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Aspects of the Dynamic Response of a Small Wind Turbine Blade in Highly Turbulent Flow: Part Ⅰ Measured Blade Response

机译:小型湍流叶片在高湍流中的动态响应方面:第一部分测得的叶片响应

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摘要

This paper presents some dynamic measurements acquired from the surface of a composite constructed test blade on an operating 400W three-bladed wind turbine. The structural design of the composite blade was modified from the original design to reduce its stiffness in flapwise bending. Signals from 10 strain gauges attached to the blade were acquired every 45 in the azimuthal domain and at a fixed rate of 140Hz in the time domain. The test turbine was located at a highly turbulent site with the turbulence intensity between 0.3 and 0.5 at all wind speeds. Signals from the gauges show the cyclic response of the blade was dominated by the 1P frequency with influences from 2P, 3P and 4P frequencies increasing with the radial position of the gauge on the blade. Cyclic variation in the root bending moment was nearly sinusoidal, with a small plateau in the peak possibly due to the effects of large yaw angle on the blade bending moment. The blade's response to yaw was investigated for both normal yaw events, i.e. those experienced by the turbine many times during a typical day, and for extreme yaw events, i.e. which occurred infrequently. During a normal yaw event with a yaw rate of 70°/s, the cyclic variation in blade strain near the hub connection increased from 210 μstrain before the event to 1500 μstrain at the peak of the event. An extreme yaw event produced a yaw rate of 160°/s with the cyclic variation in strain increasing from 200 μstrain to 2600 μstrain.
机译:本文介绍了一些动态测量结果,这些测量是从运行中的400W三叶片风力涡轮机上的复合结构测试叶片表面获得的。复合叶片的结构设计从原始设计进行了修改,以减少其在翼片弯曲中的刚度。在方位角域中每45个获取来自附着在叶片上的10个应变仪的信号,在时域中以140Hz的固定速率获取信号。测试涡轮机位于高湍流位置,在所有风速下的湍流强度在0.3到0.5之间。压力计发出的信号表明,叶片的循环响应主要由1P频率决定,而2P,3P和4P频率的影响随压力计在叶片上的径向位置的增加而增加。根部弯矩的循环变化几乎是正弦曲线的,在峰中有一个小的平台,可能是由于偏航角大对叶片弯矩的影响。研究了叶片的偏航响应,包括正常偏航事件(即在典型的一天中涡轮多次经历的事件)和极端偏航事件(即不经常发生的事件)。在偏航率为70°/ s的正常偏航事件期间,轮毂连接附近的叶片应变的周期性变化从事件之前的210μs应变增加到事件高峰时的1500μs。极端的偏航事件产生了160°/ s的偏航率,并且应变的周期性变化从200μs应变增加到2600μs。

著录项

  • 来源
    《Wind Engineering》 |2007年第1期|p.1-16|共16页
  • 作者

    S. V. R. Wilson; P. D. Clausen;

  • 作者单位

    School of Engineering, The University of Newcastle, University Drive, Callaghan, NSW 2308, Australia;

  • 收录信息 美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 风能、风力机械;
  • 关键词

  • 入库时间 2022-08-18 00:25:56

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