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 6135-01-351-2690
NSN 5998-01-147-9135
NSN 6150-01-073-0137
NSN 5855-01-338-1718
NSN 4140-01-514-6561
NSN 5998-00-597-7175
NSN 5990-01-529-6347
NSN 5996-01-314-2354
NSN 5930-01-492-8079
NSN 6685-00-067-5968
NSN 6610-01-398-8815
NSN 6620-00-411-4983