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 7035-00-299-7150
NSN 6150-00-731-2079
NSN 7035-01-517-1713
NSN 6135-01-026-9960
NSN 5920-01-579-5219
NSN 2925-00-529-8681
NSN 6220-00-414-7528
NSN 6645-00-515-6148
NSN 5935-01-195-8499
NSN 5985-01-526-2228
NSN 6610-00-551-3610
NSN 6150-00-081-2063