Thrust optimization of linear oscillatory actuator using permeance analysis method

This paper is described on optimization the thrust of linear oscillatory actuator (LOA). The objective of this optimization is to obtain the high thrust of LOA with restricted weight of LOA to make sure it operates at highest as possible the thrust while maintain it mobility features. Thus, the LOA...

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Main Authors: Abdul Shukor, Fairul Azhar, Misron, Norhisam, Mailah, Nashiren, Zare, Mohamad Reza, Wakiwaka, Hiroyuki, Nirei, Masami
Format: Article
Published: 2011
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Online Access:http://eprints.utem.edu.my/id/eprint/14152/
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spelling my.utem.eprints.141522015-01-26T03:20:27Z http://eprints.utem.edu.my/id/eprint/14152/ Thrust optimization of linear oscillatory actuator using permeance analysis method Abdul Shukor, Fairul Azhar Misron, Norhisam Mailah, Nashiren Zare, Mohamad Reza Wakiwaka, Hiroyuki Nirei, Masami TK Electrical engineering. Electronics Nuclear engineering This paper is described on optimization the thrust of linear oscillatory actuator (LOA). The objective of this optimization is to obtain the high thrust of LOA with restricted weight of LOA to make sure it operates at highest as possible the thrust while maintain it mobility features. Thus, the LOA is aim to have a starter thrust higher than 200 N while having total of weight lower than 2.0 kg. The thrust optimization is done using permeance analysis method (PAM). The thickness of the permanent magnets and the height of coils have been optimized at various total of radius of LOA in order to obtain the optimized structure of LOA. The optimized structure of LOA was decided by using two different methods. The first method is by evaluating the calculation output. The second method is by using generic algorithm. Both output of these method giving a different result in term of LOA PM’s thickness however having similar value of characteristics. The FEM and measurement results were used to verify the PAM output. Consequently, the LOA has been designed with optimum parameters which having value of starter thrust of 245 N and the total of weight is 2.0 kg . 2011-12 Article PeerReviewed Abdul Shukor, Fairul Azhar and Misron, Norhisam and Mailah, Nashiren and Zare, Mohamad Reza and Wakiwaka, Hiroyuki and Nirei, Masami (2011) Thrust optimization of linear oscillatory actuator using permeance analysis method. International Review of Electrical Engineering (I.R.E.E.). pp. 2229-2938. ISSN 1827-6679
institution Universiti Teknikal Malaysia Melaka
building UTEM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknikal Malaysia Melaka
content_source UTEM Institutional Repository
url_provider http://eprints.utem.edu.my/
topic TK Electrical engineering. Electronics Nuclear engineering
spellingShingle TK Electrical engineering. Electronics Nuclear engineering
Abdul Shukor, Fairul Azhar
Misron, Norhisam
Mailah, Nashiren
Zare, Mohamad Reza
Wakiwaka, Hiroyuki
Nirei, Masami
Thrust optimization of linear oscillatory actuator using permeance analysis method
description This paper is described on optimization the thrust of linear oscillatory actuator (LOA). The objective of this optimization is to obtain the high thrust of LOA with restricted weight of LOA to make sure it operates at highest as possible the thrust while maintain it mobility features. Thus, the LOA is aim to have a starter thrust higher than 200 N while having total of weight lower than 2.0 kg. The thrust optimization is done using permeance analysis method (PAM). The thickness of the permanent magnets and the height of coils have been optimized at various total of radius of LOA in order to obtain the optimized structure of LOA. The optimized structure of LOA was decided by using two different methods. The first method is by evaluating the calculation output. The second method is by using generic algorithm. Both output of these method giving a different result in term of LOA PM’s thickness however having similar value of characteristics. The FEM and measurement results were used to verify the PAM output. Consequently, the LOA has been designed with optimum parameters which having value of starter thrust of 245 N and the total of weight is 2.0 kg .
format Article
author Abdul Shukor, Fairul Azhar
Misron, Norhisam
Mailah, Nashiren
Zare, Mohamad Reza
Wakiwaka, Hiroyuki
Nirei, Masami
author_facet Abdul Shukor, Fairul Azhar
Misron, Norhisam
Mailah, Nashiren
Zare, Mohamad Reza
Wakiwaka, Hiroyuki
Nirei, Masami
author_sort Abdul Shukor, Fairul Azhar
title Thrust optimization of linear oscillatory actuator using permeance analysis method
title_short Thrust optimization of linear oscillatory actuator using permeance analysis method
title_full Thrust optimization of linear oscillatory actuator using permeance analysis method
title_fullStr Thrust optimization of linear oscillatory actuator using permeance analysis method
title_full_unstemmed Thrust optimization of linear oscillatory actuator using permeance analysis method
title_sort thrust optimization of linear oscillatory actuator using permeance analysis method
publishDate 2011
url http://eprints.utem.edu.my/id/eprint/14152/
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score 13.159267