充液压电阻尼圆柱壳的有限元建模

基于Mindlin板理论、压电理论、粘弹性理论和理想流体方程，对充液圆柱壳主动约束阻尼结构在流固耦合条件下的建模进行了研究。利用拉格朗日方法得到结构的动力学方程，利用GHM方法描述粘弹性阻尼的本构关系，结合流体方程建立主动约束阻尼结构在流固耦合条件下的动力学方程。建立从压电材料的电压到流固耦合边界下的圆柱壳结构振动的频响函数，利用实验结果对理论计算加以验证，结果表明该建模方法是可行的。     

球对称压电壳的随机最优控制

分析研究球对称压电壳在边界随机激励下的最优控制问题。给出压电壳的机电动力学方程、应力和电位移表达式,建立其随机最优控制问题方程;通过电势积分转化为机械振动控制方程。通过位移变换和Galerkin法,导出关于模态位移的多自由度振动最优控制方程。根据随机动态规划原理,建立HJB方程,得到压电壳的最优控制电势;并给出受控壳系统的频响函数、响应谱密度和相关函数等表达式,以计算其随机响应。最后给出数值结果,显示压电壳的随机最优控制效果。     

剪切型压电层合圆柱壳的精确解

对剪切型压电层合圆柱壳在电场和机械力作用下的应力场、位移场和电势分布进行了分析。在每层的局部坐标系下对该层的应力场、位移场和电势进行傅立叶展开, 然后采用状态空间方法得到变系数的8 维一阶常微分方程组, 采用Frobenius 方法得到应力场、位移场和电势的解。数值算例显示了电场和机械力作用下, 壳体厚度对应力场和位移场分布的不同影响。得到的3 维精确解为其他剪切型压电弹性层合壳的壳体理论提供理论依据和验证。      

材料应变率对圆柱壳轴向冲击屈曲的影响

研究了轴向冲击载荷作用下材料应变率对圆柱壳弹塑性冲击屈曲的影响,采用Ｋａｒｍａｎ－Ｄｏｎｎｅｌｌ运动方程,本构关系采用增量理论,联立Ｃｏｗｐｅｒ－Ｓｙｍｏｎｄｓ关系,求得相应的动屈服应力,借助增量数值计算方法注解运动方程,计算表明：材料的应变率敏感性显著地提高了结构的抗冲击屈曲能力;基于Ｂ－Ｒ准则的屈曲判断方法和采用Ｓｏｕｔｈｗｅｌｌ方法可以获得一致的临界屈曲载荷。     

轴向极化的层合压电圆柱壳的自由振动

从轴向极化的三维圆柱型正交各向异性压电弹性力学基本方程出发,建立了状态方程。采用细分近似方法,得到了状态变量解。分析了两端简支的层合压电圆柱壳的自由振动问题,给出了频率方程的精确形式,并作了具体计算。     

水下爆炸载荷作用下加肋圆柱壳应变响应研究

采用加肋圆柱壳结构模型模拟潜艇结构,对其在水下爆炸冲击载荷作用下的响应过程进行试验研究。结果表明:采用应变测量的方法对结构进行模态分析是可行的;受附连水质量的影响,加肋圆柱壳结构的低阶湿模态频率较干模态频率显著下降;在爆炸载荷作用下,距离爆炸点越近结构承受的冲击作用越严重,越容易产生塑性破坏;应变的最大响应是冲击波载荷和一次脉动压力载荷共同作用的结果,第二次脉动压力对结构的动态应变响应贡献不明显。     

基于压电驱动的圆柱壳内振源振动传递控制

针对圆柱壳内振源振动通过环形支承向壳体传递的问题,提出一种基于压电作动器的主被动支承隔振方案,并通过振源-主被动支承-壳体耦合系统进行振动控制分析。根据Flugge壳理论,采用波传播法建立圆柱壳体振动模型,同时采用有限元方法建立振源及主被动支承的振动模型,最终使用子结构频响函数综合获得耦合系统振动模型。基于耦合系统模型和理想控制假设,在频域给出壳体振动可控性,并通过振源-主被动支承-壳体试验系统验证控制的有效性。仿真与试验结果表明,基于压电作动器的主被动隔振方案能显著降低壳体的宽带和线谱振动。     

