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An Analytical Model of the Superplastic Bulge Forming of Sheet Metal

机译:钣金超塑性胀形的解析模型

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This paper presents analytical and experimental study on the superplastic bulge forming of hemispherical shell. Most of the simple engineering models proposed to date do not consider the stress and strain variation from apex to the periphery of the bulged shape, although its effect in the calculations of the thickness distribution is well understood. An analytical model is formulated on the basis of the incremental strain theory of plasticity and non-equal biaxial stress states in deformed shell. Simulation programs were developed to predict some deformation parameters such as stresses, strains and thickness distribution, bulging time, pressure-time cycling for constant apex strain rate deformation. In addition to the analytical calculation, Finite Element Analysis (FEA) was conducted to examine the validity of the present analytical model. Bulge forming experiments were conducted by using Ti-alloy "SP-700" sheets of thickness 0.75 mm under Ar gas pressure at the temperature 800 ℃. The suggested model showed good agreement with the experiments and FEA.
机译:本文提出了半球形壳超塑性胀形的分析和实验研究。迄今为止提出的大多数简单工程模型都没有考虑从顶点到凸出形状的外围的应力和应变变化,尽管其在厚度分布计算中的作用已广为人知。根据塑性变形的增量应变理论和变形壳的不等双轴应力状态,建立了解析模型。开发了仿真程序来预测一些变形参数,例如应力,应变和厚度分布,凸出时间,恒定顶点应变率变形的压力时间循环。除了进行分析计算外,还进行了有限元分析(FEA),以检验本分析模型的有效性。通过在800℃的Ar气压下使用厚度为0.75 mm的Ti合金“ SP-700”板进行凸出成形实验。建议的模型与实验和有限元分析吻合良好。

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