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 5925-01-492-8354
NSN 5990-01-395-4194
NSN 5999-00-248-7240
NSN 5905-00-144-8471
NSN 6610-01-030-8220
NSN 6145-01-267-9341
NSN 5935-01-285-1349
NSN 6240-00-177-0385
NSN 6240-01-616-5658
NSN 4140-01-488-3969
NSN 5835-00-165-3069
NSN 4140-00-851-2552