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 5950-00-886-8286
NSN 7035-00-238-3662
NSN 5996-01-413-0229
NSN 5999-00-597-5054
NSN 5925-00-421-3012
NSN 2925-01-041-2360
NSN 5999-00-789-9504
NSN 6610-00-658-8359
NSN 5945-01-028-6989
NSN 6240-00-001-9416
NSN 6240-00-072-0352
NSN 5905-00-293-3777