载荷比、间隙含量和晶粒尺寸对α-钛合金低应力疲劳裂纹扩展的影响

J. Robinson, C. Beevers
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引用次数: 93

摘要

摘要对三种市售纯α-钛合金进行了低应力疲劳裂纹扩展试验。在研究的∆K范围内(4 ~ 20 MN/m2),减小载荷比(R)、增大晶粒尺寸和增加间隙合金含量均能显著降低合金的生长率。得出的结论是,疲劳断裂过程包括两个阶段:(1)相对平面切面的形成(主要由∆K控制)和(2)它们通过塑性撕裂机制相互连接(主要由K最大值控制)。对疲劳断口表面的扫描电镜检查表明,单个晶粒的取向对断口表面形貌有相当大的影响。当裂纹尖端的反向塑性规模等于或小于晶粒尺寸时,就会出现这种效应。所有试样的断口表面形貌都以近似恒定的生长速率发生转变。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The Effects of Load Ratio, Interstitial Content, and Grain Size on Low-Stress Fatigue-Crack Propagation in α-Titanium
AbstractLow-stress fatigue-crack-propagation tests have been carried out on three commercially pure α-titaniumalloys. It was found that decreasing load ratio (R), increasing grain size, and increasing interstitial alloying content could all produce significant reductions in growth rate over the ∆K range studied (4–20 MN/m2). The conclusion was reached that the fatigue-fracture process comprised two stages: (1) the formation of relatively planar facets (primarily ∆K-controlled) and (2) their interconnection by a mechanism involving plastic tearing (primarily K max-controlled). Scanning electron microscope examination of the fatigue-fracture surfaces revealed that the orientations of individual grains exerted a considerable influence on fracture-surface morphology. This effect occurred when the scale of reversed plasticity at the crack tip was of the order of, or less than, the grain size. A transition in fracturesurface appearance occurred in all specimens at an approximately constant value of growth rate ...
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