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Evaluation of dual-axis fatigue testing of large wind turbine blades

机译:大型风力发电机叶片双轴疲劳试验评估

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摘要

Full-scale fatigue testing is part of the certification process for large wind turbine blades. That testing is usually performed about the flapwise and edgewise axes independently but a new method for resonant fatigue testing has been developed in which the flapwise and edgewise directions are tested simultaneously, thus also allowing the interactions between the two mutually perpendicular loads to be investigated. The method has been evaluated by comparing the Palmgren-Miner damage sum around the cross-section at selected points along the blade length that results from a simulated service life, as specified in the design standards, and testing. Bending moments at each point were generated using wind turbine simulation software and the test loads were designed to cause the same amount of damage as the true service life. The mode shape of the blade was tuned by optimising the position of the excitation equipment, so that the bending moment distribution was as close as possible to the target loads. The loads were converted to strain-time histories using strength of materials approach, and fatigue analysis was performed. The results show that if the bending moment distribution is correct along the length of the blade, then dual-axis resonant testing tests the blade much more thoroughly than sequential tests in the flapwise and edgewise directions. This approach is shown to be more representative of the loading seen in service and can thus contribute to a potential reduction in the weight of wind turbine blades and the duration of fatigue tests leading to reduced cost.
机译:全面疲劳测试是大型风力涡轮机叶片认证过程的一部分。该测试通常是围绕襟翼方向和边缘方向独立进行的,但是已经开发了一种共振疲劳测试的新方法,其中同时测试了襟翼方向和边缘方向,因此也可以研究两个相互垂直的载荷之间的相互作用。通过比较设计标准中规定的模拟使用寿命得出的沿叶片长度的选定点处的横截面周围的Palmgren-Miner损伤总和,对该方法进行了评估。使用风力涡轮机仿真软件在每个点产生弯矩,并设计测试载荷以造成与实际使用寿命相同的损坏量。通过优化励磁设备的位置来调整叶片的模式形状,以使弯矩分布尽可能接近目标载荷。使用材料强度方法将载荷转换为应变时程,并进行疲劳分析。结果表明,如果沿叶片长度方向的弯矩分布正确,则双轴共振测试比沿翼片方向和边缘方向的顺序测试对叶片的测试要彻底得多。事实表明,这种方法可以更好地代表使用中的负载,因此可以潜在地减轻风力涡轮机叶片的重量,并可以减少疲劳测试的持续时间,从而降低成本。

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