Synchronization of three homodromy coupled exciters in a non-resonant vibrating system of plane motion

In this paper, the synchronization problem of three homodromy coupled exciters in a non-resonant vibrating system of plane motion is studied. By introducing the average method of modified small parameters, we deduced dimensionless coupling equation of three exciters, which converted the problem of synchronization into that of the existence and stability of zero solutions for the average differential equations of the small parameters. Based on the dimensionless coupling torques and characteristics of the corresponding limited functions, the synchronization criterion for three exciters was derived as the absolute value of dimensionless residual torque difference between arbitrary two motors being less than the maximum of their dimensionless coupling torques. The stability criterion of its synchronous state lies in the double-condition that the inertia coupling matrix is positive definite and all its elements are positive as well. The synchronization determinants are the coefficients of synchronization ability, also called as the general dynamical symmetry coefficients. The double-equilibrium state of the vibrating system is manifested by numeric method, and the numeric and simulation results derived thereof indicate the indispensable and crucial role the structural parameters of the vibrating system play in the stability criterion of synchronous operation. Besides, by adjusting its structural parameters, the elliptical motion of the vibrating system successfully met the requirements in engineering applications.     

Composite synchronization of four exciters driven by induction motors in a vibration system

In this paper, a newly composite synchronization scheme is proposed to ensure the straight line vibration form of a linear vibration system driven by four exciters. Composite synchronization is a combination of self-synchronization and controlled synchronization. Firstly, controlled synchronization of two pairs of homodromous coupling exciters with zero phase differences is implemented by using the master–slave control structure and the adaptive sliding mode control algorithm. On basis of controlled synchronization, self-synchronization of two coupling exciters rotating in the opposite directions is studied. Based on the perturbation method, the synchronization and stability conditions of composite synchronization are obtained. The theoretical results indicate that composite synchronization of four exciters with zero phase differences can be implemented with different supply frequencies and the straight line vibration form of the linear vibration system also can be obtained. Some simulations are conducted to verify the feasibility of the proposed composite synchronization scheme. The effects of some structural parameters on composite synchronization of four exciters are discussed. Finally, some experiments are operated to validate the effectiveness of the proposed composite synchronization scheme.

     

ELECTROMECHANICAL COUPLING MODEL AND ANALYSIS OF TRANSIENT BEHAVIOR FOR INERTIAL RECIPROCATION MACHINES

Introduction Inertialvibratingmachinesexcitedbytworotatingeccentricweightsarewidelyusedto siftmaterialsinindustriessuchasmine,metallurgy,chemicalindustry,foodstuff,etc.The eccentricweightisgenerallydrivenbyanasynchronouselectromotor,anditssteady state ope…     

倍频激励双转子振动同步机理与实验研究

振动筛作为第一级钻井液净化设备, 其筛分性能直接决定后续固控系统的生产效率. 针对在筛分工程中由相同驱动频率激励的振动系统所表现出的单一振动特性难以与筛面上的物料粒度相匹配, 从而引发筛孔堵塞的问题, 本文提出了倍频激励双转子自同步振动系统. 首先根据数学模型运用广义Lagrange公式建立多自由度振动系统的运动微分方程, 并引入复变函数求解箱体的稳态幅值响应; 其次探明了振动系统实现倍频同步的前提条件和稳定性评估标准; 然后通过数值计算定量地讨论转子间的倍频动力学特征与系统结构参数之间的关系, 并结合Runge?Kutta算法建立振动系统的多自由度机电耦合动力学仿真模型, 详细讨论转子与箱体间的倍频同步机理; 最后设计实验样机, 针对系统在不同工况下的动态特性和同步运动状态展开实验测试, 进一步验证理论研究和计算机模拟的正确性. 研究表明, 系统的倍频同步能力指数随安装距离的不断增加而接近于零值附近, 此时高频转子与低频转子获得稳定同步振动的可能性越来越高; 电机同步状态几乎不受弹簧刚度的影响, 但稳态相位差值在单周期内会随激振器安装倾角和距离的变化而逐渐减小并趋于在一个恒定值. 研究成果不仅对石油工业新型振动筛系统的研制具有重要的参考价值, 也将促进其他同步振动机械的发展.      

振荡燃烧的动态测试及信息处理

作者用随机信息处理方法研究了某型火箭发动机的燃烧状况,不仅发现该型发动机存在有振荡燃烧,而且获得了振荡燃烧信息的功率谱及功率谱阵。针对振荡燃烧信息在时间域和频率域上的随机性特点,作者精心地设计了测试系统,并对系统的性能参数进行了全面标定。经多次实测证明该系统工作可靠,信噪比较高。测试与分析结果表明:该型发动机振荡燃烧的主振测率为800Hz,最大振幅为43dB;并存在有1600Hz和2500Hz两个次级振荡频率;而且该发动机的振荡燃烧是以纵向振荡为主。为研究该型火箭发动机振荡燃烧的产生原因和消除方法提供了科学依据。     

