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 2925-01-054-3190
NSN 5935-01-649-8215
NSN 6150-00-217-7200
NSN 5950-01-331-7788
NSN 5920-01-276-2282
NSN 5920-01-188-8445
NSN 6220-01-625-9473
NSN 6240-01-656-1126
NSN 6130-01-445-6165
NSN 2925-00-150-7334
NSN 6150-01-009-1335
NSN 6130-01-165-6096