Gas turbine engine shroud sealing arrangement

Details Gas turbine engine shroud sealing arrangement Gas turbine engine shroud sealing arrangement

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 11/08 (2006.01) F01D 25/24 (2006.01)

Patent

CA 2532704

A ring seal is mounted in the annular gap between a shroud platform overhanging portion and the surrounding shroud support to minimize cooling air leakage through the shroud.

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