首页> 外文期刊>Journal of Alloys and Compounds: An Interdisciplinary Journal of Materials Science and Solid-state Chemistry and Physics >On the thermal forming limit diagram (TFLD) with GTN mesoscopic damage model for AA7075 aluminum alloy: Numerical and experimental investigation
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On the thermal forming limit diagram (TFLD) with GTN mesoscopic damage model for AA7075 aluminum alloy: Numerical and experimental investigation

机译:关于AA7075铝合金GTN介于损伤模型的热成型极限图(TFLD):数值和实验研究

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The formability of high strength AA7075 aluminum alloy under elevated temperatures is vital in guiding the fabrication of automobile structural parts. The ductile fracture forming limit of AA7075 at elevated temperatures is essentially governed by thermal damage evolution. In this paper, the hot tensile test (300 degrees C-450 degrees C, strain rate 0.1s(-1)-0.001s(-1)) for AA7075 was conducted and the corresponding flow behavior was fitted by Hensiel-Spittel (HS) constitutive equation. The GTN mesoscopic damage model was implemented to take account of the damage evolution phenomenon of AA7075 at elevated temperatures. The temperature-dependent damage void volume fractions (VVF) were identified accurately based on a novel inverse identification procedure, named the CCD parameters design-FEM inverse simulation-genetic algorithm (CCD-FEIS-GA) optimization method. Subsequently, the thermal forming limit diagram (TFLD) was calculated based on the GTN damage parameters and further validated by hot Nakajima-type bulging experiment. The corresponding damage evolution behaviors and effects of critical forming parameters were discussed in detail. The comparison of experimental and numerical results showed that the formability of AA7075 firstly increases and then decreases with the increasing forming temperature, the TFLD0 reaches its maximum value when the temperature is 400 degrees C, and the formability also increases with the increasing strain rate and the decreasing surface coefficient of friction. The proposed simulated strategy coupled with mesoscopic GTN approach conduces to the accurate prediction of TFLD and damage fracture behavior of AA7075 in the hot forming process. (C) 2019 Elsevier B.V. All rights reserved.
机译:高强度AA7075铝合金在升高温度下的可成形性对于引导汽车结构部件的制造至关重要。升高温度下AA7075的延性骨折形成极限基本上受热损伤进化的管辖。本文进行了AA7075的热拉伸试验(300℃-450℃,应变率0.1s(-1s)-0.001s(-1)),并由Hensiel-Spittel(HS)安装相应的流动行为(HS )构成方程。实施了GTN介观损伤模型,以考虑升高温度AA7075的损伤演化现象。基于新的逆识别程序,准确地确定了温度依赖性损伤空隙体积分数(VVF),名为CCD参数设计-FEM逆模拟 - 遗传算法(CCD-FEI-GA)优化方法。随后,基于GTN损伤参数计算热成形限位图(TFLD),并通过热Nakajima型凸出实验进一步验证。详细讨论了相应的损伤演化行为和临界成形参数的影响。实验性和数值结果的比较表明,AA7075的可成形性首先增加,然后随着成形温度的增加而降低,当温度为400℃时,TFLD0达到其最大值,并且成形性也随着应变速率的增加而增加。降低表面摩擦系数。耦合的思科GTN方法的提出的模拟策略涉及AA7075在热成型过程中的TFLD和损伤断裂行为的精确预测。 (c)2019 Elsevier B.v.保留所有权利。

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