A multi-scale constitutive model based gas pressure determination method for the grain size evolution of superplastic forming

Q1 Engineering
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引用次数: 0

Abstract

This paper proposes an innovative multi-scale method for determining gas pressure parameters of superplastic forming, which is based on the quantitative relationship between the grain growth mechanism and fracture mechanism of Ti–6Al–4V alloy. The high-temperature tensile tests were conducted on the material at temperatures ranging from 700, 800, 840, 890, 920, and 950 °C, strain rates were selected as 10−2∼10−4/s. The grain size measurements were observed using electron back-scatter diffraction (EBSD). Particularly, the relation between grain size changes and fracture behaviour is specifically discovered using a physically-based dynamic material model (DMM), and the grain size thresholds for each forming limit are proposed. The physical fracture mechanism is named the “Grain growth based fracture (GGBF)” mechanism. Furthermore, an innovative method based on the GGBF mechanism is proposed to design the superplastic forming loading, and practical four-layer hollow structures experiments are applied to validate the fracture mechanism in superplastic forming. In total, A superplastic forming GGBF mechanism has been verified, and it is expected to be helpful for shape and property control in the forming process of complex structures.

基于多尺度构成模型的超塑性成形晶粒尺寸演化气体压力确定方法
本文基于 Ti-6Al-4V 合金晶粒生长机理与断裂机理之间的定量关系,提出了一种创新的多尺度超塑性成形气压参数测定方法。在 700、800、840、890、920 和 950 °C 温度范围内对材料进行了高温拉伸试验,应变速率选择为 10-2∼10-4/s。使用电子反向散射衍射(EBSD)对晶粒尺寸进行了测量。特别是,利用基于物理的动态材料模型(DMM),具体发现了晶粒尺寸变化与断裂行为之间的关系,并提出了每个成形极限的晶粒尺寸阈值。该物理断裂机制被命名为 "基于晶粒生长的断裂(GGBF)"机制。此外,还提出了一种基于 GGBF 机制的创新方法来设计超塑性成形加载,并应用实际的四层空心结构实验来验证超塑性成形中的断裂机制。总之,超塑性成形 GGBF 机理已得到验证,有望在复杂结构成形过程中帮助实现形状和性能控制。
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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来源期刊
International Journal of Lightweight Materials and Manufacture
International Journal of Lightweight Materials and Manufacture Engineering-Industrial and Manufacturing Engineering
CiteScore
9.90
自引率
0.00%
发文量
52
审稿时长
48 days
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