基于谐振器激励的轴承故障动力学建模研究

考虑轴承故障动力学中的高频共振以及故障激励特点,提出一种模拟系统高频共振和过渡式故障激励的轴承故障动力学建模方法。基于赫兹接触理论,将轴承部件之间的连接简化为弹簧-阻尼结构,并加入谐振器以模拟故障的宽频激励所引起的系统高频共振,从而建立轴承六自由度动力学模型。另外,传统的故障瞬变激励方法难以反映滚动体经过滚道故障的过程,考虑到滚动体与故障接触的实际情况,给出一种过渡式的故障激励方法。以传动链平台上的6304深沟球轴承为例,对轴承外圈故障下的振动响应特性进行仿真和数据处理,其仿真结果与轴承故障实测信号对比相符,仿真信号故障一阶特征阶次与理论值误差约为0.016 7%,表明模型具有一定的准确性和可靠性。     

轨下支承失效对直线轨道动态响应的影响

建立了基于Timoshenko梁模型的车辆/轨道耦合动力学模型,分析轨下支承失效对直线轨道动态响应的影响. 钢轨被视为连续弹性离散点支承上的无限长Timoshenko梁,通过假设轨道系统刚度沿纵向分布发生突变来模拟轨下支承失效状态. 推导了考虑钢轨横向、垂向和扭转运动的轮轨滚动接触蠕滑率计算公式. 利用Hertz法向接触理论和沈氏蠕滑理论计算轮轨法向力及轮轨滚动接触蠕滑力. 采用移动轨下支承模型的车辆/轨道耦合系统激振模式,考虑轨枕离散支承对系统动力响应的影响. 通过新型显式积分法求解车辆/轨道耦合动力学系统运动方程,由数值分析计算得到不同轨下支承失效状态下直线轨道的动态响应. 结果表明,轨下支承失效对直线轨道变形及加速度有显著的影响,随着失效轨下支承个数的增加,轮轨相互作用力和轨道部件的位移、加速度将会急剧增大,将加速失效区段线路状况的恶化.      

天线座驱动系统刚柔耦合动力学分析

为了分析天线座驱动系统的动力学特性,建立了一种新的多级齿轮传动系统动力学模型------刚柔耦合模型,不仅考虑了轴的变形、轴承的支撑作用,而且采用了先进的轮齿接触模型,克服了采用多体动力学方法研究齿轮系统动力学时存在的诸如忽略轴承的支撑作用、轴的变形等缺陷. 动力学分析的计算结果和理论分析结果相一致,较准确地反映了该系统的齿轮动力特性,对工程设计及性能校核具有指导意义.     

基于随机过程的固液分离旋流器磨损可靠性研究

采用Fluent软件中的RSM湍流模型和DPM模型数值模拟了颗粒的运动轨迹;在传统的磨损分析模型中引入白噪声代表分离过程的动态和随机因素,应用维纳过程理论和极限状态方程,建立了旋流器壁面磨损的动态可靠性模型,对流场和结构相互作用的固液分离旋流器进行磨损可靠性预测,并给出了模型中重要统计特征参数的估计方法。以某型号单入口式固液分离旋流器为例进行了壁面厚度磨损动态可靠性和寿命特征的具体计算,验证了本文所提模型和方法的合理性,得出该旋流器可靠度下降较快的区间为1.2×10⁷s～3×10⁷s,其平均寿命为11111h。本文的研究可为旋流器定量寿命评估和强度优化设计提供理论基础。     

空间机械臂捕获卫星过程的碰撞动力学模拟及镇定运动的鲁棒控制

讨论了漂浮基空间机械臂捕获未知运动目标卫星的接触碰撞动力学建模和接触碰撞后系统镇定运动的控制问题。利用第二类拉格朗日方法和牛顿-欧拉法分别建立了接触碰撞前漂浮基空间机械臂和目标卫星两分体系统的动力学模型;以此为基础借助于空间机械臂与目标卫星接触点间的运动几何关系、力传递关系,计算了接触碰撞所产生的影响效应;捕获卫星后,联立空间机械臂与卫星接触碰撞前的动力学模型,建立了接触碰撞后两系统组合体动力学模型;并设计了增广鲁棒控制算法,以对受碰撞冲击后处于不稳定的组合体系统进行镇定运动控制。上述控制方法能应用于空间机械臂载体位置不受控情况,并能使组合体系统控制方程关于卫星不确定参数呈线性化关系。最后,利用数值仿真模拟捕获过程系统运动状态,验证了上述鲁棒控制镇定运动的效果。     

