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 5935-01-569-3129
NSN 5975-01-010-4887
NSN 5998-01-145-5199
NSN 5965-00-170-5254
NSN 6145-00-574-1152
NSN 2925-00-137-5120
NSN 6240-01-457-3372
NSN 5990-00-318-3990
NSN 6610-01-425-1523
NSN 6650-01-609-1993
NSN 6645-01-605-1485
NSN 5895-01-325-5598