连铸坯角下裂纹形成与扩展的热弹粘塑性有限元分析

IF 3.1 2区 材料科学 Q1 METALLURGY & METALLURGICAL ENGINEERING
Yu-jun Li, Huan Li, Peng Lan, Hai-yan Tang, Jia-quan Zhang
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引用次数: 7

摘要

采用三种热-力学耦合模型,对铸坯连铸中常见的离角亚表面裂纹的形成和扩展进行了热-力学分析。建立了二维热弹粘塑性有限元模型,以预测结晶区凝固壳的结晶间隙演变、温度分布和变形行为。然后,采用三维模型计算了三次冷却区壳的生长、温度历史以及壳的应力应变发展。最后,采用另一种三维模型分析了矫直区的应力分布。结果表明:铸坯上边角裂纹是由凝固前沿裂纹敏感区产生的拉伸应变引起的,而铸坯上边角裂纹是由铸坯表面可能出现的严重温度回弹和二冷区广泛的拉应力导致的,特别是在铸坯矫直过程中。结果表明,通过优化模角半径、浇注速度和二次冷却方案,可以获得更均匀的壳体温度和厚度,从而降低应力应变集中,防止裂纹的产生。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Thermo-elasto-visco-plastic finite element analysis on formation and propagation of of-corner subsurface cracks in bloom continuous casting

The formation and propagation of the popular off-corner subsurface cracks in bloom continuous casting were investigated through thermo-mechanical analysis using three coupled thermo-mechanical models. A two-dimensional thermo-elasto-visco-plastic finite element model was developed to predict the mould gap evolution, temperature profiles and deformation behavior of the solidified shell in the mould region. Then, a three-dimensional model was adopted to calculate the shell growth, temperature history and the development of stresses and strains of the shell in the following secondary cooling zones. Finally, another three-dimensional model was used to analyze the stress distributions in the straightening region. The results showed that the off-corner cracks in the shell originated from the mould owing to the tensile strain developed in the crack sensitive regions of the solidification front, and they could be driven deeper by the possible severe surface temperature rebound and the extensive tensile stress in the secondary cooling zone, especially upon the straightening operation of the bloom casting. It is revealed that more homogenous shell temperature and thickness can be obtained through optimization of mould corner radius, casting speed and secondary cooling scheme, which help to decrease stress and strain concentration and therefore prevent the initiation of the cracks.

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来源期刊
CiteScore
4.30
自引率
0.00%
发文量
2879
审稿时长
3.0 months
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