Rim seal for a gas turbine engine

Details Rim seal for a gas turbine engine Rim seal for a gas turbine engine

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 11/12 (2006.01) F02C 7/28 (2006.01)

Patent

CA 2598329

The rim seal is positioned in an annular space between blades and a non- rotating adjacent structure in a gas turbine engine. The rim seal is connectable to the non--rotating structure and is made of an abradable material.

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