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 5965-01-267-8536
NSN 6645-01-502-3068
NSN 5985-01-633-6521
NSN 6320-01-381-7023
NSN 5996-00-441-9728
NSN 5990-01-054-4255
NSN 5855-01-252-5424
NSN 5996-01-236-5286
NSN 5960-01-512-0233
NSN 5930-00-439-6661
NSN 6610-00-004-2879
NSN 5950-01-345-1883