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    WIND TURBINE BLADE PLANFORMS WITH TWISTED AND TAPERED TIPS
    4.
    发明申请
    WIND TURBINE BLADE PLANFORMS WITH TWISTED AND TAPERED TIPS 有权
    风力涡轮机叶片具有双向和带状提示

    公开(公告)号：US20090297355A1

    公开(公告)日：2009-12-03

    申请号：US12129997

    申请日：2008-05-30

    申请人： Stefan Herr ,  Kevin W. Kinzie ,  Brandon S. Gerber ,  Kevin J. Standish ,  Klaus Koegler ,  Benoit P. Petitjean

    发明人： Stefan Herr ,  Kevin W. Kinzie ,  Brandon S. Gerber ,  Kevin J. Standish ,  Klaus Koegler ,  Benoit P. Petitjean

    IPC分类号： F01D5/14 ,  F03D11/00

    CPC分类号： F03D1/0633 ,  F05B2240/301 ,  Y02E10/721

    摘要： A blade for a wind turbine includes a total backward twist of between approximately 6 degrees and approximately 15 degrees between an outer approximately 1 percent to 10 percent of a rotor radius of the blade; and an approximate planform distribution within the following ranges r/Rc/R(LE)c/R(TE) .960.60 to 0.65%−1.42 to −1.34% .9680.54 to 0.59%−1.31 to −1.34% .9740.39 to 0.58%−1.36 to −1.22% .98060.13 to 0.57%−1.45 to −1.06% .9856−0.23 to 0.56%  −1.56 to −0.74% .9906−0.76 to 0.55%  −1.74 to −0.24% .9956−1.44 to 0.54%  −1.99 to 0.23%   1.00−2.17 to 0.54%  −2.27 to 0.44%   where “r/R” is an approximate normalized distance outward from a center of rotation of the blade along a span of the blade; and “c/R(LE)” and “c/R(TE)” are approximate relative positions of a leading (LE) and trailing edge (TE) of a chord “c” expressed as a percentage of a distance outward from the center of rotation at each r/R.

    摘要翻译： 用于风力涡轮机的叶片包括在叶片的转子半径的外部约1％至10％之间的大约6度与大约15度之间的总后向扭转; 和在以下范围内的近似平面分布r / R c / R（LE）c / R（TE）.96 0.60至0.65％-1.42至-1.34％.968 0.54至0.59％-1.31至-1.34％.974 0.39至0.58％-1.36至-1.22％.9806 0.13至0.57％-1.45至-1.06％.9856 -0.23至0.56％-1.56至-0.74％.9906 -0.76至0.55％-1.74至-0.24％.9956 -1.44至0.54％-1.99至0.23％1.00 -2.17至0.54％-2.27至0.44％，其中“r / R”是从叶片沿叶片的跨度的旋转中心向外的近似归一化距离; 和“c / R（LE）”和“c / R（TE）”是弦“c”的前导（LE）和后沿（TE）的近似相对位置，表示为距离 每个r / R处的旋转中心。

    Wind turbine blade planforms with twisted and tapered tips
    7.
    发明授权
    Wind turbine blade planforms with twisted and tapered tips 有权
    风力涡轮机叶片具有扭曲和锥形尖端

    公开(公告)号：US08061996B2

    公开(公告)日：2011-11-22

    申请号：US12129997

    申请日：2008-05-30

    申请人： Stefan Herr ,  Kevin W. Kinzie ,  Brandon S. Gerber ,  Kevin J. Standish ,  Klaus Koegler ,  Benoit P. Petitjean

    发明人： Stefan Herr ,  Kevin W. Kinzie ,  Brandon S. Gerber ,  Kevin J. Standish ,  Klaus Koegler ,  Benoit P. Petitjean

