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 5920-00-501-7834
NSN 5855-00-133-5897
NSN 5960-01-522-0391
NSN 6650-01-110-2142
NSN 5905-01-094-6735
NSN 5998-00-862-7299
NSN 5950-00-862-5278
NSN 6110-00-747-9269
NSN 6145-00-780-4510
NSN 5965-01-278-2107
NSN 6150-00-456-0421
NSN 5985-01-337-0291