Method of repairing a turbine blade and blade repaired thereby

Metal working – Method of mechanical manufacture – Impeller making

Reexamination Certificate

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C029S889000, C029S889700, C228S119000, C219S137200

Reexamination Certificate

active

06996906

ABSTRACT:
A method of repairing a turbine blade and the blade repaired thereby. The blade comprises a platform that has become bowed as a result of high temperature creep, with the result that the platform has a concave surface and an oppositely-disposed convex surface. The method generally comprises welding the concave surface to build up a weldment on the concave surface, cooling the weldment during which the weldment shrinks, the convex surface becomes flatter, and the concave surface beneath the weldment becomes flatter, and then removing a surface portion of the weldment so as to create a substantially flat weldment surface overlying the substantially straightened concave surface.

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patent: 5554837 (1996-09-01), Goodwater et al.
patent: 5846057 (1998-12-01), Ferrigno et al.
patent: 6154959 (2000-12-01), Goodwater et al.
patent: 6376801 (2002-04-01), Farrell et al.
patent: 6595749 (2003-07-01), Lee et al.
patent: 62-282796 (1987-12-01), None

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