DocumentCode :
233967
Title :
Design, sensitivity analysis and fabrication of DC Linear Direct-Drive Motor (LDDM)
Author :
Ghodsi, Mojtaba ; Ozer, Abdullah ; Al-Yahmadi, Amer ; Zadegan, Mehran Nodari ; Hosseinzadeh, Nasser
Author_Institution :
Dept. of Mech. & Ind. Eng., Sultan Qaboos Univ., Muscat, Oman
fYear :
2014
fDate :
19-22 Oct. 2014
Firstpage :
628
Lastpage :
632
Abstract :
This paper presents a new analytical model for both magnetic flux density and thrust force in a DC tubular Linear Direct-Drive Motor (LDDM). Two-dimensional finite element method (FEM) is used for numerical analysis. Magnetic flux density and thrust force computed numerically shows a good agreement with the values resulted from proposed analytical model. This research, investigates the effect of some geometrical dimensions of LDDM. The sensitivity analysis of parameters highlights the influence of air gap, permanent magnet radius, coil´s length of phases and thickness of back-iron. It is found that lower air gap and thinner back-iron cause higher ratio of maximum thrust force to mover´s mass. Furthermore, the optimum value for coil´s length is also presented. The general shape of thrust force is also confirmed by experimental results.
Keywords :
DC motor drives; air gaps; finite element analysis; linear motors; magnetic flux; sensitivity analysis; FEM; LDDM; air gap; analytical model; back-iron; dc tubular linear direct-drive motor; geometrical dimensions; magnetic flux density; mover mass; permanent magnet radius; sensitivity analysis; thrust force; two-dimensional finite element method; Brushless motors; Coils; DC motors; Force; Hysteresis motors; Magnetic flux density; Permanent magnet motors; Analytical Analysis; DC tubular Linear Direct-Drive Motor; FEM; Sensitivity Analysis;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Renewable Energy Research and Application (ICRERA), 2014 International Conference on
Conference_Location :
Milwaukee, WI
Type :
conf
DOI :
10.1109/ICRERA.2014.7016461
Filename :
7016461
Link To Document :
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