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 6610-01-382-7894
NSN 6645-01-030-8930
NSN 5925-01-655-4865
NSN 4140-01-596-0580
NSN 6645-01-646-2953
NSN 5960-01-181-2143
NSN 5910-01-062-7353
NSN 6220-01-194-1574
NSN 6650-00-504-2999
NSN 5920-01-301-7144
NSN 5960-00-289-6591
NSN 6110-00-244-1354