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    Wind turbine rotor blade and wind turbine rotor
    3.
    发明授权
    Wind turbine rotor blade and wind turbine rotor 有权
    风力发电机转子叶片和风力发电机转子

    公开(公告)号：US08100661B2

    公开(公告)日：2012-01-24

    申请号：US12218481

    申请日：2008-07-15

    申请人： Peder Bay Enevoldsen ,  Søren Hjort ,  Rune Rubak

    发明人： Peder Bay Enevoldsen ,  Søren Hjort ,  Rune Rubak

    IPC分类号： B63H1/26 ,  B63H7/02 ,  B64C11/16 ,  B64C27/46 ,  F01D5/14 ,  F03B7/00 ,  F03D11/02 ,  F04D29/38

    CPC分类号： F03D1/0633 ,  F05B2240/301 ,  F05B2250/70 ,  F05B2260/96 ,  F05B2270/20 ,  Y02E10/721

    摘要： A wind turbine rotor blade is provided which includes a root end and a tip end located opposite the root end. A leading edge extends from the root end to the tip end. A trailing edge extends from the root end to the tip end. A span direction is defined by a line extending linearly from the root end to the tip end. A chord direction is perpendicular to the span direction and lies in the plane extending through the leading edge and the trailing edge. A shoulder is the point of the maximum chord-wise extension. An airfoil portion extends from the shoulder to the tip end. The airfoil portion comprises a span-wise interval begging before the tip end and extending to or close to the tip end and in which the distribution of the chord-wise extension is increased as compared to the load optimised distribution of the chord-wise extension.

    摘要翻译： 提供了一种风力涡轮机转子叶片，其包括根端和位于根端相对的尖端。 前缘从根端延伸到尖端。 后缘从根端延伸到尖端。 跨度方向由从根端到尖端线性延伸的线限定。 弦方向垂直于跨度方向，并且位于延伸穿过前缘和后缘的平面中。 肩膀是最大和弦延伸点。 翼型部分从肩部延伸到尖端。 翼型部分包括在尖端之前乞求并且延伸到或接近尖端的跨度间隔，并且与弦向延伸部的载荷优化分布相比，弦向延伸部的分布增加。

    Optimised layout for wind turbine rotor blades
    4.
    发明授权
    Optimised layout for wind turbine rotor blades 有权
    风力发电机转子叶片优化布局

    公开(公告)号：US08678770B2

    公开(公告)日：2014-03-25

    申请号：US12594205

    申请日：2008-04-01

    申请人： Peder Bay Enevoldsen ,  Søren Hjort ,  Jesper Laursen

    发明人： Peder Bay Enevoldsen ,  Søren Hjort ,  Jesper Laursen

    IPC分类号： F03D1/06

    CPC分类号： F03D1/0633 ,  F05B2240/30 ,  F05B2250/70 ,  Y02E10/721

    摘要： A wind turbine rotor blade defined by a tip point, a shoulder, a maximum chord interval which is defined as the radial interval over which the blade chord is no less that 95% of the shoulder chord and which extends over at least 15% of the entire blade length, and an outer blade interval extending from the maximum chord interval to the tip point, wherein the outer blade interval has a concave hyperbolic chord distribution from the maximum chord interval towards the tip point. Further a method for optimizing the chord distribution of a wind turbine blade layout is provided, wherein the chord distribution is optimized by optimizing the chord distribution in the maximum chord interval by maximizing the ratio of the annual energy production to the loads acting on the blade and in the outer blade interval with respect to the annual energy production alone.

