Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-447-2504 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: 9547M19G08, 9547M19G07, 9547M19, 2840-01-447-2504, 01-447-2504, 2840014472504, 014472504
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 30, 1997 | 01-447-2504 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-447-2504
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9547M19G08 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9547M19G07 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9547M19 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-447-2504
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | 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 |
| CRITICALITY CODE JUSTIFICATION | AFEAT$$ACZBJ |
| END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME ROTOR ASSEMBLY,LOW PRESSURE TURBINE |