Design of Flexible Wing with Embedded Piezoelectric Actuator
This paper introduces a new kind of flexible wing with embedded piezoelectric actuator as framework for Micro Air Vehicles (MAV), which was fixed spar in the previous flexible wing. This made it a controllable flexible wing because the new flexible wing can not only works as previous model without c...
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Published in | Applied Mechanics and Materials Vol. 325-326; pp. 951 - 955 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
Published |
Zurich
Trans Tech Publications Ltd
13.06.2013
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Subjects | |
Online Access | Get full text |
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Summary: | This paper introduces a new kind of flexible wing with embedded piezoelectric actuator as framework for Micro Air Vehicles (MAV), which was fixed spar in the previous flexible wing. This made it a controllable flexible wing because the new flexible wing can not only works as previous model without control, but also can change its wing profiles in our purpose by using the embedded piezoelectric actuator when its necessary. The mathematical model of the deformation of piezoelectric actuator under control has developed. with which the structure of the flexible wing was designed. The simulation of dynamic characteristic of the flexible wing with embedded piezoelectric actuator has been done with ANSYS software. |
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Bibliography: | Selected, peer reviewed papers from the ICMEP 2013 International Conference on Manufacturing Engineering and Process, April 13-14, 2013, Vancouver, Canada |
ISBN: | 9783037857076 3037857072 |
ISSN: | 1660-9336 1662-7482 1662-7482 |
DOI: | 10.4028/www.scientific.net/AMM.325-326.951 |