| 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 |
US2016130952(A1) |
申请公布日期 |
2016.05.12 |
| 申请号 |
US201414903076 |
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 |
F01D5/26;F01D9/04;F01D5/28 |
主分类号 |
F01D5/26 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbine engine component (100) comprising:
a fiber structure (125, 126) forming at least a portion of an airfoil (102); a matrix (128) embedding the fiber structure; and a carbon nanotube filler (130) in the matrix. |
| 地址 |
Hartford CT US |
