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 5910-01-418-2399
NSN 6650-01-483-0938
NSN 6150-01-274-6349
NSN 5920-01-284-1786
NSN 6685-00-138-0692
NSN 7035-01-504-3462
NSN 5975-00-971-4897
NSN 5985-01-204-4503
NSN 4140-01-066-6891
NSN 5910-01-142-0070
NSN 6320-01-512-2031
NSN 5945-01-427-3790