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 6620-00-452-5738
NSN 6150-00-296-2361
NSN 6610-00-231-2730
NSN 4140-00-231-9559
NSN 6650-00-484-3389
NSN 5945-01-368-5241
NSN 5990-01-121-1175
NSN 6135-00-686-4777
NSN 5910-01-631-7483
NSN 6145-01-377-4382
NSN 5915-00-294-9295
NSN 5925-01-401-5314