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 4140-01-044-0144
NSN 6150-01-192-1127
NSN 6110-00-614-9218
NSN 6150-01-494-3618
NSN 5960-00-161-3728
NSN 6150-01-462-2642
NSN 6110-00-521-8932
NSN 5996-00-455-8299
NSN 6145-00-800-5985
NSN 5975-01-605-5192
NSN 5855-00-233-2366
NSN 5990-00-351-5479