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Aerostructural optimization of a morphing wing for airborne wind energy applications

机译:机载风能应用的变形翼的空气结构优化

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Airborne wind energy (AWE) vehicles maximize energy production by constantly operating at extreme wing loading, permitted by high flight speeds. Additionally, the wide range of wind speeds and the presence of flow inhomogeneities and gusts create a complex and demanding flight environment for AWE systems. Adaptation to different flow conditions is normally achieved by conventional wing control surfaces and, in case of ground generator-based systems, by varying the reel-out speed. These control degrees of freedom enable to remain within the operational envelope, but cause significant penalties in terms of energy output. A significantly greater adaptability is offered by shape-morphing wings, which have the potential to achieve optimal performance at different flight conditions by tailoring their airfoil shape and lift distribution at different levels along the wingspan. Hence, the application of compliant structures for AWE wings is very promising. Furthermore, active gust load alleviation can be achieved through morphing, which leads to a lower weight and an expanded flight envelope, thus increasing the power production of the AWE system. This work presents a procedure to concurrently optimize the aerodynamic shape, compliant structure, and composite layup of a morphing wing for AWE applications. The morphing concept is based on distributed compliance ribs, actuated by electromechanical linear actuators, guiding the deformation of the flexible-yet load-carrying-composite skin. The goal of the aerostructural optimization is formulated as a high-level requirement, namely to maximize the average annual power production per wing area of an AWE system by tailoring the shape of the wing, and to extend the flight envelope of the wing by actively alleviating gust loads. The results of the concurrent multidisciplinary optimization show a 50.7% increase of extracted power with respect to a sequentially optimized design, highlighting the benefits of morphing and the potential of the proposed approach.
机译:空中风能(AWE)车辆通过在极端翼装载中不断运行,通过高飞行速度允许,最大化能源生产。此外,各种风速和流量不均匀性和阵风的存在为AWE系统创造了一个复杂和苛刻的飞行环境。通过改变卷轴速度,通常通过传统的机翼控制表面和基于地面发生器的系统的情况来实现对不同流动条件的适应。这些控制自由度使得能够留在运行信封内,但在能量输出方面造成重大惩罚。通过形状 - 变形翼提供了显着更大的适应性,这通过使其翼型形状和沿着翼形牌不同水平的升力分布来实现不同飞行条件下的最佳性能。因此,对敬畏翼的柔性结构的应用非常有前途。此外,可以通过变形来实现活跃的阵风减轻,这导致重量较轻和扩展飞行信封,从而增加了AWE系统的电力产生。这项工作介绍了一种程序,以便同时优化用于AWE应用的变形翼的空气动力学形状,柔顺的结构和复合叠加。变形概念基于分布式顺应性肋,由机电线性致动器致动,引导柔性载荷复合皮肤的变形。将气动化优化的目标作为高级别要求,即通过定制机翼的形状来最大化每翼系统的平均年电力生产,并通过积极减轻机翼的飞行包络阵风负荷。同时多学科优化的结果显示了相对于依次优化设计提取的提取功率的50.7%,突出了变形的好处和所提出的方法的潜力。

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