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publicationDate 1998-04-07-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-5735448-A
titleOfInvention Method of repairing surface and near surface defects in superalloy articles such as gas turbine engine components
abstract A repair coating for superalloy articles, such as gas turbine engine components, includes a volatile organic carrier or water-based carrier, a fluxing agent, a thickening agent, balance a filler mix. The filler mix consists of at least two distinct particulate components. The mix includes a first particulate component having a composition which approximates that of the article being repaired. The mix also includes a second particulate component having a composition approximating that of the article and a melting point depressant, such as boron. This melting point depressant is substantially in excess of that in the article and sufficient to provide melting of a portion of the mix at a processing temperature below the melting temperature of the article. The above filler mix is blended with the other constituents to form the repair coating which is applied to an article. A series of heating/cooling cycles is performed to ensure that the repair cooling properly melts, wets, and bonds to the article and that the melting point depressant diffuses into the article.
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