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 6110-01-188-8017
NSN 7035-01-508-5064
NSN 5985-01-382-9220
NSN 5920-01-589-2844
NSN 6105-00-197-2128
NSN 6620-00-245-3242
NSN 6110-00-738-3400
NSN 5965-01-222-1420
NSN 6620-01-599-2011
NSN 6650-00-373-9220
NSN 6130-01-087-9669
NSN 6645-01-193-8607