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Designing superplastic forming process of a developmental AA5456 using pneumatic bulge test experiments and FE-simulation

机译:利用气动膨胀试验和有限元模拟设计发展型AA5456的超塑性成形工艺

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Relatively low tooling costs, high design complexity coupled with low forming speeds make the superplastic sheet metal forming process attractive, especially for smaller lot sizes. Due to the relatively small lot size, the effort and budget for designing superplastic forming processes is usually limited (Kappes and Liewald in J Mater Sci Eng B1:472–478, 2011). For this reason the tool design and corresponding pressure profiles in superplastic forming processes are often based on trial and error (Franchitti et al. in 11th international Esaform conference on material forming, 2008; Barnes in J Mater Eng Perform 4:440–454, 2007). Consequently a process chain should be established to design superplastic forming processes accurately and efficiently. This paper deals with the process chain to form an aluminium part superplastically. At the beginning of the process chain, there is a new, developmental aluminium alloy sheet (AA5456, s0 = 1.6 mm) designed for superplastic forming supplied by Hydro Aluminium Rolled Products GmbH. The relevant material parameters of this sheet are then determined via pneumatic bulge testing with and without in situ measurement of strains. Using these experimentally determined parameters superplastic forming process can be simulated by FE modelling (PAM-STAMP 2G). Due to in situ measurement of strains during pneumatic bulging, the comparison of experiment and FE-simulation results over the whole pneumatic bulging process could be done. This comparison shows good correlation for the observed conditions. Furthermore a cylindrical cup was simulated, evaluated via determined isobar Superplastic Forming Limit Curve (at fracture) and finally formed by pneumatic bulging. Material characterisation of the bottom of this cup showed that excessive cavitation was observed as a result of the iron-silicon particles. Superplastic forming of a bracket usually formed out of AA5083 was also simulated using material parameters of AA5456. The simulation was able to show that this part is not able to be manufactured out of AA5456 under these forming conditions, which was confirmed by forming trials performed at ALU-SPF AG.
机译:相对较低的模具成本,较高的设计复杂度以及较低的成型速度,使得超塑性金属板成型工艺具有吸引力,特别是对于较小的批量而言。由于批量相对较小,设计超塑性成形工艺的工作和预算通常有限(Kappes和Liewald,J Mater Sci Eng B1:472-478,2011)。因此,超塑性成型过程中的工具设计和相应的压力分布通常基于反复试验(Franchitti等人在第11届国际Esaform材料成型会议上,2008; Barnes in J Mater Eng Perform 4:440–454,2007 )。因此,应该建立一个过程链来准确有效地设计超塑性成形过程。本文讨论了以超塑性方式形成铝零件的工艺链。在工艺链的开始,Hydro Aluminium Rolled Products GmbH提供了一种用于超塑性成形的新型研发铝合金板(AA5456,s0 = 1.6 mm)。然后,通过气动凸起测试,在有无应变的情况下进行测量,确定该板材的相关材料参数。使用这些实验确定的参数,可以通过有限元建模(PAM-STAMP 2G)模拟超塑性成形过程。由于在气动鼓胀过程中对应变进行了现场测量,因此可以对整个气动鼓胀过程中的实验结果和有限元模拟结果进行比较。该比较显示了对于观察到的条件的良好相关性。此外,还模拟了一个圆柱杯,通过确定的等压线超塑性成形极限曲线(断裂时)进行了评估,最后通过气动鼓胀成形。该杯子底部的材料特征表明,由于铁硅颗粒,观察到了过度的气蚀现象。还使用AA5456的材料参数模拟了通常由AA5083制成的支架的超塑性成型。仿真结果表明,在这些成型条件下无法用AA5456制造该零件,这一点已通过ALU-SPF AG进行的成型试验得到了证实。

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