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 6240-01-383-7554
NSN 6320-00-433-2773
NSN 5975-01-541-4972
NSN 2925-01-216-4757
NSN 5895-01-077-6977
NSN 2925-01-154-2949
NSN 5990-01-462-1617
NSN 7035-01-556-6961
NSN 5855-01-469-2798
NSN 6110-00-305-2838
NSN 5910-01-367-2738
NSN 6130-01-331-1807