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Passive load alleviation on wind turbine blades from aeroelastically driven selectively compliant morphing

机译:气动涡轮机叶片的被动载荷减轻从气球驱动的选择性兼容变形

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Load alleviation control is highly desirable to reduce penalties associated with the added structural mass required to withstand rare load scenarios. This is particularly true for wind turbine designs incorporating long-span blades. Implementation of compliance-based morphing structures to modify the lift distribution passively has the potential to mitigate the impact of rare, but integrally threatening, loads on wind turbine blades while limiting the addition of actuation and sensing systems. We present a novel passive load alleviation concept based on a morphing flap exhibiting selective compliance from an embedded bistable element. A multifidelity, aeroelastic tool is used to study the shape adaptability of a morphing flap indicating that passive changes from high lift generation to load alleviation configurations can be achieved by exploiting the energy of the flow. This mechanism offers a method to reduce catastrophic peak loads potentially, thus offering the possibility to lower the overall structural weight of wind turbine blades.
机译:负载缓解控制非常希望减少与耐稀有负荷方案所需的结构质量相关的惩罚。对于包含长跨度叶片的风力涡轮机设计尤其如此。基于合规性的变形结构的实施以改变升力分布,被动地有可能减轻稀有,但一体地威胁,在风力涡轮机叶片上的影响,同时限制致动和传感系统的增加。我们基于从嵌入的双稳态元件的选择性顺应性的变形翼片提供了一种新的被动载荷缓解概念。多尺寸,空气弹性工具用于研究变形襟翼的形状适应性,表明通过利用流动的能量来实现从高升力产生的被动变化以加载缓解配置。该机制提供了一种可潜在地减少灾难性峰值负荷的方法,从而提供降低风力涡轮机叶片整体结构重量的可能性。

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