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 6620-01-531-3250
NSN 6145-01-587-4358
NSN 2925-01-435-9057
NSN 5965-01-432-1943
NSN 6610-01-433-6935
NSN 6610-01-176-3539
NSN 5975-00-862-4506
NSN 6105-00-112-0967
NSN 2925-01-106-8871
NSN 5965-00-577-1242
NSN 6650-01-260-7427
NSN 6685-01-487-3799