爆炸处理消除大型柱壳结构环焊缝残余应力实验研究

为探讨大型耐压柱壳结构对接环焊缝焊接残余应力消除方法,根据耐压柱壳结构环焊缝焊接工艺,设计并制作了大型耐压柱壳结构对接环焊缝模拟焊接模型,并采用沿焊缝条状布药,分别进行了单、双面布药爆炸处理消除大型耐压柱壳结构对接环焊缝焊接残余应力模型实验。结果表明:大型耐压柱壳结构对接环焊缝存在较大的焊接残余应力;单、双面爆炸处理均能有效调整、消除焊接残余应力,残余应力分布明显均匀化;焊后残余应力越大,爆炸处理效果越明显,当焊接残余应力大于0.5s时,单面爆炸处理后残余应力m下降幅度在40%以上,双面爆炸处理后残余应力m下降幅度在60%以上;采用沿焊缝条状布药,爆炸处理能有效消除沿焊缝的纵向残余应力;双面爆炸处理效果优于单面爆炸处理效果。     

爆炸处理消除16MnJ超厚钢板焊接残余应力

研究了炸药性能、药条尺寸、布药方式以及引爆方式等对消除７０ｍｍ厚１６ＭｎＪ对接接头焊接残余应力效果的影响。在此基础上提出优化的工艺方案，为将爆炸消除焊接残余应力技术应用到大型或特大型焊接结构上提供工艺参考。     

P91钢中厚壁管焊接残余应力分析

针对管道试件规格不同所要求的焊接工艺不一致问题,讨论P91钢中厚壁管对接接头所要求的双人对称焊形式下的焊接残余应力分布规律．基于ANSYS分析软件,以双移动高斯热源结合单元生死技术,利用顺序耦合方法得到P91钢中厚壁管焊接残余应力．讨论热处理工艺对于P91钢中厚壁管焊接残余应力的影响．结果表明,由于焊接工艺在环向位置上的结构反对称性使得焊接残余应力在环向上呈反对称分布;即便经过较高温度的预热处理,没有焊后热处理时最大等效应力仍超过屈服极限;进行焊后整体热处理的P91钢中厚壁管焊接残余应力得到了有效的改善,平均应力数值下降了60%~70%．     

考虑塑性和刚度不匹配的焊接残余应力估算

现有残余应力计算方法未能考虑材料塑性变形和焊接接头刚度不匹配的影响,使得焊接残余应力计算结果和实际残余应力存在较大偏差.在2219-T87铝合金钨极氩弧焊焊接头残余应力测试基础上,提出一种基于非线性有限元和材料弹性模量分区的残余应力—释放应变曲线的残余应力计算方法,研究了材料塑性变形和接头刚度不匹配对焊接残余应力计算的影响.结果表明,焊接接头中非均质材料塑性不匹配可以引起对于残余应力计算的较大误差;材料塑性变形对残余应力的影响大于接头刚度不匹配对残余应力的影响.所提出方法修正了传统方法在焊接接头的残余应力计算中由于未考虑接头非均质材料塑性不匹配而引起的误差.     

冲击法改善T91钢焊接残余应力的研究分析

基于焊后热处理可以降低T91钢焊接残余应力,但无法改变其应力状态的分布问题,本文模拟分析了冲击法对于改善焊接残余应力的影响情况。通过ANSYS软件平台,导入经焊后热处理后的残余应力为初始状态,分析了不同的冲击力度、冲击间隔、双点冲击情况对于T91钢中小径薄壁管焊接残余应力的影响。模拟结果表明:冲击处理可以在处理表面一定深度范围内引入一定区域占比的压应力,并且压应力区域随载荷的增加而加大;由于不经焊后热处理的最高应力集中在焊缝内表面区域,因此只通过冲击处理的机械方式不能得到良好的改善焊后残余应力效果。通过焊后热处理结合焊缝区外表面冲击处理,可以在降低焊接残余应力的同时引入一定比例的压应力,从而得到较好的应力状态。单点环向冲击间隔7.2°的0.2mm冲击位移载荷下,具有75%左右的外表面环向压应力产生,可作为改善T91钢中小径薄壁管焊接残余应力的方案。     

