汽车前梁多道次内高压成形

基于动力显示有限元软件eta/DYNAFORM,以汽车前梁为例,开展了回转拉伸弯曲和模具压弯多道次内高压成形工艺过程数值模拟。结合各种成形工艺下汽车前梁内高压成形极限图,分析其成形质量。在此基础上进行管坯回转拉伸预弯曲和内高压成形试验,给出了典型截面的壁厚分布,并与模拟结果进行了比较。研究结果表明,模拟结果与实验结果相一致。预弯曲成形后,管坯壁厚分布对内高压成形结果中壁厚分布具有一定的影响。多道次内高压成形模拟能够提高内高压成形模拟精度。管坯模具压弯的壁厚分布较回转拉伸弯曲的壁厚分布好,利于汽车前梁内高压成形性能提高。     

汽车转向节成形过程数值模拟及模具设计

在对汽车转向节成形工艺分析的基础上,制定其成形工艺路线.利用有限元分析软件Msc.SuperForm模拟了该零件的压弯成形过程.根据模拟结果,分析比较了几种成形工艺的特点,并综合压弯成形后坯料预锻成形过程的模拟,最终确定了合理的成形方案,进行了压弯、预锻及终锻的模具设计.     

G115钢热压弯成形工艺试验研究

分析了电站典型管件热压弯头、热压三通及热压封头的变形特点,其中热压三通的变形率最大,可达38％.并对G115钢热压弯成形进行了仿真模拟,结果可涵盖变形最为严重的情况.进而设计了热压弯工艺试验,研究了不同成形温度、道次和冷却方式对成形的影响,并对试样进行了外观检验、渗透检验、硬度检验和微观组织观察.通过热压弯工艺试验研究...     

组合摩擦对厚壁管件压弯成形的影响

在阐述了厚壁结构管件填充介质压弯成形工艺的基础上,建立了管件压弯成形过程有限元模型,研究了内外摩擦因数对管材弯曲成形过程中应力应变、成形载荷以及管壁厚度变化的影响。数值模拟结果显示:摩擦是影响管件成形的重要工艺参数。在管件的压弯成形过程中,摩擦力影响变形区的应力分布和金属流动,当选择适当的摩擦因数组合时,管件受到的应力与成形力均较小,壁厚均匀性较好。     

汽车排气管件内高压成形数值模拟及试验

利用有限元分析软件,对汽车排气管件的压弯和内高压成形过程进行了数值模拟,研究了压弯成形过程中管坯在不同弯曲变形量下的壁厚分布和内高压成形过程中压力加载路径对成形零件壁厚的影响。基于有限元模拟结果,进行了压弯成形和内高压成形实验。结果表明,压弯成形和内高压成形弯曲叠加处最易破裂;通过优化加载路径可避免缺陷,获得壁厚均匀性较好的成形零件;成形实验结果与数值模拟结果一致。     

镁合金网格壁板压弯成形数值模拟及实验研究

为探索镁合金整体壁板压弯成形的可行性,以及镁合金壁板压弯成形过程中金属的流动规律,对AZ31镁合金网格壁板压弯成形进行了数值模拟和实验研究。建立了有限元数值模拟的几何模型,采用有限元计算软件对AZ31镁合金网格壁板压弯成形过程进行了数值模拟研究,分析了镁合金网格壁板压弯成形中的温度场、应变场、应力场、破坏系数等的分布规律。确定了合适的AZ31镁合金壁板压弯成形工艺参数,并对镁合金网格壁板压弯成形进行了实验研究,获得了合格的镁合金网格壁板弯曲件,并分析了镁合金网格壁板成形件尺寸精度,模拟结果与实验结果相吻合,最大相对误差为16.7%。     

带纵筋平板的轧制成形规律与极限研究

带纵筋平板是一种结构复杂的异型板,其在轧制成形过程中型槽内金属填充不足、凸筋成形难的问题比较突出。针对该问题,提出了一种新的带纵筋平板轧制成形工艺方法,采用两道次将带纵筋平板轧制成形。将第1道次轧制的轧辊组设计成上辊有型槽、下辊有弧形的凸起结构;在第2道次轧制的轧辊组中,将上辊设计成与第1道次同尺寸的型槽,下辊设计为平辊。采用这种多道次轧制方法可以有效地促进金属向上辊型槽内流动,促进凸筋的增长。通过Abaqus有限元模拟,分析了辊型结构对筋高和成筋率的影响规律以及不同板厚的凸筋的成形极限,从而得到成形较好的工艺参数。通过开展实验,发现实验结果和模拟结果基本一致,这为后续的异型板的精密成形研究提供了理论基础。     

