粘弹层合板的稳态振动和层间应力

应用混合分层理论和Ressiner混合变分原理，在板厚方向取二次位移插值函数和三次、四次横向应力插值函数推导出粘弹层合板的动力学方程，得出简支粘弹层合板稳态振动的解。不仅得出与三层弹性板精确的自振频率吻合良好的解，而且对于粘弹层合板，所计算的自振频率和结构损耗因子也与三维结果吻合较好。计算了自由阻尼层合板对应的低阶法向位移响应幅值和层问横向应力的幅值。结果表明，较高的层间横向正应力是低频稳态振动中引起粘弹层合板分层破坏的主要因素，采用适当模量和厚度的粘弹性材料将有效地降低粘弹层合板的层间横向正应力的幅值。     

材料黏滞系数与损耗因子的频率相关性研究

针对黏弹性材料KV阻尼模型的黏滞系数与复阻尼模型的损耗因子间的关系,由单自由度体系的结构动力学分析,并基于结构振动响应的一致性,推导建立了黏滞系数与损耗因子在结构线性稳态简谐振动和自由振动时的一般关系式;并利用该关系式,试验研究了纤维混凝土材料黏滞系数和损耗因子的频率相关性.结果表明,黏滞系数与损耗因子间的关系在稳态简谐振动和自由振动时的表达形式相同,只是频率取值不同;纤维混凝土的损耗因子和黏滞系数都随频率增加而降低,且在0.5～1.0Hz频段降幅显著,而后渐趋平缓;相比于素混凝土,纤维混凝土的黏滞系数和损耗因子与激振频率的相关性更强.试验所得纤维混凝土频率相关的黏滞系数、损耗因子及推导所建立的两参数关系式为构建物理意义明确且又便于结构振动反应分析的阻尼系数或阻尼矩阵奠定了基础.      

局部约束阻尼开口柱壳的减振分析及优化

为了缩减开口柱壳结构的振动,本文基于Lagrange方程以及Sanders薄壳理论建立了局部约束阻尼开口柱壳的动力学模型,分析了粘弹性单元分段数和厚度、阻尼单元占空比以及约束层敷设角和厚度对结构前三阶模态损耗因子和固有频率的影响,得到了各参数对结构振动特性的影响规律.并以前三阶损耗因子为目标,应用NSGA-Ⅱ遗传算法对...     

基于三维弹性理论的约束阻尼结构振动阻尼特性分析

本文根据三维弹性理论建立了多层弹性－粘弹性阻尼复合板自由振动的运动方程．该方程所根据的力学模型包括了影响阻尼复合板振动的几乎全部变形因素，包括弹性层和粘弹性层的平面剪切、横向剪切、纵向拉伸以及粘弹性层在厚度方向的胀缩变形。用该方程对工程声学问题所关注的中高频域结构损耗因子进行了数值计算。此外，对“附加型”和“成品型”两种结构型式约束阻尼板损耗因子的差异，尤其是阻尼层的厚度方向胀缩变形耗能对结构损耗因子的影响，进行了计算讨论。     

高阻尼合金胶粘层合板阻尼特性研究

考虑高阻尼合金胶粘层合板中高阻尼合金的阻尼迟滞特性和胶粘剂本构中固化时间影响的关系,进行粘贴阻尼合金板后层合板结构的非线性动力有限元建模。对不同胶粘剂固化时间的高阻尼合金层合板进行数值仿真分析,用有理分式正交多项法结合非线性优化方法对仿真数据进行处理,得到不同胶粘剂固化时间下高阻尼合金层合板的固有频率和模态阻尼比。通过与锤击法模态试验所得高阻尼合金层合板模态参数对比,验证了有限元仿真模型的合理性。通过数值仿真和试验结果分析发现:粘贴阻尼合金板后层合板结构阻尼比有大幅度提高;随着胶粘剂固化时间的增加,层合板阻尼性能增强,瞬态振动也可以得到更快地衰减。表明高阻尼合金层合板的阻尼性能与阻尼合金的应变幅值有关;阻尼合金的应变幅值越大,阻尼合金层合板模态阻尼比越大,对应结构的减振性能越佳。     

基于遗传算法的约束阻尼梁减振优化分析

约束阻尼结构能有效减振, 但会增加结构的质量和体积, 基于此有必要对其 结构进行优化. 本文应用有限元软件ANSYS建立增设支撑层的约束阻尼梁模型, 根据模态应 变能原理提取约束阻尼梁的模态损耗因子, 并建立以阻尼段长度、约束层厚度、支撑层厚度、 阻尼段数目为设计变量的目标函数, 利用MATLAB多目标遗传算法进行优化运算. 计算结果表 明, 优化后的约束阻尼结构能够在引入质量较小情况下有效减小梁振动幅度, 使振动在较短 的时间内衰减.     