    摘要翻译： 由尖端，肩部，最大弦间隔限定的风力涡轮机转子叶片，其最大弦间隔被定义为叶片弦不小于肩弦的95％并且延伸至至少15％ 整个刀片长度和从最大弦间隔延伸到尖端点的外刀片间隔，其中外刀片间隔具有从最大弦间隔朝向尖端点的凹双曲线和弦分布。 还提供了一种用于优化风力涡轮机叶片布置的弦分布的方法，其中通过使年能量产生与作用在叶片上的载荷的比例最大化来优化最大弦间隔中的弦分布来优化弦分布;以及 在相对于年度能源生产的外叶间隔中。

    Optimised layout for wind turbine rotor blades
    5.
    发明申请
    Optimised layout for wind turbine rotor blades 有权
    风力发电机转子叶片优化布局

    公开(公告)号：US20100196166A1

    公开(公告)日：2010-08-05

    申请号：US12594205

    申请日：2008-04-01

    申请人： Peder Bay Enevoldsen ,  Søren Hjort ,  Jesper Laursen

    发明人： Peder Bay Enevoldsen ,  Søren Hjort ,  Jesper Laursen

    IPC分类号： F03D11/00

    CPC分类号： F03D1/0633 ,  F05B2240/30 ,  F05B2250/70 ,  Y02E10/721

    摘要： A wind turbine rotor blade defined by a tip point, a shoulder, a maximum chord interval which is defined as the radial interval over which the blade chord is no less that 95% of the shoulder chord and which extends over at least 15% of the entire blade length, and an outer blade interval extending from the maximum chord interval to the tip point, wherein the outer blade interval has a concave hyperbolic chord distribution from the maximum chord interval towards the tip point. Further a method for optimizing the chord distribution of a wind turbine blade layout is provided, wherein the chord distribution is optimized by optimizing the chord distribution in the maximum chord interval by maximizing the ratio of the annual energy production to the loads acting on the blade and in the outer blade interval with respect to the annual energy production alone.

    摘要翻译： 由尖端，肩部，最大弦间隔限定的风力涡轮机转子叶片，其最大弦间隔被定义为叶片弦不小于肩弦的95％并且延伸至至少15％ 整个刀片长度和从最大弦间隔延伸到尖端点的外刀片间隔，其中外刀片间隔具有从最大弦间隔朝向尖端点的凹双曲线和弦分布。 还提供了一种用于优化风力涡轮机叶片布置的弦分布的方法，其中通过使年能量产生与作用在叶片上的载荷的比例最大化来优化最大弦间隔中的弦分布来优化弦分布;以及 在相对于年度能源生产的外叶间隔中。

    Wind turbine rotor blade and wind turbine rotor
    6.
    发明申请
    Wind turbine rotor blade and wind turbine rotor 有权
    风力发电机转子叶片和风力发电机转子

    公开(公告)号：US20090022598A1

    公开(公告)日：2009-01-22

    申请号：US12218481

    申请日：2008-07-15

    申请人： Peder Bay Enevoldsen ,  Soren Hjort ,  Rune Rubak

    发明人： Peder Bay Enevoldsen ,  Soren Hjort ,  Rune Rubak

    IPC分类号： F03D1/06 ,  F03D3/06

    CPC分类号： F03D1/0633 ,  F05B2240/301 ,  F05B2250/70 ,  F05B2260/96 ,  F05B2270/20 ,  Y02E10/721

    摘要： A wind turbine rotor blade is provided which includes a root end and a tip end located opposite the root end. A leading edge extends from the root end to the tip end. A trailing edge extends from the root end to the tip end. A span direction is defined by a line extending linearly from the root end to the tip end. A chord direction is perpendicular to the span direction and lies in the plane extending through the leading edge and the trailing edge. A shoulder is the point of the maximum chord-wise extension. An airfoil portion extends from the shoulder to the tip end. The airfoil portion comprises a span-wise interval begging before the tip end and extending to or close to the tip end and in which the distribution of the chord-wise extension is increased as compared to the load optimised distribution of the chord-wise extension.

    摘要翻译： 提供了一种风力涡轮机转子叶片，其包括根端和位于根端相对的尖端。 前缘从根端延伸到尖端。 后缘从根端延伸到尖端。 跨度方向由从根端到尖端线性延伸的线限定。 弦方向垂直于跨度方向，并且位于延伸穿过前缘和后缘的平面中。 肩膀是最大和弦延伸点。 翼型部分从肩部延伸到尖端。 翼型部分包括在尖端之前乞求并且延伸到或接近尖端的跨度间隔，并且与弦向延伸部的载荷优化分布相比，弦向延伸部的分布增加。