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 5999-01-044-1469
NSN 5950-00-941-9463
NSN 6240-01-207-2120
NSN 5975-01-125-1830
NSN 5930-01-397-7674
NSN 6105-01-012-0965
NSN 6145-00-968-6603
NSN 5998-00-148-6198
NSN 5975-01-051-7434
NSN 7035-01-351-4111
NSN 6135-00-120-1027
NSN 7035-00-803-3056