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 5915-01-060-6686
NSN 5915-00-018-8254
NSN 5855-01-258-5161
NSN 5895-01-632-4379
NSN 6645-01-481-4418
NSN 6135-01-351-0361
NSN 2925-01-099-7075
NSN 6645-01-044-6376
NSN 6645-00-884-5845
NSN 5925-01-062-4831
NSN 5985-01-634-0635
NSN 6150-01-407-0415