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 arotor blade(6), wherein the absolute length L of the rotor blade (6) extends from thebladeattachment (11) to the blade tip (12) and the relative blade length x/Lproceeds from theblade attachment (11). The rotor blade (6) is divided into an innerlongitudinal section L;associated with the blade attachment (11) and an outer longitudinal section Laassociated with the blade tip (12), wherein the transition from the innerlongitudinalsection L i to the outer longitudinal section L a defines the cross-sectionalplane E o, andthe blade tip (12) defines the cross-sectional plane E E. As a function of therelativeblade length x/L, the rotor blade (6) has a specific aerodynamic profile witha chord t, atwist .theta., a relative thickness d/t, a relative curvature f/t, and arelative trailing edgethickness h/t. In order to reduce acoustic emissions without having to acceptappreciable losses in performance, it is proposed according to the inventionthat thecross-sectional plane E o is located at a relative blade length x/L in therange between0.80 and 0.98, the blade chord t of the aerodynamic profile in the cross-sectional planeE E is at least 60% of the blade chord t of the aerodynamic profile in thecross-sectionalplane E o, and the blade twist .theta. of the aerodynamic profile in the cross-sectional planeE E is greater than the blade twist .theta. of the aerodynamic profile in thecross-sectionalplane E o.
机译:本发明涉及一种转子叶片(6)以及具有这种叶片的风力涡轮机(1)。转子叶片(6),其中转子叶片(6)的绝对长度L从刀叶片尖端(12)上的附件(11)和相对叶片长度x / L从刀片附件(11)。转子叶片(6)分为内部纵向截面L;与叶片附件(11)和外部纵向截面L相关联一种与叶片尖端(12)相关联,其中从内部过渡纵截面L i到外部纵向截面L a定义了横截面平面E o叶片尖端(12)定义了横截面EE。相对的叶片长度x / L,转子叶片(6)具有特定的空气动力学轮廓和弦扭转角,相对厚度d / t,相对曲率f / t和a相对后缘厚度h / t。为了减少声发射而不必接受根据本发明提出了明显的性能损失。那横截面E o位于相对叶片长度x / L处,介于分别为0.80和0.98,剖面E E至少是空气动力学曲线中叶片翼弦t的60%横断面平面E o,并且叶片扭曲θ。交叉的空气动力学轮廓剖面E E大于叶片扭曲θ。空气动力学曲线横断面飞机E o。

著录项

  • 公开/公告号CA2725960A1

    专利类型

  • 公开/公告日2011-06-22

    原文格式PDF

  • 申请/专利权人 MICKELER SIEGFRIED;KELLER WALTER;

    申请/专利号CA20102725960

  • 发明设计人 MICKELER SIEGFRIED;KELLER WALTER;

    申请日2010-12-20

  • 分类号F03D1/06;F01D5/14;

  • 国家 CA

  • 入库时间 2022-08-21 18:02:03

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