飞机系统的电能质量改进:使用24脉冲变换器缓解谐波的建议

Hugo Oliveira Vilas Boas, Ângelo José Junqueira Rezek, Christel Enock Ghislain Ogoulola
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引用次数: 0

摘要

电能质量的改善和电能的可用性是飞机系统的重要问题。本文提出了一种替代24脉冲变换器系统(CS-24P),以减少交流供电系统中的第11和第13滤波器,最初安装在传统的12脉冲整流器(CS-12P)中,用于更多的电动飞机系统。所提出的CS-24P的拓扑结构包括两个特殊的三相三绕组变压器和四个串联在系统直流侧的6脉冲三相交直流变换器。为了证明本文提出的CS-24P与传统的CS-12P结合交流和直流滤波器的优势,利用Matlab/Simulink软件进行了计算机仿真,以验证利用MathCad程序进行的理论分析。理论和仿真结果表明,CS-24P输入电流的总谐波失真(% THD)在60 Hz和400 Hz时分别为6.60%和2.92%,满足IEEE-519和MIL-STD-704F的要求。得到的直流电压纹波幅值最大小于6 V,满足RTCA-DO-160F航空标准。此外,与传统的CS-12P相比,本文提出的CS-24P在交流电流和电压的% THD、功率因数、纹波幅值(峰均值)和直流电压纹波因数方面都具有令人满意的性能。利用现有的实验室资源设计并执行了一个实验室原型来验证研究。所得结果证实了所提样机在飞机系统中的技术可行性和适用性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Power Quality Improvements in Aircraft Systems: A Proposal Using a 24-pulse Converter for Harmonic Mitigation
Power quality improvements and availability of electrical power are issues of great importance to aircraft systems. This paper presents an alternative 24-Pulse Converter System (CS-24P) to reduce the 11th and 13th filters in AC supply system, initially installed in traditional 12-pulse rectifiers (CS-12P) in more electric aircraft systems. The topological structure of the proposed CS-24P comprises two special three-phase three winding transformers and four 6-pulse three-phase AC-DC converters connected in series on the DC side of the system. To show the advantages of the proposed CS-24P compared with the traditional CS-12P used with AC and DC filters, computer simulations were carried out using Matlab/Simulink software to prove the theoretical analysis performed with the help of the MathCad program. The theoretical and simulation results show that the total harmonic distortion (% THD) of the input current for the CS-24P is equal to 6.60% at 60 Hz and 2.92% at 400 Hz, respectively, which meets the IEEE-519 and MIL-STD-704F requirements. Furthermore, the ripple amplitude obtained of DC voltage is less than 6 V (maximum), which meets the RTCA-DO-160F aeronautical standard. Also, it is shown that in comparison with the traditional CS-12P, the proposed CS-24P presents a satisfactory performance in terms of % THD of AC current and voltage, power factor, ripple amplitude (peak to mean) and ripple factor of DC voltage. A laboratory prototype was designed and executed using available laboratory resources to validate the research. The obtained results confirm the technical feasibility and applicability of the proposed prototype in aircraft systems.
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