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 6620-01-595-2113
NSN 5895-01-119-7141
NSN 5855-01-484-3619
NSN 5945-00-577-0424
NSN 5935-01-647-2948
NSN 6105-00-399-0574
NSN 6145-01-459-7837
NSN 5935-01-495-2404
NSN 6130-01-557-9698
NSN 5975-00-213-7952
NSN 5895-00-552-1259
NSN 6320-01-516-3836