两自由度参数激励摆旋转运动分析和实验

研究具有支撑参数激励摆系统的支撑结构振动对摆旋转的影响,其中支撑结构是受到扭簧约束的刚性悬臂梁,参数激励摆与刚性悬臂梁的悬臂段铰接．首先,通过拉格朗日方程建立了系统两自由度的动力学方程．其次,利用多尺度法对建立的模型进行理论分析,得到悬臂梁的振动与上摆不同运动形式的关系,从而得到上摆不同运动形式下的参数平面分类和悬臂梁在上摆转动时的振动频响．最后,通过建立实验装置,观察理论预测,实验结果验证了理论分析的正确性．实验与理论对照得到,当参数激励频率接近悬臂梁的一阶固有频率时,悬臂梁的振幅变大,会破坏摆的转动稳定性．     

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运用分段线性系统分析理论,研究了间隙约束的悬臂梁振动系统在简谐激励 下系统稳态响应的动力学行为. 首先建立了间隙约束悬臂梁系统的动态响应分析模型,以传 递函数为基础,推导出系统的动力学分析方程及其求解方法. 然后对系统进行了数值求解分 析,得到了该系统稳态响应随激励幅值、激励频率、间隙接触刚度和阻尼变化的一般规律.     

旋转运动导电圆板的磁弹性参数振动分析

针对磁场中旋转运动圆板,在动能、应变能表达式基础上,根据哈密顿原理导出圆板的磁弹性振动方程．应用伽辽金积分法,得到横向磁场中旋转变速运动圆板的轴对称参数振动微分方程．通过坐标变换得到包含两个变系数项的马蒂厄振动方程．应用弗洛凯理论和平均法对系统的参数振动问题进行求解．通过数值计算得到周期稳定图、对应的振动响应特性图和相轨迹图．结果表明：在稳定区域内,系统的幅频曲线呈现为周期或概周期变化形式;在不稳定区内,系统的幅频响应曲线呈现为发散变化形式．     

气动载荷下旋转运动圆板磁弹性主共振分析

基于Kirchhoff薄板理论与哈密顿原理,建立旋转运动导电圆板的磁-气动弹性非线性动力学方程．根据电磁场基本原理得到旋转运动圆板所受电磁力表达式,同时采用一种简化的气动模型以描述作用于板上的气动载荷．基于贝塞尔函数形式振型函数的选取,应用伽辽金法得到旋转圆板的磁气动弹性轴对称非线性振动微分方程．应用多尺度法推导出主共振下系统的幅频响应方程,并依据Lyapunov方法得到系统稳态运动稳定性判据．通过算例,得到周边夹之约束下圆板主共振的幅频特性曲线图,以及振幅随磁感应强度和激励力幅值的变化曲线图;阐述了不同参数对系统共振幅值的影响规律,并对解的稳定性进行了分析．     

形状记忆合金(SMA)层合梁动力学分岔分析

针对有形状记忆合金的层合梁系统,分析了形状记忆合金层与梁中间基体的厚度比相关参数、激励强度对系统的振动幅频响应的影响。采用形状记忆合金多项式本构模型,建立层合梁的量纲归一化的运动方程,用Galerkin方法离散得到任意阶模态动力学方程,再由平均法求得幅频响应方程。利用奇异性理论计算转迁集和不同类型的幅频响应图。结果表明,一阶模态非线性振动幅频响应可分为类线性和硬特性两种类型。响应为类线性时,厚度比和激励强度在类线性区取值,形状记忆合金层对系统几乎没有减振效果;响应为硬特性时,激励幅值越大,形状记忆合金层越厚,SMA层对系统的减振效果越明显。在不同的激励及SMA层厚度下,二阶和三阶模态非线性振动幅频响应定性相同,其类型可分为:类线性、硬特性、软特性、软硬特性。     

附磁阶梯变厚度悬臂梁压电俘能器的理论建模及分析

论文建立了一种附磁阶梯变厚度压电悬臂梁的动力学模型并分析了系统的俘能特性。基于Euler-Bernoulli梁理论分段建立系统能量函数并引入非线性磁势能,利用Lagrange方程建立了系统机电耦合动力学方程;利用数值方法分析了磁间距对系统振动特性的影响,此外还研究了系统单稳态和双稳态响应,探讨了厚度比、长度比、磁间距和外激励幅值对系统动力学响应和俘能特性的影响。结果表明,磁间距是影响系统势能的主要因素,调节磁间距可使系统产生单稳态和双稳态响应,从而有效提高俘能器俘能特性;与传统等截面悬臂梁压电俘能器相比,通过优化结构参数,附磁阶梯变厚度悬臂梁压电俘能器能够发生明显的非线性振动现象,实现宽频带振动能量采集。     

