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...     

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事胀形时，胀形件贴模过程，提出了简例磨擦处理方法，给出了保证计算过程稳定性的处理方法。     

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。     

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。     

汽车桥壳液压胀形工艺的研究及最新进展

介绍了半滑动式液压胀形的基本思想以及小型汽车桥壳的液压胀形工艺过程,在普通液压机上试制出模拟样件。提出了钢管胀压成形工艺,先将两端缩径的管坯进行液压胀形得到轴对称的预成形管坯,再对其内部充液（水）并用模具压制成形,并试制出胀压成形桥壳样件。与液压胀形样件比较表明：胀压成形样件轮廓清楚,桥包部分过渡小圆角贴模性好,壁厚减薄量小,成形液压力低。     

钢制变直径容器无模液压胀形实验研究

提出采用无模液压胀形工艺制造钢制变直径容器;设计了,三种胀形预测壳体结构,包括球瓣式、双锥台式、双锥台加圆柱式结构,并进行了液压胀形实验;测得壳体变形过程中不同部位的应变变化,分析了不同结构壳体的变形规律,壳体焊缝对成形的发生和发展有一定影响,但双锥台式结构在变形过程中出现起皱并随胀形的继续而消失,三种壳体成形后外形略有不同,但均较为饱满,无残留起皱现象,说明采用该工艺制造变直径容器可行,且可根据具体工艺要求和制造条件选择壳体结构方案,以达到最佳实用效果。     

护环毛坯尺寸的确定

论述阻力环在护环液压胀形过程中的作用．对护环在液压胀形过程中的受力情况进行分析，提出形状参数的概念，并推导出形状参数的计算公式．采用大变形弹塑性有限元程度计算不同的H／d所对应的K值，用形状参数确定阻力环尺寸，较好地解决了在外补液液压胀形前护环毛坯尺寸确定的问题。     

粘塑性材料胀形过程的理论分析和实验研究

金属粘塑性成形过程泛指必须考虑应变速率影响的成形过程。目前,这种成形方法已成功地应用于生产难变形材料的重要宇航锻件,因此,引起了压力加工领域的研究人员的关注。鉴于金属在超塑性状态下成形是典型的粘塑性成形过程,本文试图以超塑性板材胀形过程为对象,对粘塑性成形过程的分析方法进行探索。作者在对考虑加工硬化影响的胀形过程所进行分析的基础上,提出一种超塑性板材胀形过程的分析方法,用这种方法可以模拟分析胀形压力为常数以及应变速率恒定的胀形过程。还可以对从过程的最后阶段到原始状态的全过程进行模拟。因此,本文提出的方法可以提供超塑性板材胀形过程的主要信息。引入作者提出的相对压力p~*,可使影响起塑性板材胀形过程的因素归结为p~*和m两个因素,同时使所得结果具有普遍意义。理论分析和计算结果表明,壁厚均匀性主要取决于m值,因而可以通过控制坯料内温度场以达到要求的壁厚均匀性。本文还提供了用作者提出的方法确定的线图,以便确定最佳的胀形压力或胀形压力随时间变化的关系。     

剪力墙模板胀模现象分析

针对导致剪力墙胀模的现象作了详细分析，对导致剪力墙混凝土浇筑中引起剪力墙模板胀模的原因进行了总结，并对如何防止胀模提出了施工过程中应注意的事项。     

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．     

板料冲压胀形过程有限元模拟与弯曲效应

采用厚曲壳大变形有限元方法，研究具有重要工业应用意义的方盒形件冲压胀形过程中的力学行为，并与实验结果进行比较，进而考察板材在冲压成形过程中弯曲效应的影响以及正确选择单元模式的必要性。     

薄板成形数值模拟的一种有效单元模型

将离散Ｋｉｒｃｈｈｏｆ理论（ＤＫＴ）平板弯曲单元和薄膜单元的组合模型引入到弹塑性有限变形的虚功率增率型原理中。采用Ｈｉｌ（１９７９）厚向各向异性屈服函数，模拟了韧性金属板材液压胀形过程的分叉失稳以及后继变形局部化的演化过程。与实验结果比较表明所建立的薄板成形有限元模型是有效的     

