Application of experimental modal analysis technique to structural design of linear vibrating screen

A large model of the screen was mounted in the laboratory for studying its modal performance. The model is suspended with steel ropes. Modal test was carried out with artificially exciting by 500 g impacting hammer and 100 kg exciting force shaker respectively. Synthesis and correction of the modal parameters are obtained from both testing methods. Design faults of vibrating screen were determined based on the analy-sis and dynamic correction of structure approaches about the screen was put forward finally.

Experimental and FEM Modal Analysis of a Deployable-Retractable Wing

The aim of this paper is to conduct experimental modal analysis and numerical simulation to verify the structural characteristics of a deployable-retractable wing for aircraft and spacecraft. A modal impact test was conducted in order to determine the free vibration characteristics. Natural frequencies and vibration mode shapes were obtained via measurement in LMS Test. Lab. The frequency response functions were identified and computed by force and acceleration signals, and then mode shapes of this morphing wing structure were subsequently identified by PolyMAX modal parameter estimation method. FEM modal analysis was also implemented and its numerical results convincingly presented the mode shape and natural frequency characteristics were in good agreement with those obtained from experimental modal analysis. Experimental study in this paper focuses on the transverse response of morphing wing as its moveable part is deploying or retreating. Vibration response to different rotation speeds have been collected, managed and analyzed through the use of comparison methodology with each other. Evident phenomena have been discovered including the resonance on which most analysis is focused because of its potential use to generate large amplitude vibration of specific frequency or to avoid such resonant frequencies from a wide spectrum of response. Manufactured deployable-retractable wings are studied in stage of experimental modal analysis, in which some nonlinear vibration resulted should be particularly noted because such wing structure displays a low resonant frequency which is always optimal to be avoided for structural safety and stability.

Design and Experiment of Triangular Prism Mast with Tape-Spring Hyperelastic Hinges

Because of the limited space of the launch rockets, deployable mechanisms are always used to solve the phenomenon. One dimensional deployable mast can deploy and support antenna, solar sail and space optical camera. Tape-spring hyperelastic hinges can be folded and extended into a rod like configuration. It utilizes the strain energy to realize self-deploying and drive the other structures. One kind of triangular prism mast with tape-spring hyperelastic hinges is proposed and developed. Stretching and compression stiffness theoretical model are established with considering the tape-spring hyperelastic hinges based on static theory. The finite element model of ten-module triangular prism mast is set up by ABAQUS with the tape-spring hyperelastic hinge and parameter study is performed to investigate the influence of thickness, section angle and radius. Two-module TPM is processed and tested the compression stiffness by the laser displacement sensor, deploying repeat accuracy by the high speed camera, modal shape and fundamental frequency at cantilever position by LMS multi-channel vibration test and analysis system, which are used to verify precision of the theoretical and finite element models of ten-module triangular prism mast with the tape-spring hyperelastic hinges. This research proposes an innovative one dimensional triangular prism with tape-spring hyperelastic hinge which has great application value to the space deployable mechanisms.

Calculation and Experiment for Dynamic Response of Bridge in Deep Water Under Seismic Excitation

The fluid-structure interaction under seismic excitation is very complicated, and thus the damage identification of the bridge in deep water is the key technique to ensure the safe service. Based on nonlinear Morison equation considering the added mass effect and the fluid-structure interaction effect, the effect of hydrodynamic pressure on the structure is analyzed. A series of underwater shaking table tests are conducted in the air and in water. The dynamic characteristics affected by hydrodynamic pressure are discussed and the distribution of hydrodynamic pressure is also analyzed. In addition, the damage of structure is distinguished through the natural frequency and the difference of modal curvature, and is then compared with the test results. The numerical simulation and test of this study indicate that the effect of hydrodynamic pressure on the structure should not be neglected. It is also found that the presence of the damage, the location of the damage and the degree of the severity can be judged through the variation of structure frequency and the difference of modal curvature.

