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A high-rate shape memory alloy actuator for aerodynamic load control on wind turbines

机译:高速形状记忆合金致动器,用于控制风力涡轮机上的空气动力学负载

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摘要

This article discusses the development of a high-rate shape memory alloy-driven actuator. The concept of the actuator was developed to act as aerodynamic load control surface on wind turbines. It was designed as a plate or beam-like structure with prestrained shape memory alloy wires embedded off its neutral axis. Moreover, the shape memory alloy material was embedded in channels through which air was forced to actively cool the wires when the recovery load was to be released. Wires were implemented on both sides of the neutral axis to deflect the beam in both directions. Thermal analysis of the cooling channels showed that they increased the cooling rate up to 10-fold in comparison to the same set-up without forced convection. Subsequently, a fuzzy logic controller was designed to control the thermo-mechanical system. The inputs were the error between the deflection and the set point, the value of the set point and the time derivative of the set point. The output consisted of two signals to the valves that controlled the flow through the channels and a signal heating signal that was split into both sets of wires, depending on its sign. The controller was tested on an antagonistic set-up, through which a similar thermo-mechanical behaviour as with the actuator was obtained, but eliminating the beam dynamics. The results were satisfactory; an actuation bandwidth of 1 Hz was attained. Subsequently, the controller was tested on the actuator. With increasing actuation frequency, until 0.6 Hz, a relatively small error between the set point and the actual deflection was observed. Above that frequency, the error increased, but the sinusoidal response was lost. This is believed to be due to snap-through behaviour around the neutral position of the actuator. This was substantiated by the apparent inability of the actuator to track the set point around the neutral position in tracking a composite sinusoidal set point.
机译:本文讨论了高速形状记忆合金驱动致动器的开发。促动器的概念被开发为充当风力涡轮机上的空气动力学负载控制面。它被设计成板状或梁状结构,并在其中性轴上嵌入了预应变的形状记忆合金丝。此外,将形状记忆合金材料嵌入通道中,当要释放恢复负载时,空气被迫通过该通道主动冷却导线。在中性轴的两侧安装了导线,以使光束在两个方向上偏转。对冷却通道的热分析表明,与没有强制对流的相同设置相比,它们将冷却速率提高了10倍。随后,设计了模糊逻辑控制器来控制热机械系统。输入是挠度和设定点之间的误差,设定点的值和设定点的时间导数。输出包括两个信号,这些信号发送给控制流经通道的阀的信号,以及一个信号加热信号,该信号根据信号的符号分为两组。该控制器在对抗装置上进行了测试,通过该装置可以获得与执行器类似的热机械行为,但消除了射束动力学。结果令人满意;达到1 Hz的驱动带宽。随后,控制器在执行器上进行了测试。随着驱动频率的增加,直到0.6 Hz,在设定点和实际挠度之间观察到相对较小的误差。高于该频率,误差增加,但正弦响应丢失。据信这是由于致动器中性位置周围的卡扣现象。通过执行器在跟踪复合正弦曲线设定点时明显无法跟踪中性位置附近的设定点来证明这一点。

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  • 作者单位

    Faculty of Aerospace Engineering, Department of Structure Integrity and Composites, Delft University of Technology, Kluyverweg Ⅰ, 2629 HS Delft, The Netherlands;

    Faculty of Aerospace Engineering, Department of Structure Integrity and Composites, Delft University of Technology, Delft, The Netherlands;

    Faculty of Aerospace Engineering, Department of Structure Integrity and Composites, Delft University of Technology, Delft, The Netherlands;

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  • 原文格式 PDF
  • 正文语种 eng
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  • 关键词

    Actuator; load control; shape memory alloy;

    机译:执行器负载控制;形状记忆合金;

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