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TURBINE SUPERALLOY COMPONENT DEFECT REPAIR WITH LOW-TEMPERATURE CURING RESIN

United States Patent Application

*** PATENT GRANTED ***
20140044939
9,127,550
A1
View the Complete Application at the US Patent & Trademark Office
Voids, cracks or other similar defects in substrates of thermal barrier coated superalloy components, such as turbine blades or vanes, are filled with resin, without need to remove substrate material surrounding the void by grinding or other processes. The resin is cured at a temperature under 200.degree. C., eliminating the need for post void-filling heat treatment. The void-filled substrate and resin are then coated with a thermal barrier coating.
Hunt, David W. (Orlando, FL), Allen, David B. (Oviedo, FL)
13/ 571,678
August 10, 2012
STATEMENT REGARDING FEDERALLY SPONSORED DEVELOPMENT [0001] Development for this invention was supported in part by Contract No. DE-FC26-05NT42644, awarded by the United States Department of Energy. Accordingly, the United States Government may have certain rights in this invention.