首页> 外文会议>ASME international manufacturing science and engineering conference 2011 >SHEET ORIENTATION EFFECTS ON THE FORMABILITY LIMITS OF THE AZ31B MAGNESIUM ALLOY AT SPF CONDITIONS
【24h】

SHEET ORIENTATION EFFECTS ON THE FORMABILITY LIMITS OF THE AZ31B MAGNESIUM ALLOY AT SPF CONDITIONS

机译:板材取向对SPF条件下AZ31B镁合金成形极限的影响

获取原文
获取原文并翻译 | 示例
获取外文期刊封面目录资料

摘要

The formability curves of the AZ31B magnesium alloy were constructed by following a novel approach that best resembles the conditions of actual Superplastic Forming (SPF) operations. Sheet samples were formed at 400 ℃ and a constant strain rate of 1×10~(-3) s~(-1), by free pneumatic bulging into a set of progressive elliptical die inserts. By doing so, the material in each of the formed domes was forced to undergo biaxial stretching at a distinct strain ratio, which is simply controlled by the geometry (aspect ratio) of the selected die insert. Material deformation was quantified using circle grid analysis (CGA), and the recorded planar strains were used to construct the forming limit diagram (FLD) of the material. The aforementioned was carried out with the sheet oriented either along or across the direction of major strains, in order to establish the relationship between the material's rolling direction and the corresponding limiting strains. Great deviations between the two sets of formability curves are realised, hence a compound forming limit diagram is constructed as an improved way for characterising the material behaviour. The presented pneumatic stretching approach is shown to produce accurate friction-independent formability diagrams, with clear distinction between the safe and unsafe deformation zones, even though the developed diagrams are confined to the biaxial strain region (right side quadrant of an FLD). Moreover, the approach proves to be a viable means for providing formability maps under conditions where traditional mechanical stretching techniques (Nakajima and Marciniak tests) are limited.
机译:AZ31B镁合金的可成形性曲线是通过遵循一种最类似于实际超塑性成形(SPF)操作条件的新颖方法构造的。通过自由气动鼓胀到一组渐进式椭圆形模具嵌件中,在400℃和1×10〜(-3)s〜(-1)的恒定应变速率下形成片状样品。通过这样做,迫使每个形成的穹顶中的材料以不同的应变率进行双轴拉伸,该应变率可以简单地由所选模具嵌件的几何形状(长宽比)控制。使用圆网格分析(CGA)量化材料变形,并使用记录的平面应变构建材料的成形极限图(FLD)。为了建立材料的轧制方向和相应的极限应变之间的关系,在板沿大应变方向上或横过大应变方向取向的情况下进行上述操作。由于实现了两组可成形性曲线之间的较大偏差,因此构造了复合成形极限图,作为表征材料性能的一种改进方法。所示的气动拉伸方法显示出可产生精确的与摩擦无关的可成形性图,在安全变形区域和不安全变形区域之间有明显的区别,即使已开发的图仅限于双轴应变区域(FLD的右侧象限)。此外,该方法被证明是在传统机械拉伸技术(中岛和Marciniak试验)受到限制的条件下提供成形图的可行方法。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号