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 5999-01-095-6749
NSN 5925-01-150-1830
NSN 6145-01-647-4096
NSN 5998-01-237-0260
NSN 6240-01-339-5100
NSN 6650-01-047-6719
NSN 5965-00-117-4214
NSN 6645-00-503-1379
NSN 5990-01-575-3275
NSN 6105-00-606-8545
NSN 5935-01-612-1021
NSN 5905-00-795-3677