Wind turbine blade with submerged boundary layer control means
    31.
    发明授权
    Wind turbine blade with submerged boundary layer control means 失效
    具有淹没边界层控制装置的风力发电机叶片

    公开(公告)号:US08579594B2

    公开(公告)日:2013-11-12

    申请号:US12733362

    申请日:2008-08-29

    Abstract: A wind turbine blade having a longitudinal direction with a root end and a tip end as well as a chord extending in a transverse direction between a leading edge and a trailing edge is described. The blade comprises a flow control surface with a suction side and a pressure side. A number of boundary layer control means is formed in the flow control surface. The boundary layer control means include a channel submerged in the flow control surface with a first end facing towards the leading edge and a second end facing towards the trailing edge of the blade. The channel comprises: a bottom surface extending from the first end to the second end, a first sidewall extending between the flow control surface and the bottom surface and extending between the first end and the second end, the first sidewall forming a first sidewall edge between the first side wall and the flow control surface, and a second sidewall extending between the flow control surface and the bottom surface and extending between the first end and the second end, the second sidewall forming a second sidewall edge between the second side wall and the flow control surface. The channel at the first end comprises a first flow accelerating channel zone adapted for accelerating a flow, and at the second end comprises a second channel zone, where the first sidewall and the second sidewall are diverging towards the trailing edge of the blade.

    Abstract translation: 描述了具有根端和尖端的纵向方向的风力涡轮机叶片以及在前缘和后缘之间沿横向方向延伸的弦线。 叶片包括具有吸力侧和压力侧的流动控制表面。 在流量控制面上形成有多个边界层控制装置。 边界层控制装置包括浸没在流量控制表面中的通道,其具有面向前缘的第一端和面向叶片后缘的第二端。 所述通道包括:从所述第一端延伸到所述第二端的底表面,在所述流动控制表面和所述底部表面之间延伸并在所述第一端和所述第二端之间延伸的第一侧壁,所述第一侧壁在第一侧壁之间形成第一侧壁边缘, 所述第一侧壁和所述流动控制表面以及在所述流动控制表面和所述底部表面之间延伸并在所述第一端和所述第二端之间延伸的第二侧壁,所述第二侧壁在所述第二侧壁和所述第二侧壁之间形成第二侧壁边缘, 流量控制面。 第一端处的通道包括适于加速流动的第一流动加速通道区域,并且在第二端部包括第二通道区域,其中第一侧壁和第二侧壁朝向叶片的后缘发散。

    Wind Turbine Blade with Narrow Shoulder and Relatively Thick Airfoil Profiles
    32.
    发明申请
    Wind Turbine Blade with Narrow Shoulder and Relatively Thick Airfoil Profiles 有权
    风力发电机叶片具有狭窄的肩膀和相对厚的翼型

    公开(公告)号:US20130115098A1

    公开(公告)日:2013-05-09

    申请号:US13810049

    申请日:2010-07-16

    Abstract: A blade (10) for a rotor of a wind turbine having a profiled contour divided into: a root region (30), an airfoil region (34), and a transition region (32) between the root region (30) and the airfoil region (34). A shoulder (40) is located at the boundary between the transition region (32) and the airfoil region (34). The blade's profiled contour comprises a local relative thickness defined as the local ratio between a maximum profile thickness (t) and the chord length (c). The ratio between the shoulder width (W) and the blade length (L) being less than or equal to 0.075, and the relative thickness (t/c) in a blade length interval of 0-0.8L is at least 22%.

    Abstract translation: 一种用于风力涡轮机转子的叶片(10),其具有轮廓轮廓,分为:根部区域(30),翼型区域(34)和根部区域(30)和翼型件之间的过渡区域(32) 区域(34)。 肩部(40)位于过渡区域(32)和翼型区域(34)之间的边界处。 叶片的轮廓轮廓包括局部相对厚度,其定义为最大轮廓厚度(t)和弦长(c)之间的局部比。 肩宽(W)和叶片长度(L)之间的比率小于或等于0.075,叶片长度间隔为0-0.8L的相对厚度(t / c)至少为22%。

    WIND TURBINE BLADE PROVIDED WITH FLOW ALTERING DEVICES
    34.
    发明申请
    WIND TURBINE BLADE PROVIDED WITH FLOW ALTERING DEVICES 有权
    风力涡轮叶片提供流动变换装置

    公开(公告)号:US20120057984A1

    公开(公告)日:2012-03-08

    申请号:US13320946

    申请日:2010-05-18

    Abstract: A blade for a rotor of a wind turbine is divided into a root region closest to the hub and an airfoil region with a lift generating profile furthest away from the hub and a transition region. A base part of the transition region has an axial induction factor, which without flow altering device deviates at least 5% from a target axial induction factor. A number of first flow altering devices are arranged so as to adjust the aerodynamic properties of a longitudinal segment of the transition region to substantially meet the target axial induction factor.

    Abstract translation: 用于风力涡轮机的转子的叶片被分成最靠近轮毂的根部区域和具有离轮毂最远的升力产生轮廓的翼型区域和过渡区域。 过渡区域的基本部分具有轴向感应系数,其没有流动改变装置偏离目标轴向感应系数至少5%。 多个第一流动改变装置被布置成调节过渡区域的纵向段的空气动力特性以基本上满足目标轴向感应系数。

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