A Comparative Study of Failure-Tolerant Three-phase RTRUs for More Electric Aircrafts

Akshay Singh, Ayan Mallik, A. Khaligh
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引用次数: 7

Abstract

The increased adoption of more electric aircrafts has been spurred by the development of onboard converters with high-efficiency and high gravimetric power density. Taking the example of a modular Regulated Transformer Rectifier Unit (RTRU) using GaN switches, this paper provides a comprehensive comparison of two possible design pathways for efficient conversion with higher power density – (i) high-frequency cascaded two-stage AC-DC conversion, and (ii) single-stage AC-DC conversion at a relatively lower frequency. The detailed system modeling and design methodology for the two converter topologies are laid out. As one of the key contributions of this work, a direct comparison of the two converter concepts based on achievable volumetric and gravimetric power densities and efficiencies has been presented. Using the developed model framework, an extensive analysis is done to gain greater insight into the effect of key design parameters on efficiency and power density. As a proof-of-concept, experimental results are presented to validate the theoretical predictions.
多电动飞机三相容错rtru的比较研究
高效率和高重量功率密度的机载变流器的发展推动了更多电动飞机的采用。本文以使用GaN开关的模块化稳压变压器整流单元(RTRU)为例,全面比较了两种可能的设计途径,以实现更高功率密度的高效转换——(i)高频级联两级AC-DC转换,以及(ii)相对较低频率的单级AC-DC转换。给出了两种转换器拓扑结构的详细系统建模和设计方法。作为这项工作的关键贡献之一,提出了基于可实现的体积和重量功率密度和效率的两种转换器概念的直接比较。使用开发的模型框架,进行了广泛的分析,以更深入地了解关键设计参数对效率和功率密度的影响。作为概念验证,给出了实验结果来验证理论预测。
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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