Titanium blades and vanes
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 6620-01-276-9825
NSN 5855-01-553-1162
NSN 5965-00-303-9701
NSN 6135-01-104-1847
NSN 5999-01-343-2531
NSN 6105-01-455-3300
NSN 5855-01-359-0373
NSN 6130-01-422-0128
NSN 6110-01-090-0417
NSN 5935-01-010-8931
NSN 5996-00-489-4756
NSN 5855-01-027-1571