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Improved Modal Dynamics of Wind Turbines to Avoid Stall-induced Vibrations

机译:改进了风力发电机的模态动力学,避免了失速引起的振动

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摘要

Stall-induced edgewise blade vibrations have occasionally been observed on three-bladed wind turbines over the last decade. Experiments and numerical simulations have shown that these blade vibrations are related to certain vibration modes of the turbines. A recent experiment with a 600 kW turbine has shown that a backward whirling mode associated with edgewise blade vibrations is less aerodynamically damped than the corresponding forward whirling mode. In this article the mode shapes of the particular turbine are analysed, based on a simplified turbine model described in a multi-blade formulation. It is shown that the vibrations of the blades for the backward and forward edgewise whirling modes are different, which can explain the measured difference in aerodynamic damping. The modal dynamics of the entire turbine is important for stability assessments; blade-only analysis can be misleading. In some cases the modal dynamics may even be improved to avoid stall-induced vibrations.
机译:在过去的十年中,偶尔会在三叶风力涡轮机上观察到失速引起的叶片侧向振动。实验和数值模拟表明,这些叶片振动与涡轮机的某些振动模式有关。最近使用600 kW涡轮机进行的实验表明,与相应的前向旋转模式相比,与边向叶片振动相关的后向旋转模式在空气动力学上的阻尼较小。在本文中,基于多叶片公式中描述的简化涡轮机模型,分析了特定涡轮机的模式形状。结果表明,叶片在前后旋风模式下的振动是不同的,这可以解释测得的空气动力学阻尼差异。整个涡轮机的模态动力学对于稳定性评估很重要。仅刀片分析可能会产生误导。在某些情况下,甚至可以改善模态动力学,以避免失速引起的振动。

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