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Design, fabrication, and experiments of an electromagnetic actuator for flapping wing micro air vehicles

机译:扑翼微型飞行器电磁致动器的设计,制造和实验

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The design and construction of a 2.6 gram electromagnetic actuator operated at resonance is presented. This design is based on wedge-shaped electromagnetic coil generating a driving torque on a rotor embedded with permanent magnets. Additional permanent magnets are used to create a virtual spring effect, supply a restoring torque to the rotor and adding nonlinear system stiffness. Flapping wing parameters were varied systematically to generate 16 unique wing profiles, from which wings were fabricated. Independent bench tests for the coil and spring magnets were used to modify analytical models of the actuator, derived in detail in a parallel study. Based on the equations of motion, estimates for the primary mode of resonance and the peak-peak stroke amplitude were determined using an approximate solution. Frequency response tests were conducted on the flapper using the set of test wings at varying supply voltages and spring configurations to verify the predicted resonate frequencies and amplitudes. Wing kinematics and mean lift measurements were performed for the flapper operating at resonance, producing a lift-to-weight ratio for the actuator of over one at 24V.
机译:提出了在谐振下操作2.6克电磁致动器的设计和结构。该设计基于楔形电磁线圈在嵌入永磁体的转子上产生驱动扭矩。额外的永磁体用于产生虚拟弹簧效果,向转子提供恢复扭矩并添加非线性系统刚度。张开翼参数系统地改变以产生16个独特的机翼型材,从而制造翅膀。线圈和弹簧磁体的独立台力测试用于修改致动器的分析模型,在并行研究中详细得出。基于运动方程,使用近似解决方案确定初级谐振模式和峰峰冲程幅度的估计。在不同的电源电压和弹簧配置处,使用一组测试翼在挡板上进行频率响应测试,以验证预测的谐振频率和幅度。针对在共振操作的挡板上进行翼运动学和平均升力测量,在24V下产生致动器的致动器的升级比。

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