ANSYS 7.0分析实例与工程应用

有限元基础与ANSYS入门

基于ANSYS的近底床悬跨海管建模技术研究

以ANSYS软件为平台建立了近底床钢管-混凝土单层悬跨海管有限元模型.该模型综合应用PIPE59,MATRIX27和COMBIN40三个单元不仅模拟了海流对管道的作用,而且还模拟了管内流体流动引起的科氏力和离心力,另外还考虑了海管与底床的弹性接触.通过与CAM和DNV工程规范对比,验证了该模型.研究结果表明,所提出的建模方法可方便地应用于含内流的近底床悬跨海管的计算

硬实种子处理机转盘ANSYS分析

针对硬实种子处理机结构设计，分析了转盘离心应力产生的原因；利用有限元理论建立了单元节点方程和整体刚度矩阵，并利用ANSYS软件对处理机转盘结构进行了动力学建模和有限元分析，以满足转盘强度、刚度使用要求，为转盘结构改进提供了理论和技术依据．

基于ANSYS的龙门式直角坐标机器人横梁分析

对龙门式直角坐标机器人的核心部件-Y轴横梁进行了有限元计算和分析。首先对直角坐标机器人的Y轴横梁进行建模,利用ANSYS软件分析计算出横梁的变形分布情况,然后对其分布规律做简要的分析,为后续的横梁结构优化设计提供理论依据。

连续移动三维瞬态激光熔池温度场数值模拟

详细介绍了在ANSYS软件平台上，建立连续移动三维瞬态激光熔池温度场计算模型的方法，计算模型中考虑了材料表面温度对激光吸收率的影响及材料相变过程对激光熔池温度场的影响。系统分析了连续移动三维激光熔池温度场随时间的变化规律。通过该计算模型，可以掌握激光加工过程中连续移动激光熔池的加热和冷却规律。计算结果表明，当激光沿45#钢基板表面由一端向另一端沿直线扫描时，由于热传导的作用，激光熔池温度随时间增加而升高，同时连续移动熔池表面温度最高点不在激光束中心，而是稍稍偏后于激光束中心。在相同激光工艺参数下，计算熔池横截面尺寸与实验所测熔池横截面尺寸相吻合，表明所建立的连续移动熔池温度场计算模型是正确和可靠的。

Application of laser cladding technology to improve the interface of thermal barrier coatings

The present study is focused on improvement of the adhesion properties of the interface between plasma-sprayed coatings and substrates by laser cladding technology (LCT), Within the laser-clad layer there is a gradient distribution in chemical composition and mechanical properties that has been confirmed by SEM observation and microhardness measurement. The residual stress due to mismatches in thermal and mechanical properties between coatings and substrates can be markedly reduced and smoothed out. To examine the changes of microstructure and crack propagation in the coating and interface during loading, the three-point bending test has been carried out in SEM with a loading device. Analysis of the distribution of shear stress near the interface under loading has been made using the FEM code ANSYS, The experimental results show clearly that the interface adhesion can be improved with LCT pretreatment, and the capability of the interface to withstand the shear stress as well as to resist microcracking has been enhanced.

钢包砼拱形防护门有限元模态分析

防护门是阵地工程中的薄弱环节,研究其在冲击载荷作用下的动态响应具有重要意义.作者利用ANSYS有限元分析软件,建立钢包混凝土拱形防护门的仿真模型.通过对模型进行模态分析,给出防护门的前10阶固有频率及相应的振型,对防护门的自振特性有了较为精确的认识,从而为进一步分析防护门的动力响应打下基础.

柱形杜瓦瓶端盖密封结构有限元分析

建立了针对柱形真空杜瓦容器端盖密封结构的轴对称模型.基于有限元软件ANSYS的结构非线性分析模块,分析了内、外密封圈与端盖的接触响应,得到了中心盖板的挠度、密封圈的变形与接触压力.求解了考虑密封圈的变形抗力时,螺栓需提供的压紧力附加值,其分析结果对类似结构杜瓦瓶的设计有一定的参考价值.

爆炸排淤填石法中淤泥的本构模型

以爆炸排淤填石法为背景,对不同应变率阶段淤泥的本构模型进行了分析,利用ANSYS/LS-DYNA动态有限元分析程序对所选择的模型进行验证和确认.计算和分析结果表明:在形成爆炸空腔的高应变率阶段,淤泥表现为理想不可压缩流体的性质;在小药量小抵抗线条件下,甚至在淤泥自重作用下的较低应变率变形阶段,其黏性效应也可以忽略不计.

热障涂层界面形貌尺寸与残余应力的关系

利用ANSYS有限元分析软件对热障涂层中的残余应力进行了模拟分析，得出了界面形貌尺寸与残余应力之间的关系。模拟结果表明，热障涂层中的残余应力是界面形貌尺寸的函数。这些结论为提高涂层界面结合强度的热障涂层界面造形提供了理论支持，也为热障涂层界面的优化提供了指导意见。

Squeeze-film Effects in MEMS Devices with Perforated Plates for Small Amplitude Vibration

Squeeze-film effects of perforated plates for small amplitude vibration are analyzed through modified Reynolds equation (MRE). The analytical analysis reckons in most important influential factors: compressibility of the air, border effects, and the resistance caused by vertical air flow passing through perforated holes. It is found that consideration of air compressibility is necessary for high operating frequency and small ratio of the plate width to the attenuation length. The analytical results presented in this paper agree with ANSYS simulation results better than that under the air incompressibility assumption. The analytical analysis can be used to estimate the squeeze-film effects causing damping and stiffness added to the system. Since the value of Reynolds number involved in this paper is low (< 1), inertial effects are neglected.

冷弯成型局部大变形测试装置的设计与研究

冷弯成型变形复杂,事先难以预测其变形效果.根据冷弯成型的特点和变形规律设计出基于万能实验机上的局部大变形测试装置,并应用此装置对冷弯成型过程进行回弹分析,为冷弯成型理论分析和使用ANSYS/LS-DYNA对冷弯成型分析提供科学依据.

Combination Of Cfd And Csd Packages For Fluid-Structure Interaction

In this article the UDF script file in the Fluent software was rewritten as the "connecting file" for the Fluent and the ANSYS/ABAQUS in order that the joined file can be used to do aero-elastic computations. In this way the fluid field is computed by solving the Navier-Stokes equations and the structure movement is integrated by the dynamics directly. An analysis of the computed results shows that this coupled method designed for simulating aero-elastic systems is workable and can be used for the other fluid-structure interaction problems.