Modal Parameters Identification of A Real Offshore Platform From the Response Excited by Natural Ice Loading

This paper investigates the possibility of utilizing response from natural ice loading for modal parameter identification of real offshore platforms.The test platform is the JZ20-2 MUQ jacket platform located in the Liaodong Bay,China.A field experiment is carried out in winter season,as the platform is excited by floating ices.The feasibility is demonstrated by the acceleration response of two different segments.By the SSI-data method,the modal frequencies and damping ratios of four structural modes can be successfully identified from both segments.The estimated information from both segments is almost identical,which demonstrates that the modal identification is trustworthy.Furthermore,by taking the Jacket platform as a benchmark,the numerical performance of five popular time-domain EMA methods is systematically compared from different viewpoints.The comparisons are categorized as:(1)stochastic methods versus deterministic methods;(2)high-order methods versus low-order methods;(3)data-driven versus covariance-driven stochastic subspace identification methods.

EXPERIMENT RESEARCH ON DYNAMIC LOAD IDENTIFICATION TECHNOLOGY BASED ON GENERALIZED ORTHOGONAL POLYNOMIAL THEORY (GOPT)

A dynamic load identification model of structural system based on the gener-alized orthogonal polynomial theory is provided, and the least Square discrete algorithm foridentifying the dynamic load is supplied. The main key is that the convolution relationsbetween the input and output of the system in time domain are transformed into linear oP-erators in generalized orthogonal domain. The new theory is fully tested and verified bythe dynamic analysis l 'modal test and dynamic load identification teSt of a simulation speci-men- It is shown that the method has some advantages, such as the simple dynamic cali-bration test, the high identification accuracy, especially for the transient load with shortsampling. These are very useful in engineering applications.

Numerical-experimental method for elastic parameters identification of a composite panel

A hybrid numerical-experimental approach to identify elastic modulus of a textile composite panel using vibration test data is proposed and investi- gated. Homogenization method is adopted to predict the initial values of elastic parameters of the composite, and parameter identification is transformed to an optimization problem in which the objective function is the minimization of the discrepancies between the experimental and numerical modal data. Case study is conducted employing a woven fabric reinforced composite panel. Three parameters （Ell, E22, G12） with higher sensitivities are selected to be identified. It is shown that the elastic parameters can be accurately identified from experimental modal data.

Numerical and Experimental Research on the Influence of the Centrifugal Pumps Rotor Damage on Their Natural Frequency Response

The paper presents process of creating a centrifugal pump rotor model in CAD environment. Modeling of a virtual object was divided into two stages, modeling of the efficient pump and the simulated failure of one of the impeller＇s blades. Comparison of the results of the resonance frequency obtained from the model analysis, with those obtained from measurements on the actual object was shown. Measurements and simulations were conducted on the pump before and after the simulated damaged of the rotor. In order to verify the model the rotor of pump was weighted and compared with the masses of the respective components obtained from the virtual object. In the second stage genuine rotor was subjected to the experimental modal analysis.

MODAL ANALYSIS OF A CHASSIS FRAME OF A HEAVY LECTRA HAUL

The chassis frame of a heavy lectra haul is analysed by both modal experiment method and finite element method (FEM ) . The first ten order modal parameters of the chassis frame have been obtained satisfactorily. These parameters have important reference value in designing the chassis frame properly and provide a necessary basis for the fault diagnostics of the truck.

某皮卡车白车身模态分析

白车身模态研究是整车研发设计中极为重要的一项,是车辆噪声与振动研究中的关键环节。为了确保车身在设计要求下的模态性能,文章基于有限元和试验模态分析理论,以计算机辅助设计(CAD)模型为基础,构建了有限元模型。在此基础上,分析前十阶模态,并进行了白车身模态试验验证。将试验测得的试验模态与计算模态进行对比,分析其各阶模态频率和振型,并对其提出了改进建议。文章运用仿真手段对白车身进行分析,可以缩短开发周期,降低成本,对白车的设计开发具有指导意义。

