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 5945-00-758-1335
NSN 5985-01-321-5084
NSN 6135-01-388-2761
NSN 6650-01-053-8726
NSN 5920-01-579-2153
NSN 6105-01-514-1743
NSN 5996-00-763-6245
NSN 5835-00-269-2232
NSN 5950-01-441-8711
NSN 5950-01-391-3749
NSN 5920-01-446-4524
NSN 5835-01-157-5886