基于碰撞升频的MEMS压电振动能量采集系统

本文提出了一种基于碰撞升频机制的微型压电能量采集系统,由一对共振频率不同的悬臂梁平行叠放组成。在外界低频振动激励下,底部低频S形金属曲梁产生共振,在运动过程中碰撞顶部高频微型压电直梁,从而将低频环境振动转换为高频压电梁的振动,解决了压电直梁的固有频率与外界激励频率不匹配问题,同时提高能量收集的效率。本文建立了悬臂梁受迫振动和碰撞耦合振动的动力学模型,讨论了压电悬臂梁的电压输出特性。通过实验测试了压电能量收集系统和单个压电悬臂梁的开路电压并计算了输出功率,结果表明当振动加速度为1.0 g时,升频式压电能量采集系统在25 Hz的激振下输出功率达到8.6 μW,高于单个压电悬臂梁的最大输出功率。     

三相驱动下含两质量块刚体的平面运动

本文研究了一类含两个质量块的振动驱动系统在粘性摩擦下的平面运动,其中两个内部质量在相互垂直的水平槽道上作三相运动。利用第二类拉格朗日方程,建立了系统的动力学方程;其次,利用系统直线运动时的理论解,验证速度Verlet积分法的可靠性;利用这种算法分析了系统的平面运动,得到了内部驱动参数与系统运动轨迹、运动速度的关系;然后,基于数值分析结果,通过调节内部驱动参数,得到了系统在不同轨迹间的六种转换形式;最后,通过组合不同的转换形式,得到了曲率连续变化的平面运动路径。     

三稳态尾流驰振能量捕获系统发电性能研究

利用流体动能能量发电为微电子器件供电已逐渐成为非线性振动领域的研究热点。利用永磁铁产生非线性回复力，将非线性回复力引入到悬臂梁压电能量捕获装置中，提出了一种三稳态尾流驰振能量压电发电装置，获得力学模型及系统控制方程，获得了三稳态系统的稳定和不稳定平衡点表达式，给出了发电系统存在三稳态运动时的结构参数的取值范围。重点研究了等平衡点不同势阱深度、等势阱深度不同平衡点位置对系统的动力学响应及发电性能的影响。结果表明，等平衡点条件下浅阱系统的起振折合流速更低、发电性能更好。     

原子力显微镜探针振动的简化模型分析

为对原子力显微镜(atomic force microscope,AFM)的微悬臂梁进行定性动力学特性分析,建立AFM微悬臂梁的简化模型,探讨AFM探针的受迫振动.通过理论计算得出AFM探针简化模型的运动方程,并得到振动波形,证明了AFM实际应用中的对称问题和"频漂"问题,并发现AFM简化模型的间歇式碰撞现象.用负弹簧模拟探针针尖与样品之间的长程引力,并通过理论计算探讨长程引力对AFM测量的影响.     

An approximate method of response analysis of vibrations for cracked beams

I.IntroductionTheinvestigationsonthed}'nan1icresponsesofcrackedbeamshavebeendonebymanyresearchers.Howeter,upti11now.totheauthors-knot"ledge,intheirwork,thereha\-ebeenmanypapersaboutnumericaln1ethodstobeusedasamainmeanstostudy,whileveryfewpapersab0utanalyt…     

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.     

A NEW APPROACH TO FREE VIBRATION ANALYSIS OF A BEAM WITH A BREATHING CRACK BASED ON MECHANICAL ENERGY BALANCE METHOD

In this paper, a new approach to free vibration analysis of a cracked cantilever beam is proposed. By considering the effect of opening and closing the crack during the beam vibration, it is modeled as a fatigue crack. Also, local stiffness changes at the crack location are considered to be a nonlinear amplitude-dependent function and it is assumed that during one half a cycle, the frequencies and mode shapes of the beam vary continuously with time. In addition, by using the experimental tests, it is shown that the local stiffness at the crack location varies continuously between the two extreme values corresponding to the fully closed and the fully open cases of the crack. Then, by using the mechanical energy balance the dynamic response of the cracked beam is obtained at every time instant. The results show that for a specific crack depth, by approaching the crack location to the fixed end of the beam, more reduction in the fundamental frequency occurs. Furthermore, for a specific crack location, the fundamental frequency diminishes and the nonlinearity of the system increases by increasing the crack depth. In order to validate the results, the variations of the fundamental frequency ratio against the crack location are compared with experimental results.     

