十二阶电压源变频器:使用平面变压器的三相六电平变频器

Haitham Kanakri;Euzeli Cipriano Dos Santos;Maher Rizkalla
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引用次数: 0

摘要

多电平逆变器(MLIs)在现代电动飞机应用的高速电机驱动系统中越来越受欢迎。然而,目前的多电平逆变器技术存在两个明显的局限性:(1)载波开关频率高,开关损耗大;(2)调制方案复杂,无法最大限度地利用直流电源。因此,要想快速发展未来的电动飞机系统,就必须开发新的拓扑结构来缓解这些限制。本文介绍了一种利用十二个开关和三个平面高频变压器的六级十二步逆变器(TSI)。采用所建议的配置可确保直流源的最大利用率,峰值相电压为 5V_{text{dc}}/3$。与传统的 MLI 相比,拟议解决方案的半导体损耗更小,超过了与中性点箝位(NPC)、飞行电容器(FC)和级联 H 桥(CHB)相关的传统 MLI。实验结果表明了 TSI 在静态和动态条件下的运行情况,以及在三种不同模式下运行的能力:三步、六步和十二步运行。论文还通过理论分析、有限元分析(FEA)和实验验证,对所提出的平面变压器进行了全面设计。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Twelve-Step Voltage Source Inverter: A Three-Phase Six-Levels Inverter Using Planar Transformers
Multi-level inverters (MLIs) are becoming increasingly popular in high-speed motor drive systems for modern electric aircraft applications. However, two significant limitations are associated with current MLIs technology: (1) the high switching losses due to the high carrier switching frequency and (2) the complex modulation schemes required to maximize the DC source utilization. Consequently, the development of new topologies to mitigate these limitations is imperative for the rapid advancement of future electric aircraft systems. This paper introduces a six-level twelve-step inverter (TSI) that utilizes twelve switches and three planar high-frequency transformers. Implementing the proposed configuration ensures maximum DC source utilization, with a peak phase voltage of $5V_{\text{dc}}/3$ . The proposed solution presents less semiconductor losses than the conventional MLIs, surpassing conventional MLIs, associated with neutral point clamped (NPC), flying capacitor (FC), and cascaded H-bridge (CHB). Experimental results demonstrate the TSI's operation under static and dynamic conditions and its capability to function in three different modes: three-step, six-step, and twelve-step operations. The paper also offers a comprehensive design of the proposed planar transformer, supported by theoretical analysis, finite element analysis (FEA), and experimental validation.
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