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 6610-00-071-0057
NSN 5925-01-256-3070
NSN 5975-01-116-2115
NSN 6620-01-215-7682
NSN 4140-00-420-0251
NSN 6645-01-042-4220
NSN 5985-00-812-2402
NSN 6110-00-775-0745
NSN 7035-01-198-1512
NSN 4140-01-295-8264
NSN 5950-00-837-3083
NSN 5920-01-555-5403