超塑胀形件壁厚分布的数值分析

在有限元数值模拟的基础上对超塑胀形圆筒件壁厚分布进行了数值分析。为使了模拟结果更接近于实验,文中考虑了应变速率敏感、模具圆半径,等因素对壁厚的影响,同时比较了正反吹成形和普通凹模成形的零件壁厚分布状况,并对壁厚分布不均匀性及其控制技术进行探讨。     

双层板渐进成形对成形件表面质量和壁厚均匀性的影响

为改善成形件的表面质量和壁厚均匀性,提出双层板渐进成形方法。以典型圆锥件为研究对象、5052铝合金板为目标板、304不锈钢板为辅助板,实验分析成形件的表面粗糙度和壁厚分布,探讨辅助板对成形件表面质量及壁厚均匀性的影响。结果表明:单层板和双层板渐进成形件表面质量差异明显,在目标板厚度≥0.6 mm的条件下,双层板渐进成形可获得表面质量更好的零件;辅助板厚度对成形件表面粗糙度也有影响,合适的辅助板厚度可改善成形件壁厚分布均匀性,增大最小厚度。     

环形件复合液压成形模拟研究

采用充液拉深筒形件再液压胀形的复合液压成形工艺成形环形件,利用DYNAFORM5.9软件对环形件复合液压成形过程进行模拟,探究不同工艺因素下预成形筒形件对环形件成形质量的影响,因素包括拉深比、最大液压、凸模圆角半径及中间退火。结果表明:随着拉深比增大,筒形件和环形件的最薄点壁厚逐渐减小;采用单拐点液压加载的筒形件充液拉深成形中最大液压愈大,得到的环形件壁厚减薄愈剧烈,最薄点壁厚愈小;随着凸模圆角半径的增加,筒形件圆角处壁厚增加,胀形后环形件最薄点壁厚减小;在复合液压成形的两工序间对筒形件进行中间退火,有利于后续加工,提高成形性能。     

超塑性自由胀形温度对Ti2AlNb板材壁厚分布的影响

为研究Ti_2AlNb合金高温超塑性自由胀形时的壁厚分布规律,对初始厚度均匀的Ti_2AlNb板材进行有限元模拟和试验研究.在胀形温度分别为910、930、950和970℃时,采用恒应变速率法对最终胀形试样的壁厚分布进行数值模拟,研究了胀形后试样的壁厚分布规律.结果表明:Ti_2AlNb板材在胀形后曲面壁厚分布不均匀,易呈现出不规则球形;胀形温度对曲面形状和壁厚具有较大的影响,变形温度对Ti_2AlNb板材超塑性自由胀形壁厚分布影响较大.在此基础上,引入温度敏感性指数n,对预测胀形壁厚的E-K模型进行修正.研究结果为Ti_2A1Nb合金在航空航天复杂薄壁结构件的超塑成形提供一定的参考依据.     

铝合金异形底盒形件预胀成形数值模拟

复杂曲面零件成形一直是诸多学者的研究热点,为了提高复杂曲面零件的成形性能以及壁厚均匀性.以铝合金异形底盒形件为研究对象,采用预胀的充液拉深技术对5A06铝合金盒形件进行数值模拟,探索预胀压力和预胀高度等参数对异形底盒形件成形的影响规律,分析成形过程中控制参数变化对零件成形性能以及壁厚分布的影响.当预胀压力为8 MPa,预胀高度为12mm,液室压力为20 MPa以及压边间隙为1.03 mm时为本模型的最合理方案.为异形底盒形件充液拉深成形的工艺参数的制定提供了参考以及对复杂零件成形的工艺分析具有一定指导意义.     

钣料正反胀形过程仿真及加压曲线优化

对圆筒形凹模约束的钣料正反胀形过程进行仿真。分析了成形过程工件形状变化及壁厚分布状况,通过仿真预测最大应变速率控制压力载荷变化,实现筒形正反胀形加压曲线的优化。     

不锈钢筒形件充液拉深的壁厚影响因素分析

将温充液拉深和拉深孔技术相结合,采用数值模拟方法对不锈钢成形过程模拟,分析了液池溢流压力与预胀初始压力等工艺条件对成型筒形件壁厚的影响规律,得到了筒形件温充液拉深的优化工艺参数。     

AZ31镁合金心形件超塑气胀成形过程数值模拟

在超塑成形条件和超塑成形机理基础上,采用有限元分析软件MSC．MARC对AZ31镁合金薄板心形件,在不同成形温度和应变速率条件下的恒应变速率超塑气胀成形过程进行了数值模拟分析．设计20组模拟参数组合对胀形件的壁厚、危险区域进行分析,得出AZ31镁合金薄板心形件具有最佳成形质量时的温度值、应变速率值以及在此条件下的压力／时间关系（P—t曲线）．同时本文对心形件的胀形过程以及成形特点进行了分析,对AZ31镁合金薄板心形件在胀形过程中．可能出现的缺陷位置做了预测．     

