发明名称 ROTOR BLADE FENCE FOR A WIND TURBINE
摘要 The present invention is directed to a rotor blade assembly for a wind turbine. The rotor blade assembly includes a rotor blade extending from a blade root to a blade tip. The rotor blade has a pressure side surface and a suction side surface. The pressure side surface and the suction side surface each extend between a leading edge and a trailing edge. The assembly also includes a blade root extension configured to attach to one of the pressure side surface or the suction side surface of the rotor blade adjacent to the blade root. The blade root extension includes at least one blade fence and at least one airflow modifying element. The blade fence extends between a proximal end and a distal end in a chord-wise direction. The proximal end is configured to attach to the rotor blade such that the distal end remains free and spaced apart from the rotor blade. The airflow modifying element is configured at the proximal end of the blade fence. As such, the blade root extension is configured to improve aerodynamic performance of the rotor blade.
申请公布号 US2015132138(A1) 申请公布日期 2015.05.14
申请号 US201314077300 申请日期 2013.11.12
申请人 General Electric Company 发明人 Herr Stefan;Nanukuttan Biju;Srikanta Santhosha Yelwal;Prabhu Karthick
分类号 F01D5/12 主分类号 F01D5/12
代理机构 代理人
主权项 1. A rotor blade assembly for a wind turbine, the rotor blade assembly comprising: a rotor blade extending from a blade root to a blade tip, the rotor blade having a pressure side surface and a suction side surface, the pressure side surface and the suction side surface each extending between a leading edge and a trailing edge; and, a blade root extension configured to attach to one of the pressure side surface or the suction side surface of the rotor blade adjacent to the blade root, the blade root extension comprising at least one blade fence and at least one airflow modifying element, the blade fence extending between a proximal end and a distal end in a chord-wise direction, the proximal end configured to attach to the rotor blade such that the distal end remains free and spaced apart from the rotor blade, the airflow modifying element configured at the proximal end of the blade fence, wherein the blade root extension is configured to improve aerodynamic performance of the rotor blade.
地址 Schenectady NY US