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 6650-01-484-2136
NSN 5935-01-240-4670
NSN 6620-01-104-5758
NSN 6610-01-211-6182
NSN 5905-00-444-8759
NSN 6645-01-108-7904
NSN 5990-01-208-4322
NSN 6220-00-379-4044
NSN 6320-00-931-4855
NSN 5965-00-156-7372
NSN 5950-01-136-0338
NSN 5925-01-386-3178