| 发明名称 |
Product, especially a gas turbine component, with a ceramic heat insulating layer |
| 摘要 |
The invention relates to a product (1), particularly a gas turbine blade that can be exposed to a hot aggressive gas (7). The product (1) has a metallic basic body (2), which is provided with a thermal barrier coating (4) having a spinel of the composition AB2O4.
|
| 申请公布号 |
US6764771(B1) |
申请公布日期 |
2004.07.20 |
| 申请号 |
US20000530653 |
申请日期 |
2000.12.22 |
| 申请人 |
SIEMENS AKTIENGESELLSCHAFT |
发明人 |
HEIMBERG BEATE;BEELE WOLFRAM;KEMPTER KARL;BAST ULRICH;HAUBOLD THOMAS;HOFFMANN MICHAEL;ENDRISS AXEL;GREIL PETER;HONG CHU-WAN;ALDINGER FRITZ;SEIFERT HANS J. |
| 分类号 |
C23C4/10;C23C30/00;F01D5/28;(IPC1-7):C23C30/00 |
主分类号 |
C23C4/10 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