Dynamic analysis of a flexible hub-beam system with tip mass

For a dynamic system of a rigid hub and a flexible cantilever beam, the traditional hybrid coordinate model assumes the small deformation in structural dynamics where axial and transverse displacements at any point in the beam are uncoupled. This traditional hybrid coordinate model is referred as the zeroth-order approximation coupling model in this paper, which may result in divergence to the dynamic problem of some rigid–flexible coupling systems with high rotational speed. In this paper, characteristics of a flexible hub-beam system with a tip mass is studied. Based on the Hamilton theory and the finite element discretization method, and in consideration of the second-order coupling quantity of the axial displacement caused by the transverse displacement of the beam, the rigid–flexible coupling dynamic model (referred as the first-order approximation coupling (FOAC) model in this paper) and the corresponding model in non-inertial system for the flexible hub-beam system with a tip mass are presented firstly, then the dynamic characteristics of the system are studied through numerical simulations under twos cases: the large motion of the system is known and is unknown. Simulation and comparison studies using both the traditional zeroth-order model and the proposed first-order model show that even small tip mass may affect dynamic characteristics of the system significantly, which may result in the largening of vibrating amplitude and the descending of vibrating frequency of the beam, and may affect end position of the hub-beam system as well. The effect of the tip mass becomes large along with the increasing of rotating speed of large motion of the system. When the large motion of the system is at low speed, the traditional ZOAC model may lead to a large error, whereas the proposed FOAC model is valid. When the large motion is at high speed, the ZOAC model may result in divergence to the dynamic problem of the flexible hub-beam system, while the proposed second model can still accurately describe the dynamic hub-beam system.     

振动陀螺仪单向时滞耦合系统的摄动分析

针对振动陀螺仪单向时滞耦合系统,研究了角速度、耦合强度、耦合时滞与系统输出信号之间的关系,着重关注耦合时滞对待检测角速度测量结果的影响．本文采用摄动法对振动陀螺仪单向时滞耦合系统进行理论分析,得到了系统输出信号、系统振动边界和待检测角速度的近似表达式,并将数值和近似计算结果进行了对比．理论分析结果与数值结果比较吻合,验证了运用摄动法分析振动陀螺仪单向时滞耦合系统的有效性,也表明了在运用摄动法分析系统时具有局限性．     

Kinematics of haylage bale in 3D space as a body of one fix point and two rotations

This paper presents mechanical-mathematical matrix simulation of haylage bale kinematics in 3D space as a body of one fix point and two rotations. There are defined: the matrices of transition from the coordinate system connected stationary with the body to the starting (global) coordinate system; the position vector, absolute linear speed and absolute linear acceleration of bale arbitrary point; the vector of absolute angular velocity and absolute angular acceleration projected in the starting and in the local coordinate systems of the body. Numerical example is provided.     

Large free vibration of thin plates: Hierarchic finite Element Method and asymptotic linearization

The aim of this work is to study the free dynamic response of thin plates characterized by geometrical nonlinearities. To achieve this task, the equation of motion of the plate is first carried out through modeling by hierarchical finite element method whose interpolating shape functions are sinusoidal. Then, the study of the nonlinear vibrations was carried out by the development of asymptotic linearization and equivalent linearization methods in modal space. The nonlinear angular frequencies are successively deduced by exciting the corresponding vibrating mode of the structure. The confrontation of these results to those obtained by the iterative method in the physical space and to those found in the literature, showed a very good agreement between the various methods. From the elementary nonlinear frequencies we showed that there exists an equivalent linear dynamical system characterized by only one equivalent linear stiffness matrix. Numerical experiments were carried out on beams and thin plates of various dimensions ratios and boundary conditions. These numerical test simulations, whether in time space or frequency space, have showed that the nonlinear elastic energy is restored by the equivalent linear dynamical system. Nevertheless, we have to say that the dynamic effects of modes above the excited one are neglected.     

受控振动系统时滞依赖稳定性判据的LMI方法

针对带有不确定性时滞的振动控制系统,引入改进的二向量内积的上确界,对Lyapunov导数进行合理放大,提出了一种新的时滞依赖鲁棒性稳定准则。根据这种新的判别方法,受控振动系统的最大时滞量可以通过Matlab控制工具箱LMI(线性矩阵不等式)得到。讨论了单自由度系统中最大时滞随系统参数的变化情况及多自由度系统中控制器最优权值R的确定。算例结果表明,在允许时滞范围内,经典的LQR控制器可以收到令人满意的效果。     

旋转运动中弹性梁耦合振动的辛方法

研究旋转梁结构的弹性耦合振动问题。通过引入对偶体系,建立了解决该类问题的辛方法。在辛体系中描述旋转梁纵向和横向耦合振动控制方程,即哈密顿正则方程。进一步求解得到结构的固有振动频率及相应的振动模态,发现固有振动频率随转动角速度先升后降以及模态之间的某种转化规律。     

Sound Radiated in a Cavity by a Vibrating Plate: Comparison between the Results of a Finite Element Method (FEMAK) and a Boundary Element Method (NoVAlea2D)

The coupling between a cavity and a vibrating plate is written as a strong coupling where both the continuity of stresses and particle velocities at the interface are taken into account. A FEM analysis reveals an important coupling between the first mode of the plate and the cavity. The pressure distribution in the cavity shows a strong quarter of a wave length pattern indicating the influence of the first Dirichlet mode in the cavity. The vibrating plate is then excited by a turbulent flow modelled by its spectral density using the Corcos model. A comparison is made between the results obtained from a FEM and a BEM formulation. Good agreements are observed concerning the plate displacements. The comparison of the cavity sound pressure levels is less good. This revised version was published online in July 2006 with corrections to the Cover Date.     

