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 6145-01-439-2662
NSN 7035-01-521-3449
NSN 5999-00-017-6957
NSN 6105-00-246-7116
NSN 5996-01-164-8266
NSN 6135-01-390-1841
NSN 6645-01-023-8020
NSN 5905-00-734-6386
NSN 5855-00-933-8286
NSN 5990-01-602-6701
NSN 6145-01-648-1491
NSN 5895-01-171-0974