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 5990-01-132-4156
NSN 5999-01-175-0032
NSN 6620-00-248-6950
NSN 5835-01-221-8030
NSN 6150-01-233-6612
NSN 5985-00-451-9823
NSN 5945-01-189-1878
NSN 6240-00-919-9186
NSN 5965-00-284-6718
NSN 5915-01-471-2012
NSN 6105-01-449-1046
NSN 6130-01-202-8025