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Design Algorithm of an Aircraft Power Generation System
IEEE Transactions on Aerospace and Electronic Systems ( IF 5.1 ) Pub Date : 2019-12-01 , DOI: 10.1109/taes.2019.2894893
Flur Rashitovich Ismagilov , Mikhail Anatolyevich Kiselev , Viacheslav Evgenievich Vavilov , Denis Valerievich Gusakov

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.

中文翻译:

飞机发电系统设计算法

该论文涉及未来和现有飞机的发电系统的设计和测试。提出了一种新的发电部件设计算法。所提出的设计算法在原型上进行了测试:使用由非晶磁性材料制成的变压器磁芯创建了全尺寸的启动发电机和变压器整流器单元原型。对每个元件和整个系统都进行了站立测试。所提出的算法可用于为具有不同电压水平的飞机创建电源系统,包括 270 Vdc 和 200 Vac。开发的发电系统在质量和效率方面比串行解决方案好 25-40%。
更新日期:2019-12-01
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