CERAMIC COATING SYSTEM AND METHOD
A gas turbine engine article includes a substrate (80) and a bond coating (82; 182) that covers at least a portion of the substrate (80) with a step (86; 186) formed in at least one of the substrate (80) and the bond coating (82; 182). A thermally insulating topcoat (84; 184) is disposed on the bond...
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Main Authors | , |
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Format | Patent |
Language | English French German |
Published |
30.06.2021
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Subjects | |
Online Access | Get full text |
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Summary: | A gas turbine engine article includes a substrate (80) and a bond coating (82; 182) that covers at least a portion of the substrate (80) with a step (86; 186) formed in at least one of the substrate (80) and the bond coating (82; 182). A thermally insulating topcoat (84; 184) is disposed on the bond coating (82; 182). The thermally insulating topcoat (84; 184) includes a first topcoat portion (92) separated by at least one fault (98; 198) that extends through the thermally insulating topcoat (84; 184) from a second topcoat portion (96). |
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Bibliography: | Application Number: EP20150180090 |