| 发明名称 |
CMC AIRFOIL WITH SHARP TRAILING EDGE AND METHOD OF MAKING SAME |
| 摘要 |
An airfoil component includes an insert that has angled faces joined at an edge that provides an airfoil trailing edge. An outer CMC fiber layer overlaps the angled faces to provide a trailing edge portion of an airfoil. |
| 申请公布号 |
WO2015041963(A1) |
申请公布日期 |
2015.03.26 |
| 申请号 |
WO2014US55543 |
申请日期 |
2014.09.15 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DUELM, SHELTON O.;MCCAFFREY, MICHAEL G. |
| 分类号 |
F01D5/14;F01D5/18;F01D5/28 |
主分类号 |
F01D5/14 |
| 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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