Original name compressor rotor, axial, turbine engine
A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. it consists of disks, blades, hubs, and the like. it is the moving part of compressor, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 6240-01-651-2850
NSN 5998-01-202-7905
NSN 6320-01-630-7629
NSN 7035-01-364-0286
NSN 5835-00-269-2232
NSN 6105-00-476-0058
NSN 5905-01-287-4398
NSN 5910-00-239-2145
NSN 5915-01-067-8365
NSN 6110-00-469-7981
NSN 6145-00-434-1681
NSN 5930-00-849-6659