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 6320-01-421-3777
NSN 5965-01-525-3145
NSN 6145-01-179-9547
NSN 5950-01-634-0677
NSN 5895-00-816-9763
NSN 5915-01-199-4481
NSN 5910-01-252-7106
NSN 6145-00-258-3608
NSN 6650-00-001-5407
NSN 5990-01-550-7827
NSN 6620-01-423-7300
NSN 5935-01-634-0668