Original name hub, compressor rotor, turbine engine
A component of a rotor, compressor, aircraft gas turbine engine. it is designed to attach to the front and/or rear of the rotor providing support, alignment, and a means of attachment for a shaft, turbine, aircraft gas turbine engine. it may have provisions for installing bearings, and/or oil and air seals. see also disk and hub, compressor, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 6110-01-227-2617
NSN 5855-01-371-6790
NSN 6620-00-114-2837
NSN 5935-01-194-6464
NSN 6650-00-312-1200
NSN 4140-00-733-7936
NSN 6650-01-158-6888
NSN 5985-01-069-8566
NSN 6645-01-058-3817
NSN 5998-01-485-5542
NSN 5985-01-016-6928
NSN 5998-01-373-7933