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 5910-00-931-0212
NSN 5996-01-362-6399
NSN 5950-01-410-7685
NSN 6610-00-800-2897
NSN 6145-00-819-0062
NSN 5935-01-297-4851
NSN 7035-01-440-8877
NSN 6145-01-505-8959
NSN 5975-01-246-5308
NSN 5950-01-123-1320
NSN 6240-00-910-3297
NSN 5999-00-740-8259