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 6685-01-610-7191
NSN 5975-01-573-3312
NSN 5910-01-138-6313
NSN 2925-00-211-4469
NSN 6620-01-572-2493
NSN 5905-01-037-7547
NSN 5925-01-191-6498
NSN 6610-00-664-2190
NSN 6130-01-568-1584
NSN 5925-00-144-0482
NSN 2925-00-088-6790
NSN 5915-01-414-2442