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 6135-01-584-0941
NSN 5930-01-500-5735
NSN 6220-01-381-0081
NSN 6645-00-099-6913
NSN 5975-01-123-4209
NSN 6240-01-577-0267
NSN 5945-00-460-4476
NSN 5910-00-543-1958
NSN 6645-01-191-9515
NSN 4140-01-477-7600
NSN 6645-00-004-8628
NSN 6620-00-043-6082