玻璃/环氧圆柱壳的冲击响应与稳定性分析

应用Love的壳体理论得到了非轴对称变形的复合材料圆柱壳的控制方程。对扰动状态的非轴对称变形,位移函数采用复Fourier级数形式,得到了Mathieu形的扰动方程,由此给出了静态临界载荷和固有频率。本文中对层合壳在轴向冲击载荷下的动态稳定性研究考虑了几何非线性,这是以往在该问题的研究中所未涉及的问题。研究表明,考虑几何非线性得到的临界载荷较线性几何关系计算结果要高5 %左右。因此,考虑几何非线性是必要的。      

薄壁圆柱壳构件受迫振动的响应特征研究

针对固支-自由约束条件下受径向谐波激励或径向冲击激励的薄壁圆柱壳构件,开展其受迫振动下的响应特征分析。首先基于Love壳体理论建立了薄壁圆柱壳构件的动力学模型,然后,根据固支-自由约束条件特点,采用轴向梁函数和周向三角函数组合的振型函数以及振型叠加法,获得了考虑粘性阻尼的薄壁圆柱壳模态坐标振动方程,进而求解受径向谐波激励或冲击激励的振动响应。通过一个具体算例,进行了不同位置上的响应幅度与相位的变化分析,并对比了模态阻尼比和激励力幅值对响应幅值的影响。     

压电曲壳单元及其形状控制

板壳结构作为航空、航天工程中的主要工作元件,要承受多种环境荷载,而对形状变化非常敏感的机翼、天线等结构,有必要进行形状控制。推导了空间压电曲壳单元的有限元方程,采用约束方程法连接压电曲壳和主体结构,建立了整体结构的有限元分析模型,并基于等效应变原则验证了模型的正确性。在此基础上,利用最小二乘法对结构进行了形状控制,得到压电驱动器上电压的最优分布。算例表明:该文模型能提高计算精度和速度,达到形状控制的要求。     

Analytical solution for the axisymmetric plane strain electroelastic dynamics of a special non-homogeneous piezoelectric hollow cylinder

By virtue of the introduction of a dependent variable and the separation of variables technique, the axisymmetric plane strain electroelastic dynamic problem of a special non-homogeneous piezoelectric hollow cylinder is transformed to a Volterra integral equation of the second kind about a function with respect to time, which can be solved successfully by means of the interpolation method. Then the solutions of displacements, stresses, electric displacements and electric potential are obtained. The present method is suitable for a piezoelectric hollow cylinder with an arbitrary thickness subjected to arbitrary mechanical and electrical loads. Numerical results are finally presented.     

旋转压电复合圆柱的弹性分析

针对由各向同性弹性核和压电层组成的两层复合圆柱的旋转问题,给出了弹性力学解。先从压电层的静电平衡方程出发,得到含一个待定常数的电位移形式解,并由此分别给出弹性核和压电层的位移通解,然后利用力学和电学边界条件以及界面处的连续条件确定出所有各层中引入的待定常数,最终得到原问题的解。数值结果表明：当压电层的内外表面均接地时,压电层中的径向应力幅值随弹性核材料的杨氏模量增大而增大,而环向应力则正好相反。弹性核材料的泊松比及外加在压电层内外表面上的电势对旋转两层复合圆柱内的应力响应均有显著的影响。     

Vibration of axisymmetric composite piezoelectric shells coupled with internal fluid

This paper presents the theoretical and finite element formulations of piezoelectric composite shells of revolution filled with compressible fluid. The originality of this work lies (i) in the development of a variational formulation for the fully coupled fluid/piezoelectric structure system, and (ii) in the finite element implementation of an inexpensive and accurate axisymmetric adaptive laminated conical shell element. Various modal results are presented in order to validate and illustrate the efficiency of the proposed fluid–structure finite element formulation. Copyright © 2007 John Wiley & Sons, Ltd.     

柱面扁壳面畸变的实验研究

为控制覆盖件成形中的面畸变,以矩形柱面扁壳为模型,实验研究了其拉深件及切边后的面畸变,分析了面畸变形成机制及成形条件、切边对面畸变的影响.结果表明:柱面扁壳成形后在柱面方向出现面畸变,面畸变沿柱面方向呈M型且基本成对称的分布,切边后面畸变减小,而且畸变形态转变为U型分布.面畸变随板料厚度的增加、压边力的增加、屈服强度的降低、凸模曲率半径的减小而减小.     

