13.77 in.Min; 13978 in.Max legnth of body; first end of shaft 2.740 in.Mininum; 2.750 in.Max lg; end drilled concentric with center of body; 27.64 in.Diameter; 1.344 in.Deep; thread 1/2-13 unc; class 3b to a depth of 1.250 in.; 2ns end of shaft 5.078 in.Length; external thread 1-3/8-12 unf, class 2a, 0.750 in.Diameter of internal drilled bell shape hole; three lobe vane with keyway; center of keyway to coincide with center of lobe
An item consisting of blades, vanes, hubs, pins, etc., attached upon a shaft. The rotor is designed to increase the airflow within the compressor at the proper velocity, pressure, and direction. For rotors used on aircraft engine compressors see rotor,compressor,gas turbine engine.
Classification: Parts nesoi, of compressors other than refrigerating and air conditioning compressors
NSN 6145-01-526-1651
NSN 7035-00-574-4223
NSN 6620-01-442-7951
NSN 5920-01-492-4462
NSN 5905-01-232-1148
NSN 5835-00-373-2671
NSN 5990-00-444-0612
NSN 5998-01-085-1898
NSN 2925-01-093-5479
NSN 6645-01-599-2311
NSN 5985-01-503-8976
NSN 5925-00-454-8068