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 6130-01-358-6814
NSN 7035-01-089-4485
NSN 6135-00-377-9165
NSN 7035-01-344-0209
NSN 5925-01-119-7888
NSN 5920-00-885-0367
NSN 5915-00-587-7215
NSN 4140-00-466-9268
NSN 2925-00-626-5027
NSN 6110-01-333-7012
NSN 5998-00-372-6047
NSN 5999-01-659-0116