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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Development of an Inertial Linear Ultrasonic Motor with a Double-Stator Structure Based on Bending Mode

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影响因子:2.7

DOI码:10.3390/app14188533

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:APPLIED SCIENCES-BASEL

关键字:linear ultrasonic motors inertial piezoelectric actuators finite element model bending mode

摘要:An inertial linear ultrasonic motor with a novel double-stator structure is proposed for achieving higher performance and resolution in this paper. Utilizing a symmetrical structure and single sawtooth wave signal, the prototype is capable of outputting effective linear motion based on inertial movement. The validity and rationality of the prototype are investigated by conducting finite element analyses. The experimental setups are built up to acquire the output characteristics of the motor . The experimental results indicate that the motor can achieve a maximum output velocity of 8.746 mm/s and thrust force of 1 .645 N, which is almost twice the output performance of a motor with a single stator. The displacement solution of the motor can be adjusted by changing the amplitude of the voltage, with a resolution of 27 nm. Simultaneously, the relationships between the output characteristics and the input parameters are measured and analyzed during the experiments. Compared to the actuators with complex structures and multi-signal drives, the proposed motor exhibits the merits of higher output performance with the double-stator structure , providing an alternative direction for the further development of the inertial linear ultrasonic motor .

论文类型:期刊论文

学科门类:工学

文献类型:J

卷号:14

期号:18

是否译文:

发表时间:2024-01-01

收录刊物:EI、SCIE

合写作者:Xiong, Yue,Hong, Xinwei,Wen, Jiaquan,Zhang, Jie,Zhao, Rongcheng