封头的多点成形工艺分析和数值模拟研究

结合多道次成形和分段成形工艺方式,文章对封头的多点成形过程进行了工艺分析。通过对其成形过程的有限元数值模拟,研究了封头多道次成形和分段成形的成形规律,制定了封头的多点成形工艺,并进行了实验验证。结果表明,通过合理的成形工艺,可以用多点成形设备成形封头,并能得到良好的成形效果。     

铝合金控制臂辊锻制坯模锻工艺数值模拟

针对控制臂现阶段模锻成形工艺工序多,生产率低,劳动强度大等缺点,提出辊锻制坯一模锻成形工艺,设计辊锻制坯各道次的尺寸参数,用数值模拟代替物理试验预测金属成形过程。通过对控制臂辊锻成形过程的数值模拟,并对辊锻后坯料进行弯曲、终锻成形,获得较好的锻件,为指导此锻件的生产实践提供了理论依据。     

某汽车减震器多道次渐进成形数值模拟分析

以某汽车减震器为例,通过分析零件结构,得出单道次不能成形的结论;于是采用多道次成形,根据成形理论基础,设计加工工艺过程,计算每道次材料的减薄率,提出每次减薄率分别为0.23、0.30、0.46的三道次成形策略。建立有限元模型进行数值模拟,比较分析厚度值,模拟厚度结果符合工艺设计最小壁厚0.7mm的要求。模拟证明了某汽车减震器多道次渐进成形方案设计的正确性,为渐进成形在侧壁较陡制件上的推广应用及多道次的工艺设计提供了一定的理论依据。     

FEM modelling for press bend forming of doubly curved integrally stiffened aircraft panel

In order to establish an FEM model for aircraft integral panel press bend forming process, a special simulation procedure and a calculation method for the punch and die boundary condition based on the bending line coordinates were proposed. The simulation of a seven-step press bend forming process of doubly curved integrally stiffened aircraft panels was realized, and it could well simulate the real fabrication process, so that it could assist in studying this complicated forming process. Stress and strain distributions were analyzed, which reveals the deformation mechanics of this process. With quantitative comparisons, it can be concluded that forming quality of the seven step press bend forming is quite good, considering both the forming precision and the surface quality.     

FEM equivalent model for press bend forming of aircraft integral panel

An original plastic equivalent model was proposed to solve the problem of excessive FEM simulation time when designing the press bend forming path and optimizing the process parameters of press bend forming of the integrally stiffened aircraft panels. Based on the in-depth analysis of the mechanics of the bending and springback of the detailed model and the equivalent model of the integral panels, the plastic equivalent model of the virtual material with special initial yield stress and hardening coefficients was constructed. FEM results indicate that the objective of getting the similar contour with the same press bend forming path is achieved with the error less than 6%, and the efficiency of FEM simulation is improved by more than 80%. The plastic equivalent model is valuable and essential for the further research on the press bend forming process of large scale complicated integral panels.     

Optimization of press bend forming path of aircraft integral panel

In order to design the press bend forming path of aircraft integral panels,a novel optimization method was proposed, which integrates FEM equivalent model based on previous study,the artificial neural network response surface,and the genetic algorithm.First,a multi-step press bend forming FEM equivalent model was established,with which the FEM experiments designed with Taguchi method were performed.Then,the BP neural network response surface was developed with the sample data from the FEM experiments.Furthe...     

