Original name vane, compressor stator, turbine engine
A component of a vane assembly, compressor, aircraft gas turbine engine. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5895-00-355-3327
NSN 2925-01-101-4655
NSN 5945-01-287-3589
NSN 5895-01-186-4368
NSN 6110-01-456-8815
NSN 5930-01-634-0659
NSN 5910-01-525-3725
NSN 5835-01-553-6772
NSN 6145-01-308-2228
NSN 5945-01-214-9527
NSN 2925-01-535-7235
NSN 6240-00-551-3144