Orginal 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 6620-01-426-2220
NSN 5895-00-245-6287
NSN 5920-01-357-0997
NSN 6320-01-364-1840
NSN 5960-00-489-2805
NSN 5895-00-299-0350
NSN 5975-00-144-7878
NSN 6320-01-495-0512
NSN 6240-01-158-3562
NSN 5905-01-060-9092
NSN 5910-01-258-2123
NSN 6130-01-150-8388