整体壁板压弯成形中的筋条失稳预测(英文)

为实现对整体壁板压弯成形中筋条失稳的预测,基于能量法、弹塑性力学和数值解析提出压弯成形过程中筋条临界失稳载荷的求解方法。在设计的压弯模具上进行压弯失稳试验。结果表明,基于本文提出的方法所得的理论临界失稳载荷与试验结果吻合较好。采用本文所提出的方法可以对铝合金高筋整体壁板压弯成形中的筋条失稳问题进行合理地预测。     

基于Dynaform的飞机封严板压窝成形工艺分析与优化设计

飞机封严板在敲制成形沉头窝孔后,表面出现不同程度的起皱变形问题,且难以消除.采用非线性有限元分析软件Dynaform对飞机封严板窝孔成形过程进行数值模拟.经研究分析发现,成形过程中由于封严板没有压边支撑,且成形方式过于粗糙剧烈,导致封严板起皱变形.针对这些问题制定了相应措施,改变以往的敲窝成形方法,发明了一种气动压窝器...     

伺服成形技术及其若干发展动向

伺服压力机是近年来塑性成形领域最重大的创新之一,将伺服压力机以及基于伺服压力机的成形工艺统称为伺服成形技术.简要介绍了伺服成形技术的特点和目前的应用情况,重点论述了该技术当前的若干发展新动向,包括伺服压力机设计方法的研究、新型功能部件和储能技术开发、滑块运动路径设计与优化、伺服成形机理及成形过程的数值模拟、智能制造中的...     

Process planning for laser-assisted forming

Laser forming has emerged as a viable means of assisting conventional forming processes with geometrical accuracy-related problems. By combining the incremental nature of laser forming with conventional processes such as brakeforming which forms material by a single continuous movement of the tooling, the exact specified bend angle and radius of curvature of the bent component may be approached. This may be achieved by sequential or simultaneous application of the conventional tooling and the laser beam. The laser beam may be applied once to the forming zone or multiple laser beam scans may be used.

The combined process allows the forming of highly accurate sheet metal products in a cost effective way, through the possibility to make corrections to the bend angle in a controlled way. Furthermore, the combined process makes it possible to form intricate products that cannot be bent on a press brake due to collision problems or problems emanating from spring-back.

Consequently there are new implications for process planning in brakeforming when a laser beam is used in combination. These implications are discussed for some primitive applications.     

基于PS2F软件的型材拉弯成形工艺研究

运用拉弯成形专用模拟软件PS2F对角形截面不锈钢型材拉弯件的成形过程进行了模拟研究.并以某型地铁车体不锈钢角形截面弯梁为典型件,对其拉弯成形工艺进行数值分析和优化,通过分析起皱等成形缺陷,开发出高精度拉弯胎具.试验结果表明成形件轮廓精度大幅度提高,并消除了起皱、截面畸变等成形缺陷,产品质量精度完全满足生产要求.     

Investigation into forming sequences for the incremental forming of doubly curved plates using the line array roll set (LARS) process

The line array roll set (LARS) process [7] proposed by the authors is an effective metal forming process used to manufacture doubly curved metal plates. To obtain a final shape with the desired bend radii and to minimize any possible defects, the process for forming the desired shape should be systematically and accurately designed. The major purpose of the present work is to analyze the effect of the forming sequences in the LARS process. The experiments are conducted using three types of forming sequences, and the final bend radii and the quality of the formed plates produced by the LARS process are evaluated. It is found that it is more effective to form a doubly curved plate through a singly curved shape in order to improve the quality of the formed plate. A series of forming experiments with various bending radii are conducted and the interaction phenomena in double curvature bending are observed.     

飞机蒙皮振动辅助拉伸成形工艺分析

拉伸成形结束后,由于残余应力的存在导致蒙皮零件产生较大的回弹,会严重影响蒙皮的使用质量。基于回弹产生的原因,从工件的应力-应变机制阐述了振动减小残余应力的机理,提出了一种振动辅助飞机蒙皮拉伸成形的新工艺方法,给出了该工艺的主要参数——频率、振幅在应用选择上的依据条件及实际运用中可选择的合理范围。以飞机前缘蒙皮拉伸成形为例,通过数值仿真模拟,分析了施加振动对成形蒙皮零件回弹的影响以及频率、振幅对改善回弹的影响,并通过实验加以验证。结果表明,在飞机蒙皮拉伸成形过程中,施加振动可以更加有效地减小零件的回弹,当选取的工艺参数频率为30 Hz左右、振幅在1.5 mm左右时回弹值最小,效果最佳。