A Novel Hybrid Wireless Power Transfer Coupler for Unmanned Aerial Vehicle Application

IF 4.8 Q1 ENGINEERING, ELECTRICAL & ELECTRONIC
IEEE open journal of power electronics Pub Date : 2026-01-01 Epub Date: 2026-01-13 DOI:10.1109/OJPEL.2025.3649320
Pan Sun;Yaodong Xiang;Guoli Feng;Enguo Rong;Yilin Liu;Xiaochen Zhang
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Abstract

The special structure of unmanned aerial vehicles (UAVs) poses challenges to the integrated design method and power transmission capability of the couplers used for their wireless charging. This paper proposes a new inductive and capacitive combined hybrid wireless power transfer coupler for UAV. Among them, the capacitive coupler is designed as a six-plate structure. A receiving plate and a shielding plate are installed on each of the two landing gears of the UAV, and the transmitting plates are installed on the ground. The FR4 epoxy insulating material is filled between the plates to increase the coupling capacitance. The inductive coupler adopts a square coil form, which is installed on the belly of the UAV. Inductive coupler and capacitive coupler compensate each other for reactive power while transmitting power, which eliminates the need for additional compensation network components on the receiving side. Secondly, based on the single-sided LCLC compensation network, this paper presents a parameter design method that can adjust the power transmission ratio of inductive and capacitive couplers. Then, the component stress analysis was conducted. Compared with the inductive power transfer (IPT) and capacitive power transfer (CPT) systems that have the same coupler and similar compensation network, the proposed system significantly reduced the stress on the coupler. Finally, an experimental prototype is established to verify the scheme. The experimental results show that the system can transmit 500 W at an efficiency of 80.7%, which means it can be used for wireless charging of UAV.
一种用于无人机的新型混合无线传输耦合器
无人机的特殊结构对其无线充电耦合器的集成设计方法和功率传输能力提出了挑战。提出了一种用于无人机的新型电感式和电容式组合混合无线传输耦合器。其中,电容耦合器设计为六极板结构。UAV的两个起落架上各安装一个接收板和一个屏蔽板,发射板安装在地面上。板间填充FR4环氧绝缘材料,增加耦合电容。电感耦合器采用方形线圈形式,安装在无人机的腹部。电感耦合器和电容耦合器在发送功率时相互补偿无功功率,从而消除了接收侧额外补偿网络组件的需要。其次,在单面LCLC补偿网络的基础上,提出了一种可以调节电感耦合器和电容耦合器传动比的参数设计方法。然后对构件进行应力分析。与具有相同耦合器和相似补偿网络的电感功率传输(IPT)和电容功率传输(CPT)系统相比,该系统显著降低了耦合器的应力。最后,建立了实验样机对该方案进行了验证。实验结果表明,该系统能以80.7%的效率传输500 W的电能,可用于无人机的无线充电。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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CiteScore
8.60
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0.00%
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审稿时长
8 weeks
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