Design of an HTS levitated double-sided HTSLSM for maglev

Zheng, L; Jin, J; Guo, Y; Zhu, J

Design of an HTS levitated double-sided HTSLSM for maglev

Zheng, L Jin, J Guo, Y

Zhu, J

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Publication Type:: Conference Proceeding
Citation:: Physics Procedia, 2012, 36 pp. 1031 - 1036
Issue Date:: 2012-01-01

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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	Zhu, J https://orcid.org/0000-0002-9763-4047	en_US
dc.date.issued	2012-01-01	en_US
dc.identifier.citation	Physics Procedia, 2012, 36 pp. 1031 - 1036	en_US
dc.identifier.issn	1875-3884	en_US
dc.identifier.uri	http://hdl.handle.net/10453/120373
dc.description.abstract	© 2012 Published by Elsevier B.V. Selection and/or peer-review under responsibility of the Guest Editors. A hybrid high temperature superconducting (HTS) linear synchronous propulsion system composed of a double-sided HTS linear synchronous motor (HTSLSM) in the middle and HTS magnetic suspension sub-systems on both sides has been proposed for a middle-low-speed maglev. Three carriages has been made up for the proposed maglev, and each carriage consists of four HTSLSM modules. The HTSLSM has been designed to reach a speed of 69 km/h and a maximum thrust of 48.9 kN for each motor. The finite element analysis has been used for the theoretical verification. The results obtained show that the HTS linear propulsion system satisfies the principal requirements for the maglev.	en_US
dc.relation.ispartof	Physics Procedia	en_US
dc.relation.isbasedon	10.1016/j.phpro.2012.06.101	en_US
dc.rights	info:eu-repo/semantics/openAccess
dc.title	Design of an HTS levitated double-sided HTSLSM for maglev	en_US
dc.type	Conference Proceeding
utslib.citation.volume	36	en_US
utslib.for	0913 Mechanical 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 Electrical and Data Engineering
pubs.organisational-group	/University of Technology Sydney/Strength - CCET - Centre for Clean Energy Technology
utslib.copyright.status	open_access	*
pubs.publication-status	Published	en_US
pubs.volume	36	en_US

Abstract:

© 2012 Published by Elsevier B.V. Selection and/or peer-review under responsibility of the Guest Editors. A hybrid high temperature superconducting (HTS) linear synchronous propulsion system composed of a double-sided HTS linear synchronous motor (HTSLSM) in the middle and HTS magnetic suspension sub-systems on both sides has been proposed for a middle-low-speed maglev. Three carriages has been made up for the proposed maglev, and each carriage consists of four HTSLSM modules. The HTSLSM has been designed to reach a speed of 69 km/h and a maximum thrust of 48.9 kN for each motor. The finite element analysis has been used for the theoretical verification. The results obtained show that the HTS linear propulsion system satisfies the principal requirements for the maglev.

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http://hdl.handle.net/10453/120373