Design Algorithm of an Aircraft Power Generation System

被引：5
作者：
Ismagilov, Flur Rashitovich [1 ]
Kiselev, Mikhail Anatolyevich [2 ]
Vavilov, Viacheslav Evgenievich [1 ]
Gusakov, Denis Valerievich [1 ]
机构：
[1] Ufa State Aviat Tech Univ, Ufa, Russia
[2] State Res Inst Aviat Syst, Moscow 125319, Russia
来源：
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2019年 / 55卷 / 06期
关键词：
Aircraft; Optimization; Windings; Aerospace electronics; Power generation; Standards; Rectifiers; Design algorithm; permanent magnet (PM) machines; power generation; pulse transformers;
D O I：
10.1109/TAES.2019.2894893
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The paper deals with the design and testing of a power generation system for the future and existing aircrafts. A new design algorithm of the power generation components is presented. The proposed design algorithm was tested on a prototype: a full-size starter-generator and transformer-rectifier unit prototype was created with a transformer magnetic core made up of an amorphous magnetic material. Its stand tests were carried out both for each element and for the entire system. The proposed algorithm can be used to create power supply systems for aircraft with different voltage levels, including 270 Vdc and 200 Vac. The developed power generation system turned out to be 25-40% better than serial solutions by mass and efficiency.
引用
收藏
页码：2899 / 2910
页数：12
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