4.5 Article

Efficiency Improvement of Magnetic Coupler with Nanocrystalline Alloy Film for UAV Wireless Charging System with a Carbon Fiber Fuselage

期刊

ENERGIES
卷 15, 期 22, 页码 -

出版社

MDPI
DOI: 10.3390/en15228363

关键词

carbon fiber; eddy current loss; magnetic coupler; nanocrystalline alloy; unmanned aerial vehicle; wireless charging

向作者/读者索取更多资源

Existing research on UAV wireless charging systems has often overlooked the impact of the UAV fuselage on the efficiency of the magnetic coupler. This study proposes a design that utilizes nanocrystalline cores to reduce the loss caused by the UAV fuselage. By optimizing the parameters of the asymmetric circular coils and modeling the fuselage as an additional coil, the impact of eddy current loss induced by the fuselage is revealed. The use of an optimized nanocrystalline alloy film further improves the efficiency of the coupler.
Existing research on the magnetic coupler of unmanned aerial vehicle (UAV) wireless charging systems usually ignores the UAV fuselage, but the fuselage causes eddy current loss and reduces a system's efficiency. Therefore, aiming at the above problems, this paper proposes a design for a magnetic coupler using nanocrystalline cores to reduce the loss caused by the UAV fuselage. First, the parameters of the asymmetric circular coils were designed for higher mutual inductance. The losses caused by the windings and cores were also calculated. Second, for the loss effect of the carbon fiber fuselage, the fuselage was modeled as an additional coil coupled with both the transmitting and receiving coils. The fact that the eddy current induced by the fuselage leads to efficiency reduction is revealed, which has been generally ignored by previous research. Then, the effect of the nanocrystalline alloy was analyzed based on the magnetic circuit model. An optimized nanocrystalline alloy film was applied to reduce eddy current loss and improve coupler efficiency. Finally, an experimental prototype with a 500 W output, 90.3% efficiency, and a 300 mm air gap were fabricated. When compared to the design without UAV material considerations, the coupler efficiency was improved by 7.9%.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.5
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据