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Design Optimization of Reluctance-Synchronous Linear Machines for Electromagnetic Aircraft Launch System
This paper describes the design optimization and analysis of reluctance-synchronous linear motor with a solid or laminated moving part (secondary). The calculation of the motor performance is described using analytical formulation and numerical method. The main advantage of this system is the remova...
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Published in: | IEEE transactions on magnetics 2009-01, Vol.45 (1), p.389-395 |
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container_title | IEEE transactions on magnetics |
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creator | Mirzaei, M. Abdollahi, S.E. |
description | This paper describes the design optimization and analysis of reluctance-synchronous linear motor with a solid or laminated moving part (secondary). The calculation of the motor performance is described using analytical formulation and numerical method. The main advantage of this system is the removal of permanent-magnet secondary and replacing it with a reluctance-type secondary. The first purpose of this paper is designing a reluctance-synchronous linear motor with the maximum-output thrust force and optimum power factor. In this model, a long primary (armature) and a short secondary are evaluated. Distributed winding is considered for design and analysis. Finally, air-gap winding configuration is evaluated. |
doi_str_mv | 10.1109/TMAG.2008.2008977 |
format | article |
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The calculation of the motor performance is described using analytical formulation and numerical method. The main advantage of this system is the removal of permanent-magnet secondary and replacing it with a reluctance-type secondary. The first purpose of this paper is designing a reluctance-synchronous linear motor with the maximum-output thrust force and optimum power factor. In this model, a long primary (armature) and a short secondary are evaluated. Distributed winding is considered for design and analysis. Finally, air-gap winding configuration is evaluated.</description><identifier>ISSN: 0018-9464</identifier><identifier>EISSN: 1941-0069</identifier><identifier>DOI: 10.1109/TMAG.2008.2008977</identifier><identifier>CODEN: IEMGAQ</identifier><language>eng</language><publisher>New York, NY: IEEE</publisher><subject>Aircraft components ; Aircraft propulsion ; Cross-disciplinary physics: materials science; rheology ; Design and analysis ; Design engineering ; Design optimization ; Electromagnetic analysis ; Electromagnetic forces ; electromagnetic launcher ; Electromagnetic launching ; Exact sciences and technology ; Finite element methods ; finite-element method ; Magnetic flux ; Magnetism ; Materials science ; Mathematical analysis ; Mathematical models ; Motors ; Optimization ; Other topics in materials science ; Physics ; Reactive power ; reluctance-synchronous linear motor ; Saturation magnetization ; Synchronous motors ; Winding</subject><ispartof>IEEE transactions on magnetics, 2009-01, Vol.45 (1), p.389-395</ispartof><rights>2009 INIST-CNRS</rights><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. (IEEE) 2009</rights><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c386t-ec354dfe7cc31113a9567251991d9bb1f5e88274e0613eedd32cad7226892e573</citedby><cites>FETCH-LOGICAL-c386t-ec354dfe7cc31113a9567251991d9bb1f5e88274e0613eedd32cad7226892e573</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/4773609$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>309,310,314,780,784,789,790,4050,4051,23930,23931,25140,27924,27925,54796</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=21235373$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Mirzaei, M.</creatorcontrib><creatorcontrib>Abdollahi, S.E.</creatorcontrib><title>Design Optimization of Reluctance-Synchronous Linear Machines for Electromagnetic Aircraft Launch System</title><title>IEEE transactions on magnetics</title><addtitle>TMAG</addtitle><description>This paper describes the design optimization and analysis of reluctance-synchronous linear motor with a solid or laminated moving part (secondary). The calculation of the motor performance is described using analytical formulation and numerical method. The main advantage of this system is the removal of permanent-magnet secondary and replacing it with a reluctance-type secondary. The first purpose of this paper is designing a reluctance-synchronous linear motor with the maximum-output thrust force and optimum power factor. In this model, a long primary (armature) and a short secondary are evaluated. Distributed winding is considered for design and analysis. Finally, air-gap winding configuration is evaluated.</description><subject>Aircraft components</subject><subject>Aircraft propulsion</subject><subject>Cross-disciplinary physics: materials science; rheology</subject><subject>Design and analysis</subject><subject>Design engineering</subject><subject>Design optimization</subject><subject>Electromagnetic analysis</subject><subject>Electromagnetic forces</subject><subject>electromagnetic launcher</subject><subject>Electromagnetic launching</subject><subject>Exact sciences and technology</subject><subject>Finite element methods</subject><subject>finite-element method</subject><subject>Magnetic flux</subject><subject>Magnetism</subject><subject>Materials science</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Motors</subject><subject>Optimization</subject><subject>Other topics in materials science</subject><subject>Physics</subject><subject>Reactive power</subject><subject>reluctance-synchronous linear motor</subject><subject>Saturation magnetization</subject><subject>Synchronous motors</subject><subject>Winding</subject><issn>0018-9464</issn><issn>1941-0069</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2009</creationdate><recordtype>article</recordtype><recordid>eNp9kcFvFCEUxidGE9fqH2C8EBONl6k8YGA4bmqtJts0sfVMKPOmSzMDKzCH9a-XdTc9ePACvPD7vuR7X9O8BXoOQPXnu-v11TmjtP97aKWeNSvQAlpKpX7erCiFvtVCipfNq5wf6yg6oKtm-wWzfwjkZlf87H_b4mMgcSQ_cFpcscFhe7sPbptiiEsmGx_QJnJt3ba-MhljIpcTupLibB8CFu_I2ieX7FjIxi5VSW73ueD8unkx2injm9N91vz8enl38a3d3Fx9v1hvWsd7WVp0vBPDiMo5DgDc6k4q1oHWMOj7exg77HumBFIJHHEYOHN2UIzJXjPsFD9rPh59dyn-WjAXM_vscJpswJrAcCF6paWo4Kf_giAVcKmqdUXf_4M-xiWFGsP0ndQMRC8rBEfIpZhzwtHskp9t2hug5tCROXRkDvWYU0dV8-FkbLOz05jqwn1-EjJgvOOKV-7dkfOI-PQtqoOkmv8BlvCaLA</recordid><startdate>200901</startdate><enddate>200901</enddate><creator>Mirzaei, M.</creator><creator>Abdollahi, S.E.</creator><general>IEEE</general><general>Institute of Electrical and Electronics Engineers</general><general>The Institute of Electrical and Electronics Engineers, Inc. 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The calculation of the motor performance is described using analytical formulation and numerical method. The main advantage of this system is the removal of permanent-magnet secondary and replacing it with a reluctance-type secondary. The first purpose of this paper is designing a reluctance-synchronous linear motor with the maximum-output thrust force and optimum power factor. In this model, a long primary (armature) and a short secondary are evaluated. Distributed winding is considered for design and analysis. Finally, air-gap winding configuration is evaluated.</abstract><cop>New York, NY</cop><pub>IEEE</pub><doi>10.1109/TMAG.2008.2008977</doi><tpages>7</tpages></addata></record> |
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subjects | Aircraft components Aircraft propulsion Cross-disciplinary physics: materials science rheology Design and analysis Design engineering Design optimization Electromagnetic analysis Electromagnetic forces electromagnetic launcher Electromagnetic launching Exact sciences and technology Finite element methods finite-element method Magnetic flux Magnetism Materials science Mathematical analysis Mathematical models Motors Optimization Other topics in materials science Physics Reactive power reluctance-synchronous linear motor Saturation magnetization Synchronous motors Winding |
title | Design Optimization of Reluctance-Synchronous Linear Machines for Electromagnetic Aircraft Launch System |
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