圆柱壳体振动特性研究与有限元计算验证

采用解析理论和有限元方法研究计算了圆柱壳体的固有频率与固有振型,发现环向封闭的圆柱壳具有同一节点形式的两种固有振型,对应两种固有振型的固有频率值相同。     

稀土永磁减振器特性的数值模拟分析

简要介绍了目前稀土永磁减振器的研究现状和单质量稀土永磁减振器的结构与工作原理,运用大型有限元软件ANSYS对稀土永磁减振器的工作过程进行数值模拟,分析其在工作过程中的磁通密度、磁力线分布、力学特性以及它们之间的相互关系。研究表明:稀土永磁减振器具有较好的非线性减振效果;ANSYS在模拟稀土永磁减振器工作过程时,能形象直观的反映其在工作过程中的各种特性参数。     

Noise and vibration measurements in a Viking military vehicle

Noise and whole-body vibration measurements were made in a Viking military vehicle to determine the variation that should be expected during repeat measures, the effect of speed (up to 60 km/h in 5 km/h increments), and during travel over different types of terrain (comprising concrete road, gravel track and rough cross-country). Measurements were made at various crew positions (including the driver and commander) in both the front and the rear cabs in the vehicles. Three translational axes of vibration were measured in each seat. Two speeds were investigated over road (35 km/h and 55–60 km/h) and gravel (20 km/h and 35 km/h) surfaces. The effect of varying speed of the vehicle on the measured noise and vibration magnitudes was also investigated. The highest sound pressure level (L_Aeq) of 104 dB(A) was measured at the commander’s standing position during travel over concrete road at 55 km/h. Higher noise levels occurred for a standing commander compared with when sitting on the seat. A maximum single axis frequency-weighted vibration magnitude of 1.0 m/s² r.m.s. was measured on the driver’s seat during travel over track at 35 km/h. Higher vibration magnitudes occurred during travel over track compared with travel over road. Both noise and vibration exposure of crew within the Viking vehicle increased with increasing speed of the vehicle.     

Finite-time tracking control and vibration suppression based on the concept of virtual control force for flexible two-link space robot

The dynamic modeling, finite-time trajectory tracking control and vibration suppression of a flexible two-link space robot are studied. Firstly, the dynamic model of the system is established by combining Lagrange method with assumed mode method. In order to ensure that the base attitude and the joints of space robot can reach the desired positions within a limited time, a non-singular fast terminal sliding mode (NFTSM) controller is designed, which realizes the finite-time convergence of the trajectory tracking errors. Subsequently, for the sake of suppressing the vibrations of flexible links, a hybrid tra-jectory based on the concept of the virtual control force is developed, which can reflect the flexible modes and the trajectory tracking errors simultaneously. By modifying the original control scheme, a NFTSM hybrid controller is proposed. The hybrid control scheme can not only realized attitude stabili-zation and trajectory tracking of joints in finite time, but also provide a new method of vibration sup-pression. The simulation results verify the effectiveness of the designed hybrid control strategy.     

加肋圆柱壳结构的FE-IE算法网格尺度划分原则

为了研究结构有限元耦合流体无限元算法的网格尺度划分原则,提出有限元-无限元算法中结构湿表面的网格尺度划分原则。数值计算结果表明,对加肋圆柱壳而言,在保证一个肋骨间距至少有2个有限元单元的前提下,将结构主振型弯曲波波长作为有限元-无限元算法中结构湿表面网格尺度划分的参考标准是可行的,即保证一个主振型分量波长内至少有6个有限元单元。提出以结构主振型分量的弯曲波波长(而不是最短的结构波长)作为有限元-无限元算法中网格尺度划分的参考标准,所得结论对于有限元-无限元算法中结构湿表面的网格划分以及控制内域流体有限元数量均具有十分重要的参考意义。     

Study on dynamic response of multi-degree-of-freedom explosion vessel system under impact load

In order to study the dynamic response and calculate the axial dynamic coefficient of the monolayer cylindrical explosion vessel, the wall of vessel is simplified as a multi-degree-of-freedom (MDoF) undamped elastic foundation beam. Decoupling the coupled motion equation and using Duhamel's integrals, the solutions in generalized coordinates of the equations under exponentially decaying loads, square wave loads and triangular wave loads are calculated. These solutions are consistent in form with the solutions of single-degree-of-freedom (SDoF) undamped forced vibration simplified model. Based on the model, equivalent MDoF design method (also called MDoF dynamic coefficient method) of cylindrical explosion vessel is proposed. The traditional method can only predict the dynamic coefficient of torus portion around the explosion center, but this method can predict that of the vessel wall at any axial n dividing point position. It is verified that the prediction accuracy of this model is greatly improved compared with the SDoF model by comparing the results of this model with SDoF model and numerical simulation in different working conditions. However, the prediction accuracy decreases as the scaled distance decreases and approaches the end of the vessel, which is related to the accuracy of the empirical formula of the implosion load, the simplification of the explosion load direction, the boundary conditions, and the loading time difference.     

梁的横向振动频率方程的一般表达式

本文推导出梁的横向振动频率方程的一般表达式。十七种在各种边界条件下的梁的横向振动频率方程均是它的特殊情况。     

柴油机检测与诊断系统的研制

本文以作者参加研制的柴油机检测与诊断系统为对象,在分析柴油机故障机理及特点的基础上,详细论述了检测与诊断系统的组织与结构,检测参数的选择与取舍,信号数据的采集与处理和系统故障诊断等方面的问题。文章着重论述了转速的测量及其在柴油机检测与诊断系统中的应用,柴油机高压油路的检测与诊断,ＤＳＰ系统软件的开发及其在柴油机表面振动诊断中的应用。     

Influence of active constrained layer damping on the coupled vibration response of functionally graded magneto-electro-elastic plates with skewed edges

This article makes the first attempt in assessing the influence of active constrained layer damping (ACLD) treatment towards precise control of frequency responses of functionally graded skew-magneto-electro-elastic (FGSMEE) plates by employing finite element methods. The materials are functionally graded across the thickness of the plate in terms of modest power-law distributions. The principal equations of motion of FGSMEE are derived via Hamilton’s principle and solved using condensation technique. The effect of ACLD patches are modelled by following the complex modulus approach (CMA). Additionally, distinctive emphasis is laid to evaluate the influence of geometrical skewness on the attenuation capabilities of the plate. The accuracy of the current analysis is corroborated with comparison of previous researches of similar kind. Additionally, a complete parametric study is directed to understand the combined impacts of various factors like coupling fields, patch location, fiber orientation of piezoelectric patch in association with skew angle and power-law index.