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 6135-00-452-2266
NSN 5975-01-544-2235
NSN 5855-00-361-0167
NSN 5999-01-260-5256
NSN 5835-00-221-1005
NSN 5920-01-435-5091
NSN 6320-00-937-5625
NSN 5905-01-589-1569
NSN 6105-01-056-5258
NSN 5910-00-452-5957
NSN 5905-00-350-4105
NSN 6145-00-434-1681