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Failure Test and Finite Element Simulation of a Large Wind Turbine Composite Blade under Static Loading

机译:大型风力涡轮机复合叶片静载荷下的失效测试与有限元模拟

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This study presented a failure analysis of a 52.3 m composite wind turbine blade under static loading. Complex failure characteristics exhibited at the transition region of the blade were thoroughly examined and typical failure modes were indentified. In order to predict multiple failure modes observed in the tests and gain more insights into the failure mechanisms of the blade, a Finite Element (FE) simulation was performed using a global-local modeling approach and Progressive Failure Analysis (PFA) techniques which took into account material failure and property degradation. Failure process and failure characteristics of the transition region were satisfactorily reproduced in the simulation, and it was found that accumulated delamination in spar cap and shear web failure at the transition region were the main reasons for the blade to collapse. Local buckling played an important role in the failure process by increasing local out-of-plane deformation, while the Brazier effect was found not to be responsible for the blade failure.
机译:这项研究提出了52.3 m复合风力涡轮机叶片在静态载荷下的失效分析。彻底检查了叶片过渡区域表现出的复杂故障特征,并确定了典型的故障模式。为了预测在测试中观察到的多种故障模式并深入了解刀片的故障机理,使用了全局局部建模方法和渐进式故障分析(PFA)技术进行了有限元(FE)仿真。说明材料故障和性能下降。在模拟中令人满意地再现了过渡区域的失效过程和失效特征,并且发现,翼梁盖中的累积分层和过渡区域的剪切腹板失效是叶片塌陷的主要原因。局部屈曲通过增加局部平面外变形而在失效过程中起着重要作用,而发现Brazier效应与叶片失效无关。

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