH THE NEW MATERIAL; INCREASED LIFE OF BLADE; BLADES ARE STILL DOVETAIL AND ARE IDENTICAL TO THE OLD CONFIGURATION P/N 1475M47P01; NEW BLADES ARE INTERCHANGEABLE IN COMPLETE SETS ONLY; INTERMIXING OF BLADES, OLD AND NEW, WILL NOTBE ALLOWED; SINCE DOVETAILS ARE IDENTICAL AND WILL FIT IN THE SAME DISK, NO CHANGES TO DISK |
|
|