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 5935-01-448-1911
NSN 6145-00-441-2512
NSN 5996-01-078-7645
NSN 6320-01-481-7322
NSN 5855-01-020-7982
NSN 5920-01-124-9883
NSN 2925-01-018-1348
NSN 5925-01-168-7370
NSN 6105-00-474-1463
NSN 6610-01-311-5872
NSN 5855-00-494-9581
NSN 6145-00-891-6779