Steady-state responses of a belt-drive dynamical system under dual excitations

The stable steady-state periodic responses of a belt-drive system with a one-way clutch are studied. For the first time, the dynamical system is investigated under dual excitations. The system is simultaneously excited by the firing pulsations of the engine and the harmonic motion of the foundation. Nonlinear discrete-continuous equations are derived for coupling the transverse vibration of the belt spans and the rotations of the driving and driven pulleys and the accessory pulley. The nonlinear dynamics is studied under equal and multiple relations between the frequency of the fir- ing pulsations and the frequency of the foundation motion. Furthermore, translating belt spans are modeled as axially moving strings. A set of nonlinear piecewise ordinary differ- ential equations is achieved by using the Galerkin truncation. Under various relations between the excitation frequencies, the time histories of the dynamical system are numerically simulated based on the time discretization method. Further- more, the stable steady-state periodic response curves are calculated based on the frequency sweep. Moreover, the convergence of the Galerkin truncation is examined. Numer- ical results demonstrate that the one-way clutch reduces the resonance amplitude of the rotations of the driven pul- ley and the accessory pulley. On the other hand, numerical examples prove that the resonance areas of the belt spans are decreased by eliminating the torque-transmitting in the opposite direction. With the increasing amplitude of the foun- dation excitation, the damping effect of the one-way clutch will be reduced. Furthermore, as the amplitude of the firing pulsations of the engine increases, the jumping phenomena in steady-state response curves of the belt-drive system with or without a one-way clutch both occur.

Wind-induced response analysis of conical membrane structures

Conical membrane structures are a typical form of tensile membrane structures. In the past, most studies focused on the static performance, but few on dynamic performance. In this paper, systematic parameter analysis of wind-induced response of conical membrane structures has been performed with nonlinear random simulation method in a time domain, by considering some parameters, such as span, rise-span ratio, prestress of membrane, and characteristic of the approaching wind flow. Moreover, formulas of the dynamic coefficient and nonlinear adjustment factor are advised, which can be conveniently used in wind-resistant design of conical membrane structures.

Seismic response of tall building considering soil-pile-structure interaction

The seismic behavior of tall buildings can he greatly affected by non-linear soil-pile interaction during strong earthquakes.In this study a 20-storey building is examined as a typical structure supported on a pile foundation for different conditions:(1) rigid base,i.e.no deformation in the foundation:(2) linear soil-pile system;and (3) nonlinear soil-pile system. The effects of pile foundation displacements on the behavior of tall building are investigated,and compared with the behavior of buildings supported on shallow foundation.With a model of non-reflective boundary between the near field and far field, Novak's method of soil-pile interaction is improved.The computation method for vibration of pile foundations and DYNAN computer program are introduced comprehensively.A series of dynamic experiments have been done on full-scale piles, including single pile and group,linear vibration and nonlinear vibration,to verify the validity of boundary zone model.

Investigation of Induced Unbalance Magnitude on Dynamic Characteristics of High-speed Turbocharger with Floating Ring Bearings

Due to operational wear and uneven carbon absorption in compressor and turbine wheels, the unbalance(me) vibration is induced and could lead to sub?synchronous vibration accidents for high?speed turbocharger(TC). There are very few research works that focus on the magnitude e ects on such induced unbalance vibration. In this paper, a finite element model(FEM) is developed to characterize a realistic automotive TC rotor with floating ring bearings(FRBs). The nonlinear dynamic responses of the TC rotor system with di erent levels of induced unbalance magni?tude in compressor and turbine wheels are calculated. From the results of waterfall and response spectral intensity plots, the bifurcation and instability phenomena depend on unbalance magnitude during the startup of TC. The sub?synchronous component 0.12× caused rotor unstable is the dominant frequency for small induced unbalance. The nonlinear e ects of induced unbalance in the turbine wheel is obvious stronger than the compressor wheel. As the unbalance magnitude increases from 0.05 gbration 1·mm to 0.2 g·mm, the vibration component changes from mainly 0.12× to synchronous vi×. When unbalance increases continuously, the rotor vibration response amplitude is rapidly growing and the 1× caused by the large unbalance excitation becomes the dominant frequency. A suitable un?balance magnitude of turbine wheel and compressor wheel for the high?speed TC rotor with FRBs is proposed: the value of induced un?balance magnitude should be kept around 0.2 g·mm.

