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公开(公告)号：US20110142666A1
公开(公告)日：2011-06-16
申请号：US12946259
申请日：2010-11-15
IPC分类号： F03D11/00
CPC分类号： F03D1/0683 , F03D1/0675 , F05B2240/301 , F05B2260/96 , Y02E10/721
摘要： A rotor blade assembly for a wind turbine is 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 further includes a noise reducer configured on a surface of the rotor blade, the noise reducer comprising a plurality of serrations, each of the plurality of serrations defining a centerline. The centerline of each of the plurality of serrations defines a individual tailored angle dependent on at least one of span-wise location, local chord, width, length, bend angle, and thickness
摘要翻译： 公开了一种用于风力涡轮机的转子叶片组件。 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。 转子叶片还包括构造在转子叶片的表面上的减噪器，所述降噪器包括多个锯齿，所述多个锯齿中的每一个限定中心线。 多个锯齿中的每一个的中心线限定取决于跨度位置，局部弦，宽度，长度，弯曲角度和厚度中的至少一个的单独定制的角度
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公开(公告)号：US08523515B2
公开(公告)日：2013-09-03
申请号：US12946259
申请日：2010-11-15
CPC分类号： F03D1/0683 , F03D1/0675 , F05B2240/301 , F05B2260/96 , Y02E10/721
摘要： A rotor blade assembly for a wind turbine is 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 further includes a noise reducer configured on a surface of the rotor blade, the noise reducer comprising a plurality of serrations, each of the plurality of serrations defining a centerline. The centerline of each of the plurality of serrations defines a individual tailored angle dependent on at least one of span-wise location, local chord, width, length, bend angle, and thickness.
摘要翻译： 公开了一种用于风力涡轮机的转子叶片组件。 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。 转子叶片还包括构造在转子叶片的表面上的减噪器，所述降噪器包括多个锯齿，所述多个锯齿中的每一个限定中心线。 多个锯齿中的每一个的中心线根据跨度位置，局部弦，宽度，长度，弯曲角度和厚度中的至少一个来定义单独的裁切角度。
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公开(公告)号：US20130251535A1
公开(公告)日：2013-09-26
申请号：US13424518
申请日：2012-03-20
IPC分类号： F03D11/00
CPC分类号： F03D1/0633 , F03D1/0675 , F05B2240/30 , Y02E10/721
摘要： In one aspect, a winglet for a rotor blade is disclosed. The winglet may generally include a winglet body extending at least partially between a winglet origin and a blade tip. The winglet body may define a sweep and a pre-bend. The sweep defined between the winglet origin and the blade tip may range from about 0.5% to about 4.0% of a span of the rotor blade. The pre-bend defined between the winglet origin and the blade tip may range from about 1.5% to about 4.5% of the span of the rotor blade
摘要翻译： 一方面，公开了一种用于转子叶片的翼片。 小翼通常可以包括至少部分地在小翼起点和叶片尖端之间延伸的小翼体。 小翼体可以定义扫描和预弯曲。 限定在小翼起点和叶片尖端之间的扫掠可以在转子叶片的跨度的约0.5％至约4.0％的范围内。 限定在小翼起点和叶片尖端之间的预弯可以在转子叶片的跨度的约1.5％至约4.5％的范围内
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公开(公告)号：US20130280085A1
公开(公告)日：2013-10-24
申请号：US13453213
申请日：2012-04-23
申请人： Klaus Ulrich Koegler
发明人： Klaus Ulrich Koegler
IPC分类号： F03D1/06
CPC分类号： F03D1/0633 , F05B2240/30 , F05B2260/962 , Y02E10/721
摘要： A rotor blade assembly for a wind turbine is disclosed. In one embodiment, the rotor blade assembly includes a rotor blade having exterior 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 further defines a span and a chord. The rotor blade assembly further includes a noise reducer configured on an exterior surface of the rotor blade. The noise reducer includes a plurality of noise reduction features. Each of the plurality of noise reduction features defines a centerline. In a planform view, the centerline of each of the plurality of noise reduction features is approximately parallel to a local flow streamline for that noise reduction feature at the trailing edge 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。 在一个实施例中，转子叶片组件包括转子叶片，其具有限定压力侧，吸力侧，前缘和在尖端和根部之间延伸的后缘的外表面。 转子叶片进一步限定跨度和弦。 转子叶片组件还包括构造在转子叶片的外表面上的减噪器。 降噪器包括多个降噪特征。 多个降噪特征中的每一个限定了中心线。 在平面图视图中，多个降噪特征中的每一个的中心线近似平行于在转子叶片的后缘处的该降噪特征的局部流线。
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公开(公告)号：US08479581B2
公开(公告)日：2013-07-09
申请号：US13099644
申请日：2011-05-03
摘要： A device for measuring fluid pressure, includes at least one flexible layer having a first surface adapted for fixing the layer to a structure, and having a second surface having at least one recess; at least one pressure sensor, provided in the at least one recess; and at least two wires connected to the at least one pressure sensor for connecting the at least one pressure sensor to a signal receiving unit. Further, a method for measuring fluid pressure is provided.
