Was compressor rotor, axial, turbine engine; dual rotors, 9 stages; high bypass fan
A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. It consists of disks, blades, hubs, and the like. It is the moving part of a turbine assembly, 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 6240-01-350-3533
NSN 5960-01-486-3060
NSN 6145-01-274-6190
NSN 5920-01-270-7795
NSN 6130-01-461-3145
NSN 5999-01-224-7003
NSN 5985-01-064-0037
NSN 6650-01-066-7272
NSN 5935-01-533-7443
NSN 6650-01-260-8690
NSN 5920-01-044-9021
NSN 6145-00-635-9957