IF 2.2 3区 工程技术 Q3 MATERIALS SCIENCE, MULTIDISCIPLINARY
T. Virazels, S. Lister, O. Levano-Blanch, M. Jackson, J. A. Rodríguez-Martínez, J. C. Nieto-Fuentes
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引用次数: 0

摘要

本文探讨了现场辅助烧结技术生产的钛合金中高速冲击破碎的力学原理。为此,我们采用了 Nieto-Fuentes 等人最近开发的实验装置(J Mech Phys Solids 174:105248, 2023a;Int J Impact Eng 180:104556, 2023b),对圆环和圆柱体进行动态膨胀试验。实验包括使用单级轻型气枪对静止的圆环/圆柱体发射锥鼻圆柱形弹丸,速度范围为(约248~/text {m}//text {s}/)到(约390~/text {m}//text {s}/)、对应于试样中的估计应变率从10050到19125不等。弹丸圆柱形部分的直径超过了圆环/圆柱体的内径,导致后者在弹丸前进时膨胀,从而形成多个颈部和碎片。已对两种不同的合金进行了测试:Ti6Al4V 和 Ti5Al5V5Mo3Cr。这些材料广泛应用于航空和航天工业,用于制造压缩机部件(盘和叶片)和惠普尔防护罩等结构件,这些部件经常暴露在高强度的机械负荷下,包括高速撞击。然而,尽管 Ti6Al4V 和 Ti5Al5V5Mo3Cr 具有重要的科学和技术意义,并且对其机械和断裂行为进行了广泛研究,但据作者所知,迄今为止还没有对这些合金的动态破碎行为进行过系统研究。因此,本文提出了一个雄心勃勃的碎裂测试计划,分别在环和圆柱体上进行了 27 次和 29 次实验。利用现场辅助烧结技术生产多材料部件的能力,测试了整体和多材料样品--一半是 Ti6Al4V 样品,一半是 Ti5Al5V5Mo3Cr 样品。对碎片进行了收集、称重、确定尺寸,并使用扫描电子显微镜进行了分析。实验结果表明,颈部数量、碎片数量以及颈部变成碎片的比例一般会随着膨胀速度的增加而增加。根据线性稳定性分析(Zhou 等人,载于 Int J Impact Eng 33:880-891 2006;Vaz-Romero 等人,载于 Int J Solids Struct 125:232-243, 2017)的预测,对颈部之间的平均距离进行了评估,结果显示理论预测与实验结果之间的一致性令人满意。此外,实验结果还与文献(Nieto-Fuentes et al. in J Mech Phys Solids 174:105248, 2023a;Zhang and Ravi-Chandar in Int J Fract 142:183-217, 2006;Zhang and Ravi-Chandar in Int J Fract 150:3-36, 2008)中报道的各种金属和合金的测试结果进行了比较,以研究材料行为对碎片尺寸和颈部间距统计的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
High-velocity fragmentation of titanium alloy rings and cylinders produced using Field-Assisted Sintering Technology

This paper explores the mechanics of high-velocity impact fragmentation in titanium alloys produced by Field-Assisted Sintering Technology. For that purpose, we have utilized the experimental setups recently developed by Nieto-Fuentes et al. (J Mech Phys Solids 174:105248, 2023a; Int J Impact Eng 180:104556, 2023b) for conducting dynamic expansion tests on rings and cylinders. The experiments involve firing a conical-nosed cylindrical projectile using a single-stage ight-gas gun against the stationary ring/cylinder at velocities ranging from \(\approx 248~\text {m}/\text {s}\) to \(\approx 390~\text {m}/\text {s}\), corresponding to estimated strain rates in the specimen varying from \(\approx 10050~\text {s}^{-1}\) to \(\approx 19125~\text {s}^{-1}\). The diameter of the cylindrical part of the projectile exceeds the inner diameter of the ring/cylinder, causing the latter to expand as the projectile moves forward, resulting in the formation of multiple necks and fragments. Two different alloys have been tested: Ti6Al4V and Ti5Al5V5Mo3Cr. These materials are widely utilized in aeronautical and aerospace industries for constructing structural elements such as compressor parts (discs and blades) and Whipple shields, which are frequently exposed to intense mechanical loading, including high-velocity impacts. However, despite the scientific and technological significance of Ti6Al4V and Ti5Al5V5Mo3Cr, and the extensive research on their mechanical and fracture behaviors, to the best of the authors’ knowledge, no systematic study has been conducted thus far on the dynamic fragmentation behavior of these alloys. Hence, this paper presents an ambitious fragmentation testing program, encompassing a total of 27 and 29 experiments on rings and cylinders, respectively. Monolithic and multimaterial samples—half specimen of Ti6Al4V and half specimen of Ti5Al5V5Mo3Cr—have been tested, taking advantage of the ability of Field-Assisted Sintering Technology to produce multimaterial parts. The fragments have been collected, weighed, sized, and analyzed using scanning electron microscopy. The experiments have shown that the number of necks, the number of fragments, and the proportion of necks developing into fragments generally increase with expansion velocity. The average distance between necks has been assessed against the predictions of a linear stability analysis (Zhou et al. in Int J Impact Eng 33:880–891 2006; Vaz-Romero et al. in Int J Solids Struct 125:232–243, 2017), revealing satisfactory agreement between theoretical predictions and experimental results. In addition, the experimental results have been compared with tests reported in the literature for various metals and alloys (Nieto-Fuentes et al. in J Mech Phys Solids 174:105248, 2023a; Zhang and Ravi-Chandar in Int J Fract 142:183–217, 2006, Zhang and Ravi-Chandar in Int J Fract 150:3–36, 2008) to examine the influence of material behavior on the statistics of fragments size and necks spacing.

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来源期刊
International Journal of Fracture
International Journal of Fracture 物理-材料科学:综合
CiteScore
4.80
自引率
8.00%
发文量
74
审稿时长
13.5 months
期刊介绍: The International Journal of Fracture is an outlet for original analytical, numerical and experimental contributions which provide improved understanding of the mechanisms of micro and macro fracture in all materials, and their engineering implications. The Journal is pleased to receive papers from engineers and scientists working in various aspects of fracture. Contributions emphasizing empirical correlations, unanalyzed experimental results or routine numerical computations, while representing important necessary aspects of certain fatigue, strength, and fracture analyses, will normally be discouraged; occasional review papers in these as well as other areas are welcomed. Innovative and in-depth engineering applications of fracture theory are also encouraged. In addition, the Journal welcomes, for rapid publication, Brief Notes in Fracture and Micromechanics which serve the Journal''s Objective. Brief Notes include: Brief presentation of a new idea, concept or method; new experimental observations or methods of significance; short notes of quality that do not amount to full length papers; discussion of previously published work in the Journal, and Brief Notes Errata.
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