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 5855-01-414-6265
NSN 5895-00-112-8767
NSN 5985-01-048-1676
NSN 5999-01-390-2012
NSN 5905-01-652-3073
NSN 4140-01-100-1223
NSN 6130-01-624-9826
NSN 5998-01-589-7744
NSN 6240-01-658-9176
NSN 5998-01-564-5881
NSN 6610-01-491-6226
NSN 6620-00-530-3939