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 4140-01-300-4151
NSN 5998-01-107-8674
NSN 6320-01-036-2598
NSN 5950-01-300-4078
NSN 6110-01-419-4351
NSN 6130-01-287-9841
NSN 5930-01-547-0628
NSN 6320-00-174-1362
NSN 7035-00-421-8710
NSN 5975-01-335-4250
NSN 5960-00-987-1897
NSN 6220-01-200-6461