热剪切旋压过程中芯模对零件形貌和壁厚分布的影响

为了揭示芯模对钛合金加热剪切旋压成形的作用机制,采用数值模拟方法,对比分析了贴模和不贴模加热剪切旋压件的形貌以及壁厚分布。结果表明:成形前期,二旋压件的平直度和锥度均较好,成形中后期(65%)后,不贴模旋压件母线会塌陷。工件在变形区的壁厚减薄由纯剪切变形和拉伸变形共同作用产生,且纯剪切变形起主导作用。贴模旋压件壁部壁厚较均匀,而不贴模旋压件的波动较大,呈现中部小两端大的趋势。成形中后期的母线塌陷使得不贴模旋压件壁厚减薄不足,因此其靠近凸缘部位的壁厚远大于该区域贴模旋压件的壁厚。为了提高不贴模旋压件的直线度和锥度,不贴模旋压过程中需要对工件凸缘施加约束以防止母线的塌陷,或预先通过设定合适的旋轮轨迹进行塌陷补偿。     

轴对称超塑充模胀形件轮廓厚度分布的影响因素及其内部空洞发展

轴对称超塑充模胀形件轮廓厚度分布的影响因素及其内部空洞发展李园春，刘马宝，吴诗惇关于超塑充模胀形的有限元模拟研究极少，这与充模过程中动态边界条件难于处理和计算过程不稳定有关．且它们没有研究降低胀形件厚度分布不均匀性问题，而厚度分布不均是超塑胀形走向实...     

半球面形件拉延变形过程数值模拟

运用有限元模拟软件对不锈钢带凸缘半球面形件进行了拉延过程模拟.分析了凹模圆角半径、摩擦系数对拉延过程的影响,模拟了它们在不同工艺参数下的拉延过程,并从中分析出最佳的工艺参数.从模拟结果中得出当凹模圆角半径R=10mm左右时成形性与拉延质量最佳.     

基于DEFORM-3D的火车车轮预成形工艺参数的分析和优化

影响火车车轮与成形质量的因素很多。本文选择镦粗压下量、摩擦因子以及成形速度三个主要的因素对预成形质量进行分析。通过数值模拟得到了最优的镦粗压下量310mm ,摩擦因子 f=0.3以及成形速度v=40mm/s。通过对火车车轮预成形工艺的分析和研究,掌握了工艺规律并为预成形工艺方案的确定、预成形生产以及后续工艺的研究提供了理论依据。     

Influence of process parameters on deep drawing of AA6111 aluminum alloy at elevated temperatures

To gain a deep insight into the hot drawing process of aluminum alloy sheet, simulations of cylindrical cup drawing at elevated temperatures were carried out with experimental validation. The influence of four important process parameters, namely,punch velocity, blank holder force(BHF), friction coefficient and initial forming temperature of blank on drawing characteristics(i.e.minimum thickness and thickness deviation) was investigated with the help of design of experiments(DOE), analysis of variance(ANOVA) and analysis of mean(ANOM). Based on the results of ANOVA, it is shown that the blank holder force has the greatest influence on minimum thickness. The importance of punch velocity for thickness deviation is 44.35% followed by BHF of 24.88%,friction coefficient of 15.77% and initial forming temperature of blank of 14.995%. After determining the significance of each factor on forming characteristics, how the individual parameter affects characteristics was further analyzed by ANOM.     

超塑约束胀形贴模过程及厚度分布的FEM模拟

采用大变形刚粘塑性有限元法．成功地模拟了圆板料向轴对称锥形凹模内超塑约束胀形时，胀形件贴模过程。提出了简便摩擦处理方法．给出了保证计算过程稳定性的处理方法。     

Inconel718合金多层夹芯筒结构LBW/SPF技术研究

研究了超细晶Inconel718合金激光对接板高温塑性及多层夹芯筒结构的LBW/SPF成形技术。结果表明:垂直焊缝拉伸时最大延伸率发生在温度为950℃、应变速率为3.1×10-4s-1条件下,为400.6%,平行焊缝拉伸时最大延伸率发生在温度为965℃,应变速率为6.2×10-4s-1条件下,为164.0%。对接板在950～980℃相对胀形高度均高于1.0。通过设计直径可变的卡具以及采取点焊加固等措施,解决了多层夹芯结构的激光焊接难题。激光穿透焊参数:功率1 200 W,焊速1 200 mm/min,离焦量-1 mm,保护气体流量0.6 L/min,超塑成形参数:温度Tf=965℃,压力Pf=4.2 MPa,时间tf=130 min。采用LBW/SPF技术制造的多层夹心筒结构具有外观形状好、壁厚分布均匀、内部结构对称度高等优点。     

