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WIND TURBINE, WIND POWER GENERATION DEVICE PROVIDED THEREWITH, AND WIND TURBINE DESIGN METHOD

机译:风轮机,具有该风轮机的风力发电装置以及风轮机设计方法

摘要

Provided is a wind turbine blade that delivers the desired aerodynamic characteristics under conditions where the upper limit of the chord length near the blade root is limited. The wind turbine blade includes a blade body (3) whose chord length increases from a blade tip (1b) toward a blade root (1a). The blade body (3) includes a blade tip region (1c) located near the blade tip and whose chord length increases gradually toward the blade root (1a), the blade tip region (1c) having a substantially constant first design lift coefficient, a maximum-chord-length position (1d) located near the blade root (1a) and having a maximum chord length, the maximum-chord-length position (1d) having a second design lift coefficient higher than the first design lift coefficient, and a transition region (1e) located between the blade tip region (1c) and the maximum-chord-length position (1d). The transition region (1e) has a design lift coefficient increasing gradually from the first design lift coefficient to the second design lift coefficient in a direction from the blade tip (1b) toward the blade root (1a).
机译:提供一种风力涡轮机叶片,其在叶片根部附近的弦长的上限受到限制的条件下提供期望的空气动力学特性。风力涡轮机叶片包括叶片主体(3),该叶片主体的弦长从叶片尖端(1b)朝向叶片根部(1a)增加。叶片主体(3)包括位于叶片尖端附近并且其弦长朝向叶片根部(1a)逐渐增加的叶片尖端区域(1c),该叶片尖端区域(1c)具有基本恒定的第一设计升力系数a。位于叶片根部(1a)附近并具有最大弦长的最大弦长位置(1d),最大弦长位置(1d)的第二设计升力系数高于第一设计升力系数,以及位于叶片尖端区域(1c)和最大弦长位置(1d)之间的过渡区域(1e)。过渡区域(1e)的设计升力系数在从叶片顶端(1b)朝向叶片根部(1a)的方向上从第一设计升力系数逐渐增加到第二设计升力系数。

著录项

  • 公开/公告号EP2631474A4

    专利类型

  • 公开/公告日2015-05-06

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HEAVY INDUSTRIES LTD.;

    申请/专利号EP20110834441

  • 发明设计人 FUKAMI KOJI;

    申请日2011-10-20

  • 分类号F03D1/06;

  • 国家 EP

  • 入库时间 2022-08-21 15:06:47

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