Skip to main navigation Skip to search Skip to main content

Optimal design of high power linear permanent magnet synchronous motor for aircraft launch

  • Shuanghui Hao*
  • , Zili Tang
  • , Ruizheng Long
  • , Minghui Hao
  • *Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Design optimization and analysis of the high power linear permanent magnet synchronous motor for aircraft launch are presented in this paper. This motor has a decentralized stator that runs the entire length of travel. A plate with an array of permanent magnets is used as the secondary. This structure enables easier manufacture, flexible system assembling, and autonomous decentralized control employed for energy saving. The thrust and cogging force of the motor are highly affected by the motor structural parameters. The influences of these structural parameters on the thrust and cogging force are analyzed by finite element analysis method; experiment studies are carried out to support the theoretical analysis.

Original languageEnglish
Title of host publicationFuture Material Research and Industry Application, FMRIA 2011
Pages1160-1168
Number of pages9
DOIs
StatePublished - 2012
Externally publishedYes
Event2011 SSITE International Conference on Future Material Research and Industry Application, FMRIA 2011 - Macau, China
Duration: 1 Dec 20112 Dec 2011

Publication series

NameAdvanced Materials Research
Volume455-456
ISSN (Print)1022-6680

Conference

Conference2011 SSITE International Conference on Future Material Research and Industry Application, FMRIA 2011
Country/TerritoryChina
CityMacau
Period1/12/112/12/11

Keywords

  • Electromagnetic launching
  • High power
  • Linear permanent magnet synchronous motors
  • Motor design

Fingerprint

Dive into the research topics of 'Optimal design of high power linear permanent magnet synchronous motor for aircraft launch'. Together they form a unique fingerprint.

Cite this