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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Main Authors | , , |
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Format | Patent |
Language | English French German |
Published |
24.09.2008
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Subjects | |
Online Access | Get full text |
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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. |
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Bibliography: | Application Number: EP20070254846 |