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 7035-01-297-5877
NSN 6650-01-367-2949
NSN 6320-01-442-3428
NSN 5999-01-475-9138
NSN 5945-01-149-7382
NSN 5925-00-179-8327
NSN 2925-00-225-5386
NSN 5975-00-633-8532
NSN 6620-00-589-0071
NSN 6220-01-071-9428
NSN 2925-01-127-0167
NSN 5915-01-430-2228