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Full Length Article | Open Access

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

Rui QIa,b, Liang WANGa,b( ), Jiamei JINa,b, Lusheng YUANa,b, Ziyu SHENa,b, Yuning GEa,b
State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing 210016, China
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Peer review under responsibility of Editorial Committee of CJA

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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.

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Chinese Journal of Aeronautics

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Cite this article:
QI R, WANG L, JIN J, et al. An embedded piezoelectric actuator for active vibration control: Concept, modeling, simulation, and investigation. Chinese Journal of Aeronautics, 2025, 38(4). https://doi.org/10.1016/j.cja.2024.103345

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Received: 20 March 2024
Revised: 26 May 2024
Accepted: 11 July 2024
Published: 16 December 2024
© 2024 The Author(s). Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).