NSN 2835-00-907-0627
Part Details | NONAIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2835-00-907-0627 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, NONAIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, NONAIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 6930782, 693078-2, TIP0098911JAN71, TIP00989-11JAN71, 6930782, 693078-2, 6930782, 693078-2, 2835-00-907-0627, 00-907-0627, 2835009070627, 009070627
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
28 | JAN 01, 1960 | 00-907-0627 | 50592 ( ROTOR, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-00-907-0627
Part Number | Cage Code | Manufacturer |
---|---|---|
693078-2 | 72599 | ALLIEDSIGNAL INCDBA ALLIED-SIGNAL AEROSPACE CO |
TIP00989-11JAN71 | 97403 | CECOM LR CENTER |
693078-2 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
693078-2 | 70210 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2835-00-907-0627
Characteristic | Specifications |
---|---|
SPECIAL FEATURES | MATERIAL STEEL PER AMS 5365;2.011 IN LONG; VANES 6.495 IN. MIN AND 6.505 IN. MAX OD TAPERED TO 4.428 IN. MIN AND 4.434 IN. MAX DIA; BORE 1.0007 IN. MIN AND 1.0009 IN MAX DIA FOR FORST STAGE; PER AF TO. 2G-GTP70-24,FIG 14, INDEX 84 |
REFERENCE DATA AND LITERATURE | AF TO. 2G-GTP70-24,FIG. 14,INDEX 84 |
END ITEM IDENTIFICATION | GTCP70-52 |