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 6685-00-602-7209
NSN 6130-01-288-6365
NSN 5835-01-281-7281
NSN 6645-01-054-7101
NSN 5990-00-186-2445
NSN 2925-01-543-0073
NSN 5915-00-644-0356
NSN 5965-00-946-5156
NSN 5965-01-431-8147
NSN 5965-01-078-1312
NSN 5915-00-823-4980
NSN 6110-00-553-1853