A flexoelectric cantilever beam actuated by the converse flexoelectric effect is evaluated and its analytical and experimental data are compared in this study. A line-electrode on the top beam surface and a bottom surface electrode are used to generate an electric field gradient in the beam, so that internal stresses can be induced and applied to distributed actuations. The dynamic control effectiveness of the beam is investigated with a mathematical model and is validated by laboratory experiments. Analyses show that the actuation stress induced by the converse flexoelectric effect is in the longitudinal direction and results in a bending control moment to the flexoelectric beam since the stress in the thickness is inhomogeneous. It is found that thinner line-electrode radius and thinner flexoelectric beam lead to larger control effects on the beam. The position of the line-electrode on the top surface of the beam also influences the control effect. When the line-electrode is close to the fixed end, it induces a larger tip displacement than that is close to the free end. Analytical results agree well with laboratory experimental data. This study of flexoelectric actuation and control provides a fundamental understanding of flexoelectric actuation mechanisms.
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August 2018
Research-Article
Dynamic Flexoelectric Actuation and Vibration Control of Beams
Mu Fan,
Mu Fan
State Key Laboratory of Mechanics and Control
of Mechanical Structures,
Interdisciplinary Research Institute of Aeronautics
and Astronautics,
Nanjing University of Aeronautics
and Astronautics,
Room 217, Building A18, #29 Yu Dao Street,
Nanjing 210016, China
e-mail: mfanz@nuaa.edu.cn
of Mechanical Structures,
Interdisciplinary Research Institute of Aeronautics
and Astronautics,
Nanjing University of Aeronautics
and Astronautics,
Room 217, Building A18, #29 Yu Dao Street,
Nanjing 210016, China
e-mail: mfanz@nuaa.edu.cn
Search for other works by this author on:
Bolei Deng,
Bolei Deng
StrucTronics and Control Lab,
School of Aeronautics and Astronautics,
Zhejiang University,
Hangzhou 310058, China
e-mail: dengbolei@zju.edu.cn
School of Aeronautics and Astronautics,
Zhejiang University,
Hangzhou 310058, China
e-mail: dengbolei@zju.edu.cn
Search for other works by this author on:
Hornsen Tzou
Hornsen Tzou
Fellow ASME
State Key Laboratory of Mechanics and Control
of Mechanical Structures,
Interdisciplinary Research Institute of Aeronautics
and Astronautics,
Nanjing University of Aeronautics
and Astronautics,
Room 202, Building A18, #29 Yu Dao Street,
Nanjing 210016, China
e-mail: hstzou@nuaa.edu.cn
State Key Laboratory of Mechanics and Control
of Mechanical Structures,
Interdisciplinary Research Institute of Aeronautics
and Astronautics,
Nanjing University of Aeronautics
and Astronautics,
Room 202, Building A18, #29 Yu Dao Street,
Nanjing 210016, China
e-mail: hstzou@nuaa.edu.cn
Search for other works by this author on:
Mu Fan
State Key Laboratory of Mechanics and Control
of Mechanical Structures,
Interdisciplinary Research Institute of Aeronautics
and Astronautics,
Nanjing University of Aeronautics
and Astronautics,
Room 217, Building A18, #29 Yu Dao Street,
Nanjing 210016, China
e-mail: mfanz@nuaa.edu.cn
of Mechanical Structures,
Interdisciplinary Research Institute of Aeronautics
and Astronautics,
Nanjing University of Aeronautics
and Astronautics,
Room 217, Building A18, #29 Yu Dao Street,
Nanjing 210016, China
e-mail: mfanz@nuaa.edu.cn
Bolei Deng
StrucTronics and Control Lab,
School of Aeronautics and Astronautics,
Zhejiang University,
Hangzhou 310058, China
e-mail: dengbolei@zju.edu.cn
School of Aeronautics and Astronautics,
Zhejiang University,
Hangzhou 310058, China
e-mail: dengbolei@zju.edu.cn
Hornsen Tzou
Fellow ASME
State Key Laboratory of Mechanics and Control
of Mechanical Structures,
Interdisciplinary Research Institute of Aeronautics
and Astronautics,
Nanjing University of Aeronautics
and Astronautics,
Room 202, Building A18, #29 Yu Dao Street,
Nanjing 210016, China
e-mail: hstzou@nuaa.edu.cn
State Key Laboratory of Mechanics and Control
of Mechanical Structures,
Interdisciplinary Research Institute of Aeronautics
and Astronautics,
Nanjing University of Aeronautics
and Astronautics,
Room 202, Building A18, #29 Yu Dao Street,
Nanjing 210016, China
e-mail: hstzou@nuaa.edu.cn
Contributed by the Technical Committee on Vibration and Sound of ASME for publication in the JOURNAL OF VIBRATION AND ACOUSTICS. Manuscript received May 4, 2017; final manuscript received January 5, 2018; published online February 23, 2018. Assoc. Editor: Mahmoud Hussein.
J. Vib. Acoust. Aug 2018, 140(4): 041005 (10 pages)
Published Online: February 23, 2018
Article history
Received:
May 4, 2017
Revised:
January 5, 2018
Citation
Fan, M., Deng, B., and Tzou, H. (February 23, 2018). "Dynamic Flexoelectric Actuation and Vibration Control of Beams." ASME. J. Vib. Acoust. August 2018; 140(4): 041005. https://doi.org/10.1115/1.4039238
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