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High strain rate superplastic forming into rectanglar part of SiC particle reinforced 2124 aluminum alloy composite sheet

机译:SiC颗粒增强2124铝合金复合板的高应变率超塑性成型成矩形矩形部分

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The forming test was performed at 773Kusing a 250mm×250mm blank sheet by the gas pressure,which was preset to achieve the average strain rateof 0.1/s. The rectanglar part is successfully formedwith in about 10 seconds and the maximum thicknessreduction strain is over 100% at the corner of the part.The high forming rate leads to the uniform thicknessdistributions of the formed part and it coincides withthe bulge forming test conducted by authors in theprevious work. From the results of measuring thechange in contour shape and thickness distributions,the forming process is proved as follows. The sheetis bulged freely in the die at first and then attachesthe bottom or side wall, finally formed along thecorner of the die. The process coincides with the shapepredicted in the calculation of the gas pressure pattern.
机译:通过气体压力在773杆250mm×250mm坯料纸上进行成形试验,预设为达到0.1 / s的平均菌株率。 矩形部分在大约10秒内成功形成,并且最大厚度菌株在该部分的拐角处超过100%。高形成速率导致所形成的部分的均匀厚度分布,并且它与作者进行的凸起形成试验相一致 不知情的工作。 从测量轮廓形状和厚度分布的测量结果,如下证实了成形过程。 薄片首先在模具中自由膨胀,然后附着在底部或侧壁上,最后沿着模具的TheCorner形成。 该方法与在计算气体压力模式的计算中的形状恰当。

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