多电动飞机双有源桥式变换器电流解析方程

A. Fernandez-Hernandez, A. Garcia‐Bediaga, I. Villar, G. Abad
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引用次数: 3

摘要

体积和重量功率密度的改进是电动飞机(MEA)的主要目标之一。影响这两个参数的变量数量很大,其影响难以预测。此外,在许多应用中也采用DAB变换器,作为储能系统(ESS)或直流母线之间的潮流调节。选择最合适的调制是一项设计挑战。因此,本文给出了文献中不同调制方式下DAB变换器的开关电流、均方根电流和AVG电流的解析方程。为此,对通过变压器的电压和电流波形进行了表征。然后,利用这些波形来提取电流的解析方程,以便将来评估功率损耗。最后,建立了PLECS仿真模型,以验证本文所得到的解析方程。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Analytical Equations of the Currents in Dual Active Bridge Converter for More Electric Aircraft
Volumetric and gravimetric power density improvements are one of the main objectives in More Electric Aircraft (MEA). The number of variables which influence both parameters is wide, and its impact is difficult to predict. Also, there are many applications in which DAB converter is employed, as energy-storage systems (ESS) or power flow regulation among DC buses. The selection of the most appropriate modulation is a design challenge. Therefore, this paper presents the analytical equations of switching, RMS and AVG currents for different modulation methods proposed in literature for DAB converter. To this end, voltage and current waveforms through the transformer have been characterized. Afterwards, these waveforms are employed to extract the analytical equations of the currents for future power losses evaluation. Finally, PLECS simulation model have been developed to validate the analytical equations obtained in this paper for a MEA case study.
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