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 6135-01-265-1384
NSN 6110-01-437-8559
NSN 6685-00-110-9800
NSN 5998-00-581-3867
NSN 5910-01-516-5832
NSN 5895-01-548-5188
NSN 6685-00-100-1511
NSN 6110-00-188-9874
NSN 5925-01-171-1833
NSN 6105-00-575-9720
NSN 6135-01-226-4071
NSN 5950-01-619-0938