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 5925-01-594-1873
NSN 6645-01-251-2613
NSN 6150-00-478-0555
NSN 5835-01-065-2734
NSN 6130-00-882-6161
NSN 5999-00-968-6393
NSN 5915-01-514-8689
NSN 5835-01-360-1058
NSN 6650-01-607-5817
NSN 5925-00-332-9957
NSN 2925-00-928-5931
NSN 6685-00-255-0396