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首页> 外文期刊>IEEE Transactions on Aerospace and Electronic Systems >Design Algorithm of an Aircraft Power Generation System
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Design Algorithm of an Aircraft Power Generation System

机译：飞机发电系统的设计算法

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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.
机译：本文涉及对未来和现有飞机发电系统的设计和测试。提出了一种新的发电组件的设计算法。所提出的设计算法在原型上进行了测试：使用由无定形磁性材料组成的变压器磁芯来创建全尺寸起动发电机和变压器 - 整流器单元原型。它的支架测试是针对每个元素和整个系统进行的。所提出的算法可用于为具有不同电压电平的飞机产生电源系统，包括270 VDC和200 VAC。开发的发电系统比质量和效率优于串行解决方案，优于25-40％。

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