内外流作用下深海悬垂取水管动力响应的模型试验

研究内外流对大直径、内流流速高的深海悬垂取水管道动态响应的影响,对实际工程中的取水管道应用提供参考。基于小尺度模型试验,分析内外流作用下管道的动力响应特性,以及顶部连接方式和底部配重块对其响应的影响规律。结果表明:涡激振动响应的主导模态和主导频率主要取决于外流流速,内流流速的变化对主振频率无明显影响,但会增加管道向高阶模态转换的趋势。外流增加会导致P1管道的振动响应从单一模态转向多模态参与,且涡流脱落与固有频率之间的“锁定”和模态转换现象更明显。当存在外流时,管道的位移振幅大小主要受到外流流速影响。外流参与会增加运动的周期性,但随着外部流速增加,取水管道因涡激运动从单一频率的振动转变为复杂的多频率振动,导致运动周期性逐渐减弱。顶部固定的管道底部位移振幅均方根值更大。低外流流速时,管道配重显著影响了管道的振幅,特别是当配重占据管道自重的50%及以上时,振幅的变化与无集中质量时存在明显差异。研究成果在优化内外流条件下悬垂式取水管道的理论模型方面具有显著意义,可为实际深海浮式取水管道的设计与工程实施提供一定参考。

门式精密数控机床结构模态分析与优化研究

以一种门式精密数控机床的主体结构为研究对象。首先,采用有限元分析法对该机床结构的前四阶模态固有频率和振型进行计算模态分析,得到其前四阶模态固有频率分别为186.04、241.18、321.51、382.51 Hz,并分析了其模态振型变形趋势;然后,通过模态分析试验系统对机床进行试验模态分析,得到机床的前四阶模态固有频率和振型,以及第一阶模态固有频率相对较低,振型为机床前后俯仰运动等结果,与计算模态分析结果一致;最后,计算模态分析与试验模态分析的结果对比表明,横梁与滑枕的配重过大、立柱和主轴箱的结构抗弯能力不足是机床结构的薄弱环节,并针对薄弱环节提出了相应的优化方案,为门式精密数控机床的优化设计及动态特性提升提供了理论参考依据。

飞机典型结构模态测试优化激励方法的试验研究

针对飞机典型结构,开展模态测试试验。飞机典型结构模型相对较小,试验过程中不同位置激振力产生的响应存在相互耦合,导致很难获取结构某些振型的纯模态。为避免上述情况发生,试验过程中采用3种不同的激励方法。通过改变激励点位置、激励方向和激振器与结构之间的连接方式,获取不同激励方法下的结构模态测试结果。比较测试结果可以得出,选择不同的激励方法,能够获取不同的纯模态振型,此结论对于进行试验方案的设计和完善具有一定的参考和指导意义。

卧式泵模态仿真分析与试验测试研究

固有频率是评价离心泵稳定性的重要因素之一,文章研究了单级端吸卧式泵模态分析和试验测试方法,建立了卧式泵的有限元模型,考虑与测试状态相同的边界条件进行仿真分析,同时通过锤击法进行试验测试,得到了卧式泵的固有频率和振型。结果表明:水平方向固有频率仿真与试验误差最大为5.1%,竖直方向固有频率仿真与试验误差最大为16.9%,卧式泵模态振型仿真与试验结果一致,仿真分析方法可用于指导离心泵模态性能设计优化。

基于试验模态分析的圆锯片降低振动研究

金属圆锯片属于面积较大的薄板类零件,其在锯切加工过程中普遍存在着严重的振动问题。为提高圆锯片的锯切性能,降低其工作时的振动,在对圆锯片振动分析及其试验模态理论研究和试验分析的基础上,对比两种不同基体结构圆锯片的固有特性,分析其固有频率及振型的变化,推断基体上开减振孔对锯片整体性能,尤其是对圆锯片振动特性的的影响。试验证明,开减振孔锯片可有效降低圆锯片的振动,为圆锯片降低振动的结构设计及基体冲孔的优化设计提供理论指导。

