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 4140-01-628-2318
NSN 5975-00-216-4848
NSN 6645-01-400-2119
NSN 5998-00-809-9835
NSN 5999-00-496-6069
NSN 5855-01-203-4719
NSN 6320-01-592-6248
NSN 5895-01-168-9754
NSN 5915-01-466-8148
NSN 5915-01-659-5345
NSN 6645-01-175-9875
NSN 6620-00-453-8180