跳到主要导航 跳到搜索 跳到主要内容

Thermal design of an integrated inductor for 45kW aerospace starter-generator

  • A. La Rocca
  • , M. Raza Khowja
  • , G. Vakil
  • , C. Gerada
  • , P. Wheeler
  • , L. Yan
  • University of Nottingham

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper presents a combined electromagnetic and thermal design of integrated inductor, for the application of a 45kW aircraft starter-generator. The inductor is designed at high current density by using the apporach of area product, followed by the finite element analysis, which validates the electromagnetic performance of integrated inductor. The total power losses at 8, 20, and 32kRPM are evaluated in order to investigate the thermal design of a combined starter-generator and integrated inductor system, whilst, achieving the full integration from a thermal management point of view. As both starter/generator and inductor share common cooling configuration; performance of a direct and an indirect cooling options are compared. The direct cooling configuration, based on a semi-flooded design, can lead to a temperature reduction up to 90°C in the most critical components.

源语言英语
主期刊名2020 IEEE Transportation Electrification Conference and Expo, ITEC 2020
出版商Institute of Electrical and Electronics Engineers Inc.
703-708
页数6
ISBN(电子版)9781728146294
DOI
出版状态已出版 - 6月 2020
活动2020 IEEE Transportation Electrification Conference and Expo, ITEC 2020 - Chicago, 美国
期限: 23 6月 202026 6月 2020

出版系列

姓名2020 IEEE Transportation Electrification Conference and Expo, ITEC 2020

会议

会议2020 IEEE Transportation Electrification Conference and Expo, ITEC 2020
国家/地区美国
Chicago
时期23/06/2026/06/20

指纹

探究 'Thermal design of an integrated inductor for 45kW aerospace starter-generator' 的科研主题。它们共同构成独一无二的指纹。

引用此