| 发明名称 |
COMPONENT FOR A TURBOMACHINE AND METHOD FOR MANUFACTURING SUCH A COMPONENT |
| 摘要 |
A component for use in an engine in which the component is subjected to at least one of a high temperature, a corrosive atmosphere, an oxidizing atmosphere, a high mechanical load, a cyclic thermal load and transient conditions such that the component is prone to crack formation and propagation. At least one base material includes a self healing system in a form of an added active phase, the self healing system including at least one of a melting point depressant and a substance having a softening or a melting point below or within a range of an operating temperature of the component.
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| 申请公布号 |
US2012251777(A1) |
申请公布日期 |
2012.10.04 |
| 申请号 |
US201213425658 |
申请日期 |
2012.03.21 |
| 申请人 |
DUVAL SOPHIE BETTY CLAIRE;BECKEL DANIEL;GRASSO PIERRO-DANIELE;STANKOWSKI ALEXANDER;SZWEDOWICZ JAROSLAW LESZEK;ALSTOM TECHNOLOGY LTD |
发明人 |
DUVAL SOPHIE BETTY CLAIRE;BECKEL DANIEL;GRASSO PIERRO-DANIELE;STANKOWSKI ALEXANDER;SZWEDOWICZ JAROSLAW LESZEK |
| 分类号 |
B32B5/16;B05D1/10;B32B5/02;B32B15/02;B32B18/00;C09D1/00;H05B6/00 |
主分类号 |
B32B5/16 |
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