2015
DOI: 10.1108/compel-11-2013-0366
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Torque ripple reduction of synchronous reluctance machines

Abstract: Purpose – The purpose of this paper is to investigate the influence of stator and rotor pole number combinations together with the flux-barrier layers number on the performance of synchronous reluctance machine with emphasis on output torque capability and torque ripple. Design/methodology/approach – AC synchronous reluctance machine (SynRM) or permanent magnet assisted SynRM presently receives a great deal of interest, since there is le… Show more

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Cited by 14 publications
(8 citation statements)
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“…(a) the number of stator slots should be maximized as much as possible; (b) the number of rotor layers can be selected based on [14] or the following Table 1 given in [22,23]. Then, to choose the flux-barriers angles, we propose an angle β (see Figure 2) and use it to control the rotor slot pitch angle γ.…”
Section: Flux-barrier Angle Selectionmentioning
confidence: 99%
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“…(a) the number of stator slots should be maximized as much as possible; (b) the number of rotor layers can be selected based on [14] or the following Table 1 given in [22,23]. Then, to choose the flux-barriers angles, we propose an angle β (see Figure 2) and use it to control the rotor slot pitch angle γ.…”
Section: Flux-barrier Angle Selectionmentioning
confidence: 99%
“…Eventually, the positive and negative torque pulsations may cancel each other, resulting in a reduced torque ripple for the SynRM. Based on [14,22,23], we can propose a new approach that can produce a preliminary SynRM design with low torque ripple and better average torque by considering the following steps:…”
Section: Flux-barrier Angle Selectionmentioning
confidence: 99%
“…1 includes Heights of the barriers (h b1 , h b2 , h b3 ), Length of the barriers (l b1 , l b2 , l b3 ), Angular positions at airgap, (∆δ 1 , ∆δ 2 , ∆δ 3 ) defined with respect to centre of the shaft, Flux barrier tip angles (β 1 , β 2 , β 3 ) measured between the ends of the flux barriers, defined with respect to centre of the shaft, Iron rib thickness(t i ), the thickness between the end of the flux barriers and periphery of the rotor and Air gap length (a g ). The lamination of the prototype rotor used for analysis is based on significant contributions made in [3,12,26], and is shown in Fig. 2.…”
Section: Finite Element Model Validationmentioning
confidence: 99%
“…The flux barrier tip angles [11,12] (β 1 , β 2 , β 3 ), describes the extent bounded by the flux barrier ends in degrees. .…”
Section: Influence Of Flux Barrier Tip Anglesmentioning
confidence: 99%
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