基于超二次曲面的非球形离散单元模型研究

通过对颗粒体系接触过程的运动学和动力学分析,建立了一种基于超二次曲面的非球形离散单元模型,该模型避免了球形接触模型描述颗粒形状的局限性,使离散单元法更接近物理事实,并在此基础上提出了计算求解模型的数值方法,实现了对复杂形状的颗粒体系的模拟计算。将所建立的数值计算方法进行了编程实现,并对模型和算法进行了算例测试,证实了本文所建立的非球形离散单元模型的可行性和正确性。测试结果表明,本文的模型能够比较准确地模拟复杂颗粒体系的真实运动,可为复杂颗粒体系的模拟研究提供一种新的数值计算方法。     

吸气式高超声速飞行器动力学建模研究进展

高超声速飞行以及飞行器机身/超燃冲压发动机一体化设计的典型特点导致吸气式高超声速飞行器具有不同于常规飞行器的飞行动力学特性,而飞行器总体设计和控制系统设计都必须考虑这些新动力学特性的影响,因此为吸气式高超声速飞行器建立能够包含这些新特性的飞行动力学模型非常重要.本文对吸气式高超声速飞行器动力学建模的相关研究进行了总结: 首先,简略地回顾了从超燃冲压发动机研究到飞行器系统研究发展历程; 其次,详细阐述了宽飞行包线、高超声速效应、超燃冲压发动机约束、气动/推进耦合和气动弹性效应等吸气式高超声速飞行器的新动力学特性;然后,讨论了在选择坐标系、抽象飞行器外形、建立弹性机身模型、建立空气动力模型、建立超燃冲压发动机系统模型以及推导运动方程等每个具体步骤中需要考虑的问题和可用的方法;最后,评述了现有吸气式高超声速飞行器动力学模型,并指明了未来发展方向.      

飞机网式拦阻系统动力学分析

介绍了飞机拦阻网系统的工作原理,并通过对系统各构件的受力特点分析,建立了飞机在拦阻过程中的动力学模型,从理论上得出了在拦阻网工作过程中飞机速度随位移衰减的关系式,同时可估算飞机滑行距离和网绳拉力.     

车轮多边形激励下高速列车制动界面摩擦学行为分析

高速列车车轮多边形磨耗是一种沿车轮周向的不均匀磨耗,是列车服役过程中常见的车轮失效现象,其产生的剧烈轮轨激励严重威胁车辆系统服役可靠性.制动系统作为保障高速列车服役安全的核心部件,其界面摩擦学行为直接受到轮轨激励的影响.为探究车轮多边形激励下的制动界面摩擦学行为,建立了刚柔耦合车辆动力学模型和制动系统热机耦合有限元模型,并分别通过线路试验和台架试验验证了模型的正确性.然后,提出一种考虑车轮多边形激励的制动界面摩擦学行为分析方法,能够真实地反映服役过程中制动界面摩擦学行为.基于此,研究了不同车辆运行速度下车轮多边形激励对制动系统动态接触、温度以及振动特性的影响规律.结果表明：车轮多边形磨耗导致系统接触面积、摩擦热、接触应力和振动等摩擦学行为更为复杂且剧烈.此外,系统接触面积标准差和振动加速度均方根值随速度的增加而增大.因此,车轮多边形磨耗对制动界面摩擦学行为具有不可忽略的影响.该研究成果可为制动系统界面摩擦学行为研究及结构优化设计提供有效方法与工程指导.     

