| 申请日期 | 2025-07-17 | 申请号 | CA2626908 |
| 公开（公告）号 | CA2626908C | 公开（公告）日 | 2015-08-11 |
| 公开国别 | CA | 申请人省市代码 | 全国 |
| 申请人 | SNECMA | ||
| 简介 | The process for depositing a thermal barrier on a monocrystalline superalloy (10) that is useful in a part of turbine blade of a turbomachine, comprises directly depositing zirconium on the superalloy. Independent claims are included for : (1) a part having the monocrystalline superalloy; and (2) a turbine blade. | ||
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