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 6220-01-339-5261
NSN 6130-00-725-3383
NSN 5895-01-230-5391
NSN 5998-01-492-6632
NSN 5895-00-518-1593
NSN 6240-01-200-7937
NSN 5930-00-752-7455
NSN 6320-01-481-7322
NSN 5925-01-472-7344
NSN 6320-00-937-5625
NSN 6130-01-250-2822
NSN 5855-01-330-1217