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Numerical and Experimental Studies on Extrusion of Fan-shaped Shell of Magnesium Alloy

机译:镁合金框壳挤出的数值和实验研究

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This paper presents a case study of optimizing the forming process for a fan-shaped shell component. Numerical simulation was used to study the backward extrusion process of a fan-shaped shell. The underfill defect produced at the opening of the extruded shell due to the billet shape was solved and the minimal base thickness required to avoid the presence of the underfill defect at the bottom corner of the component was defined through the numerical simulation. The extrusion drawing and forming process of the fan-shaped shell were designed on the basis of the results of the numerical simulation. Forming experiments had been performed on the fan-shaped shell at 380 oC and cracking was found on the outside wall in the center of the extruded shell. Choked groove on the inner wall of the die and reducing the lubrication had been used to avoid the presence of cracking. The fan-shaped shell of AZ31 magnesium alloy has been successfully formed by the three-stage forming process of hot upsetting, hot backward extrusion and cold sizing.
机译:本文介绍了优化扇形壳体部件的成形过程的案例研究。数值模拟用于研究扇形外壳的后向挤压过程。通过数值模拟来限定由于坯料形状引起的挤出壳体的开口时产生的底部填充缺陷求解,并且避免在部件的底部处存在填充缺陷所需的最小碱度厚度。基于数值模拟的结果设计了扇形壳体的挤出图和形成过程。在挤出壳体中心的外壁上发现了在扇形壳体上对扇形壳体进行形成实验,并且在挤出壳的中心的外壁上发现。在模具的内壁上窒息槽并减少润滑以避免裂缝的存在。 AZ31镁合金的扇形外壳已通过热镦,热向挤压和冷施加的三级成型过程成功形成。

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