| 发明名称 |
VIBRATION-DAMPED COMPOSITE AIRFOILS AND MANUFACTURE METHODS |
| 摘要 |
A turbine engine component (100) comprises a fiber structure (125, 126) forming at least a portion of an airfoil (102). A matrix (128) embeds the fiber structure. A carbon nanotube filler (130) is in the matrix. |
| 申请公布号 |
EP3022396(A4) |
申请公布日期 |
2017.03.08 |
| 申请号 |
EP20140826032 |
申请日期 |
2014.06.26 |
| 申请人 |
United Technologies Corporation |
发明人 |
VOLETI, Sreenivasa R.;QUINN, Christopher M. |
| 分类号 |
F01D5/16;F01D5/28;F04D29/02;F04D29/32 |
主分类号 |
F01D5/16 |
| 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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