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 5998-01-178-8565
NSN 6645-01-408-3042
NSN 6150-01-569-2986
NSN 6240-01-611-1005
NSN 6610-00-388-9188
NSN 6105-00-165-3744
NSN 6240-01-104-5693
NSN 5990-00-826-7928
NSN 2925-01-418-3296
NSN 6685-01-013-8915
NSN 6320-01-572-6395
NSN 5925-01-587-4415