DYNAMIC ANALYSIS OF A SPATIAL COUPLED TIMOSHENKO ROTATING SHAFT WITH LARGE DISPLACEMENTS

The dynamic simulation is presented for an axial moving flexible rotating shafts, which have large rigid motions and small elastic deformation. The effects of the axial inertia, shear deformation, rotating inertia, gyroscopic moment, and dynamic unbalance are considered based on the Timoshenko rotating shaft theory. The equations of motion and boundary conditions are derived by Hamilton principle, and the solution is obtained by using the perturbation approach and assuming mode method. This study confirms that the influence of the axial rigid motion, shear deformation, slenderness ratio and rotating speed on the dynamic behavior of Timoshenko rotating shaft is evident, especially to a high-angular velocity rotor.

Dynamic Characteristics of the Crankshaft System with Coupling Effect

The nonlinear dynamic model of the marine diesel crankshaft system with a propeller and 6 cranks is established, in which the variable moment of inertia of the linkage and the piston, coupling effect between torsional and axial vibration, the actuating force applied on the piston, the actuating torque and force applied on the propeller is included. The governing equations of the model denote a strong nonlinear and non autonomous system. By numeric simulation, the dynamic response of the system to initial displacement and initial speed, variable moment of inertia, the pressure applied on the piston by combustion gas, the torque and the axial force applied on the propeller by fluid is researched respectively. According to the research results, the variable moment of inertia and coupling effect between torsional and axial vibration are the fundamental reason for nonlinear vibration. Different actuating factors can not only result in different frequency components of the response, but make the same frequency component have different vibration amplitude. The dynamic behavior of the system is not influenced obviously by the actuating torque and force applied on the propeller. There is obvious difference in sensitivity of the dynamic response in the different direction to the same actuating factor.

基于动态啮合刚度的直齿圆柱齿轮动态特性研究

齿轮系统转速直接影响齿轮系统的动态特性,然而在啮合刚度的计算中该因素却被许多学者们忽略。为了研究转速对啮合刚度的影响,基于有限元框架使用平均加速度法提出了一种计算与转速相关的动态啮合刚度的算法,同时对不同转速下的动态啮合刚度进行仿真计算与分析,最后进一步探究了受动态啮合刚度影响后的齿轮系统所具有的相关动态特性。分析表明,动态啮合刚度始终围绕着静态啮合刚度上下波动;随着转速的增加,其波动幅度增加,振荡次数减少;随着转速的变化,动态啮合刚度计算的动态传动误差振幅相对于静态啮合刚度而言大小关系不一致,且计算的齿轮系统共振转速区间或超前或滞后于静态啮合刚度模型;动态啮合刚度影响特定转速区间的齿轮系统的振动周期。对与转速相关的动态啮合刚度的研究可为直齿圆柱齿轮传动性能的改善及减振降噪提供参考。

Nonlinear Dynamical Responses of Rotary Cylindrical Shells with Internal Resonance

The nonlinear forced vibration response of a thin, elastic, rotary cylindrical shell to a harmonic excitation is investigated in this study. Nonlinearities due to the large-amplitude shell motion are considered by using Donnelfs nonlinear shallow-shell theory, with consideration of the effect of viscous structural damping. Different from the conventional DonnclFs nonlinear shallow-shell equations, an improved nonlinear model without employing the Airy stress function is utilized to study the nonlinear dynamics of thin shells. The system is discretized using the Galerkin method, while a model involving two degrees of freedom and allowing for the traveling wave response of the shell is adopted. The method of harmonic balance is applied to study the nonlinear dynamic responses of the t wo-degree-of-freedom system. In addition, the st ability of steady-state solutions is analyzed in detail. Finally, results are given for exploring the effects of different parameters on the nonlinear dynamic response with internal resonance.

