| 发明名称 |
Laminate for gas turbine blades or thermal shield, comprises a substrate, an attachment layer, a zirconium oxide layer stabilized by yttrium, an inner ceramic layer on the metallic attachment layer, and an outer ceramic layer |
| 摘要 |
<p>The laminate (1) for gas turbine blades or thermal shield, comprises a substrate (4), an attachment layer (7), a zirconium oxide layer stabilized by yttrium, an inner ceramic layer (10) on the metallic attachment layer, and an outer ceramic layer (13) having 100 wt.% of pyrochlore.</p> |
| 申请公布号 |
FR2902692(A1) |
申请公布日期 |
2007.12.28 |
| 申请号 |
FR20060011248 |
申请日期 |
2006.12.22 |
| 申请人 |
SIEMENS AKTIENGESELLSCHAFT |
发明人 |
KAISER AXEL;SCHUMANN ECKART;SUBRAMANIAN RAMESH |
| 分类号 |
B32B15/00;C23C30/00 |
主分类号 |
B32B15/00 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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