Volume 39 Issue 12
Dec.  2024
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ZHANG Hui, SUN Wei, LUO Haitao. Semi-analytical modeling and vibration reduction analysis of composite thin plate with MFC[J]. Journal of Aerospace Power, 2024, 39(12):20220990 doi: 10.13224/j.cnki.jasp.20220990
Citation: ZHANG Hui, SUN Wei, LUO Haitao. Semi-analytical modeling and vibration reduction analysis of composite thin plate with MFC[J]. Journal of Aerospace Power, 2024, 39(12):20220990 doi: 10.13224/j.cnki.jasp.20220990

Semi-analytical modeling and vibration reduction analysis of composite thin plate with MFC

doi: 10.13224/j.cnki.jasp.20220990
  • Received Date: 2022-12-29
    Available Online: 2024-05-10
  • Piezoelectric fiber composite (MFC) was used for active vibration control of cantilevered fiber reinforced composite sheet, its semi-analytical modeling method was studied, and the damping effect of active control was analyzed through theory and experiment. In the process of modeling, the contribution of MFC sensors/actuators to the mass matrix and stiffness matrix of the cantilever plate structure system was considered, and the Rayleigh damping and active damping provided by velocity feedback control were introduced together, so that the semi-analytical dynamic model can truly predict the active vibration reduction effect of MFC. A case study was carried out, and the rationality of the semi-analytical model was proved by the established experimental system. At the same time, theoretical analysis proved that the free attenuation vibration of composite plate can be suppressed obviously by MFC active control under the specified three kinds of loads: step, triangle and sinusoidal excitation. Furthermore, the vibration reduction effect of active control was quantitatively analyzed by experiments, showing that the free attenuation vibration of composite plate can be suppressed by MFC active control by 79.63%. Finally, based on the created semi-analytical dynamic model, the effects of control gain and MFC actuator position on active control were analyzed.

     

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