Design and Experimental Verification of a High Force Density Tubular Permanent Magnet Linear Motor for Aerospace Application

被引:0
|
作者
Kano, Yoshiaki [1 ]
Satou, Kousuke [2 ]
机构
[1] Daido University
[2] KYB Corporation
关键词
Aerospace applications;
D O I
10.4271/2019-01-1911
中图分类号
学科分类号
摘要
This paper presents the design and construction of a high force density tubular permanent-magnet (PM) linear motor. A strut structure of a tubular PM linear motor developed to improve resistance to impurities and structural rigidity is described. In the design, computationally efficient two-dimensional finite-element analysis is used to estimate the motor force density. The motor's design is optimized for the major pole number/slot number combinations of 8/24, 16/24, 20/24, 28/24, 32/24, and 40/24. The optimized motor design of a three-phase 16/24 combination with one-layer winding achieved the highest force-to-mass density. The force-to-mass density of the designed motor is higher than that of the first prototype motor by a factor of 5. The validity of the proposed design method and the expected drive characteristics are experimentally verified using the prototype. © 2019 SAE International. All Rights Reserved.
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页码:818 / 827
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