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Repair process for coated articles

A non-coating and coating technology, applied in coating, manufacturing tools, engine manufacturing, etc., can solve problems such as difficult joints, difficult to properly coat, long spraying time, etc.

Inactive Publication Date: 2008-01-23
GENERAL ELECTRIC CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For example, there will be overspray at the edge of the part to be filled, the manipulator has limited vision and cannot reach certain areas, the seam between the original coating and the repair patch is difficult to fit closely, elements with complex geometries (such as propellers, blades and shrouds) are difficult to apply properly and / or time-consuming and costly to apply

Method used

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  • Repair process for coated articles
  • Repair process for coated articles
  • Repair process for coated articles

Examples

Experimental program
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Embodiment Construction

[0013] The present invention discloses a method for repairing a damaged portion of a coating on a metal component. Damage to the coating can be in the form of spalling, oxidation, cracking, corrosion and / or abrasion. Referring now to FIG. 1 , an exemplary process flow diagram, generally indicated at 10 , is shown. The method 10 generally includes sintering a mixture comprising particles of a brazing alloy and particles of a coating composition to form a composite preform 12; placing the composite preform on an uncoated (due to damage) surface 14 of a metal component and heating the metal element and / or preform to a temperature 16 effective to form a brazed joint between the preform and the metal element. Advantageously, the method disclosed herein can significantly reduce the number and cost of overhaul cycles while allowing the coated metal component to have coating integrity and reliability. Another advantageous feature of the disclosed method is that the joint between the...

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Abstract

A process for repairing a metal component includes sintering a mixture comprising particles of a coating composition and particles of a brazing alloy to form a composite preform; disposing the composite preform on an uncoated surface of the metal component; and heating the preform to a temperature effective to form a brazed joint between the composite preform and the metal component.

Description

technical field [0001] The present disclosure generally relates to methods of repairing damaged portions of coated metal components. More specifically, it relates to methods of repairing damaged portions of coatings on turbine engine components. Background technique [0002] Metal components are used in a wide variety of industrial applications under different operating conditions. In many cases, the components have coatings that impart various properties, such as corrosion resistance, heat resistance, oxidation resistance, and / or wear resistance. For example, various components of a turbine engine, typically capable of withstanding operating temperatures of about 1100 degrees Celsius (° C.) to about 1150° C., are often coated with a thermal barrier coating (TBC) to effectively increase the temperature at which they can operate. Typically, the TBC is applied over an intermediate bond coat (sometimes referred to as a "bond coat," "stick coat," or "bond coat") that is applie...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23P6/00B23K1/00
CPCF01D5/005B23P6/005F05B2230/31B23K1/0018F05D2230/22F05D2230/31F05D2230/237B23K2201/001F01D5/288Y02T50/67F05B2230/237C23C4/005Y02T50/672C23C26/02F05B2230/22B23K2101/001C23C4/01Y02T50/60
Inventor D·V·布奇W·M·米利蒂M·D·阿尔内特
Owner GENERAL ELECTRIC CO