Notice of RetractionNumerical Simulation of AZ31 Magnesium Alloy Isothermal Forming

Xu-bin Li, Zhiming Zhang
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引用次数: 0

Abstract

The equipment is a spaceflight electronic system. We have adopted the extrusion method under equal extruding temperature of 350 - 380°C. Based on stress-strain data gaining from isothermal compression experiment, adopts rigid - plastic finite element method, simulating isothermal-extrusion deformation of which the component is wrought magnesium alloy, emphatically discussing deformation force and metal flowing law in the course of isothermal-extrusion deformation. According to the simulation result of stress field, strain field, velocity field and so on, the method can forecast producing defect produced in the course of deformation and offer the reliable reference basis for isothermal extrusion deformation. As a result, diversion method are adopted. We have succeeded in extruding the part and attaining the mechanics performance of the equipment, size precision which reaches the requirements.
关于AZ31镁合金等温成形数值模拟的通知
该设备是一个航天电子系统。我们采用了在350 - 380℃等挤压温度下的挤压方法。基于等温压缩实验获得的应力应变数据,采用刚塑性有限元法,模拟了以变形镁合金为构件的等温挤压变形,着重讨论了等温挤压变形过程中的变形力和金属流动规律。根据应力场、应变场、速度场等的模拟结果,该方法可以预测变形过程中产生的生产缺陷,为等温挤压变形提供可靠的参考依据。因此,采用了导流法。成功地对零件进行了挤压,使设备的力学性能、尺寸精度达到了要求。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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