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 5985-01-081-5251
NSN 6650-01-495-1269
NSN 5915-00-994-5087
NSN 6220-01-284-3963
NSN 6320-01-431-4359
NSN 6105-01-406-1425
NSN 6220-00-412-2741
NSN 5945-01-281-7259
NSN 5905-00-119-9114
NSN 6220-01-288-8582
NSN 5996-01-212-9866
NSN 6110-01-581-3148