磁橡胶约束阻尼壳的宽频振动控制能力研究

不同于传统被动约束阻尼处理(PCLD),磁橡胶约束阻尼处理(MRLD)采用磁化的铁-橡胶混合粉末替代PCLD的粘弹性材料,不是通过粘结而是磁力吸附在钢制振动体上,在振动时交界面处发生滑移使部分能量转化为热能,从而降低振动.采用假设模态法计算PCLD的频率响应,再基于周期耗能相等原理.将MRID与PCLD等价,得到MRLD壳的模态损耗因子,研究了MRLD处理对简支壳阻尼的影响.分析结果表明:对于1000～3365Hz间前11阶模态频率的MRLD壳振动,当激振力低于16～20倍的起滑激励力F0时,MRLD均可获得比PCLD更好的阻尼;但各模态的F0的差异仅在3～4倍内;因此在前11阶模态频率范围内,激振力可以存在一个交集,在此交集内可同时引起各阶模态的阻尼层发生滑移,从而能控制壳的宽频振动.     

粘-弹层合悬臂板瞬态响应的近似解析解

采用双向梁函数组合级数逼近的方法构造粘-弹层合悬臂板的横向位移函数,用里兹法得悬臂板在集中力作用下的弯曲变形。用拉格朗日方程求出了板自由振动的频率和结构损耗因子;给出粘-弹层合悬臂板在集中力突然撤去以后瞬态响应的近似解析解。另外,分析了阻尼层损耗因子、弹性模量及厚度对响应的影响。     

基于正交试验设计的空间弯管阻尼配置优化

提出采用局部环绕阻尼层的方法对管路进行减振,并通过正交试验分析得出了最佳的阻尼配置方案.考虑弯曲成形过程中的厚度与截面形状变化,建立了空间弯管的有限元精确模型;针对粘弹性阻尼层力学特性随频率变化的特点,采用迭代法计算粘弹性结构的固有频率,依据模态应变能法,求解模态损耗因子.管路的模态试验验证了有限元模型及动力特性计算方法的正确性.最后利用L18(37)正交表对阻尼层的6个主要参数进行方差计算,详细分析了各因素对频率和损耗因子指标的影响,给出了频率改变较小情况下损耗因子最大的最佳阻尼配置.     

基于局部移动Kriging无网格方法的层合板自由振动分析

利用基于局部移动Kriging插值无网格法对层合板自由振动进行了数值分析,基于一阶剪切层合理论导出了层合板振动的控制方程和边界条件,进一步得到了自由振动的离散化特征方程。由于Kriging插值函数具有Kronecker delta函数性质,可以直接施加本质边界条件。通过本文给出的方法,对不同边界条件、不同跨厚比、不同材料参数和铺设角度的层合板的振动频率进行了计算,均得到满意结果。最后用该方法对层合板的铺设角度进行优化设计,得到了与已有文献完全一致的优化结果。数值结果充分表明了无网格Kriging方法分析层合板自由振动问题的有效性和高精确度。     

APPROXIMATE SOLUTIONS FOR TRANSIENT RESPONSE OF CONSTRAINED DAMPING LAMINATED CANTILEVER PLATE

The series composed by beam mode function is used to approximate the displacement function of constrained damping of laminated cantilever plates, and the transverse deformation of the plate on which a concentrated force is acted is calculated using the principle of virtual work.By solving Lagrange＇s equation, the frequencies and model loss factors of free vibration of the plate are obtained, then the transient response of constrained damping of laminated cantilever plate is obtained, when the concentrated force is withdrawn suddenly.The theoretical calculations are compared with the experimental data, the results show：both the frequencies and the response time of theoretical calculation and its variational law with the parameters of the damping layer are identical with experimental results.Also, the response time of steel cantilever plate, unconstrained damping cantilever plate and constrained damping cantilever plate are brought into comparison, which shows that the constrained damping structure can effectively suppress the vibration.     

粘弹层合板的自由振动和横向应力

Based on Reddy＇s layerwise theory, the governing equations for dynamic response of viscoelastic laminated plate are derived by using the quadratic interpolation function for displacement in the direction of plate thickness. Vibration frequencies and loss factors are calculated for free vibration of simply supported viscoelastic sandwich plate, showing good agreement with the results in the literature. Harmonious transverse stresses can be obtained. The results show that the transverse shear stresses are the main factor to the delamination of viscoelastic laminated plate in lower-frequency free vibration, and the transverse normal stress is the main one in higher-frequency free vibration. Relationship between the modulus of viscoelastic materials and transverse stress is analyzed. Ratio between the transverse stress＇s maximum value and the in-plane stress＇s maximum-value is obtained. The results show that the proposed method, and the adopted equations and programs are reliable.     

