Back to Search Start Over

A piezo-driven flapping wing mechanism for micro air vehicles.

Authors :
Peng, Yuxin
Cao, Jie
Liu, Li
Yu, Haoyong
Source :
Microsystem Technologies. Apr2017, Vol. 23 Issue 4, p967-973. 7p.
Publication Year :
2017

Abstract

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. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
09467076
Volume :
23
Issue :
4
Database :
Academic Search Index
Journal :
Microsystem Technologies
Publication Type :
Academic Journal
Accession number :
121742739
Full Text :
https://doi.org/10.1007/s00542-015-2762-6