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 5855-01-329-6087
NSN 5920-01-504-6598
NSN 6320-00-925-0558
NSN 5835-01-654-4570
NSN 6320-01-046-5228
NSN 5855-01-435-5548
NSN 2925-00-735-4979
NSN 5985-01-397-4941
NSN 6645-00-987-3409
NSN 5855-01-571-1557
NSN 5855-01-020-7982
NSN 5998-01-465-0659