齿侧间隙非线性函数拟合阶次的选取研究

针对齿侧间隙非线性函数拟合阶次的选取问题,以斜齿轮传动系统为例,对齿轮系统进行了理论建模、仿真分析,并对实际齿轮系统进行了实验研究。首先,采用集中质量法建立了考虑轴向振动的齿轮非线性系统模型,并对数学模型进行了无量纲化,对齿侧间隙函数分别进行了无拟合、4阶拟合和8阶拟合处理;然后,采用Runge-Kutta数值积分法进行了数值仿真分析,得到了齿轮系统x、y、z三个方向的幅值-频率比响应曲线图,研究了拟合阶次对系统x、y、z三个方向动态特性的影响;最后,进行了齿轮系统动态测试,得到了齿轮系统x、y、z三个方向的振动响应图,根据仿真与实验结果得出了结论。研究结果表明:不同处理方式下的齿轮系统振动响应在z向的差异较大,拟合阶次的选取应重点考虑z向;在x、y方向,齿侧间隙非线性4阶拟合函数会提前改变齿面接触状态且共振振幅分别增大1倍和1/3倍;对于多间隙的齿轮非线性系统,对齿侧间隙进行无拟合处理,可能导致计算困难和结果不准确;在固有频率附近,对齿侧间隙进行4阶拟合处理能够最大程度弥补其他非线性因素带来的影响;在其他频率范围,对齿侧间隙进行8阶拟合处理会更接近真实齿轮系统。齿侧间隙非线性函数的拟合处理在提高了计算效率的同时,也提高了模型的准确性。

大型风电齿轮箱系统耦合动态特性研究

综合考虑轮齿啮合时变刚度、齿轮传递误差、齿轮啮合冲击以及风载变化等因素影响,建立具有多级齿轮传动的大型风电齿轮箱齿轮-传动轴-轴承-箱体系统耦合非线性动力学模型。对风电齿轮箱系统有限元模型进行耦合模态分析,运用模态叠加法对齿轮箱系统在内部激励与外部激励综合作用下的振动响应进行求解。将仿真结果与实验数据对比,进而得到齿轮箱各点振动位移、速度、加速度及结构噪声等系统动态评价指标,为大型风电齿轮箱动态特性的准确评价及齿轮系统动态性能优化设计提供理论依据。

正交面齿轮传动系统非线性振动特性研究

作为一种新型传动形式,面齿轮传动在高速大功率场合的应用越来越多,其非线性振动特性分析对提高其工作可靠性具有重要意义。为研究正交面齿轮传动系统的非线性动力学特性,建立了包含支承、齿侧间隙、时变啮合刚度、综合传动误差、阻尼和外激励等参数的系统弯-扭耦合动力学模型,并使用PNF(Poincar-Newton-Floquet)方法对系统的动力学微分方程进行求解。计算结果表明:随着转速增大,系统呈现混沌-周期-混沌的运动特征,不同的混沌区域间存在周期窗口;在不同的参数条件下系统会出现4种动态响应,即简谐响应、次谐波响应、拟周期响应及混沌响应;不同的响应特性对应的动载系数幅值差别非常大,应尽量调节系统转速,使系统的动态响应保持在周期窗口内。

弧齿锥齿轮传动系统的非线性振动特性研究

基于集中参数法建立了弧齿锥齿轮的多自由度弯-扭-轴-摆耦合振动三维空间十二自由度动力学模型。模型中考虑了传动轴和轴承的弹性变形以及齿轮的啮合刚度激励、误差激励和啮合冲击激励。在忽略扭摆振动的基础上,系统等效处理为八自由度模型,通过引入状态变量并用五阶变步长自适应Runge-Kutta数值积分方法直接求解该多自由度模型,得到系统的动态响应。随激励频率ωh的改变,系统将出现单周期简谐、多周期次谐、拟周期和混沌响应,且发现各周期响应的过渡是通过拟周期的分叉实现的。

不同冲击力作用下人体动力学响应特性研究

为研究人体的冲击动态响应特性，６位受试者以坐姿承受垂直位冲击实验。冲击加速度为３Ｇ、５Ｇ、１０Ｇ左右。１１只猴各承受了１～５０Ｇ连续冲击。测试了受试对象多个部位的响应。人及猴响应的加速度峰值与座椅加速度峰值基本上呈正相关关系。由于不同部位主共振峰一致，表明人体是以整体对冲击响应的，冲击Ｇ值的大小影响人体频响特性。随着冲击Ｇ值的增加，人体的共振频率左移，第二峰的峰值随着增高，１０Ｇ时基本上融合为一个共振峰，致使主共振频率的峰值右移，显示出非线性。该规律与作者的振动研究结果一致。结果提示对于非线性系统可分段线性化逼近，可分别用不同的单自由度线性模型估计人体的动态响应。文中还讨论了冲击动态响应研究的方法学问题。

