Turbine shroud cooling system

Details Turbine shroud cooling system Turbine shroud cooling system

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 11/24 (2006.01) F01D 5/14 (2006.01) F01D 5/22 (2006.01) F01D 25/12 (2006.01) F01D 25/14 (2006.01) F01D 25/26 (2006.01) F02C 7/18 (2006.01)

Patent

CA 2502810

A cooled turbine shroud assembly includes a first cooling path and a second cooling path adapted to provide shroud impingement air at different pressures to enhance efficiency. The cooling air is preferably acquired from a common source of secondary air. In one aspect the assembly, a shroud support supports a shroud ring and the cooling paths are separated in part by a flexible seal.

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