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