A stationary arched metal segment used to establish clearance and a seal for the tip of a blade, turbine rotor, aircraft gas turbine engine. The inner dimension may have open honeycomb or composition filled surface or may be formed by the knife edge metal protrusions of a seal ring, labyrinth, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 6135-01-512-8740
NSN 6240-00-004-2516
NSN 5920-00-180-4278
NSN 5910-00-989-6531
NSN 5920-01-068-3135
NSN 5996-01-384-2115
NSN 5905-00-446-1985
NSN 5935-00-732-0545
NSN 5975-01-506-4240
NSN 6135-01-597-7685
NSN 6650-01-556-3508
NSN 6110-01-086-2607