Rotor diameter is 13.692min to 13.696 max high
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, nonaircraft gas turbine engine and/or the rotor, fan, nonaircraft gas turbine engine through a shaft, turbine, nonaircraft gas turbine engine. It consists of disks, blades, hubs, and the like. It is the moving part of a turbine assembly, nonaircraft gas turbine engine. It has facilities for attaching to a shaft, turbine, nonaircraft gas turbine engine.
Classification: Parts of nonaircraft gas turbines
NSN 6620-00-360-1379
NSN 5999-01-633-3040
NSN 5985-00-869-5347
NSN 6110-01-337-7562
NSN 6110-01-462-0214
NSN 6145-00-369-3880
NSN 5945-01-613-0706
NSN 5895-01-219-0132
NSN 6150-00-013-5613
NSN 5998-01-447-1070
NSN 6105-00-553-8943
NSN 6110-00-012-5514