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 6320-00-994-0179
NSN 6685-00-051-1369
NSN 5855-00-401-3442
NSN 6610-01-451-1217
NSN 4140-01-160-8503
NSN 5996-00-300-4499
NSN 6240-00-353-5753
NSN 5910-00-930-3098
NSN 5920-00-203-5938
NSN 5915-01-261-7839
NSN 6110-00-833-7778
NSN 5915-00-925-2513