Ac-Dc multi pulse converter for dc power distribution system in aircraft

IF 3.1 Q1 ENGINEERING, MULTIDISCIPLINARY
Erol Can, Ugur Kilic
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引用次数: 0

Abstract

ABSTRACTThe Transformer Rectifier Unit (TRU) in aircraft is DC power supplies. Three-phase AC power supplies are available as long as they work. DC power distribution, on the other hand, provides DC power directly to all DC users, providing input power to the emergency AC distribution system so that the static inverter can generate AC power. To the voltages produced by TRUs to be less oscillating and of higher quality, multi-pulse ones are studied and recommended for aircraft systems. In this study, Zener diode filtered multi-pulse rectifier, which can further reduce the oscillations in the output voltage, is recommended for aircraft. Three-phase half-wave rectifier design and analysis are presented to better demonstrate the effectiveness of Zener diode regulation in multi-pulse TRUs. First, the parts of the power system, which includes the rectifier circuit of a two-engine aircraft and fed by this rectifier, are given. The circuit structure and working order of the rectifier are given with mathematical explanations. In the application phase, low oscillating output voltages and currents are obtained by creating currents and voltages on the load for different Zener voltages. Conventional rectifiers and the proposed rectifier are tested on the same loads, and comparisons are done.KEYWORDS: TRUZener diode regulationtwo-engine aircraft Disclosure statementThe author does not have any competing financial, professional, or personal interests from other parties.Additional informationNotes on contributorsErol CanErol Can received his master’s degree in 2010 from the Department of Electrical Engineering at Karadeniz Technical University. He received his Ph.D. from the Department of Electric at Gazi University in 2016. He still works at Erzincan Binali Yıldırım University as Assoc. Prof. Dr.Ugur KilicUgur Kilic received his master’s degree in 2016 from the Department of Electrical and Electronics Engineering at Fırat University. He received his Ph.D. from the Department of Avionics at Eskisehir Technical University in 2021. He still works at Erzincan Binali Yıldırım University as Asst. Prof. Dr.
用于飞机直流配电系统的交直流多脉冲变换器
摘要飞机上的变压器整流单元(TRU)是直流电源。三相交流电源只要能正常工作就可以使用。而直流配电则直接向所有直流用户提供直流电源,为应急交流配电系统提供输入电源,使静态逆变器产生交流电源。为了使truu产生的电压振荡更小、质量更高,研究并推荐了多脉冲truu用于飞机系统。本研究推荐采用齐纳二极管滤波的多脉冲整流器,进一步减小了输出电压的振荡。为了更好地说明齐纳二极管调节在多脉冲tru中的有效性,给出了三相半波整流器的设计和分析。首先,给出了包括双发飞机整流电路和由该整流电路供电的动力系统的组成部分。给出了整流器的电路结构和工作顺序,并进行了数学解释。在应用阶段,通过在负载上创建不同齐纳电压的电流和电压来获得低振荡输出电压和电流。对传统整流器和该整流器在相同负载下进行了测试,并进行了比较。关键词:TRUZener二极管法规双引擎飞机披露声明作者没有任何与其他各方竞争的财务,专业或个人利益。serol canol Can于2010年获得Karadeniz Technical University电子工程系硕士学位。2016年获加济大学电气系博士学位。他仍然在Erzincan Binali Yıldırım大学担任助理。ugur Kilic博士于2016年获得Fırat大学电气与电子工程系硕士学位。他于2021年获得Eskisehir Technical University航空电子系博士学位。他仍然在Erzincan Binali Yıldırım大学担任助理教授和博士。
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来源期刊
INTERNATIONAL JOURNAL OF MODELLING AND SIMULATION
INTERNATIONAL JOURNAL OF MODELLING AND SIMULATION Engineering-Industrial and Manufacturing Engineering
CiteScore
6.10
自引率
32.30%
发文量
66
期刊介绍: This journal was first published in 1981 and covers languages, hardware, software, methodology, identification, numerical methods, graphical methods, VLSI, microcomputers in simulation, and applications in all fields. It appears quarterly.
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