A Holistic Electrical Machine Design Tool for More-Electric and Hybrid-Electric Aircraft

被引：0
|
作者：
Golovanov, Dmitry [1 ]
Gerada, David [1 ,2 ]
Papini, Luca [1 ]
Xu, Zeyuan [1 ,2 ]
Gerada, Chris [1 ,2 ]
机构：
[1] Univ Nottingham, Dept Elect Engn, Nottingham, England
[2] Univ Nottingham, Sch Engn, Ningbo, Zhejiang, Peoples R China
来源：
2018 IEEE INTERNATIONAL CONFERENCE ON ELECTRICAL SYSTEMS FOR AIRCRAFT, RAILWAY, SHIP PROPULSION AND ROAD VEHICLES & INTERNATIONAL TRANSPORTATION ELECTRIFICATION CONFERENCE (ESARS-ITEC) | 2018年
关键词：
high power density; permanent magnet machines; multi-domain; optimization; coolant; flow-rate;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
The power density of electrical machines required for more-electric and hybrid-electric aircraft has become a critical aspect and target of optimization. This paper looks at the development aspects of a multi-domain tool to aid for system-level optimization of electrical machines within next-generation high power-density aerospace applications. The electromagnetic, thermal and mechanical aspects are wholly integrated, thus enabling the optimization including the non-active mass. The implementation and overall architecture are described with the aim of investigating the impact of coolant flowrate, coolant mediumas well as efficiency on the achievable power tomass ratio.
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收藏
页数：6
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