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 2925-01-299-6967
NSN 5835-00-733-9145
NSN 6105-01-445-4574
NSN 5999-01-278-2813
NSN 5920-01-421-0291
NSN 6650-01-359-8537
NSN 5996-01-449-0666
NSN 5990-00-848-8870
NSN 6220-01-024-5931
NSN 6645-01-324-1956
NSN 6650-00-668-5703
NSN 6685-01-342-8985