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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Bibliographic Details
Main Authors READ, KATHRYN S, ZALESKI, ELISA M, BOCHIECHIO, MARIO P
Format Patent
LanguageEnglish
French
German
Published 06.04.2016
Subjects
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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).
Bibliography:Application Number: EP20150187651