| 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 |
US2016230569(A1) |
申请公布日期 |
2016.08.11 |
| 申请号 |
US201415022631 |
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 |
F01D5/28;F01D5/14 |
主分类号 |
F01D5/28 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An airfoil component comprising:
an insert having angled faces joined at an edge that provides an airfoil trailing edge; and an outer CMC fiber layer overlapping the angled faces to provide a trailing edge portion of an airfoil. |
| 地址 |
Hartford CT US |
