PROCESS FOR COATING GAS TURBINE ENGINE COMPONENTS COMPRISING MULTI-PHASE PRE-REACTED THERMAL BARRIER COATINGS AND COATED GAS TURBINE ENGINE COMPONENTS
A process for coating a component (42) including applying a thermal barrier coating material (48) to a bond coat (44) and selectively infiltrating a blocking material (50) into the thermal barrier coating material (48).
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Main Authors | , , |
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Format | Patent |
Language | English French German |
Published |
06.04.2016
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Subjects | |
Online Access | Get full text |
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Summary: | A process for coating a component (42) including applying a thermal barrier coating material (48) to a bond coat (44) and selectively infiltrating a blocking material (50) into the thermal barrier coating material (48). |
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Bibliography: | Application Number: EP20150187651 |