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 6150-01-278-6900
NSN 6150-00-261-4889
NSN 5905-01-651-6725
NSN 5935-01-200-0830
NSN 5960-01-142-1995
NSN 5990-01-498-0641
NSN 6150-00-580-0511
NSN 6240-01-608-4401
NSN 6610-00-051-4139
NSN 5998-01-010-2809
NSN 5950-01-317-0109
NSN 6320-01-556-2011