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 6620-01-617-3915
NSN 6130-01-153-2265
NSN 5855-00-149-0766
NSN 5975-01-415-3331
NSN 6610-01-408-1134
NSN 5925-00-597-1558
NSN 6645-00-483-1415
NSN 5998-00-733-7717
NSN 5905-01-461-0886
NSN 5920-01-366-4543
NSN 5835-01-580-0446
NSN 5920-01-542-9143