The Study of the Autonomous Power Supply System of the More/All Electric Aircraft in AC/DC and DC/DC Processing

被引:1
|
作者
Setlak, Lucjan [1 ]
Kowalik, Rafal [1 ]
Redo, Wojciech [2 ]
机构
[1] Polish Air Force Acad, Dept Avion & Control Syst, PL-08521 Deblin, Poland
[2] Polish Air Force Acad, Ctr Training & Improvement Air Personnel, PL-08521 Deblin, Poland
关键词
study; power electronics systems; more/all electric aircraft; AC/DC and DC/DC processing;
D O I
10.1109/EECS.2017.63
中图分类号
TP301 [理论、方法];
学科分类号
081202 ;
摘要
The paper presents analysis, simulations and a mathematical model of transducers in the field of processing (conversion) of AC/DC and DC/DC. The proposed transducer model is designed for use in aviation, among others, it may be considered for use on both civil aircrafts of Airbus and Boeing companies (A-380 and A-350XWB, B-787) and Lockheed Martin (JSF F-35 and F-22 Raptor) military aircrafts compatible with the concept of more/all electric aircraft. The subject, and also the aim of this paper is to analyze and present the mathematical model and simulations of selected transducers in AC/DC and DC/DC processing. Based on the above, the final part of the paper presents an analysis of waveform simulations of selected transducers in the field of AC/DC and DC/DC processing performed in the Matlab/Simulink programming environment. In the final part the paper presents the main conclusions arising from the study of the basic component in terms of PES system, namely transducers AC/DC and DC/DC.
引用
收藏
页码:305 / 310
页数:6
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