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 7035-00-009-8705
NSN 5960-00-752-6175
NSN 6620-00-439-2442
NSN 6610-00-146-3499
NSN 6620-00-663-8962
NSN 7035-01-222-0729
NSN 5985-01-613-2382
NSN 6240-01-067-1494
NSN 6610-01-211-0835
NSN 6685-00-723-8814
NSN 5935-01-596-5821
NSN 6110-00-308-3993