| 申请日期 | 2025-08-18 | 申请号 | FR17055211 |
| 公开（公告）号 | FR3067392A1 | 公开（公告）日 | 2018-12-14 |
| 公开国别 | FR | 申请人省市代码 | 全国 |
| 申请人 | SAFRAN | ||
| 简介 | A coated gas turbine engine part includes a substrate and a calcium-magnesium-alumino-silicate (CMAS) protection layer present on the substrate. The protection layer includes a first phase of a calcium-magnesium-alumino-silicate CMAS protection material capable of forming an apatite or anorthite phase in the presence of calcium-magnesium-alumino-silicates CMAS and a second phase including particles of at least one rare-earth REa silicate dispersed in the first phase. | ||
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