Meshfree Method Numerical Simulation of Sheet Metal Forming Process

Metal forming plays an important role in manufacturing industry and is widely applied in industries.The tradi- tional finite element method(FEM)numerical simulation is commonly used to predict metal forming process.Conventional finite element analysis of metal forming processes often breaks down due to severe mesh distortion,therefore time-consuming remeshing is necessary.Meshfree methods have been developed since 1977 and can avoid this problem.This new generation of computational methods reduces time-consuming model generation and refinement effort,and its shape function has higher order connectivity than FEM's.In this paper the velocity shape functions are developed from a reproducing kernel approximation that satisfies consistency conditions and is used to analyze metal tension rigid viscoplastic deforming and Magnesium Alloy(MB 15)sheet superplastic ten- sion forming.A meshfree method metal forming modeling program is set up,the partition of unity method is used to compute the integrations in weak form equations and penalty method is used to impose the essential boundary condition exactly.Metal forming examples,such as sheet metal superplastic tension forming and metal rigid viscoplastic tension forming,are analyzed to demon- strate the performance of mesh free method.     

Meshfree Method Numerical Simulation of Sheet Metal Forming Process

Metal forming plays an important role in manufacturing industry and is widely applied in industries. The traditional finite element method (FEM) numerical simulation is commonly used to predict metal forming process. Conventional finite element analysis of metal forming processes often breaks down due to severe mesh distortion, therefore time-consuming remeshing is necessary. Meshfree methods have been developed since 1977 and can avoid this problem. This new generation of computational methods reduces time-consuming model generation and refinement effort, and its shape function has higher order connectivity than FEM's. In this paper the velocity shape functions are developed from a reproducing kernel approximation that satisfies consistency conditions and is used to analyze metal tension rigid viscoplastic deforming and Magnesium Alloy (MB15) sheet superplastic tension forming. A meshfree method metal forming modeling program is set up, the partition of unity method is used to compute the integrations in weak form equations and penalty method is used to impose the essential boundary condition exactly. Metal forming examples, such as sheet metal superplastic tension forming and metal rigid viscoplastic tension forming, are analyzed to demonstrate the performance of meshfree method.     

控制厚度分布的变摩擦正反向超塑成形

为研究摩擦力在超塑成形中对工件厚度分布的影响规律,以正反向超塑成形侧壁厚度均匀的TC4深筒形件为背景,采用MARC有限元数值模拟分析了预成形模和终成形模的表面摩擦系数在正反向超塑成形时对成形件壁厚分布的影响.结果表明:合理地增大预成形模的表面摩擦力能显著增加预成形的局部减薄作用,对于提高零件最终壁厚分布均匀性有利.同时,终成形模摩擦力的减小,可以使板料趋于整体变形,壁厚分布趋于均匀.根据数值模拟结果进行了变摩擦正反向超塑成形试验,制得了厚度分布在1.50～1.78mm范围内的航天用TC4钛合金深筒形件,比普通正反向超塑成形件厚度分布(1.18～2.24mm)有了很大改善.     

铝合金管件液压胀形的实验及仿真分析

为深入了解薄壁管在不同加载路径下的成形情况及变形规律,采用仿真分析与实验测试相结合的方法对薄壁管件在内部液压下的塑性变形特征进行研究,并自行搭建了能够实现铝合金管件液力成形的实验系统,进行了不同工况下的胀形试验.基于ABAQUS非线性有限元软件对铝合金管件液压胀形过程进行数值模拟,通过将仿真结果与实验结果进行对比,验证了有限元模型的正确性,以此为基础,对胀形管件的失效形式、壁厚分布以及合理的加载路径进行研究,并总结了胀形管件的变形规律,为研究复杂变截面管件液压成形提供了有益的参考.     

管接头复合成形新工艺及有限元模拟

提出了一种新的管接头复合成形（缩口－轴压－胀形）工艺,总结了该工艺的优点,分析了该工艺的模具结构及材料变形,并用刚塑性有限元对该工艺的成形过程进行了模拟．     

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.