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Process for manufacturing a wind turbine blade with pre-designed segment

机译:具有预先设计的区段的风力涡轮机叶片的制造方法

摘要

A method of manufacturing a wind turbine blade by using the design of a longitudinal segment of a first wind turbine blade for the design of a second wind turbine blade is described. The first wind turbine blade and the second wind turbine blade each comprise a longitudinally extending base part having 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. The method comprises the steps of a) taking a first blade design of a first base part of a first longitudinal section of the airfoil region of a first blade, b) using the first blade design for the first base part on a first longitudinal section of the airfoil region of a second blade, so that an induction factor of the first base part on the second blade without flow altering devices at a rotor design point deviates from a target induction factor, and c) providing the first longitudinal section of the second blade with first flow altering devices so as to adjust the aerodynamic properties of the first longitudinal segment to substantially meet the target induction factor at the design point on the second blade. The first longitudinal segment extends along at least 20% of a longitudinal extent of the airfoil region of the second blade.
机译:描述了一种通过将第一风力涡轮机叶片的纵向段的设计用于第二风力涡轮机叶片的设计来制造风力涡轮机叶片的方法。第一风力涡轮机叶片和第二风力涡轮机叶片均包括纵向延伸的基部,该基部具有轮廓轮廓,该轮廓轮廓包括压力侧和吸力侧以及前缘和后缘,并且弦在前缘和后缘之间延伸。后缘,轮廓轮廓在受到入射气流的冲击时产生升力,轮廓轮廓沿径向被分为最接近轮毂的具有基本圆形或椭圆形轮廓的根部区域,具有升力产生轮廓的翼型区域距轮毂最远,最好是在根部区域和机翼区域之间的过渡区域,该过渡区域的轮廓在径向上从根部区域的圆形或椭圆形轮廓逐渐变化到机翼的产生升力的轮廓地区。该方法包括以下步骤:a)对第一叶片的翼型区域的第一纵向截面的第一基础部分进行第一叶片设计,b)对第一基础部分的第一纵向部分使用第一叶片设计。第二叶片的翼型区域,从而在转子设计点处没有流量改变装置的第二叶片上的第一基础部分的感应系数偏离目标感应系数,并且c)提供第二叶片的第一纵向截面用第一流动改变装置来调节第一纵向节段的空气动力学特性,以在第二叶片的设计点上基本满足目标进气系数。第一纵向段沿着第二叶片的翼型区域的纵向范围的至少20%延伸。

著录项

  • 公开/公告号DK2432992T3

    专利类型

  • 公开/公告日2020-04-14

    原文格式PDF

  • 申请/专利权人 LM WIND POWER A/S;

    申请/专利号DK20100720913T

  • 发明设计人 FUGLSANG PETER;FUGLSANG LARS;BOVE STEFANO;

    申请日2010-05-18

  • 分类号F03D1/06;

  • 国家 DK

  • 入库时间 2022-08-21 11:17:50

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