    IPC分类号： F04D29/38

    CPC分类号： F03D1/0633 ,  F05B2240/301 ,  Y02E10/721

    摘要： A blade for a wind turbine includes a total backward twist of between approximately 6 degrees and approximately 15 degrees between an outer approximately 1 percent to 10 percent of a rotor radius of the blade; and an approximate planform distribution within the following ranges r/Rc/R(LE)c/R(TE) .960.60 to 0.65%−1.42 to −1.34% .9680.54 to 0.59%−1.31 to −1.34% .9740.39 to 0.58%−1.36 to −1.22% .98060.13 to 0.57%−1.45 to −1.06% .9856−0.23 to 0.56%  −1.56 to −0.74% .9906−0.76 to 0.55%  −1.74 to −0.24% .9956−1.44 to 0.54%  −1.99 to 0.23%   1.00−2.17 to 0.54%  −2.27 to 0.44%   where “r/R” is an approximate normalized distance outward from a center of rotation of the blade along a span of the blade; and “c/R(LE)” and “c/R(TE)” are approximate relative positions of a leading (LE) and trailing edge (TE) of a chord “c” expressed as a percentage of a distance outward from the center of rotation at each r/R.

    摘要翻译： 用于风力涡轮机的叶片包括在叶片的转子半径的外部约1％至10％之间的大约6度与大约15度之间的总后向扭转; 和在以下范围内的近似平面分布r / R c / R（LE）c / R（TE）.96 0.60至0.65％-1.42至-1.34％.968 0.54至0.59％-1.31至-1.34％.974 0.39至0.58％-1.36至-1.22％.9806 0.13至0.57％-1.45至-1.06％.9856 -0.23至0.56％-1.56至-0.74％.9906 -0.76至0.55％-1.74至-0.24％.9956 -1.44至0.54％-1.99至0.23％1.00 -2.17至0.54％-2.27至0.44％，其中“r / R”是从叶片沿叶片的跨度的旋转中心向外的近似归一化距离; 和“c / R（LE）”和“c / R（TE）”是弦“c”的前导（LE）和后沿（TE）的近似相对位置，表示为距离 每个r / R处的旋转中心。

    Extension for rotor blade in wind turbine
    8.
    发明授权
    Extension for rotor blade in wind turbine 有权
    风力发电机转子叶片扩展

    公开(公告)号：US08834127B2

    公开(公告)日：2014-09-16

    申请号：US13228650

    申请日：2011-09-09

    申请人： Philippe Giguere ,  Stefan Herr ,  Peter James Fritz ,  Scott Gabell Riddell ,  Jeffrey Eric Bergman

    发明人： Philippe Giguere ,  Stefan Herr ,  Peter James Fritz ,  Scott Gabell Riddell ,  Jeffrey Eric Bergman

    IPC分类号： F03D1/06 ,  F03D7/02

    CPC分类号： F03D7/0232 ,  F03D1/0633 ,  F05B2240/30 ,  Y02E10/721 ,  Y02E10/723

    摘要： A rotor blade assembly for a wind turbine and a method for increasing a loading capability of a rotor blade within a maximum load limit for a wind turbine are disclosed. The rotor blade assembly includes a rotor blade having surfaces defining a pressure side, a suction side, a leading edge, and a trailing edge extending between a tip and a root. The rotor blade assembly further includes an extension connected to a surface of the rotor blade, the extension having at least one design characteristic configured for increasing a loading capability of the rotor blade within a maximum load limit for the wind turbine. The design characteristic is one of extension length, extension width, extension curvature, span-wise extension location, chord-wise extension location, or extension angle with respect to a chord line of the rotor blade.

