Metal treatment – Process of modifying or maintaining internal physical... – Surface melting
Patent
1994-07-26
1996-08-27
Simmons, David A.
Metal treatment
Process of modifying or maintaining internal physical...
Surface melting
228119, 22826230, 22826231, B23K 3100
Patent
active
055497675
ABSTRACT:
An improved method is described for repairing Co-base superalloy gas turbine engine components by applying a mixture of base alloy powder and base alloy powder with a melting point depressant to the surface of the component and heating at 2250.degree.-2300.degree. F. to diffuse the melting point depressant isothermally into the base alloy. A protective coating is then applied, during which a heating cycle which ages the base material is used. The resultant component has high temperature creep properties which are significantly better than achieved using the prior art process. The same temperature cycle is also useful in the initial heat treatment of Co-base superalloys, and can also be used for rejuvenation of components which have experienced extensive exposure to engine operating conditions.
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Kurpaska S. Michael
Pietruska Norman
Phipps Margery S.
Simmons David A.
United Technologies Corporation
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