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 6645-01-620-4837
NSN 5895-01-222-6064
NSN 6620-01-359-0476
NSN 6610-01-199-9367
NSN 5930-01-318-1134
NSN 5975-01-041-8298
NSN 6650-00-193-7358
NSN 6135-01-039-2882
NSN 2925-01-224-1885
NSN 6110-01-034-1687
NSN 5905-00-824-8582
NSN 5935-00-894-4331