发明名称 Aerofoil tip vortex reducing structure
摘要 For reducing wind turbine tip vortices, each blade tip comprises two or more vanes 3,6 or winglets separated by a gap 7 through which flow that would have formed a vortex core is passed from the upwind to the downwind blade sides. The trailing vane trailing edge is close to the main blade trailing edge. The pressure of fluid passing through the gap falls to the downwind side pressure so flow is ejected in a direction opposite that of blade motion to suppress rapidly revolving vortex core formation. A shroud 10 may cover two vane tips to prevent the formation of secondary vortices. The vane stagger at their roots is greater than that of the main foil and reduces along the length of the vane. The leading vane may be tilted towards the suction surface and the same length or shorter than the trailing vane which may tilt towards the pressure surface.
申请公布号 GB2468903(A) 申请公布日期 2010.09.29
申请号 GB20090005213 申请日期 2009.03.26
申请人 RONALD DENZIL PEARSON 发明人 RONALD DENZIL PEARSON
分类号 F03D1/06;B64C23/06;B64C27/46 主分类号 F03D1/06
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