共查询到17条相似文献,搜索用时 150 毫秒
1.
可控约束阻尼层板的控制实验研究 总被引:5,自引:0,他引:5
对具有可控约束阻尼层的板进行了振动控制实验研究. 以压电片作为作动器,根据测量的结构振动信号,反馈控制约束层的变形,抑制板的振动. 对试验件进行了试验模态分析,讨论了压电片的附加位置;采用比例反馈对试验件进行了控制试验;试验给出了控制效果和压电片面积的关系. 研究结果证明,这种利用粘弹性阻尼抑制结构的高频振动,利用压电材料的逆压电效应控制结构的低频振动的主被动杂交控制方式对薄壁结构的振动抑制效果显著,控制频率范围宽,可靠性高. 相似文献
2.
自感知主被动阻尼悬臂梁动态特性分析 总被引:3,自引:0,他引:3
由Hamilton原理导出了压电层作约束层作约束层的自感知主被动阻尼控制结构的振动控制方程;由自感知电压引入速度负反馈闭环控制,并由假设模态法将位移按模态展开,求解了悬臂梁结构的动态特征;对被动控制、自感知主动控制、自感知主被动控制的控制效果进行了分析比较;分析了粘弹层厚度变化、材料参数变化以及压电层厚度、位置等结构参数变化对控制效果及模态频率的影响;并对自感知主被动阻尼控制结构的特点和设计中应注 相似文献
3.
基于弹性、粘弹性和压电材料本构方程,应用能量法建立了主动约束层阻尼(ACLD)圆柱壳体的有限元动力学方程。通过对压电传感层自感电压的比例、微分反馈控制,对主动约束层阻尼(ACLD)圆柱壳体进行了主被动一体化振动控制,研究了复合圆柱壳体的动力学响应特性。讨论了主动约束层阻尼(ACLD)片体的位置、覆盖率、粘弹性层厚度及控制增益等关键参数对圆柱壳体振动特性的影响。研究表明:主动约束层阻尼(ACLD)片体的粘贴位置与模态有关,针对不同模态,应采用不同的粘贴位置;覆盖率、粘弹性层厚度及控制增益等直接影响到振幅衰减程度,通过对片体位置、覆盖率、粘弹性层厚度及控制增益等关键参数的优化,能有效降低主动约束层阻尼圆柱壳体的振动,具有十分重要的工程应用价值。 相似文献
4.
5.
采用压电机敏元件进行结构振动控制Ⅲ:控制系统设计与实验研究 总被引:5,自引:0,他引:5
采用作者在上篇导出的压电耦合体动力学模型,给出了压电主动阻尼控制系统的设计方法;导出了压电耦合梁系统的作动方程和检测方程的显式表达式。以此为基础,以简单梁为对象,对压电检测器和作动器的性能、粘结层的影响、压电主动阻尼控制及压电主、被动阻尼双控制进行了实验研究 相似文献
6.
主动约束层阻尼振动控制研究进展 总被引:4,自引:0,他引:4
主动约束层阻尼(Active Constrained Layer Damping, ACLD)是以可控的压电材料代替被动约束层中不可控的约束层,通过可控的约束层主动地控制黏弹性材料的剪切变形以进一步增大其对振动能量耗散的主动阻尼形式,它充分结合了主动控制与被动阻尼作用各自的优势,使得其在结构振动控制方面显示出极好的应用价值.本文首先解释了ACLD的基本结构和阻尼机理,然后综述了最近几年有关ACLD在结构建模,控制方案及结构优化等方面的最新研究进展,最后指出了应用前景并总结了进一步研究的问题. 相似文献
7.
8.
支架振动的主动控制研究 总被引:1,自引:1,他引:1
利用压电材料的机电耦合特性,采用数值分析和实验相结合的方法研究了压电材料对支架的振动控制。利用Hamilton原理,采用速度反馈,并考虑压电材料的机电耦合效应推导了振动主动控制有限元方程,分析了不同约束,不同压电片布置情况下支架的振动控制,实现了压电片的优化布置,同时用实验验证了数值分析的正确性。 相似文献
9.
10.
基于弹性、粘弹性、电磁学理论,应用Hamilton原理,导出了覆盖电磁约束层阻尼(EMCLD)主动控制方式的梁的控制方程,并针对覆盖EMCLD的悬臂梁,进行了主动控制仿真模拟,得到了较好的控制效果,分析了控制电流和阻尼层厚度对控制效果的影响.结果表明电磁约束阻尼技术具有结构简单、作动方式合理、耗能低的优点,是一种有效的振动主动控制方式. 相似文献
11.
This paper concerns in the active and passive hybrid control of vibration of the thin plate with Local Active Constrained
damping Layer (LACL). The governing equations of system are formulated based on the constitutive equations of elastic, viscoelastic,
piezoelectric materials. Galerkin method and GHM method are employed to transform partial differential equations into ordinary
ones with a lower dimension. LQR method of classical control theory is used in simulating calculation. Numeral results show
that the active and passive hybrid control manner obtained in this paper is a better one for vibration control of the plate.
Project supported by the National Science Foundation of China (19632001) and the Research Foundation of Xian Jiaotong University 相似文献
12.
