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Control Framework and Integrative Design Method for an Adaptive Wind Turbine Blade

机译:自适应风力涡轮机叶片的控制框架和一体化设计方法

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A control framework and integrative design method for an adaptive wind turbine blade is presented. The blade is adapted by actively transforming the twist angle distribution (TAD) along the blade. This can alleviate fatigue loads and improve wind capture. In this paper, we focus on wind capture. The proposed design concept consists of a rigid spar that is surrounded by a series of flexible blade sections. Each section has two zones of stiffness. The sections are actuated at each end to deform the TAD. A quasi-static control technique is proposed for the TAD. The controller sets the position of the blade actuators that shape the TAD during steady-state operation. A design procedure is used to define the required TAD as a function of the wind speed. This is based on an optimization procedure that minimizes the deviation between the actual TAD and that found in the aerodynamic design. The design inputs for this optimization problem include the stiffness for each zone of the section, and the actuator locations along the blade. Given the optimal TAD at each wind speed, the free position of the blade is established using a dynamic programming technique. The position is selected based on minimal actuation energy according to wind conditions at any installation site. The proposed framework is demonstrated using a National Renewable Energy Laboratory (NREL) certified wind turbine model with recorded wind data. An increase in efficiency of 3.8% with only a deviation of 0.34% from the aerodynamic TAD is observed.
机译:提出了一种自适应风力涡轮机叶片的控制框架和一体化设计方法。叶片通过主动地沿着刀片而被主动地改变扭曲角度分布(TAD)来调整。这可以减轻疲劳载荷并改善风捕获。在本文中,我们专注于风捕获。所提出的设计概念由刚性翼梁组成,刚性翼梁被一系列柔性刀片部分包围。每个部分都有两个刚度的区域。这些部分在每个端部致动以使TAD变形。为TAD提出了一种准静态控制技术。控制器在稳态操作期间设置刀片致动器的位置,该刀片致动器在稳态操作期间塑造TAD。设计过程用于定义所需的TAD作为风速的函数。这是基于优化过程,最小化实际TAD与空气动力学设计中的偏差。用于该优化问题的设计输入包括部分的每个区域的刚度,以及沿刀片的致动器位置。给定每个风速时的最佳TAD,使用动态编程技术建立刀片的自由位置。根据任何安装现场的风力条件,基于最小致动能选择该位置。使用具有记录风数据的全国可再生能源实验室(NRER)认证的风力涡轮机模型来证明拟议的框架。观察到从空气动力学TAD的偏差增加3.8%的效率增加。

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