A piezo-driven flapping wing mechanism for micro air vehicles

Yuxin Peng, Jie Cao, Li Liu, Haoyong Yu*

*此作品的通讯作者

科研成果: 期刊稿件文章同行评审

19 引用 (Scopus)

摘要

In this paper, a novel flapping wing mechanism driven by a linear actuator is proposed. The linear actuator consists of a piezoelectric element and a permanent magnet. Based on the principle of impact drive mechanism, the linear actuator can move a reciprocating linear motion with a long travel range, which can be directly converted to a flapping motion via a crank-slider mechanism. In comparison with conventional flapping wing mechanisms driven by a rotary motor with a crank-rocker mechanism, no gearbox is needed in our design. Therefore, the proposed flapping wing mechanism can be made with small volume and light weight. A prototype was designed and constructed and experiments were carried out to test the performance of the flapping wing mechanism. The experimental results confirm that the designed flapping wing mechanism can obtain a continuous flapping motion by moving the linear actuator reciprocatingly.

源语言英语
页(从-至)967-973
页数7
期刊Microsystem Technologies
23
4
DOI
出版状态已出版 - 1 4月 2017

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