多体系统动力学中关节效应模型的研究进展

在一般的多体系统动力学研究中认为运动关节是理想运动副. 然而,实际中的运动关节不仅含有间隙与摩擦,还有间隙引起的关节元素之间的接触碰撞、局部变形和磨损. 多体系统动力学中的关节效应不仅引起了系统的振动和噪声,减小了系统的可靠性和寿命,而且损失了系统的精度和稳定性. 为此,对近十几年多体系统动力学中关节效应的研究进行了详细分析,总结了关节效应中间隙运动学模型、接触力模型与磨损模型在多体系统动力学中的建模过程. 其中,着重分析了多体系统动力学中关节磨损效应的研究进展,并对常用的Reye'shypothesis 和Archard 磨损模型进行了比较,详细地分析了Archard 磨损模型的演变形式以及主要磨损参数(接触应力,接触面积和滑移距离),特别分析了关键磨损参数接触应力的建模方法,解释了基于Winkler 弹性基础理论在求解接触应力时遇到的困难. 另外,介绍了4 种间隙运动副(转动副、移动副、圆柱副和球面副) 的运动学模型. 分析了考虑关节磨损多体系统动力学模型的一般建模方法,并以平面五杆机构为例说明了其建模过程.最后,简要地展望了多体系统动力学中关节效应模型的发展趋势以及应用前景.      

具有裂纹-碰摩耦合故障转子-轴承系统的动力学研究

以非线性动力学和转子动力学理论为基础，分析了带有碰摩和裂纹耦合故障的弹性转子系统的复杂运动，在考虑轴承油膜力的同时构造了含有裂纹和碰摩故障转子系统的动力学模型。针对短轴承油膜力和碰摩-裂纹转子系统的强非线性特点，采用Runge-Kutta法对该系统由碰摩和裂纹耦合故障导致的非线性动力学行为进行了数值仿真研究，发现该类碰摩转子系统在运行过程中存在周期运动、拟周期运动和混沌运动等丰富的非线性现象，该研究结果为转子-轴承系统故障诊断、动态设计和安全运行提供理论参考。     

Research of giant magnetostrictive actuator’s nonlinear dynamic behaviours

The multi-coupled nonlinear factors existing in the giant magnetostrictive actuator (GMA) have a serious impact on its output characteristics. If the structural parameters are not properly designed, it is easy to fall into the nonlinear instability, which has seriously hindered its application in many important fields. The electric–magnetic-machine coupled dynamic mathematical model for GMA is established according to J-A dynamic hysteresis model, ampere circuit law, nonlinear quadratic domain model and structure dynamics equation. Nonlinear dynamic analysis method is applied to study the nonlinear dynamic behaviour of the key structure parameters to reveal their influence on the system stability. The design principle of structural parameters is obtained by studying stability of GMA, which provides theoretical basis and technical support for the structural stability design.     

A DYNAMIC MODEL FOR ROCKET LAUNCHER WITH COUPLED RIGID AND FLEXIBLW MOTION

The dynamics of a coupled rigid-flexible rocket launcher is reported. The coupled rigid-flexible rocket launcher is divided into two subsystems, one is a system of rigid bodies,the other a flexible launch tube which can undergo large overall motions spatially. First, the mathematical models for these two subsystems were established respectively. Then the dynamic model for the whole system was obtained by considering the coupling effect between these two subsystems. The approach, which divides a complex system into several simple subsystems first and then obtains the dynamic model for the whole system via combining the existing dynamic models for simple subsystems, can make the modeling procedure efficient and convenient.     

Study of the open and closed loop characteristics of a tractor and a single axle towed implement system

Accurate automatic guidance of towed implements is important for performing agricultural field operations and for gaining the ultimate benefit from such systems. The study of open and closed loop system responses of a vehicle-implement system can be helpful in the design of practical guidance controllers. Open loop analysis of the kinematic and dynamic models revealed that the higher order dynamics captured by the tractor and implement dynamic model had an impact on simulated responses at higher operating velocities and on higher input frequencies. In addition, a dynamic model with tire relaxation length dynamics was also studied. The various model responses were compared with the experimental responses. Closed loop system characteristics were studied by using a linear quadratic regulator (LQR) controller. The tractor position and heading and implement heading states along with respective rate states were fed back to close the loop. Steering dynamics were also added to the dynamic model closed loop analysis, which helped to achieve a realistic closed loop steering angle history. The closed loop system dynamics became faster as the forward velocity was increased. The open and closed loop response analysis performed in this work provided an understanding about the system at various forward velocities, which will help to design and develop efficient and robust tractor and towed implement guidance controller.     