作大范围空间运动柔性梁的刚-柔耦合动力学

研究带中心刚体的作大范围空间运动梁的刚-柔耦合动力学问题．从精确的应变-位移关系式出发,在动力学变分方程中,考虑了横截面转动的惯性力偶和与扭转变形有关的弹性力的虚功率,用速度变分原理建立了考虑几何非线性的空间梁的刚-柔耦合动力学方程,用有限元法进行离散．通过对空间梁系统的数值仿真研究扭转变形和截面转动惯量对系统动力学性态的影响．     

Active vibration control of a dynamical system via negative linear velocity feedback

In this paper, a negative velocity feedback is added to a dynamical system which is represented by second-order nonlinear differential equations having quadratic coupling, quadratic, and cubic nonlinearities. The system describes the vibration of the system subjected to multi-parametric excitation forces. The method of multiple scale perturbation technique is applied to obtain the response equation near the simultaneous internal and super-harmonic resonance case of this system. The stability to the system is investigated applying frequency response equations. The numerical solution and the effects of some parameters on the vibrating system are investigated and reported. The simulation results are achieved using MATLAB 7.0 program. A comparison is made with the available published work.     

Nonlinear instabilities in a vibratory gyroscope subjected to angular speed fluctuations

Nonlinear instabilities in a single-axis vibrating MEMS gyroscope that is subjected to periodic fluctuations in input angular rates are investigated. For the purpose of characterizing the bifurcation behavior associated with the steady-state, when the angular rate input is subject to small intensity periodic fluctuations, dynamic behavior of periodically perturbed nonlinear gyroscopic systems is studied in detail. An asymptotic approach based on the method of averaging has been employed for this purpose, and closed-form conditions for the frequency response due to parametric resonances have been obtained. This behavior has been illustrated via amplitude-frequency plots.     

Nonlinear dynamic analysis on rigid-flexible coupling system of an elastic beam

Previous work examined the effect of the attached stiffness matrix terms on stability of an elastic beam undergoing prescribed large overall motion. The aim of the present work is to extend the nonlinear formulations to an elastic beam with free large overall motion. Based on initial stress method, the nonlinear coupling equations of elastic beams are obtained with free large overall motion and the attached stiffness matrix is derived by solving sub-static formulation. The angular velocity and the tip deformation of the elastic pendulum are calculated. The analytical results show that the simulation results of the present model are tabled and coincide with the one-order approximate model. It is shown that the simulation results accord with energy conservation principle.     

Coupling of assumed stress finite element and boundary element methods with stress-traction equilibrium

In this study, the stress based finite element method is coupled with the boundary element method in two different ways. In the first one, the ordinary distribution matrix is used for coupling. In the second one, the stress traction equilibrium is used at the interface line of both regions as a new coupling process. This new coupling procedure is presented without a distribution matrix. Several case studies are solved for the validation of the developed coupling procedure. The results of case studies are compared with the distribution matrix coupling, displacement based finite element method, assumed stress finite element method, boundary element method, ANSYS and analytical results whenever possible. It is shown that the coupling of the stress traction equilibrium with assumed stress finite elements gives as accurate results as those by the distribution matrix coupling.     

管道流固耦合振动的行波方法研究

应用波动方法分析载流管道流固耦合振动问题。采用直梁模型，推导了管道流固耦合系统的轴向、横向波导方程及平面管系的坐标转换矩阵，通过节点位移连续和力平衡条件建立了耦合系统的散射模型。最终分析了两种耦合对载流管道振动的影响机理及流速变化对管道振动稳定性的影响。数值算例表明本文方法的正确性及有效性。     

Resonance capture in a damped three-degree-of-freedom system: Experimental and analytical comparison

The dynamical behavior of a three-degree-of-freedom system is considered in the presence of a 1:1 resonance between two components with non-linear inertial coupling. One of the resonant frequencies is fixed, characterizing a translational oscillation, while the second frequency varies slowly in time and describes the angular velocity of an unbalanced rotational component. As the angular velocity approaches the translational frequency of oscillation, the system can either become locked into a sustained resonance or pass through the 1:1 resonance depending on the parameter values and initial conditions. When the system is attracted to a state of sustained resonance, the amplitude of the translational oscillations and the steady-state frequency of the sustained resonance vary, depending on the parameter values of the system. As the applied torque increases, both the resonant frequency and oscillation amplitude increases. If the applied torque is too large, the sustained resonance no longer exists and the system cannot be attracted to a long-term resonant motion. These variations in the response with parametric changes are described from a reduced-order model obtained with the method of averaging and are also seen in numerical simulations of the original equations of motion. Finally, the results are verified in an experimental rotordynamic system.