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 6105-01-567-9369
NSN 5855-00-885-8452
NSN 6685-00-484-5721
NSN 6130-01-606-9717
NSN 5925-01-260-5247
NSN 6220-01-234-5200
NSN 5996-01-237-1615
NSN 5935-00-102-1552
NSN 5920-01-247-7424
NSN 5895-01-026-1994
NSN 5965-00-518-0958
NSN 6105-01-388-1926