钛合金在真空和空气环境下内部疲劳裂纹尖端的变形机制

IF 5.7 2区材料科学 Q1 ENGINEERING, MECHANICAL

International Journal of Fatigue Pub Date : 2024-12-03 DOI:10.1016/j.ijfatigue.2024.108729

Louis Hébrard, Thierry Palin-Luc, Nicolas Ranc, Arnaud Weck, Thierry Douillard, Nicholas Blanchard, Sylvain Dancette, Jean-Yves Buffiere

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引用次数: 0

摘要

在含有可控内缺口的Ti-6Al4V试样上进行了高周疲劳（VHCF）状态下（NR>；107 - 108循环）的超声完全反向拉伸疲劳试验。使用了两组样品。第一个包括沿试样纵轴的中心烟囱，其将空气带入内部缺口；在第二个系列中，缺口没有连接到表面。利用电子显微镜（EBSD， TKD和TEM）研究了断裂试样断口下的微观组织。在真空环境下生长的裂纹表面下观察到纳米颗粒和纳米空洞的形成，而在与环境空气相连的裂纹表面下则没有。在后一种情况下，观察到广泛的条纹。在每个条纹下方观察到拉伸孪晶的形成。

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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Deformation mechanisms at the tip of internal fatigue cracks in vacuum and in the presence of an air environment in a Ti alloy

Ultrasonic fully reversed tension fatigue tests have been performed in the Very High Cycle Fatigue (VHCF) regime (NR>107−108cycles) on Ti-6Al4V specimens containing a controlled internal notch. Two sets of samples have been used. The first one contains a central chimney along the specimen longitudinal axis which brings air to the internal notch; in the second series the notches are not connected to the surface. The microstructure present below the fracture surface of the broken specimens has been studied by electron microscopy (EBSD, TKD and TEM). The formation of nanograins and nanovoids was observed below the surface of the cracks growing in a vacuum environment but not below the surface of cracks connected with ambient air. In the latter case extensive striations were observed. Below each striation the formation of tensile {101̄2} twins was observed.

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来源期刊

International Journal of Fatigue 工程技术-材料科学：综合

CiteScore

10.70

自引率

21.70%

发文量

619

审稿时长

58 days

期刊介绍： Typical subjects discussed in International Journal of Fatigue address: Novel fatigue testing and characterization methods (new kinds of fatigue tests, critical evaluation of existing methods, in situ measurement of fatigue degradation, non-contact field measurements) Multiaxial fatigue and complex loading effects of materials and structures, exploring state-of-the-art concepts in degradation under cyclic loading Fatigue in the very high cycle regime, including failure mode transitions from surface to subsurface, effects of surface treatment, processing, and loading conditions Modeling (including degradation processes and related driving forces, multiscale/multi-resolution methods, computational hierarchical and concurrent methods for coupled component and material responses, novel methods for notch root analysis, fracture mechanics, damage mechanics, crack growth kinetics, life prediction and durability, and prediction of stochastic fatigue behavior reflecting microstructure and service conditions) Models for early stages of fatigue crack formation and growth that explicitly consider microstructure and relevant materials science aspects Understanding the influence or manufacturing and processing route on fatigue degradation, and embedding this understanding in more predictive schemes for mitigation and design against fatigue Prognosis and damage state awareness (including sensors, monitoring, methodology, interactive control, accelerated methods, data interpretation) Applications of technologies associated with fatigue and their implications for structural integrity and reliability. This includes issues related to design, operation and maintenance, i.e., life cycle engineering Smart materials and structures that can sense and mitigate fatigue degradation Fatigue of devices and structures at small scales, including effects of process route and surfaces/interfaces.