基于径向基点插值法的旋转Mindlin板高次刚柔耦合动力学模型

将无网格径向基点插值法(radial point interpolation method,RPIM)用于中心刚体?旋转柔性板的动力学分析.基于浮动坐标系方法和一阶剪切变形理论即Mindlin板理论,考虑剪切变形的影响,并计入板面内变形的非线性耦合变形项,采用径向基点插值法描述板的变形场,保留动能中有关非线性耦合变形项...     

Bifurcation of multi-freedom gear system with spalling defect

This study focuses on the bifurcation characteristics of the four degree-of-freedom gear system with local spalling defect to explore the spalling nonlinear dynamic mechanism. The dynamic model of the gear system with spalling defect, time-variant mesh stiffness, and nonlinear clearance is established to investigate the effect of spalling defect on mesh stiffness and dynamic bifurcation. The primary resonance and internal resonance responses of the spalling model are analyzed by the averaging method, and the bifurcation characteristics with the evolvement of spall and internal excitation are studied by employing the singularity theory for the two-state variable system, which reveal the different bifurcation characteristics caused by the spalling defect. The results obtained herein can provide a theoretical basis to spalling fault diagnosis of gearbox.     

Non-linear parametric modelling of a high-speed rail hydraulic yaw damper with series clearance and stiffness

At high operational speeds, the train system becomes very sensitive to parameter variations of components. Therefore, it is imperative to incorporate more accurate component models in the vehicle dynamics studies. This study addresses a more subtle and comprehensive non-linear parametric model of a high-speed rail hydraulic yaw damper. A new concept of a hydraulic yaw damper model is suggested, in which the small mounting clearance, the series stiffness, and the viscous damping are built in. The series stiffness is the tandem result of the dynamic oil stiffness, the rubber attachment stiffness, and the mounting seat stiffness. A dynamic oil property model is established and coupled to the entire modelling process, in which the density, the dynamic viscosity, the volumetric elastic modulus, and the stiffness of the oil are all changeable in terms of the instantaneous working pressure, the oil temperature, and the entrapped air ratio of the oil. The dynamic flow loss and the valve system dynamics are also incorporated. Experiments validated that the established non-linear parametric model is accurate and robust in predicting the damping characteristics within an extremely wide speed range. The validated damper model was then successfully applied to a thorough parameter sensitivity analysis and damping nature prediction under practical, in-service conditions. The established damper model couples all the main influential factors that are not or are insufficiently considered in normal-speed problems; thus, it will be more accurate and appropriate for furthering high-speed problem studies.     

Modeling of the vehicle shimmy system with consideration of clearance of the steering linkage mechanism

The mechanism of vehicle shimmy has been paid much attention in the past decades. In which, the clearance of the steering linkage is usually neglected. Yet the prior research of the authors proved that the clearance can make great effects on the dynamic performance of the linkage. Therefore, based on nonlinear dynamics, a six-DOF dynamic model of vehicle shimmy system with consideration of the clearance was established. In which, the nonlinearity due to clearance of the movement pair in steering mechanism was taken into account. Numerical examples showed that the clearance of the movement pair could make great effects on the dynamic behavior of the vehicle shimmy system, and it is one of the key factors leading to chaos motion of the shimmy system, which provided theoretical basis for vehicle shimmy control.     

履带车辆路面激励响应的简化计算

为了快速计算履带车辆在路面不平度激励下的动力学响应,基于合理假设采用理论力学方法建立了某履带车辆的简化动力学模型,用ADAMS 软件建立了同种工况下的履带车辆动力学模型,并把两种模型的求解结果进行了对比,验证了简化模型的合理性. 研究结果为基于简化模型的动力学方程对车辆悬挂系统进行优化和逆动力学分析奠定了基础.