304L/Q235B大面积金属板爆炸焊接物质点法模拟分析

大面积金属板材304L/Q235B的爆炸焊接过程涉及炸药爆轰、金属板材的高速碰撞和塑性变形等。采用有限元法计算模拟这个问题时,网格单元会发生扭曲畸变现象,导致计算精度下降,甚至出现单元负体积而使计算终止,并且炸药爆轰形成气体产物飞散过程也很难模拟。为了能模拟大面积金属板材的爆炸焊接整个过程并获得合理的技术工艺参数,采用物质点法进行三维数值模拟分析。物质点法作为一种无网格法,在模拟冲击动力学问题中主要采用显式积分算法。通过将拉格朗日质点单元与固定的欧拉背景网格相结合,可以实现爆炸焊接的复板与基板的高速碰撞、炸药滑移爆轰、金属板面的塑性变形过程的数值模拟,并给出爆炸复合板材的形变、有效塑性应变和复板与基板的碰撞速度的计算结果。采用物质点法模拟的复合板材变形与爆炸焊接实验结果基本一致。计算复板与基板的碰撞速度这个重要的物理参数时,物质点法与Richter理论公式的相对误差不超过13%。数值计算和实验结果表明,物质点法在数值精度和计算效率方面具有优势,物质点法是研究金属焊接爆炸问题的一种有效数值方法。     

爆炸法消除焊接残余应力

随着工业的发展,焊接技术在工业生产中的地位显得越来越重要。但是,由于焊接是局部加热,温度梯度很大,使焊件内部产生了很大的焊接残余应力。因为焊接残余应力的存在,致使焊件的静强度、刚度、稳定性及抗疲劳、抗脆性破坏、抗应力腐蚀等性能均低于同类材料的非焊接件。这就造成了它的使用寿命大大降低。在许多结构的破坏事故中,不少是由于焊接残余应力的存在所造成。为此研究消除焊接残余应力,对生产和科学实验都具有很大的意义。     

滑移爆轰问题无网格MPM法数值模拟

利用MPM(material point method)计算方法,以爆炸焊接作为实例,对炸药滑移爆轰过程和金属飞板与基板之间的碰撞变形进行了数值模拟.并将无网格MPM法的数值计算结果与近似解析公式的计算结果进行了比较,二者基本吻合,有力地证明了无网格MPM法在求解爆炸冲击问题中的有效性和健壮性.     

5级人防口部粘钢封堵接头抗爆实验研究

通过粘钢实现一典型汽车库人防口部封堵的设计方案,并对原设计方案进行相似设计后,对粘钢接头结构实验模型在核爆炸压力模拟器中进行模爆实验,得到沿竖向支座钢板的位移和应变时程曲线,并和有限元数值解进行了对比,其结果均较吻合,通过沿竖向支座钢板的应变分布规律得到钢板-混凝土界面之间的粘结应力;检验了在5级人防爆炸冲击波作用下,混凝土墙与钢板间粘结面承载力的可靠性;分析了5级人防爆炸荷载作用下支座钢板沿竖向应力的分布规律,为确定混凝土墙与钢板之间粘结应力的计算方法提供了参考。     

滑移爆轰密封的初步数值模拟

利用有限元方法,通过数值模拟得到爆炸密封铝、铜封管密封所需炸药药量;在此基础上,利用光滑粒子法对爆炸密封模型进行优化,分析炸药、保护外壳等形状等对封管密封性能的影响。基于对计算结果的分析,确定实验模型。实验回收结果和数值模拟结果符合较好,表明数值模拟结果对实验设计有指导作用。     

Comprehensive numerical analysis of a three-pass bead-in-slot weld and its critical validation using neutron and synchrotron diffraction residual stress measurements

The current paper presents a finite element simulation of the residual stress field associated with a three pass slot weld in an AISI 316LN austenitic stainless steel plate. The simulation is split into uncoupled thermal and mechanical analyses which enable a computationally less expensive solution. A dedicated welding heat source modelling tool is employed to calibrate the ellipsoidal Gaussian volumetric heat source by making use of extensive thermocouple measurements and metallographic analyses made during and after welding. The mechanical analysis employs the Lemaitre–Chaboche mixed hardening model. This captures the cyclic mechanical response which a material undergoes during the thermo-mechanical cycles imposed by the welding process. A close examination of the material behaviour at various locations in the sample during the welding process, clearly demonstrates the importance of defining the correct hardening and high temperature softening behaviour. The simulation is validated by two independent diffraction techniques. The well-established neutron diffraction technique and a very novel spiral slit X-ray synchrotron technique were used to measure the residual stress–strain field associated with the three-pass weld. The comparison between the model and the experiment reveals close agreement with no adjustable parameters and clearly validates the used modelling procedure.     