The equations of motion governing the vibration of a cantilever beam with partially treated self-sensing active constrained
layer damping treatment(SACLD) are derived by application of the extended Hamilton principle. The assumed-modes method and
closed loop velocity feedback control law are used to analyze and control the flexural vibration of the beam. The influence
of the bonding layer and piezoelectric layer thickness, material properties, placements of the piezoelectric patch and feedback
control parameters on the actuation ability of the vibration suppression are investigated. Some design considerations for
pure passive, pure active control, and self-sensing active constrained layer damping are discussed.
The present work is supported by the National Natural Science Foundation of China (No. 59635140). 相似文献
13.
Seyedeh Marzieh Hosseini Alireza Shooshtari Hamed Kalhori S. Nima Mahmoodi 《Nonlinear dynamics》2014,78(1):571-583
This paper aims to study the nonlinear-forced vibrations of a viscoelastic cantilever with a piecewise piezoelectric actuator layer on its top surface using the method of Multiple Scales. The governing equation of motion is a second-order nonlinear ordinary differential equation with quadratic and cubic nonlinearities which appear in stiffness, inertia, and damping terms. The nonlinear terms are due to the piezoelectricity, viscoelasticity, and geometry of the system. Forced vibrations of the system are investigated in the cases of primary resonance and non-resonance hard excitation including subharmonic and superharmonic resonances. Analytical expressions for frequency responses are derived, and the effects of different parameters including damping coefficient, thickness to width ratio of the beam, length and position of the piezoelectric layer, density of the beam, and the piezoelectric coefficient on the frequency-response curves are discussed for each case. It is shown that in all these cases, the response of the system follows a softening behavior due to the existence of the piezoelectric layer. The piezoelectric layer provides an effective tool for active control of vibration. In addition, the effect of the viscoelasticity of the beam on passive control of amplitude of vibration is illustrated. 相似文献
14.
15.
弹性板振动的多模态主动控制 总被引:2,自引:0,他引:2
采用多对压电片对板振动的多阶模态进行主动控制。为了改善结构振动控制的效果,本文对选用结构振动能量和控制信号能量作为控制目标函数的LQR控制算法作了初步研究。首先,按能量准则推导了控制目标函数中权系数矩阵(Q矩阵和R矩阵)的理论计算公式,为权系数矩阵的选取提供了一定的理论依据。然后,运用该算法,在研究了单对压电片进行振动主动控制的基础上.本文深入分析了压电层合板振动的多阶模态控制的问题,用Matlab进行系统仿真,得到了压电层合板受到初始位移激励下板中心点的位移和控制电压大小随时间变化的曲线。数值模拟的结果表明,该方法能达到更有效控制结构振动和减小控制能量消耗的目的.进一步验证了该方法能达到有效控制结构振动和减小控制能量消耗的目的。 相似文献
16.
New matrix method for analyzing vibration and damping effect of sandwich circular cylindrical shell with viscoelastic core 总被引:2,自引:0,他引:2
Based on the linear theories of thin cylindrical shells and viscoelastic materials, a governing equation describing vibration of a sandwich circular cylindrical shell with a viscoelastic core under harmonic excitation is derived. The equation can be written as a matrix differential equation of the first order, and is obtained by considering the energy dissipation due to the shear deformation of the viscoelastic core layer and the interaction between all layers. A new matrix method for solving the governing equation is then presented With an extended homogeneous capacity precision integration approach. Having obtained these, vibration characteristics and damping effect of the sandwich cylindrical shell can be studied. The method differs from a recently published work as the state vector in the governing equation is composed of displacements and internal forces of the sandwich shell rather than displacements and their derivatives. So the present method can be applied to solve dynamic problems of the kind of sandwich shells with various boundary conditions and partially constrained layer damping. Numerical examples show that the proposed approach is effective and reliable compared with the existing methods. 相似文献
17.
由于周期性隔振结构动力计算中较少考虑轨道交通载荷及材料黏弹性,因此,本文以黏弹性层状周期板为研究对象,提出了垂向移动简谐载荷下,可以考虑材料黏弹性及板内横向剪切变形的黏弹性层状周期板动力计算近似理论并给出解析解答.设板中性面的横向剪切变形为横截面的整体剪切变形,利用Reissner-Mindlin假设及提出的剪切变形补充计算条件,得到了中性面法线转角与中性面剪应力的关系.基于平衡方程和应力连续条件,建立了黏弹性层状周期板振动控制方程,推导了对边简支对边自由条件下,板垂向位移的简化Fourier级数形式解.与经典层合板模型和有限元计算结果进行了比较,验证了本文解答的有效性.结果表明:(1)黏弹性层状周期板可以显著降低单一材料板在自振频率处的振动响应,但会引起局部低频频段的振动放大;(2)板的垂向位移随着载荷速度的增大而增大,当载荷速度超过300 km/h后,其对板振动响应的影响减弱;(3)黏弹性层剪切模量存在最佳设计值,可使结构的隔振性能最佳;(4)黏弹性层的阻尼特性在低频范围内对结构振动影响较小;(5)可在满足工程实际的情况下适当增加板长,以提高结构的隔振性能. 相似文献