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 5935-01-129-4882
NSN 5965-00-763-8015
NSN 5999-01-444-1389
NSN 7035-00-834-2090
NSN 5985-01-020-6356
NSN 6645-01-142-2416
NSN 5990-00-497-9234
NSN 6645-01-083-4759
NSN 6240-01-004-7515
NSN 6130-01-230-8391
NSN 2925-01-159-8312
NSN 5855-01-497-0467