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 5945-00-204-0041
NSN 6130-00-259-1697
NSN 5960-00-810-3594
NSN 5950-01-431-9068
NSN 5945-00-231-9091
NSN 5935-01-284-9109
NSN 5965-01-006-8613
NSN 6620-00-106-9658
NSN 5910-00-723-9361
NSN 5835-00-092-1136
NSN 7035-01-222-2534
NSN 5895-00-776-6079