| 发明名称 |
TURBOENGINE BLADING MEMBER |
| 摘要 |
A turboengine blading member includes at least one airfoil and at least one platform provided at least one of a base and a tip of the airfoil. The airfoil has a profile body, a leading edge provided at a first side of the profile body, and a trailing edge section extending from a second side of the profile body and opposite the leading edge. The profile body is connected to the at least one platform. The trailing edge section cantilevers from the profile body and is provided without connection to the platform. |
| 申请公布号 |
US2017081961(A1) |
申请公布日期 |
2017.03.23 |
| 申请号 |
US201615271806 |
申请日期 |
2016.09.21 |
| 申请人 |
ANSALDO ENERGIA IP UK LIMITED |
发明人 |
BRANDL Herbert;KRUECKELS Joerg;ZIERER Thomas |
| 分类号 |
F01D5/18;F01D5/30 |
主分类号 |
F01D5/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turboengine blading member, the blading member comprising at least one airfoil and at least one platform provided at at least one of a base and a tip of the airfoil, the airfoil comprising a profile body, a leading edge provided at a first side of the profile body, and a trailing edge section extending from a second side of the profile body and opposite the leading edge, wherein the profile body is connected to the at least one platform, wherein the trailing edge section cantilevers from the profile body and is provided without connection to the platform. |
| 地址 |
London GB |