    摘要翻译： 公开了一种用于风力涡轮机的转子叶片组件和用于在风力涡轮机的最大负载极限内增加转子叶片的负载能力的方法。 转子叶片组件包括具有限定压力侧，吸力侧，前缘和在尖端和根部之间延伸的后缘的表面的转子叶片。 转子叶片组件还包括连接到转子叶片的表面的延伸部分，该延伸部具有至少一个设计特征，该特征构造用于在风力涡轮机的最大负载极限内增加转子叶片的负载能力。 设计特征是相对于转子叶片的弦线的延伸长度，延伸宽度，延伸曲率，跨度延伸位置，弦向延伸位置或延伸角之一。

    Wind turbine rotor blade with trailing edge extension and method of attachment
    9.
    发明授权
    Wind turbine rotor blade with trailing edge extension and method of attachment 有权
    具有后缘延伸的风力涡轮机转子叶片和附接方法

    公开(公告)号：US08506250B2

    公开(公告)日：2013-08-13

    申请号：US13276560

    申请日：2011-10-19

    申请人： Bharat Bagepalli ,  Stefan Herr

    发明人： Bharat Bagepalli ,  Stefan Herr

    IPC分类号： F01D5/16

    CPC分类号： F03D1/0675 ,  F03D80/00 ,  F05B2240/30 ,  F05B2280/4003 ,  Y02E10/721 ,  Y10T29/49337

    摘要： A wind turbine rotor blade assembly includes a rotor blade having a pressure side, a suction side, a leading edge, and a trailing edge extending in a generally span-wise direction between a tip and a root. An edge extension is attached along the trailing edge and includes a first strip member having a span-wise attachment section attached to pressure side, and a second strip member having a span-wise attachment section attached to the suction side. Each of the first and second strip members has an outboard edge and an extension section that projects chord-wise beyond the trailing edge. The extension sections are adhesively attached to each other outboard of the trailing edge along a span-wise length of the first and second strip members and define an adhesively bonded closure edge of the edge extension. A method is also provided for forming an edge extension on a wind turbine rotor blade.

    摘要翻译： 风力涡轮机转子叶片组件包括具有压力侧，吸力侧，前缘和在尖端和根部之间沿大致跨度方向延伸的后缘的转子叶片。 边缘延伸部沿着后缘附接​​并且包括具有附接到压力侧的跨度连接部分的第一条带部件和具有附接到吸力侧的跨度附接部分的第二条带部件。 第一和第二条带部件中的每一个具有外侧边缘和延伸部分，该延伸部分在弦后方突出超过后缘。 延伸部分沿着第一和第二条状部件的跨度长度粘合地附接到后缘的外侧，并且限定边缘延伸部的粘合的封闭边缘。 还提供了一种在风力涡轮机转子叶片上形成边缘延伸的方法。

    Method and apparatus for increasing lift on wind turbine blade
    10.
    发明授权
    Method and apparatus for increasing lift on wind turbine blade 有权
    增加风力发电机叶片升力的方法和装置

    公开(公告)号：US08303250B2

    公开(公告)日：2012-11-06

    申请号：US12649682

    申请日：2009-12-30

    申请人： Omer Mohammed ,  Stefan Herr

    发明人： Omer Mohammed ,  Stefan Herr

    IPC分类号： B64C9/00 ,  F03D7/00

    CPC分类号： F03D7/0236 ,  F03D7/0232 ,  F05B2240/202 ,  F05B2240/31 ,  Y02E10/721 ,  Y02E10/723 ,  Y10T29/49337

    摘要： A lift generating apparatus for a wind turbine rotor blade comprising a first sidewall and an opposing second sidewall coupled together at a leading edge and at a trailing edge. The lift generating apparatus includes at least one forward blade extension coupled to the rotor blade to define a first airflow channel between the forward blade extension and the rotor blade. The lift generating apparatus also includes at least one aft blade extension coupled to the rotor blade to define a second airflow channel between the aft blade extension and the rotor blade.

    摘要翻译： 一种用于风力涡轮机转子叶片的升降机产生装置，包括在前缘和后缘处联接在一起的第一侧壁和相对的第二侧壁。 升降机产生装置包括耦合到转子叶片的至少一个前叶片延伸部，以在前叶片延伸部和转子叶片之间限定第一气流通道。 升降机产生装置还包括耦合到转子叶片的至少一个后叶片延伸部，以在后叶片延伸部和转子叶片之间限定第二气流通道。