正交异性扁薄球壳的非线性轴对称振动

给出了一种研究圆柱正交异性扁薄球壳非线性轴对称自由振动的新的时间模态方法。首先,使用变分法导出了决定振动频率的一对代数-微分方程。然后,利用作者提出的改进的修正迭代法求得了渐进解。这使此种壳体的非线性振动的进展获得扩充研究。     

基于压电智能结构的镗削振动主动控制的仿真与实验研究

在镗削加工中,由于镗杆长颈比较大,因此,普遍存在镗削振动问题,这种振动限制了切削效率,影响了工件表面质量。提出以压电振动干扰抑制镗削振动的设想,建立了含有压电控制单元的镗削振动系统动力学模型;基于该模型设计了实验装置。理论仿真和实验分析结果表明,该装置能够有效抑制镗削过程中镗杆的振动,且结构简单,易于实现。     

A strong solution for a generalized plane strain unsymmetrical piezoelectric bi-layer laminates

Interfacial stresses, electric fields, and electric displacements of a piezoelectric unsymmetrical bi-layer orthotropic laminate are presented. A state space equation for orthotropic piezoelectric material is derived from three-dimensional piezoelectric elasticity directly. With the application of the transfer matrix and recursive solution approach, a strong solution for the unsymmetrical piezoelectric generalized plane strain bi-layer laminated structure is sought after considering all elastic and piezoelectric constants of materials. Electromechanical boundary layer effect is identified quantitatively at free edges. To facilitate the discussion on the results, the corresponding calculations from finite element models are compared with those of the strong solution.     

Anti‐plane mechanical and in‐plane electrical fields for a finite electrode/punch on a finite piezoelectric layer

The problems of a surface electrode and a rigid punch on a finite piezoelectric layer are considered in this paper. The resultant force and the accumulated electric charge on the electrode/punch are prescribed. Closed‐form solutions for the electromechanical fields at the electrode/punch tip are obtained and are expressed in terms of the applied strain and electric field intensity factors. For infinite layer thickness, the strain and electric field intensity factors are obtained in closed‐form. For finite layer thickness, the strain and electric field intensity factors are obtained numerically by the singular integral equation technique. The effect of layer thickness on the electrode/punch tip fields is discussed. It is found that the field intensities at the electrode/punch tip can be reduced considerably by decreasing layer thickness. In addition to the single electrode/punch problem, this paper also provides a solution technique for two collinear surface electrodes/punches on a finite piezoelectric layer. The effect of the relative distance between the two electrodes/punches on the electromechanical fields in the piezoelectric layer is also discussed.     

Electro-magneto temperature-dependent vibration analysis of functionally graded-carbon nanotube-reinforced piezoelectric Mindlin cylindrical shells resting on a temperature-dependent,orthotropic elastic medium

Vibration smart control analysis of a temperature-dependent functionally graded-carbon nanotube-reinforced piezoelectric cylindrical shell embedded in an orthotropic elastic medium is investigated. The mixture law is used for obtaining the material properties of the structure. The structure is subjected to a 2D magnetic field. Considering the first-order shear deformation theory, the motion equations are obtained. Based on an analytical method and differential quadrature method, the frequency is calculated. The effects of applied voltage, magnetic field, volume percent, and distribution type of carbon nanotubes, temperature, orthotropic elastic medium, and length to radius ratio of the shell are shown on system frequency.     

Non‐linear random response of laminated composite shallow shells using finite element modal method

This paper investigates the large‐amplitude multi‐mode random response of thin shallow shells with rectangular planform at elevated temperatures using a finite element non‐linear modal formulation. A thin laminated composite shallow shell element and the system equations of motion are developed. The system equations in structural node degrees‐of‐freedom (DOF) are transformed into modal co‐ordinates, and the non‐linear stiffness matrices are transformed into non‐linear modal stiffness matrices. The number of modal equations is much smaller than the number of equations in structural node DOF. A numerical integration is employed to determine the random response. Thermal buckling deflections are obtained to explain the intermittent snap‐through phenomenon. The natural frequencies of the infinitesimal vibration about the thermally buckled equilibrium positions (BEPs) are studied, and it is found that there is great difference between the frequencies about the primary (positive) and the secondary (negative) BEPs. All three types of motion: (i) linear random vibration about the primary BEP, (ii) intermittent snap‐through between the two BEPs, and (iii) non‐linear large‐amplitude random vibration over the two BEPs, can be predicted. Copyright © 2006 John Wiley & Sons, Ltd.