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 6105-01-338-7761
NSN 5835-01-424-0054
NSN 5915-01-380-8723
NSN 5985-01-112-6382
NSN 5920-00-471-2548
NSN 5905-01-457-2332
NSN 5950-01-607-4000
NSN 5950-01-012-3939
NSN 5895-00-280-2155
NSN 5915-01-590-4900
NSN 5960-00-101-5461
NSN 5920-01-341-2094