黏弹性层合悬臂薄壁圆柱壳的模态特性研究

基于薄壳理论和黏弹性理论, 得出了黏弹性层合悬臂薄壁圆柱壳模态特性的半解析解. 根据乐甫薄壳理论, 建立了基层和黏弹性阻尼层薄壁圆柱壳的一阶状态微分方程, 结合黏弹性阻尼层的变形协调关系和层间作用力关系, 利用传递矩阵法得出了整体结构的传递矩阵, 采用高精度的精细积分法得出了固有频率、模态损耗因子和三维模态振型, 最后通过有限元法进行了比较, 通过算例验证了传递矩阵法对黏弹性层合薄壁圆柱壳模态特性研究的有效性.     

Double Hopf bifurcation of composite laminated piezoelectric plate subjected to external and internal excitations

The double Hopf bifurcation of a composite laminated piezoelectric plate with combined external and internal excitations is studied. Using a multiple scale method, the average equations are obtained in two coordinates. The bifurcation response equations of the composite laminated piezoelectric plate with the primary parameter resonance, i.e.,1:3 internal resonance, are achieved. Then, the bifurcation feature of bifurcation equations is considered using the singularity theory. A bifurcation diagram is obtained on the parameter plane. Different steady state solutions of the average equations are analyzed.By numerical simulation, periodic vibration and quasi-periodic vibration responses of the composite laminated piezoelectric plate are obtained.     

Vibration and damping analysis of a composite plate with active and passive damping layer

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Free vibration of circular cylindrical shell with constrained layer damping

Free vibration characteristics of circular cylindrical shell with passive constrained layer damping (PCLD) are presented. Wave propagation approach rather than finite element method, transfer matrix method, and Rayleigh-Ritz method is used to solve the problem of vibration of PCLD circular cylindrical shell under a simply supported boundary condition at two ends. The governing equations of motion for the orthotropic cylindrical shell with PCLD are derived on the base of Sanders’ thin shell theory. Numerical results show that the present method is more effective in comparison with other methods. The effects of the thickness of viscoelastic core and constrained layer, the elastic modulus ratio of orthotropic constrained layer, the complex shear modulus of viscoelastic core on frequency parameter, and the loss factor are discussed.     

Active vibration control of thin constrained composite damping plates with double piezoelectric layers

Vibrations and the damping behaviour of thin constrained composite plates with double piezoelectric layers are analytically explored by using Fourier transformation and classical laminated plate theory. Electric potential equations in the double piezoelectric layers are solved with respect to closed and open circuit boundary conditions, an exterior dielectric slab and active control. The natural frequencies and loss factors of the constrained smart composite plates with passive control methods are not notably changed in comparison with those of the constrained composite plates without piezoelectric effects since vibrational energy does not efficiently convert to electrical energy. The loss factors of the composite plates with active constrained damping increase and the natural frequencies have significant variations as the proportional derivative gains increase. Transverse displacement power spectra of the piezoelectric composite plates with active control are compared with those of the piezoelectric composite plates with passive control showing that active control has the best suppression performance of vibrations for the constrained laminated plates with double piezoelectric layers. Radial power spectral density, phase angles and cylindrical-wave power spectral density are calculated. Interesting patterns of wave propagation are explained when plane wave expansion is used to obtain Bessel cylindrical waves.     

结构阻尼时域本构模型及其应用

阻尼合金作为一种新型结构功能材料在不少领域已获应用，由于其阻尼值较大且随频率呈复杂交化关系，传统的线性粘性阻尼理论或经典的非频变结构阻尼理论难以精确地描述其耗能行为。本文应用粘弹性阻尼理论，根据阻尼合金储能模量和损耗因子在频域的实测数据．应用最优化方法拟合出标准线性体模型中的本构参数；根据积分形式的三参量本构关系和变形体虚功原理，推导出了有限元形式的动力学方程；讨论了三参数初值的选取；对包含卷积积分的有限元动力学方程通过数学推导将其化为三阶线性微分方程组，再转化为标准状态变量方程，应用数值求解。数值计算实例证明了所提方法的正确和有效性。     

层合闭口厚柱壳的温度应力

基于层合柱壳混合状态方程和边界条件的弱形式，建立了两端固支层合闭口柱壳的温度应力混合方程，给出了任意厚度合闭口柱壳在温度荷载和机械荷载共同作用下的解析解。