Generic functional modelling of multi-pulse auto-transformer rectifier units for more-electric aircraft applications

被引:12
|
作者
Yang, Tao [1 ]
Bozhko, Serhiy [1 ]
Wheeler, Patrick [1 ]
Wang, Shaoping [2 ]
Wu, Shuai [2 ]
机构
[1] Univ Nottingham, Dept Elect & Elect Engn, Nottingham NG7 2RD, England
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100083, Peoples R China
关键词
Asymmetric transformer; Functional modelling; More-Electric Aircraft; Multi-pulse rectifier; Transformer rectifier unit; MOTOR-DRIVES;
D O I
10.1016/j.cja.2018.03.010
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The Auto-Transformer Rectifier Unit (ATRU) is one preferred solution for high-power AC/DC power conversion in aircraft. This is mainly due to its simple structure, high reliability and reduced kVA ratings. Indeed, the ATRU has become a preferred AC/DC solution to supply power to the electric environment control system on-board future aircraft. In this paper, a general modelling method for ATRUs is introduced. The developed model is based on the fact that the DC voltage and current are strongly related to the voltage and current vectors at the AC terminals of ATRUs. In this paper, we carry on our research in modelling symmetric 18-pulse ATRUs and develop a generic modelling technique. The developed generic model can study not only symmetric but also asymmetric ATRUs. An 18-pulse asymmetric ATRU is used to demonstrate the accuracy and efficiency of the developed model by comparing with corresponding detailed switching SABER models provided by our industrial partner. The functional models also allow accelerated and accurate simulations and thus enable whole-scale more-electric aircraft electrical power system studies in the future. (C) 2018 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd.
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页码:883 / 891
页数:9
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