Understanding deformation and fracture mechanism of Ti-55531 alloy under complex loading conditions: a case of pre-tensioned torsion

IF 9.6 1区 材料科学 Q1 MATERIALS SCIENCE, MULTIDISCIPLINARY
Kong-Liang Hu, Chao-Wen Huang, Hong-Tao Zeng, Jiang Yang, Dan Liu, Tian-Xin Li, Ming-Pan Wan, Yong-Qing Zhao
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Abstract

The deformation and fracture failure of aerospace structural components are primarily affected by complex loading conditions. This study aims to investigate how various pre-tension strains (0%, 4% and 6%) influence the torsional properties, deformation and fracture mechanism of the Ti–5Al–5Mo–5V–3Cr–1Zr (Ti-55531) alloy with the bimodal microstructure. The results indicate that increasing the pre-tension strain gradually decreases the torsional strength of specimens. However, their torsional ductility initially increases (from 0 to 4% pre-tension strain) and then decreases (from 4 to 6% pre-tension strain). This can be attributed to the significant influence of different pre-tension strains on the deformation mechanism of each phase in the alloy. Under pure torsion loading, the primary α (αp) phase mainly undergoes the {0002} basal slip for deformation. However, at a pre-tension strain of 4%, the torsional deformation mechanism of αp transforms into crossing reaction between the {\(10\overline{1 }0\)} prismatic slips. As the pre-tension strain further increases to 6%, {\(10\overline{1 }1\)} pyramidal slips were further activated. Moreover, with an increase in pre-tension strain, there is a significant rise multiple slips probability within the αp during torsional deformation. On contrary, for the secondary α (αs) phase, the probability of {\(10\overline{1 }1\)}α twins formation during torsional deformation firstly rises and then reduces. These findings indicate that α phase, particularly αp, plays a crucial role in accommodating deformation. This discovery offers valuable insights for further adjustments and optimizations of material microstructure and properties. Additionally, modifying external load can alter the stress state of components and enhance their fracture resistance during service, thereby broadening their range of applications and improving material reliability.

Graphical abstract

Abstract Image

了解复杂加载条件下 Ti-55531 合金的变形和断裂机理:预拉伸扭转案例
航空航天结构部件的变形和断裂失效主要受复杂加载条件的影响。本研究旨在探讨各种预拉伸应变(0%、4% 和 6%)如何影响具有双峰微观结构的 Ti-5Al-5Mo-5V-3Cr-1Zr (Ti-55531)合金的扭转性能、变形和断裂机制。结果表明,增加预拉应变会逐渐降低试样的抗扭强度。然而,它们的扭转延展性最初会增加(从 0% 到 4% 的预拉伸应变),然后会降低(从 4% 到 6% 的预拉伸应变)。这可能是由于不同的预拉伸应变对合金中各相的变形机制有显著影响。在纯扭转加载下,初级α(αp)相主要通过{0002}基底滑移进行变形。然而,当预拉伸应变为 4% 时,αp 的扭转变形机制转变为{(10\overline{1 }0)} 棱柱滑移之间的交叉反应。当预拉伸应变进一步增加到 6% 时,{(10\overline{1 }1\)} 金字塔形滑移被进一步激活。此外,随着预拉伸应变的增加,在扭转变形过程中,αp内部的多重滑移概率显著上升。相反,对于次生α(αs)相,扭转变形过程中{(10\overline{1 }1)}α twins形成的概率先上升后下降。这些发现表明α相,尤其是αp,在适应变形方面起着至关重要的作用。这一发现为进一步调整和优化材料的微观结构和性能提供了宝贵的启示。此外,改变外部载荷可以改变部件的应力状态,增强其在使用过程中的抗断裂性,从而拓宽其应用范围,提高材料的可靠性。
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来源期刊
Rare Metals
Rare Metals 工程技术-材料科学:综合
CiteScore
12.10
自引率
12.50%
发文量
2919
审稿时长
2.7 months
期刊介绍: Rare Metals is a monthly peer-reviewed journal published by the Nonferrous Metals Society of China. It serves as a platform for engineers and scientists to communicate and disseminate original research articles in the field of rare metals. The journal focuses on a wide range of topics including metallurgy, processing, and determination of rare metals. Additionally, it showcases the application of rare metals in advanced materials such as superconductors, semiconductors, composites, and ceramics.
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