摘要翻译： 用于测量流体压力的装置包括至少一个柔性层，其具有适于将层固定到结构的第一表面，并且具有至少一个凹部的第二表面; 设置在所述至少一个凹部中的至少一个压力传感器; 以及连接到所述至少一个压力传感器的至少两根线，用于将所述至少一个压力传感器连接到信号接收单元。 此外，提供了一种用于测量流体压力的方法。
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公开(公告)号：US09039380B2
公开(公告)日：2015-05-26
申请号：US13459412
申请日：2012-04-30
申请人： Klaus Ulrich Koegler , Stefan Herr , Ramesh Vedula
发明人： Klaus Ulrich Koegler , Stefan Herr , Ramesh Vedula
IPC分类号： F03D1/06
CPC分类号： F03D1/0675 , Y02E10/721
摘要： A winglet for a rotor blade is disclosed. The winglet may generally include a winglet body extending between a first end and a second end. The winglet body may define a sweep and may have a curvature defined by a curve fit including a first radius of curvature and a second radius of curvature. The sweep between the first end and the second end may range from about 580 millimeters to about 970 millimeters. Additionally, the first radius of curvature may range from about 1500 millimeters to about 2500 millimeters and the second radius of curvature may range from about 1200 millimeters to about 2000 millimeters.
摘要翻译： 公开了一种用于转子叶片的小翼。 小翼通常可以包括在第一端和第二端之间延伸的小翼体。 小翼体可以限定扫掠并且可以具有由包括第一曲率半径和第二曲率半径的曲线拟合限定的曲率。 第一端和第二端之间的扫掠范围可以为约580毫米至约970毫米。 另外，第一曲率半径可以在约1500毫米至约2500毫米的范围内，第二曲率半径可以在约1200毫米至约2000毫米的范围内。
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公开(公告)号：US08858174B2
公开(公告)日：2014-10-14
申请号：US13106007
申请日：2011-05-12
申请人： Dongjai Lee , Stefan Herr , Klaus Ulrich Koegler
发明人： Dongjai Lee , Stefan Herr , Klaus Ulrich Koegler
CPC分类号： F03D7/0224 , F03D7/0276 , F05B2270/101 , F05B2270/32 , F05B2270/327 , F05B2270/328 , F05B2270/335 , Y02E10/723
摘要： The present subject matter relates to methods and systems for operating a wind turbine that, in some embodiments may include a gearbox. The wind turbine is provided with a blade having an adjustable pitch angle and the tip speed ratio (TSR) of the blade is monitored. In operation, the method and system is configured to increase the pitch angle of the blade concurrently with an increase in TSR to maintain turbine operation within an identified high power coefficient (Cp) operational region for the blade. TSR may be monitored by monitoring one of the velocity of the tip of the blade, wind speed, the rotational speed of the blade, or the rotational speed of a component within the gearbox.