空洞敏感材料超塑胀形过程的压力—时间曲线优化设计

压力－时间曲线在超塑胀形工艺参数的选择和工艺过程优化设计中至关重要。利用刚粘塑性有限元技术对含有细微空洞超塑性材料的胀形过程进行了数值模拟,并采用最大等效应变速率恒定的压力控制策略对胀形过程压力－时间曲线进行了优化设计。以半球壳和圆筒形零件为例,对自由胀形和充模胀形两种成形方式给出了压力－时间曲线设计实例,并对计算结果进行了讨论。本计算模型可推广至其他超塑性成形问题。     

Numerical simulation on the process of multi-point forming for tube

To apply the multi-point forming technology to the field of tube processing,the process of multi-point forming for tube is studied.Numerical simulation for the process of multi-point forming for tube is achieved by using elastic-plastic FEM in ABAQUS.During simulation,reasonable coefficient of mass scaling and friction model of penalty function are used.The influence of several major technological parameters on the process is analyzed.When the tube diameter is 60 mm and the forming curvature radius is 1000 mm,the distortion rate of cross-section and the absolute forming error gradually decrease with the increasing of tube wall thickness;However,when the tube wall thickness is constant,the smaller the curvature radius,the larger the distortion rate of cross-section,but as to forming part,its absolute forming error becomes smaller.     

Superplasticity and superplastic bulging behavior of ZrO<Subscript>2</Subscript>/Ni nanocomposite

ZrO2/Ni nanocomposite was produced by pulse electrodeposition and its superplastic properties were investigated by the tensile and bulging tests. The as-deposited nickel matrix has a narrow grain size distribution with a mean grain size of 45 nm. A maximum elongation of 605% was observed at 723 K and a strain rate of 1.67×10-3s-1 by tensile test. Superplastic bulging tests were subsequently performed using dies with diameters of 1 mm and 5 mm respectively based on the optimal superplastic forming temperature. The effects of forming temperature and gas pressure on bulging process were experimentally investigated. The results indicated that ZrO2/Ni nanocomposite samples can be readily bulged at 723 K with H/d value (defined as dome apex height over the die diameter) larger than 0.5, indicating that the nanocomposite has good bulging ability. SEM and TEM were used to examine the microstructure of the as-deposited and bulged samples. The observations showed that significant grain coarsening occurs during superplastic bulging, and the microstructure is found to depend on the forming temperature.     

Optimizing loading path and die linetype of large length-to-diameter ratio metal stator screw lining hydroforming

In order to meet the high temperature environment requirement of deep and superdeep well exploitation, a technology of large length-to-diameter ratio metal stator screw lining meshing with rotor is presented. Based on the elastic-plasticity theory, and under the consideration of the effect of tube size, material mechanical parameters, friction coefficient and loading paths, the external pressure plastic forming mechanical model of metal stator screw lining is established, to study the optimal loading path of metal stator lining tube hydroforming process. The results show that wall thickness reduction of the external pressure tube hydroforming(THF) is about 4%, and three evaluation criteria of metal stator screw lining forming quality are presented: fillet stick mold coefficient, thickness relative error and forming quality coefficient. The smaller the three criteria are, the better the forming quality is.Each indicator has a trend of increase with the loading rate reducing, and the adjustment laws of die arc transition zone equidistance profile curve are acquired for improving tube forming quality. Hence, the research results prove the feasibility of external pressure THF used for processing high-accuracy large length-to-diameter ratio metal stator screw lining, and provide theoretical basis for designing new kind of stator structure which has better performance and longer service life.     

半球底筒形件充液拉深加载路径优化研究

针对半球底筒形零件充液拉深过程中悬空区形成的"软拉深筋",通过理论分析、数值模拟和工艺试验对与半球成形阶段直接相关的液压加载路径进行优化研究.理论推导得出液压载荷加载范围,并以其为基础进行多种加载路径条件下的数值模拟,获得不同加载路径对破裂关键点的壁厚及应变的影响规律,结合试验确定了合理的液压加载路径.结果表明:零件半球部分成形过程中破裂关键点在优化的加载路径条件下既可产生必要的有益摩擦,改善成形过程的应力应变状态,又可避免破裂关键点的过度减薄,提高了零件壁厚分布的均匀性和成形极限.