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METHOD OF MAKING A COMBUSTION TURBINE COMPONENT USING THERMALLY SPRAYED TRANSIENT LIQUID PHASE FORMING LAYER

United States Patent Application

20110171394
A1
View the Complete Application at the US Patent & Trademark Office
A method of making a combustion turbine component includes thermal spraying a transient liquid phase (TLP) forming layer onto a combustion turbine component substrate and thermal spraying a main material layer onto the TLP forming layer. The combustion turbine component substrate, TLP forming layer, and main material layer are heat treated to thereby bond the main material layer to the combustion turbine component substrate.
Allen, David B. (Oviedo, FL)
12/ 198,464
August 26, 2008
GOVERNMENT CONTRACT [0001] The U.S. Government has a paid-up license in this invention and the right in limited circumstances to require the patent owner to license others on reasonable terms as provided for by the terms of contract No. DE-FC26-05NT42644 awarded by the Department of Energy.