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 6130-01-445-4816
NSN 6240-00-344-8582
NSN 6610-00-148-2922
NSN 6145-01-124-0035
NSN 6145-00-903-4619
NSN 6110-01-564-1383
NSN 5990-01-317-4427
NSN 6320-01-411-6610
NSN 5910-01-118-4691
NSN 5915-01-661-1817
NSN 6105-01-323-1811
NSN 5925-00-550-4946