首页> 外国专利> AEROACOUSTIC ROTOR BLADE FOR A WIND TURBINE, AND WIND TURBINE EQUIPPED THEREWITH

AEROACOUSTIC ROTOR BLADE FOR A WIND TURBINE, AND WIND TURBINE EQUIPPED THEREWITH

机译:用于风轮机的风声转子叶片及其所装备的风轮机

摘要

The invention concerns a rotor blade (6) and a wind turbine (1) with such a rotor blade (6), wherein the absolute length L of the rotor blade (6) extends from the blade attachment (11) to the blade tip (12) and the relative blade length x/L proceeds from the blade attachment (11). The rotor blade (6) is divided into an inner longitudinal section Li associated with the blade attachment (11) and an outer longitudinal section La associated with the blade tip (12), wherein the transition from the inner longitudinal section Li to the outer longitudinal section La defines the cross-sectional plane E0, and the blade tip (12) defines the cross-sectional plane EE. AS a function of the relative blade length x/L, the rotor blade (6) has a specific aerodynamic profile with a chord t, a twist Θ, a relative thickness d/t, a relative curvature f/t, and a relative trailing edge thickness h/t. In order to reduce acoustic emissions without having to accept appreciable losses in performance, it is proposed according to the invention that the cross-sectional plane E0 is located at a relative blade length x/L in the range between 0.80 and 0.98, the blade chord t of the aerodynamic profile in the cross-sectional plane EE is at least 60% of the blade chord t of the aerodynamic profile in the cross-sectional plane E0, and the blade twist Θ of the aerodynamic profile in the cross-sectional plane EE is greater than the blade twist Θ of the aerodynamic profile in the cross-sectional plane E0.
机译:本发明涉及一种转子叶片(6)和具有这种转子叶片(6)的风力涡轮机(1),其中,转子叶片(6)的绝对长度L从叶片附件(11)延伸至叶片尖端( 12),相对刀片长度x / L从刀片附件(11)开始。转子叶片(6)被分为与叶片附件(11)相关的内部纵向部分Li和与叶片尖端(12)相关的外部纵向部分La,其中从内部纵向部分Li到外部纵向部分的过渡截面La限定了横截面E0,而叶片尖端(12)限定了横截面EE。作为叶片相对长度x / L的函数,转子叶片(6)具有特定的空气动力学轮廓,其弦长为t,扭曲为Θ,相对厚度为d / t,相对曲率为f / t,相对尾随为边缘厚度h / t。为了减少声发射而不必承受明显的性能损失,根据本发明提出,横截面E0位于相对叶片长度x / L处,该相对叶片长度在0.80至0.98之间,叶片弦长横截面EE中的空气动力学轮廓的t至少是横截面E0中空气动力学轮廓的叶片弦t的60%,而空气动力学轮廓的叶片扭曲Θ在横截面EE中在横截面平面E0中,它大于空气动力学轮廓的叶片扭曲θ。

著录项

  • 公开/公告号IN2010KO01424A

    专利类型

  • 公开/公告日2011-12-16

    原文格式PDF

  • 申请/专利权人

    申请/专利号IN1424/KOL/2010

  • 发明设计人 SIEGFRIED MICKELER;WALTER KELLER;

    申请日2010-12-21

  • 分类号F01D5/14;

  • 国家 IN

  • 入库时间 2022-08-21 17:24:19

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