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Analysis of Morphing Trailing Edge Flap with Embedded Multistable Variable Stiffness Laminates

机译:嵌入多稳态可变刚度层压板的变形后缘襟翼分析

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This paper presents an analysis of morphing trailing edge design of a wind turbine rotor blade with multistable elements embedded inside it. Morphing trailing edge devices are promising candidates for reducing loads in variable wind conditions, turbulent flows as well as capable of changing the shape rapidly. However, conventional actuation systems are quite complex and prone to high maintenance cost. The application of multistable laminates allow large deformations with modest actuation demand without the need for a continuous supply of energy. The multistable plates undergo snap-through with the help of mechanical forces and with Macro Fiber Composite (MFC) actuator patches. A parametric study is conducted to study the best location of the MFC patches to allow snap-through with lower voltages than straight fiber laminates without losing bistability. The multistable rectangular plate with variable stiffness (VS) laminates is then embedded in the flap section to achieve deflection of the flap as the multistable plate snaps.
机译:本文分析了其中嵌入了多稳定元件的风力涡轮机转子叶片的变形后缘设计。变形后缘装置有望在减少可变风况,湍流以及迅速改变形状的情况下减轻负荷。然而,常规的致动系统非常复杂并且易于产生高昂的维护成本。多稳态层压板的应用允许大变形和适度的致动需求,而无需持续提供能量。借助机械力和Macro Fiber Composite(MFC)执行器补片,可将多稳态板快速插入。进行了参数研究,以研究MFC贴片的最佳位置,以允许以比直纤维层压板更低的电压进行击穿,而不会失去双稳性。然后将具有可变刚度(VS)层压板的多稳态矩形板嵌入襟翼部分,以在多稳态板卡扣时实现襟翼的挠曲。

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