正交面齿轮传动系统的非线性振动特性

基于集中参数理论,考虑支撑的弹性变形、啮合齿轮副的时变啮合刚度激励和误差激励,建立正交面齿轮传动系统的多自由度弯曲-扭转-轴向移动耦合振动三维空间动力学模型;采用有限元方法计算点接触面齿轮传动系统的轮齿啮合刚度;借助动态相对传动误差,合并两轮转动自由度,将系统等效处理为5自由度非线性振动方程;采用自适应变步长Runge-Kutta数值积分方法,获得该系统的动态响应,并分析间隙对动载荷系数的影响。研究结果表明:随着啮合频率的变化,系统将出现单周期、2倍周期、拟周期和混沌响应;在周期响应状态下动载荷系数对间隙较敏感;间隙的改变对齿轮副的冲击状态没有影响,需通过调整支撑刚度等参数来实现单边冲击。

隔震结构非线性随机地震响应分析的复模态法

本文对多自由度双线性滞变隔震结构在过滤白噪声地震激励下的随机响应问题进行了系统研究。首先建立了结构非线性运动方程 ;然后根据非线性随机振动理论对运动方程进行等效线性化 ;最后用复模态法获得了等效线性方程的解析解 ,将复杂的非线性随机响应问题简化为求解一元非线性代数方程问题 ,并给出了算例。从而建立了多自由度隔震结构非线性随机响应复模态分析的一整套计算方法。

不确定非线性结构动力响应的区间分析方法

研究多自由度非线性不确定参数系统的动力响应问题．以区间数学为基础,将不确定性参数用区间进行定量化,借助一阶Taylor级数,给出了近似估计非线性振动系统动力响应范围的区间分析方法．从数学证明和数值算例两方面,将其与概率摄动有限元法进行了比较,结果显示区间分析方法对不确定参数先验信息具有要求较少、精度较高的优点．

高速柔性转子系统非线性振动响应特征分析

针对高速柔性转子多支点支承的结构特点及转子动力特性设计的需要,分析松动支承对转子动力特性的影响,仿真研究得到多支点支承高速柔性转子系统的非线性振动响应特征。研究结果表明:工作在多阶临界转速以上的转子系统,存在松动支承时,工作中的柔性转子可能存在周期、拟周期、混沌运动。进而研究了松动支承位置、不平衡量、松动间隙等参数对多支点支承柔性转子振动响应的影响,分析结果为多支点支承高速柔性转子系统的动力学设计提供了理论方法。

扭转微镜的动力学模型及其动态特性分析

扭转微镜中的静电和机械两个物理场是非线性耦合的,因此系统的数学模型及动态特性分析就变得很复杂。首先建立了扭转微镜的非线性动力学模型,然后采用直接积分法求解了系统的阶跃响应,通过数值模拟发现系统的固有频率随施加电压增大而减小、振动平衡位置随电压增大发生偏移等现象。对这些非线性现象进行了分析,有助于微镜系统设计和扩展微镜系统的应用范围。

行星齿轮系统弯扭耦合振动的增量谐波平衡法

针对行星齿轮传动机构弯扭耦合振动方程是半正定方程而无法直接采用增量谐波平衡法进行求解的问题,引入微小相对位移量来描述行星齿轮系统中各个部件之间的相对运动.采用运动转移矩阵将半正定方程转化为正定方程,同时考虑齿轮啮合刚度时变的非线性特性,采用增量谐波平衡法分析了行星齿轮系统非线性动力学响应.通过与数值求解方法Newmark-β法相对比,计算结果一致,验证了本文方法的正确性及高效性.

基于数值试验的波浪载荷激励船舶振动响应研究

即使未发生砰击振动和显著非线性波激振动,船体由较低频波浪诱导产生的振动响应中依然存在高频振动分量且高频振动衰减缓慢。从单自由度系统简谐激励振动理论入手,指出响应解析解中常被忽略的伴随自由振动项是导致高频振动的一个因素,在系统阻尼较小、自振频率较低时瞬态响应成分短时间内难以衰减,推导了位移、速度、加速度和内力响应中高频成分的占比规律。分析了波浪载荷作用于船体时"时变、场变"的性质,及船舶小阻尼系统的特点,认为伴随自由振动在波浪载荷激励振动响应预报领域中有重要地位,对比时域法和频域法在理论基础上的差异,发现了时域法在处理该问题时的优越性。通过对双体船进行数值仿真,结合海浪资料对该船16个航行工况的振动响应进行预报,结果表明各振动响应中均存在稳态高频分量且占比较高,得出了高频分量与频率比关系的规律性结论,为时域中波激振动的进一步研究提供了思路。