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 5935-01-584-1741
NSN 6320-01-228-2380
NSN 6150-00-281-9482
NSN 5925-00-279-3479
NSN 6130-00-596-6695
NSN 6105-01-498-4994
NSN 5998-01-014-1008
NSN 6105-00-159-7801
NSN 6650-00-456-1736
NSN 5915-01-462-5900
NSN 5999-00-276-3782
NSN 6130-01-610-8670