Process for repairing wide cracks

A process for repairing cracks in a workpiece (10), such as a turbine engine component, comprises the steps of: providing a workpiece (10) having a crack (12) to be repaired; applying a nickel or cobalt base alloy material (20) to a root of the crack in an amount sufficient to fill a portion of the...

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Bibliographic Details
Main Authors ABRILES, BETH K, MOOR, JAMES J, HYDE, JOHN H
Format Patent
LanguageEnglish
French
German
Published 24.09.2008
Subjects
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Summary:A process for repairing cracks in a workpiece (10), such as a turbine engine component, comprises the steps of: providing a workpiece (10) having a crack (12) to be repaired; applying a nickel or cobalt base alloy material (20) to a root of the crack in an amount sufficient to fill a portion of the crack (12); subjecting the workpiece (10) with the nickel or cobalt base alloy material to a first heat treatment at a temperature in the range of from about 1065,55 to 1260,00°C for a time period in the range of from about 5.0 to 30 minutes; applying a weld material (22) to the crack; and subjecting the workpiece with the weld material to a second heat treatment.
Bibliography:Application Number: EP20070254846