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)
28JAN 01, 196000-907-062750592 ( ROTOR, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-00-907-0627
Part Number Cage Code Manufacturer
693078-272599ALLIEDSIGNAL INCDBA ALLIED-SIGNAL AEROSPACE CO
TIP00989-11JAN7197403CECOM LR CENTER
693078-299193HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
693078-270210HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
Technical Data | NSN 2835-00-907-0627
Characteristic Specifications
SPECIAL FEATURESMATERIAL 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 LITERATUREAF TO. 2G-GTP70-24,FIG. 14,INDEX 84
END ITEM IDENTIFICATIONGTCP70-52