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 5905-01-416-6483
NSN 7035-01-529-0126
NSN 6150-01-506-5337
NSN 6135-01-025-8109
NSN 5998-01-349-6383
NSN 6105-01-200-4649
NSN 5855-01-217-6857
NSN 5950-01-063-7181
NSN 5985-01-556-9912
NSN 4140-00-517-7902
NSN 6105-01-504-4368
NSN 7035-01-501-5938