A study on the relief of residual stresses in weldments with explosive treatment

Explosive treatment is an efficient and economical technique in reducing welding residual stresses. The whole course of residual stress reduction is investigated both numerically and experimentally, in order to discover the mechanism of the explosive treatment and optimizing the technique. It is proved that the reflection and superposition of stress waves aroused by explosive loading lead to redistribution and remarkable reduction of welding residual stresses. Moreover, the optimum working conditions, such as detonator shape, width, location, explosive loading and velocities, are also discussed. The numerical results and the experimental ones are in reasonable agreement with each other.     

CTOD试验焊缝表面开缺口试样裂纹前沿平直度研究

对于裂纹尖端张开位移(CTOD)试验,焊缝试样中预制疲劳裂纹前沿平直度直接影响了试样制备的合格率,是试验的关键难题之一．试验中常对试样进行预处理以提高裂纹前沿平直度,但由此也使试验结果与实际情况产生一定差异．本文深入研究规范BS7448: Part2中对焊缝试样取样方向的规定,对表面开缺口试样裂纹尖端焊接残余应力进行分析,运用大型有限元软件ANSYS模拟90mm厚钢板焊接过程,求解了横向残余应力沿板厚方向及焊缝方向的分布规律,研究出横向残余应力分布是影响焊缝试样预制裂纹前沿平直度的主要原因,并通过试验进行验证．试验结果表明,表面开缺口试样可不经过局部韧带压缩等预处理而得到合格的裂纹前沿平直度,试验不改变原焊缝残余应力,可测得更加接近焊缝实际情况的CTOD韧度值,给CTOD试验中合理选取焊缝试样取样方向提供了新思路．     

宽幅钢箱梁环焊缝焊接顺序优化研究

基于热弹塑性有限元法,采用ANSYS软件建立了网格疏密过渡的单箱五室钢箱梁壳单元模型;结合高效的分段移动热源,实现了对大型复杂长焊缝结构焊接全过程的数值模拟,并定性对比了宽幅钢箱梁在不同的环焊缝焊接顺序下顶板和底板的变形情况.分析结果表明:腹板焊缝的焊接顺序对竖向最大变形值(绝对值)的影响不大,其值主要取决于顶板和底板...     

爆炸焊接复合界面波与温度场物质点法分析

爆炸焊接是一门双金属复合工程技术,在炸药爆轰载荷驱动下,飞板高速冲击基板时,两金属板复合界面处在高温高压作用下材料发生塑性流动并形成周期性波状界面,波状界面的形成与复合界面处的材料熔化和变形直接相关。本文应用物质点法对爆炸焊接界面波的形成和界面温度场进行数值模拟,同时开展双金属爆炸焊接实验,并结合物质点法的三维数值模拟对爆炸焊接界面波的形态和界面材料高温软化进行分析。     

Numerical simulation of friction stir butt welding process for AA5083-H18 sheets

Thermo-mechanical simulation of the friction stir butt welding (FSBW) process was performed for AA5083-H18 sheets, utilizing a commercial finite volume method (FVM) code, STAR-CCM+, which is based on the Eulerian formulation. Distributions of temperature and strain rate histories were calculated under the steady state condition and simulated temperature distributions (profiles and peak values) were compared with experiments. It was found that including proper thermal boundary condition for the backing plate (anvil) is critical for accurate simulation results. Based on the simulation, thermal and deformation histories of material elements were also calculated, useful to predict material characteristics of the weld such as hardness or grain size, and possibly for the susceptibility of weld to abnormal grain growth (AGG) after post-weld heat treatment.     

Measurement of residual stress in the weld overlay piping components

In general industry, especially in the nuclear industry, welding overlay repair is an important repair method mainly used to rebuild piping systems suffering from intergranular stress-corrosion cracking (IGSCC).The pipe surface is mechanically ground to obtain a smooth surface after the welding overlay repair. A better understanding of the effect of repair and grinding processes on the residual stresses at the surface of weld overlay is required. To obtain this understanding, it is necessary to measure directly the distribution of residual stresses on the specimen. It is expected that compressive residual stress should be induced at the inner wall surface of the pipe for prevention of IGSCC.The performance evaluation of welding overlay repair relies on whether or not the level and characteristic of the residual stress can be measured accurately. In this study, the hole-drilling strain-gage method, using the incremental drilling technique, was adopted to estimate the residual stresses on the inner and outer walls of the weld overlay pipe. The experimental results indicate that the residual stress at the pipe inner surface is compressive while that of the outer surface is tensile. Also, it is found that the depth affected by grinding is about 1.016 mm.