摘要翻译： 本主题涉及用于操作风力涡轮机的方法和系统，在一些实施例中可以包括齿轮箱。 风力涡轮机设置有具有可调俯仰角的叶片，并且监视叶片的叶尖速度比（TSR）。 在操作中，该方法和系统被配置为随着TSR的增加同时增加叶片的俯仰角，以维持涡轮机在用于叶片的高功率系数（Cp）操作区域内的运行。 TSR可以通过监测叶片尖端的速度，风速，叶片的转速或齿轮箱内的部件的转速来监测。
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8.发明授权Methods for using site specific wind conditions to determine when to install a tip feature on a wind turbine rotor blade 有权使用场地风力条件来确定何时在风力涡轮机转子叶片上安装尖端特征的方法公开(公告)号：US08448527B2
公开(公告)日：2013-05-28
申请号：US13273451
申请日：2011-10-14
IPC分类号： G01P5/06
CPC分类号： F03D1/0675 , F03D17/00 , Y02E10/721
摘要： A method for utilizing site specific data to determine whether to install a tip feature on a rotor blade of a wind turbine is disclosed. The method generally includes monitoring with a sensor at least one wind condition at a wind turbine site, determining an actual tip deflection threshold for a rotor blade of a wind turbine located at the wind turbine site based on the least one wind condition, comparing the actual tip deflection threshold to a predetermined tip deflection threshold for the rotor blade and determining whether to install a tip feature on the rotor blade based on the comparison between the actual tip deflection threshold and the predetermined tip deflection threshold.
摘要翻译： 公开了一种利用场地特定数据来确定是否在风力涡轮机的转子叶片上安装尖端特征的方法。 该方法通常包括使用传感器监测风力涡轮机现场处的至少一个风况，基于至少一个风况来确定位于风力涡轮机位置处的风力涡轮机的转子叶片的实际尖端偏转阈值，将实际 基于所述实际尖端偏转阈值与所述预定尖端偏转阈值之间的比较，确定是否将转子叶片上的尖端特征安装在所述转子叶片上的预定尖端偏转阈值。
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公开(公告)号：US08308433B2
公开(公告)日：2012-11-13
申请号：US12894453
申请日：2010-09-30
IPC分类号： F03D7/02
CPC分类号： G01M5/0016 , F03D7/0224 , F05B2220/709 , F05B2260/96 , G01L15/00 , G01M9/06 , Y02E10/723
摘要： A wind turbine system is presented. The wind turbine system includes a blade comprising an airfoil and a sensing device disposed on a surface of the airfoil, wherein the sensing device generates signals that are representative of pressure deflection on the surface of the airfoil. The wind turbine system further comprises a processing subsystem that receives location details of the sensing device and a transfer function corresponding to the airfoil, determines a location of a stagnation point on the surface of the airfoil based upon the signals and the location details, and determine an angle of attack (AOA) on the surface of the airfoil based upon the location of the stagnation point and the transfer function.
摘要翻译： 介绍了风力发电机组系统。 风力涡轮机系统包括叶片，其包括设置在翼型件的表面上的翼型件和感测装置，其中感测装置产生代表翼型件表面上的压力偏转的信号。 风力涡轮机系统还包括处理子系统，其接收感测装置的位置细节和对应于翼型的传递函数，基于信号和位置细节确定翼型表面上的停滞点的位置，并且确定 基于停滞点和传递函数的位置，在翼面的表面上的迎角（AOA）。
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公开(公告)号：US09103325B2
公开(公告)日：2015-08-11
申请号：US13424518
申请日：2012-03-20
IPC分类号： F03D1/06
CPC分类号： F03D1/0633 , F03D1/0675 , F05B2240/30 , Y02E10/721
摘要： In one aspect, a winglet for a rotor blade is disclosed. The winglet may generally include a winglet body extending at least partially between a winglet origin and a blade tip. The winglet body may define a sweep and a pre-bend. The sweep defined between the winglet origin and the blade tip may range from about 0.5% to about 4.0% of a span of the rotor blade. The pre-bend defined between the winglet origin and the blade tip may range from about 1.5% to about 4.5% of the span of the rotor blade.
摘要翻译： 一方面，公开了一种用于转子叶片的翼片。 小翼通常可以包括至少部分地在小翼起点和叶片尖端之间延伸的小翼体。 小翼体可以定义扫描和预弯曲。 限定在小翼起点和叶片尖端之间的扫掠可以在转子叶片的跨度的约0.5％至约4.0％的范围内。 限定在小翼起点和叶片尖端之间的预弯可以在转子叶片的跨度的约1.5％至约4.5％的范围内。
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