Vibration control of the composite beam integrated with curved piezoelectric "bers is investigated. Sensory and actuating equations of the curved piezoelectric "bers embedded in a composite slender beam are derived, and expressed in terms of line integrals. In addition, a new method for designing "b
Modeling and analysis of curved beams with debonded piezoelectric sensor/actuator patches
β Scribed by Dongchang Sun; Liyong Tong
- Publisher
- Elsevier Science
- Year
- 2002
- Tongue
- English
- Weight
- 324 KB
- Volume
- 44
- Category
- Article
- ISSN
- 0020-7403
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β¦ Synopsis
In this paper, a mathematical model for thin-walled curved beams with partially debonded piezoelectric actuator=sensor patches is presented for investigating the e ect of debonding of the actuator=sensor on their open-and closed-loop behaviors. The actuator equations and the sensor equations of the curved beam in perfectly bonded and debonded regions are derived. In the perfect bonding region, the adhesive layer is modeled to carry constant peel and shear stresses; while in the debonding area, it is assumed that there is no peel and shear stress transfer between the host beam and the piezoelectric layer. Both displacement continuity and force equilibrium conditions are imposed at the interfaces between the bonded and debonded regions. Based on the model and the sensing equation of the sensor, a closed-loop vibration control for the curved beams is performed. To obtain the frequency response from the presented model, a solution scheme for solving the complex governing equations is given. Using this model and the solution scheme, the e ects of the debonding of actuator and sensor patches on open-and closed-loop control are investigated through an example. The results show that edge debonding of the piezoelectric patch has a signiΓΏcant side e ect on the closed-loop control of the curved beams.
π SIMILAR VOLUMES
An analytical modeling of a circular curved beam with asymmetric surface-bonded piezoelectric actuators is developed in the paper. A circular unimorph with small curvature consists of a thin elastic layer and a thin piezoelectric layer. The unimorph is equivalent as a single layer structure, its sta
A detailed model for the beams with partially debonded active constraining damping (ACLD) treatment is presented. In this model, the transverse displacement of the constraining layer is considered to be non-identical to that of the host structure. In the perfect bonding region, the viscoelastic core