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 5910-01-528-1109
NSN 6110-01-296-0742
NSN 5905-01-246-6708
NSN 6135-01-466-0192
NSN 6110-01-113-6569
NSN 5855-01-351-6875
NSN 5930-01-045-4106
NSN 5975-00-003-7844
NSN 5925-01-381-2528
NSN 5945-01-222-0675
NSN 6645-00-413-0461
NSN 5930-00-285-8727