Dynamic analysis of a deployable/retractable damped cantilever beam

Deployable/retractable damped cantilever beams are a class of time-varying parametric structures which have attracted considerable research interest due to their many potential applications in the intelligent robot field and aerospace. In the present work, the dynamic characteristics of a deployable/retractable damped cantilever beam are investigated experimentally and theoretically. The time-varying damping, as a function of the beam length, is obtained by both the enveloped fitting method and ...     

The composite damping capacity of sandwich cantilever beams

The governing equation of the flexural forced vibration of a cantilever sandwich beam excited by a sinusoidal displacement at the clamped end is developed by utilizing the conventional Hamilton's Principle. The effect of damping of the composite beam is incorporated into the elastic equation of motion by utilizing the Correspondence Principle of the linear viscoelastic theory. Several plots for different values of the composite damping factor are presented. For comparison, an experimental setup was utilized to test different composite beams. The variation of the experimental results with those derived theoretically seem to be in agreement within the frequency range of the first few modes.     

考虑液面波动和液体压缩时一侧受液作用悬臂梁的横振分析

本文分析一侧部分受有液体作用悬臂梁的横向自由振动，同时考虑了液面波动和液体可压缩性对悬臂梁自振特性的影响。利用一组广义三角级数的正交完备性，求得了悬臂梁与液体耦联振动的振型函数和频率方程的精确解析解，最后给出了几个数值算例。     

Large oscillations of beams and columns including self-weight

Large-amplitude, in-plane beam vibration is investigated using numerical simulations and a perturbation analysis applied to the dynamic elastica model. The governing non-linear boundary value problem is described in terms of the arclength, and the beam is treated as inextensible. The self-weight of the beam is included in the equations. First, a finite difference numerical method is introduced. The system is discretized along the arclength, and second-order-accurate finite difference formulas are used to generate time series of large-amplitude motion of an upright cantilever. Secondly, a perturbation method (the method of multiple scales) is applied to obtain approximate solutions. An analytical backbone curve is generated, and the results are compared with those in the literature for various boundary conditions where the self-weight of the beam is neglected. The method is also used to characterize large-amplitude first-mode vibration of a cantilever with non-zero self-weight. The perturbation and finite difference results are compared for these cases and are seen to agree for a large range of vibration amplitudes. Finally, large-amplitude motion of a postbuckled, clamped–clamped beam is simulated for varying degrees of buckling and self-weight using the finite difference method, and backbone curves are obtained.     

Constrained parameter-splitting perturbation method for the improved solutions to the nonlinear vibrations of Euler–Bernoulli cantilevers

In this paper, a new method named constrained parameter-splitting perturbation method for improving the solutions obtained from the parameter-splitting perturbation method is proposed for solving the problems in some extremal cases, such as the strongly nonlinear vibration of an Euler–Bernoulli cantilever. The proposed method takes the advantages of both the perturbation method and the harmonic balance method. The idea is that the solution obtained by the parameter-splitting perturbation method is substituted into the equation of motion and then the accumulative error of the equation is minimized for determining the unknown splitting parameters under the constraints constructed under the frame of harmonic balance method. The forced vibration of an oscillator with cubic geometric nonlinearity and inertia nonlinearity and the forced vibration of a planar microcantilever beam with a lumped tip mass are studied as examples to reveal the efficacy of the proposed method. The inspection of the steady-state response including its stability is conducted by means of comparing the frequency-response curves obtained by the proposed method with those obtained by the numerical continuation method and harmonic balance method, respectively, to show the efficacy and the advantages of the proposed method. Meanwhile, the nonlinear ordering effect on the solutions of the proposed method is also studied by comparing the results obtained by using different nonlinear orderings in the systems. In the last, we found through convergence examinations that it is necessary to have corrections to the erroneous solution which are obtained by harmonic balance method and Floquet theory in stability analysis.

     

Suppression of multiple modal resonances of a cantilever beam by an impact damper

Impact dampers are usually used to suppress single mode resonance. The goal of this paper is to clarify the difference when the impact damper suppresses the resonances of different modes. A cantilever beam equipped with the impact damper is modeled. The elastic contact of the ball and the cantilever beam is described by using the Hertz contact model. The viscous damper between the ball and the cantilever beam is modeled to consume the vibrational energy of the cantilever beam. A piecewise ordina...