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 4140-01-284-6485
NSN 6620-00-267-5273
NSN 5950-01-648-2677
NSN 6135-01-171-9299
NSN 6145-00-987-3401
NSN 5996-00-832-6020
NSN 5950-01-073-5630
NSN 5895-00-056-8573
NSN 5965-00-035-4556
NSN 5960-00-018-3477
NSN 6110-00-004-8883
NSN 6150-01-181-5612