大跨钢桁架拱桥地震响应有限元分析

采用ANSYS建立某大跨钢桁架拱桥有限元模型,对其进行模态分析;采用瑞利阻尼理论,通过拱桥前2阶圆频率计算质量阻尼和刚度阻尼;采用动力时程分析法对拱桥进行地震响应有限元分析.结果表明:横向位移的最大峰值由水平地震波载荷沿横桥向输入决定,纵向位移的最大峰值由水平地震波载荷沿纵桥向输入决定,竖向位移的最大峰值由重力载荷工况决定.     

LNG储罐外壁地震响应有限元分析

利用ADINA分别建立LNG储罐空罐SHELL壳体单元及3D-SOLID实体单元有限元模型.对2种模型进行模态分析,验证SHELL单元模型的有效性.在El Centro地震波作用下对LNG储罐混凝土外壁进行地震响应分析.结果表明:在地震作用下,LNG储罐外壁的位移和加速度沿罐高方向逐渐增大;空罐时,LNG储罐外壁位移及加速度时程曲线与地震波形基本一致.     

航天器模态分析-试验体系工程实践研究

传统航天器结构模态试验通常会用来检验结构有限元分析模型,但往往是通过人工调整有限元模型参数来修正模型,分析与试验联系不紧密,影响后续分析结果的精度、研制周期和经费等.为改变航天器模态分析及试验现状,文中介绍了模态分析-试验体系工程研制流程在理论上的可行性,并以某缩比舱段为例,基于Virtualab-Nastran软件平台,完整实施模态分析-试验体系过程,包括预试验分析、模态试验、模型修正等过程,紧密联系模态分析、试验,并依据试验结果准确快速修正有限元模型,使分析结果与试验接近,实现精确建模.     

基于Kriging模型的航空发动机管道系统有限元模型修正

为获得精确可靠的航空发动机外部管道结构动力学模型,采用将Kriging模型与多目标遗传算法(MOGA)相结合的模型修正方法进行有限元模型修正.首先进行管道模型的模态试验和有限元建模,分别获得模态参数的试验值和有限元分析值；然后在合理的参数选取和试验设计(DOE)的基础上,拟合得到Kriging模型；最后基于Kriging模型采用多目标遗传算法进行有限元模型修正,并对比了不同修正方法的精度和修正效果.结果表明：采用Kriging模型进行有限元模型修正可以有效提升修正效果,获得更为准确的有限元模型；对于航空发动机管道系统,基于Kriging模型的模型修正方法相较于基于灵敏度分析的模型修正方法具有更高的修正效率和修正精度.     

Modal analysis of active flexible multibody systems

When performing modal analyses of active flexible multibody systems, both controller effects and flexible body dynamics should be included in a multidisciplinary system model. This paper deals with the theory of solving the closed-loop eigenvalue problem for active flexible multibody systems with multiple-input multiple-output proportional-integral-derivative (PID) type feedback controllers and multiple degrees of freedom finite element models. Modal analyses are performed on both a simple and complex active flexible multibody system in order to illustrate the difference between current modal analysis method for such systems and the proposed theory derived in this paper.     

Modal approximation of xenon oscillations in nuclear reactors — an FEM-based approach

A modal expansion method for modelling dynamic space-dependent effects (xenon oscillations) in large nuclear reactors is presented. Based on the finite element method (FEM), modal expansion functions for various cases with practical significance can be calculated. In this way it is possible to derive a low order state space model describing the considered effect. The use of this model in on-line controller design and simulation is intended. Modal methods in connection with modern numerical algorithms turned out to be effective to treat distributed parameter systems governed by elliptic differential equations. This will be demonstrated by application to a VVER-1000 pressurized water reactor.     

A method for controller parameter estimation based on perturbations

Simulation and prediction of eigenfrequencies and mode shapes for active flexible multibody systems is an important task in disciplines such as robotics and aerospace engineering. A challenge is to accurately include both controller effects and flexible body dynamics in a multidisciplinary system model appropriate for modal analysis. A method for performing modal analyses of such systems in a finite element environment was recently developed by the authors. On issue is, however, that for engineers working in a finite element environment, the controller properties are not always explicitly available prior to modal analyses. The authors encountered this problem when working with the design of a particular offshore windmill. The controller for the windmill was delivered in the form of a dynamic link library (dll) from a third party provider, and when performing virtual testing of the windmill design, it was of great importance to use the “real” controller in the form of the provided dll, rather than re-model it in for instance Simulink or EASY5. This paper presents a method for estimating the controller parameters of PID-type controllers when solving the closed-loop eigenvalue problem for active flexible multibody systems in a finite element environment. The method is based on applying incremental changes, perturbations, to relevant system variables while recording reactions from other system variables. In this work, the theory of the method is derived and the method is tested through several numerical examples.     

A structural defect identification approach based on a continuum damage model

This paper introduces a structural identification technique built on finite element (FE) model updating. The FE model is parameterized by a structural parameter that continuously describes the damage in the structure, and besides, an evolution equation of this damage parameter is presented. The model updating is accomplished by determining the subset of this damage parameters that minimizes a global error derived from the dynamic residue vectors, which is obtained by introducing the experimental modal properties into the original model eigenproblem. A mode-shape projection technique is used in order to achieve compatibility between the dimension of the experimental and analytical models. The adjusted model maintains basic properties of the analytical model as the sparsity and the symmetry, which plays an important role in model updating-based damage identification. The verification and assessment of the current structural defect identification is performed on a analytically derived bidimensional truss structure and on a cantilever bidimensional Euler–Bernouilli beam through a virtual test simulator. This simulator is used to realistically simulate the corrupting effects of noise, filtering, digital sampling and truncation of the modal spectrum. The eigensystem realization algorithm along with the common-based normalized system identification were utilized to obtain the required natural frequencies and mode shapes.     

