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    • 17. 发明公开
    • Wind turbine blade comprising vortex generators
    • Windturbinenschaufel mit Wirbelerzeugern
    • EP2548801A1
    • 2013-01-23
    • EP11175052.7
    • 2011-07-22
    • LM Wind Power A/S
    • Madsen, Jesper
    • B64C23/06F03D1/06F03D7/02F03D11/00
    • F03D1/0675F05B2240/32Y02E10/721
    • Disclosed is a wind turbine blade and a method for retrofitting a wind turbine blade, the wind turbine blade extending in a longitudinal direction along a pitch axis and having a tip end and a root end as well as a blade length, the wind turbine blade further comprising a profiled contour including a pressure side and a suction side, as well as a leading edge and a trailing edge with a chord having a chord length extending there between, the profiled contour, when being impacted by an incident airflow generating a lift, wherein the suction side of the wind turbine blade is provided with a plurality of vortex generators positioned along a mounting line having a proximal end point nearest the root end and a distal end point nearest the tip end, wherein the mounting line is a concave line seen from the trailing edge of the wind turbine blade.
    • 公开了一种风力涡轮机叶片和用于改装风力涡轮机叶片的方法,所述风力涡轮机叶片沿着俯仰轴线在纵向方向上延伸并且具有尖端和根端以及叶片长度,所述风力涡轮机叶片进一步 包括具有压力侧和吸力侧的轮廓轮廓,以及前缘和后缘,所述前缘和后缘在被产生升力的入射气流冲击时具有在其间延伸的弦长,弦廓长度在其间延伸,其中, 风力涡轮机叶片的吸入侧设置有沿着安装线定位的多个涡流发生器,该安装线具有最靠近根端的近端点和最靠近末端的远端点,其中安装线是从 风力涡轮机叶片的后缘。
    • 19. 发明公开
    • Wind turbine blade provided with flow altering devices
    • 配有变流装置的风力涡轮机叶片
    • EP2253839A1
    • 2010-11-24
    • EP09160501.4
    • 2009-05-18
    • LM GLASFIBER A/S
    • Fuglsang, PeterBove, StefanoFuglsang, Lars
    • F03D1/06
    • F03D1/0641F03D1/0675F05B2240/301F05B2240/32Y02E10/721Y10T29/49318Y10T29/49337
    • A blade for a rotor of a wind turbine having a substantially horizontal rotor shaft is described. The rotor comprises a hub, from which the blade extends substantially in a radial direction when mounted to the hub. The blade comprises a profiled contour comprising a pressure side and a suction side as well as a leading edge and a trailing edge with a chord extending between the leading edge and the trailing edge, the profiled contour generating a lift when being impacted by an incident airflow, the profiled contour in the radial direction being divided into a root region with a substantially circular or elliptical profile closest to the hub, an airfoil region with a lift generating profile furthest away from the hub, and preferably a transition region between the root region and the airfoil region, the transition region having a profile gradually changing in the radial direction from the circular or elliptical profile of the root region to the lift generating profile of the airfoil region, wherein the airfoil region comprises at least a first longitudinal segment extending along at least 20% of a longitudinal extent of the airfoil region, the first longitudinal segment comprising a first base part having a leading edge and a trailing edge with a chord extending between the leading edge and the trailing edge. The first base part has an axial induction factor, which without flow altering device deviates at least 5% from a target axial induction factor at a design point. The first longitudinal segment is provided with a number of first flow altering devices arranged so as to adjust the aerodynamic properties of the first longitudinal segment to substantially meet the target axial induction factor at the design point.
    • 描述了用于具有基本上水平的转子轴的风力涡轮机的转子的叶片。 转子包括轮毂,当安装到轮毂时,叶片基本上从径向延伸。 所述叶片包括成形轮廓,所述成形轮廓包括压力侧和吸力侧以及具有在所述前缘和所述后缘之间延伸的弦的前缘和后缘,所述成形轮廓在被入射气流冲击时产生升力 ,径向方向上的成形轮廓被分成具有最接近轮毂的基本圆形或椭圆形轮廓的根部区域,具有离轮毂最远的升力生成轮廓的翼型区域,并且优选地在根部区域与根部区域之间的过渡区域 所述过渡区域具有从所述根部区域的所述圆形或椭圆形轮廓到所述翼型区域的所述升力生成轮廓在径向方向上逐渐变化的轮廓,其中所述翼型区域包括至少第一纵向区段,所述第一纵向区段沿着 翼型区域的纵向范围的至少20%,第一纵向区段包括第一基础区段 t具有前缘和后缘以及在前缘和后缘之间延伸的翼弦。 第一个基座部件具有轴向感应系数,在设计点,没有变流装置偏离目标轴向感应系数至少5%。 第一纵向段设置有多个第一变流装置,该第一变流装置布置成调节第一纵向段的空气动力学特性以基本上满足设计点处的目标轴向感应因子。