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Horizontal dual-point excitation and fatigue test of full-scale wind turbine blade

机译:全尺寸风力涡轮机叶片水平双点励磁及疲劳试验

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In order to meet the requirements of large-blade fatigue testing, a horizontal dual-point linear exciter loading program is developed. In this paper, Lagrange's equation and FEM method are used to simulate the dual-point excitation theory model. The horizontal dual-point excitation characteristics of the blade are validated by the experimental method. The relationship among the dual-point exciting force, cycle time and bending moment during blade fatigue test in flap wise direction is studied. The advantages of horizontal dual-point excitation in blade fatigue test are analysed. Compared with vertical single-point excitation when the equal bending moment is reached, the exciting force and energy consumption required for dual-point excitation are reduced by 60.0% and 96.8%. Resonant frequency of the test system is improved by reducing the dead weight because of dual-point horizontal excitation. The entire blade fatigue test time is shortened by 7.4%. The use of horizontal dual-point excitation could save energy and shorten the entire fatigue test time.
机译:为了满足大型刀片疲劳测试的要求,开发了一种水平双点线性激励机加载程序。本文采用拉格朗日的等式和有限元方法来模拟双点激励理论模型。通过实验方法验证刀片的水平双点激励特性。研究了双点激动力,循环时间和弯曲时刻在襟翼方向上的叶片疲劳试验期间的关系。分析了叶片疲劳试验中水平双点激发的优点。与垂直单点激发相比达到相等的弯矩时,双点激发所需的励磁力和能量消耗减少了60.0%和96.8%。通过双点水平激励降低耐死重,可以改善测试系统的谐振频率。整个刀片疲劳试验时间缩短了7.4%。水平双点激励的使用可以节省能量并缩短整个疲劳测试时间。

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