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 6105-01-444-3418
NSN 5965-00-560-5804
NSN 6650-00-078-5773
NSN 6220-01-351-1555
NSN 5965-01-566-7184
NSN 6620-01-431-9176
NSN 6105-01-598-7590
NSN 2925-00-233-5644
NSN 6150-01-024-9952
NSN 2925-01-343-5887
NSN 6610-01-109-6405
NSN 7035-00-763-6180