Characteristics and Optimization of a PMLSM for HTS Magnetic Suspension Propulsion System

Zheng, L; Jin, J; Guo, Y; Xu, W; Lu, H; Zhu, J

Characteristics and Optimization of a PMLSM for HTS Magnetic Suspension Propulsion System

Zheng, L Jin, J Guo, Y

Xu, W Lu, H

Zhu, J

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Publisher:: ASEMA and HTS World Pty. Ltd. Australia
Publication Type:: Journal Article
Citation:: Journal of Applied Superconductivity and Electromagnetics, 2011, 1 (1), pp. 66 - 74
Issue Date:: 2011-01

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Field	Value	Language
dc.contributor.author	Zheng, L	en_US
dc.contributor.author	Jin, J	en_US
dc.contributor.author	Guo, Y https://orcid.org/0000-0001-6182-0684	en_US
dc.contributor.author	Xu, W	en_US
dc.contributor.author	Lu, H https://orcid.org/0000-0001-5655-0237	en_US
dc.contributor.author	Zhu, J https://orcid.org/0000-0002-9763-4047	en_US
dc.date.issued	2011-01	en_US
dc.identifier.citation	Journal of Applied Superconductivity and Electromagnetics, 2011, 1 (1), pp. 66 - 74	en_US
dc.identifier.issn	1836-7151	en_US
dc.identifier.uri	http://hdl.handle.net/10453/15380
dc.description.abstract	¾Permanent magnet (PM) linear synchronous motors (PMLSMs) can be integrated with a high temperature superconducting (HTS) magnetic suspension system to be used in such as electromagnetic aircraft launcher and maglev transportation which have a levitated object moving on a long linear track. This paper presents the design and electromagnetic characteristic analysis of a long-primary single-sided PMLSM for a HTS bulk-PM guideway repulsion magnetic suspension propulsion system. Based on the characteristics and performance analysis of the PMLSM, a new type of HTS suspension propulsion system driven by a double-sided PMLSM with an optimal PM structure is then proposed. The running characteristics of the linear propulsion systems are studied through finite element analysis (FEA) with comprehensive performance results obtained for practical development.	en_US
dc.publisher	ASEMA and HTS World Pty. Ltd. Australia	en_US
dc.relation.ispartof	Journal of Applied Superconductivity and Electromagnetics	en_US
dc.title	Characteristics and Optimization of a PMLSM for HTS Magnetic Suspension Propulsion System	en_US
dc.type	Journal Article
utslib.citation.volume	1	en_US
utslib.for	0906 Electrical and Electronic Engineering	en_US
pubs.embargo.period	Not known	en_US
pubs.organisational-group	/University of Technology Sydney
pubs.organisational-group	/University of Technology Sydney/Faculty of Engineering and Information Technology
pubs.organisational-group	/University of Technology Sydney/Faculty of Engineering and Information Technology/School of Computer Science
pubs.organisational-group	/University of Technology Sydney/Faculty of Engineering and Information Technology/School of Electrical and Data Engineering
pubs.organisational-group	/University of Technology Sydney/Faculty of Engineering and Information Technology/School of Mechanical and Mechatronic Engineering
pubs.organisational-group	/University of Technology Sydney/Strength - CAI - Centre for Artificial Intelligence
pubs.organisational-group	/University of Technology Sydney/Strength - CCET - Centre for Clean Energy Technology
utslib.copyright.status	open_access
pubs.consider-herdc	true	en_US
pubs.issue	1	en_US
pubs.volume	1	en_US

Abstract:

¾Permanent magnet (PM) linear synchronous motors (PMLSMs) can be integrated with a high temperature superconducting (HTS) magnetic suspension system to be used in such as electromagnetic aircraft launcher and maglev transportation which have a levitated object moving on a long linear track. This paper presents the design and electromagnetic characteristic analysis of a long-primary single-sided PMLSM for a HTS bulk-PM guideway repulsion magnetic suspension propulsion system. Based on the characteristics and performance analysis of the PMLSM, a new type of HTS suspension propulsion system driven by a double-sided PMLSM with an optimal PM structure is then proposed. The running characteristics of the linear propulsion systems are studied through finite element analysis (FEA) with comprehensive performance results obtained for practical development.

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http://hdl.handle.net/10453/15380