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HOT GAS PATH COMPONENT FOR TURBINE SYSTEM

United States Patent Application

20130094971
A1
View the Complete Application at the US Patent & Trademark Office
A hot gas path component for a turbine system is disclosed. The hot gas path component includes a shell having an exterior surface and an interior surface. The hot gas path component further includes a porous medium having an exterior surface and an interior surface, the exterior surface positioned adjacent to the interior surface of the shell. The porous medium is configured for flowing a cooling medium therethrough.
Lacy, Benjamin Paul (Greer, SC), Brzek, Brian Gene (Clifton Park, NY), Malish, Rebecca Christine (Schenectady, NY)
GENERAL ELECTRIC COMPANY (Schenectady NY)
13/ 271,724
October 12, 2011
[0001] This invention was made with government support under contract number DE-FC26-05NT42643 awarded by the Department of Energy. The government has certain rights in the invention.