Abstract
This paper presents a design study of a 3-phase AC main exciter (ME) for an aircraft starter-generator. A computationally efficient methodology for optimizing the design of the ME is presented. The optimisation is carried out using coupled two-dimensional (2D) magnetostatic finite element solver and particle swarm optimisation procedure (PSO). The ME design is then analysed using 3D FE to account for the end-winding effects, and the results are fed into a lumped-parameter circuit model of the ME. The circuit model allows for the operating modes of the ME being analysed in a computationally efficient manner also accounting for non-linearities. The theoretical findings are experimentally validated on a prototype generator.
Translated title of the contribution | Design Study of a Three-Phase Exciter for Aircraft Starter/Generator |
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Original language | English |
Title of host publication | 2011 IEEE Energy Conversion Congress and Exposition |
Place of Publication | NEW YORK |
Publisher | IEEE Computer Society |
Pages | 3998-4004 |
Number of pages | 7 |
ISBN (Print) | 978-1-4577-0541-0 |
DOIs | |
Publication status | Published - 17 Sep 2011 |
Event | IEEE Energy Conversion Congress and Exposition (ECCE) - Phoenix, Argentina Duration: 17 Sep 2011 → 22 Sep 2011 |
Conference
Conference | IEEE Energy Conversion Congress and Exposition (ECCE) |
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Country/Territory | Argentina |
City | Phoenix |
Period | 17/09/11 → 22/09/11 |
Bibliographical note
Conference Organiser: IEEEKeywords
- aircraft starter-generator
- main exciter
- design optimisation