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 5905-01-268-0498
NSN 5930-01-469-5426
NSN 6220-01-168-5108
NSN 6240-01-610-8705
NSN 6645-01-356-5663
NSN 5975-01-311-2520
NSN 5920-01-246-4330
NSN 5855-00-494-9581
NSN 6620-00-052-3277
NSN 5895-01-333-2375
NSN 6645-01-515-5756
NSN 6135-01-278-9717