基于LMSTest.Lab的小型农业作业机振动测试与分析

为分析小型农业作业机的模态振型及可靠性,应用LMS Test.Lab测试系统,对JSX5D小型农业作业机进行模态试验与分析,得到其固有频率、阻尼比以及相应的振型等模态参数。试验结果表明该机基频较高,而阻尼比较低,分别为196.72 Hz和不大于4.41%,说明该机具有很好的刚度。但扶手部分阻尼比仅为0.57%,为降低工作时的振动强度,应加入合适的阻尼材料;发动机和齿轮箱机械接口的振动方向与该类接口的法线方向一致,说明该类接口的连接刚度较弱,应加强接口的连接刚度,保证作业机的动力输出。

120kg点焊机器人试验模态分析

用试验模态分析方法对A型和B型两台点焊机器人的动态特性进行了分析研究，得出机器人在典型位姿下的低阶固有频率。通过对机器人在不同位姿下的模态特性分析，指出机器人整体结构中相对薄弱的环节，并指出，机器人各构件的质量和刚度分布应相互协调和匹配，其合理与否对机器人的动态性能有较大影响。最后提出了机器人结构设计的改进方案。

某商用车驾驶室白车身模态分析

以某商用车驾驶室白车身为原型,利用模态分析方法对其动力学特征参数进行分析.在理论(正问题)和实验(反问题)两个互补的模态分析过程中,利用有限元模型进行理论模态分析,为实验模态分析的实施打下良好基础.分别采用最小二乘复指数法(LSCE)和最小二乘复频域法(LSCF)进行实验模态分析,得到各阶模态振型并对理论分析的结果进行修正.经过两种结果的比较和分析,最终得出准确的模态分析结果并对白车身原型提出改进意见.生产厂商依据改进意见进行工艺改进,通过用户实际使用证实了改进方案的有效性和正确性.

高速动车组车下设备对车体振动传递与模态频率的影响机理研究

提出包含车下设备的高速动车组整备状态车体模态频率数值计算方法,并通过有限元分析及模态试验,验证该方法的准确性。理论研究车下设备对车体振动传递特性的影响,定义车体的名义垂向一阶弯曲模态频率,并结合数值计算、振动传递分析与模态试验分析,分析车下设备悬挂参数对车体模态频率的影响机理。研究表明,采用弹性吊挂的车下设备将与车体形成耦合振动系统,且耦合振动系统在原车体垂向一阶弯曲模态频率附近产生一个新的低频振动分量和一个新的高频振动分量;低频振动振型为车下设备垂向振动与车体垂向一阶弯曲振动同相,高频振动振型为二者反相振动;随着车下设备悬挂刚度的变化,车体的名义垂向一阶弯曲频率将会发生"频率跳变"现象。

镁合金AZ91D的阻尼减振性能

为了解镁合金减振效果与频率、振幅等因素的关系,对AZ91D镁合金的实际减振行为有明确的把握,对镁合金AZ91D、变形镁合金AZ31、铝合金以及钢4种材料进行室温下的阻尼一频率测量,发现在相同振幅和频率下,镁合金AZ91D具有比铝合金、钢和变形镁合金高出3～5倍的阻尼性能,并在6 Hz左右出现阻尼峰。通过对镁合金与铝合金发动机箱盖在冲击脉冲载荷作用下的振动进行三阶模态分析,发现镁合金试件的阻尼比,除第三阶比铝合金试件稍微偏小外,其余各阶均高于铝合金试件。镁合金试样的第一阶模态阻尼比比铝合金试件高出17．6％,而第二阶模态阻尼比高出41.3％,另外镁合金试样的第一阶模态质量比铝合金试样高出45．O％,而第二阶模态质量高出15．3％,表明镁合金发动机箱盖在使用中镁合金的稳定性、抗冲击性能以及对冲击载荷的减幅等方面都具有良好的动力学表现。