Orig name turbine rotor, turbine engine; dual rotors, variable stator, high bypass fan
A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of a fan, aircraft gas turbine engine. It has facilities for attachment to a shaft, turbine, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5975-01-542-9066
NSN 5999-00-243-9820
NSN 5950-01-419-2850
NSN 2925-01-027-1293
NSN 5945-01-014-6378
NSN 5895-01-492-0077
NSN 5990-01-173-7238
NSN 7035-00-300-3208
NSN 5945-00-895-8017
NSN 5990-00-127-2306
NSN 4140-01-103-3377
NSN 5910-01-606-4490