发明名称 |
Light weight shroud fin for a rotor blade |
摘要 |
A turbine blade is provided and includes a tip end carrying a shroud and at least one fin, which extends radially away from the shroud. The fin includes a first sidewall and a second sidewall, which are spaced apart, arranged parallel to each other, and are connected to the shroud, and a cutting edge, which is connected to the first and second sidewalls. The cutting edge thereby creates a hollow space between the sidewalls, the shroud, and the cutting edge, and further extends radially away from the first and second sidewalls. Also provided is a method of manufacturing the blade by casting the blade as single piece with the hollow fin or by forging the blade; and machining the fin to create the first and second sidewalls and cutting edge thereby opening the hollow space between said sidewalls and the cutting edge. |
申请公布号 |
US8967972(B2) |
申请公布日期 |
2015.03.03 |
申请号 |
US201213668136 |
申请日期 |
2012.11.02 |
申请人 |
ALSTOM Technology Ltd. |
发明人 |
Brandl Herbert;Tsypkakyin Igor;Indlekofer Philipp |
分类号 |
F01D5/08;F01D5/02;B23P15/02;F01D5/22;F01D5/18 |
主分类号 |
F01D5/08 |
代理机构 |
Buchanan Ingersoll & Rooney PC |
代理人 |
Buchanan Ingersoll & Rooney PC |
主权项 |
1. A turbine blade comprising a tip end carrying a shroud and at least one fin, which extends radially away from the shroud, the fin comprises a first sidewall and a second sidewall, which are spaced apart from each other, and are connected to the shroud, and a cutting edge, which is connected to the first and second sidewalls, said cutting edge thereby creating a hollow space between the sidewalls, the shroud, and the cutting edge, and further extends radially away from the first and second sidewalls;
wherein the wall thickness of the first and second sidewalls are constant in a radial direction for at least 50% of the sidewall height. |
地址 |
Baden CH |