杨淋

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教授 硕士生导师

招生学科专业:
机械工程 -- 【招收硕士研究生】 -- 航空学院
航空宇航科学与技术 -- 【招收硕士研究生】 -- 航空学院
机械 -- 【招收硕士研究生】 -- 航空学院

毕业院校:南京航空航天大学

学位:工学博士学位

联系方式:yanglin@nuaa.edu.cn

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Mechanical simulation and contact analysis of the hybrid longitudinal-torsional ultrasonic motor

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DOI码:10.1016/j.ultras.2019.105982

所属单位:南京航空航天大学

教研室:航空学院-精密驱动与控制研究所

发表刊物:Ultrasonics

关键字:Ultrasonic motors Longitudinal-torsional vibration Finite element Mechanical simulation Contact analysis ADINA

摘要:A slender type of ultrasonic motor using longitudinal-torsional hybrid vibration is proposed and investigated in this paper. To acquire the response and mechanical capacity of the assembled and complete hybrid longitudinal-torsional ultrasonic motor, a 3D finite element model has been established by the commercial FE software ADINA. The numerical results agree with the experimental results in terms of the trend and the order of magnitude, meaning that it is easy to evaluate the mechanical characteristics of the motor before prototype manufacture. Meanwhile, the radial, circumferential and axial displacements of the contact nodes can be obtained to simulate the actual elliptical motions of the stator teeth. In addition, the practical contact mechanism between the stator and rotor can be accurately reflected by the stress nephogram of the contact surfaces. This research provides a convenient method for the structure optimization and mechanical capacity prediction of the hybrid longitudinal-torsional ultrasonic motor.

论文类型:期刊论文

学科门类:工学

文献类型:J

卷号:100

期号:UNSP 105982

是否译文:

发表时间:2019-08-20

收录刊物:EI、SCI

合写作者:Ren, Weihao,Ma, Chengcheng,Chen, Liang