发明名称 Turbine blade
摘要 A blade is provided and includes a platform and a root configured to be connected to a blade carrier. Airfoil portions extend from opposite sides of the platform. Each airfoil portion defines an operating surface being the surface facing the other airfoil portion. An operating surface of one of the airfoil portions defines a suction side and the other operating surface of the other airfoil portion defines a pressure side.
申请公布号 US9017035(B2) 申请公布日期 2015.04.28
申请号 US201012958727 申请日期 2010.12.02
申请人 Alstom Technology Ltd. 发明人 Marmilic Robert;Simon-Delgado Carlos;Brandl Herbert
分类号 F01D5/18;F01D5/14 主分类号 F01D5/18
代理机构 Buchanan Ingersoll & Rooney PC 代理人 Buchanan Ingersoll & Rooney PC
主权项 1. A blade comprising: a platform; and at least one root configured to be connected to a blade carrier, wherein airfoil portions extend from opposite circumferential sides of the platform, each airfoil portion defining an operating surface being a surface facing the other airfoil portion, wherein an operating surface of one of the airfoil portions defines a suction side and the other operating surface of the other airfoil portion defines a pressure side, wherein, when assembled, the two airfoils portions of the blade and another blade adjacent thereto and connected to each other together define an airfoil, and wherein the airfoil portions each extend to a trailing edge of the airfoil and define a gap between a facing edge at the corresponding trailing edge, respectively, the gap extending the length of the trailing edge of the airfoil.
地址 Baden CH
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