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 6110-00-982-9714
NSN 5935-00-817-3843
NSN 5996-01-045-0955
NSN 5990-01-633-9503
NSN 5925-01-478-3541
NSN 5895-01-302-1206
NSN 5910-01-425-5191
NSN 5998-01-319-7109
NSN 6320-00-456-2092
NSN 5985-01-259-2701
NSN 6110-01-658-9219
NSN 5990-01-287-9447