An embedded piezoelectric actuator for active vibration control: Concept, modeling, simulation, and investigation

Piezoelectric active vibration control holds paramount importance in space structures. An embedded piezoelectric actuator with a sandwich configuration is proposed, which enhances control accuracy by integrating various components. Firstly, the electromechanical coupling characteristics of the actuator are revealed, and the model is established. Secondly, the equivalent model of a cylindrical cantilever beam is investigated as the object, and the feasibility of the vibration control of the actuator is verified by simulation. Finally, the prototype comprised of two actuators, which respectively use the proposed embedded actuators for producing the vibration and suppressing the vibration, is developed, and the measurement system is constructed. Experimental results demonstrate the excellent control efficiency in two orthogonal directions, achieving a minimum vibration amplitude control of 0.001 02 mm and a maximum vibration control of −42.74 dB. The integrated structure offers fast response, lightness, adaptability, and high control efficiency, which is conducive to enhancing the vibration control.

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Publication Details

Journal
Chinese Journal of Aeronautics
Published
2024-12-16
DOI
https://doi.org/10.1016/j.cja.2024.103345
Citations
5
Primary Topic
Aeroelasticity and Vibration Control
Type
article
Field-Weighted Citation Impact
6.49
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article

An embedded piezoelectric actuator for active vibration control: Concept, modeling, simulation, and investigation

Lusheng Yuan, Rui Qi, Yuning Ge, Liang Wang et al.
5 citations
Chinese Journal of Aeronautics
Aeroelasticity and Vibration Control
6.49
article

An embedded piezoelectric actuator for active vibration control: Concept, modeling, simulation, and investigation

Lusheng Yuan, Rui Qi, Yuning Ge, Liang Wang, Ziyu Shen, Jiamei JIN
article en
5 citations

Abstract

Piezoelectric active vibration control holds paramount importance in space structures. An embedded piezoelectric actuator with a sandwich configuration is proposed, which enhances control accuracy by integrating various components. Firstly, the electromechanical coupling characteristics of the actuator are revealed, and the model is established. Secondly, the equivalent model of a cylindrical cantilever beam is investigated as the object, and the feasibility of the vibration control of the actuator is verified by simulation. Finally, the prototype comprised of two actuators, which respectively use the proposed embedded actuators for producing the vibration and suppressing the vibration, is developed, and the measurement system is constructed. Experimental results demonstrate the excellent control efficiency in two orthogonal directions, achieving a minimum vibration amplitude control of 0.001 02 mm and a maximum vibration control of −42.74 dB. The integrated structure offers fast response, lightness, adaptability, and high control efficiency, which is conducive to enhancing the vibration control.

Chinese Journal of AeronauticsVol. 38(4)
Nanjing University of Aeronautics and Astronautics (CN)
Affordable and clean energy
Openalex Percentile: Top 4%
Aeroelasticity and Vibration Control
6.49
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