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 6150-01-290-9384
NSN 6135-00-057-2005
NSN 5905-01-314-7734
NSN 5925-01-421-9793
NSN 4140-01-261-0032
NSN 6620-01-413-9243
NSN 5996-01-366-4150
NSN 6685-00-128-2318
NSN 5855-01-243-2355
NSN 5920-00-908-1929
NSN 2925-01-629-9416
NSN 6145-01-422-4485