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METHOD OF COATING CORNER INTERFACE OF TURBINE SYSTEM

United States Patent Application

20130323430
A1
View the Complete Application at the US Patent & Trademark Office
A method of coating a corner interface of a turbine system includes placing a mesh assembly proximate the corner interface. The method also includes depositing a coating onto and through the mesh assembly and into the corner interface, wherein the mesh assembly dampens a kinetic energy of the coating and secures the coating proximate the corner interface.
Taxacher, Glenn Curtis (Simpsonville, SC)
GENERAL ELECTRIC COMPANY (Schenectady NY)
13/ 485,237
May 31, 2012
FEDERAL RESEARCH STATEMENT [0001] This application was made with U.S. Government support under Agreement No. DE-FC26-05NT42643 awarded by the Department of Energy. The U.S. Government may have certain rights in this invention.