| 发明名称 |
SYSTEMS AND METHOD FOR A COMPOSITE BLADE WITH FILLET TRANSITION |
| 摘要 |
A system includes a turbomachine blade segment including an airfoil with an exterior surface, and a platform coupled to the airfoil having a first side and a second side. The system also includes a concave fillet transition extending between the airfoil and the platform. The concave fillet transition includes one or more interface ply segments extending across the exterior surface of the airfoil and the first or the second side of the platform to form a continuous surface between the airfoil and the platform. |
| 申请公布号 |
US2014271208(A1) |
申请公布日期 |
2014.09.18 |
| 申请号 |
US201313842639 |
申请日期 |
2013.03.15 |
| 申请人 |
General Electric Company |
发明人 |
Garcia-Crespo Andres Jose;de Diego Peter |
| 分类号 |
F01D5/30 |
主分类号 |
F01D5/30 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system, comprising:
a turbomachine blade segment, comprising:
an airfoil comprising an exterior surface;a platform coupled to the airfoil, the platform comprising a first side and a second side; anda concave fillet transition extending between the airfoil and the platform, wherein the concave fillet transition comprises one or more interface ply segments extending across the exterior surface of the airfoil and the first or the second side of the platform to form a continuous surface between the airfoil and the platform. |
| 地址 |
US |
