| 发明名称 |
COMPRESSED CHOPPED FIBER COMPOSITE STRUCTURAL GUIDE VANE |
| 摘要 |
The present disclosure relates generally to the field of guide vanes for gas turbine engines. More specifically, the present disclosure relates to a compressed chopped fiber structural guide vane for a gas turbine engine. |
| 申请公布号 |
US2016160680(A1) |
申请公布日期 |
2016.06.09 |
| 申请号 |
US201414540664 |
申请日期 |
2014.11.13 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Turner Matthew A.;Alarcon Andrew G.;Bugaj Shari L.;Levasseur Glenn |
| 分类号 |
F01D25/00;F01D25/04;F01D9/04 |
主分类号 |
F01D25/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A structural guide vane for a gas turbine engine comprising:
an airfoil including an axial leading edge and an axial trailing edge; wherein the airfoil is composed of a compressed chopped fiber composite. |
| 地址 |
Farmington CT US |
