Performance analysis of more electric aircraft starter/generator by different electric loads

被引：0

作者：

Kaya, Ufuk ^{[1
]}

Oksuztepe, Eyyup ^{[1
]}

机构：

[1] Firat Univ, Dept Avion, Sch Aviat, Elazig, Turkiye

来源：

INTERNATIONAL JOURNAL OF SUSTAINABLE AVIATION | 2023年 / 9卷 / 02期

关键词：

more electric aircraft; MEA; starter; generator; aircraft; permanent magnet synchronous machine; PMSM; electrical power generation; GENERATOR; SYSTEM; CHALLENGES;

D O I：

10.1504/IJSA.2023.129931

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The more electric aircraft is a trending topic in aviation studies. This topic comprises a wide range of applications that are directly related to electrical machines and power electronics. The starter/generator is one of these remarkable applications, and it is used for main engine cranking and required electrical power generation. In comparison with conventional starter and generator systems, the starter/generator is more robust, reliable, and cheap. Also, it requires almost no maintenance. Considering the increased demand for electrical power in commercial and military aircraft, the interest in starter/generators is increased in terms of scientific studies and industrial applications. In this study, a 20 kW starter/generator based on a three-phase surface-mounted permanent magnet synchronous machine is proposed and model reliability is tested with different types of and power-rated electrical loads. The proposed model is simulated at MATLAB/Simulink with Simscape blocks. The results show that the SG has sufficient performance for starter, and generator operation.

引用

页码：115 / 131

页数：18

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