Model updating based on incomplete modal data

The objective of model updating is to improve the accuracy of a dynamic model based on the correlation between the measured data and the analytical (finite element) model. In this paper, we intend to update the mass and stiffness matrices of an analytical model when only modal frequencies or spatially incomplete modal data are available. While the proposed method is systematic in nature, it also preserves the initial configuration of the analytical model, and physical equality and/or inequality constraints ...     

大跨钢箱梁悬索桥地震响应有限元分析

根据某大跨钢箱梁悬索桥的设计图纸,采用ANSYS建立其有限元模型,采用壳单元对主梁进行模拟.通过不断调试找出最佳的主缆初始应力,完成悬索桥的初始找形分析.对悬索桥进行预应力模态分析,采用瑞利阻尼理论,通过悬索桥有限元模型的前2阶圆频率计算模型的质量阻尼和刚度阻尼.采用动力时程分析法对悬索桥进行地震响应有限元分析.结果表明:横桥向位移的最大峰值由横桥向地震波输入决定,纵桥向位移的最大峰值以及竖桥向位移的最大峰值主要由重力载荷工况决定,地震载荷工况对其贡献非常小.     

某磁浮飞轮转子系统有限元分析

为更好地分析计算磁浮飞轮转子系统的动力学特性,对其进行有限元仿真.基于已有的磁浮轴承控制律,根据相关参数计算出转子系统平衡位置处的线性化位移刚度,建立弹性支撑的磁浮飞轮转子有限元模型,用ANSYS对转子进行模态分析,研究支撑刚度和离心应力对转子系统模态和频率的影响.结果可为磁浮飞轮的信号测试和模态控制提供参考.     

Finite element-based analysis of shunted piezoelectric structures for vibration damping

Piezoelectric patches shunted with passive electrical networks can be attached to a host structure for reduction of structural vibrations. This approach is frequently called “shunted piezo damping” and has the advantage of guaranteed stability and low complexity in implementation. For numerical treatment of such structures, a finite element modelling methodology is presented that incorporates both the piezoelectric coupling effects of the patches and the electrical dynamics of the connected passive electrical circuits. It allows direct computation of the achieved modal damping ratios as a major design criterion of interest. The damping ratios are determined from the eigenvalue problem corresponding to the coupled model containing piezoelectric structure and passive electrical circuit. The model includes local stiffening and mass effects as a result of the attached patches and, therefore, enables accurate prediction of the natural frequencies and corresponding modal damping ratios. This becomes crucial for choosing the patch thickness to achieve optimal modal damping for a given host structure. Additionally, structures with complex geometry or spatially varying material properties can easily be handled. Furthermore, the use of a finite element formulation for the coupled model of piezoelectric patches and a host structure facilitates design modifications and systematic investigations of parameter dependencies. In this paper, the impact of parameters of the passive electrical network on modal damping ratios as well as the variation of the patch thickness are studied. An application of this modelling method is realized by commercial software packages by importing fully coupled ANSYS^© – models in MATLAB^©. Afterwards, modal truncation is applied, the dynamic equations of the passive electrical network are integrated into the piezoelectric model and eigenvalue problems are solved to extract the increase in modal damping ratios. The numerical results are verified by experiments.     

航空发动机风扇转子试验器动力学特性研究

以某型航空发动机风扇转子为参考,在结构相似和动力学特性相似约束条件下开展了风扇转子试验器的设计与动力学特性研究工作.利用转子动力学有限元分析技术研究了各参数对风扇转子试验器模态的影响,结合其动力学相似设计的一般流程,得到了通过调整风扇转子试验器参数实现试验器动力学特性控制的一般方法,给出了风扇转子动力学试验器的具体设计参数.     

柴油机曲轴的多柔体动力学仿真与疲劳分析

将多柔体动力学方法引入到曲轴计算中,并结合有限元法和模态叠加法建立柴油机曲轴动力学仿真模型.通过动力学仿真分析曲轴的应力和位移等动力响应,为曲轴的动态疲劳分析提供依据,为曲轴设计提供参考.     

柔性轮对结构振动对车辆动力学性能的影响

为研究轮对柔性对车辆动力学的影响,建立高速列车轮对的有限元模型,对轮对进行自由模态分析.通过模态综合法获取柔性轮对模态信息,应用多体系统动力学理论建立柔性轮对-刚性轨道接触力学模型;建立包含高速旋转柔性轮对的车辆-轨道耦合动力学模型,研究高速列车在直线和曲线通过时轮对结构振动对车辆动力学性能的影响.结果表明:轮对的结构振动对轮轨接触点位置、蠕滑率、蠕滑力和脱轨因数等均产生较明显的影响,但是对轮重减载率影响较小,因此应采用更加精确的柔性轮轨耦合模型研究轮轨相互作用、轮轨滚动接触疲劳和轮轨噪声等.