The Mechanism of Internal Fatigue-Crack Initiation in a Titanium Alloy with Lamellar and Equiaxed Microstructure

Xiangnan Pan, Shouwen Xu, G. Qian, A. Nikitin, A. Shanyavskiy, T. Palin-Luc, Youshi Hong
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引用次数: 1

Abstract

Traditionally, the primary or equiaxed α grains of titanium alloys are regarded as the defects to cause crack initiation due to their cyclic brittleness, and fatigue cracks will initiate from the α grains rather than the lamellar microstructure (LM) clusters. Here, we found that fatigue crack is prone to initiate from a large microstructure domain of a big α+β cluster or an α grain in a titanium alloy with the composition of coarse LM clusters and fine equiaxed α grains. Then, the mechanisms of crack initiation for the cases of high-cycle fatigue and very-high-cycle fatigue under stress ratio R = -1, 0.1 and 0.5 are addressed, showing that the numerous cyclic pressing process dominates the microstructure evolution with grain size refinement and nanograin formation underneath the fracture surfaces in the crack initiation region under negative stress ratios.
层状等轴组织钛合金内部疲劳裂纹萌生机制研究
传统上认为,钛合金的初晶或等轴α晶粒具有循环脆性,是导致裂纹萌生的缺陷,而不是由片层组织(LM)团簇引发疲劳裂纹。研究发现,在由粗LM晶簇和细等轴α晶组成的钛合金中,疲劳裂纹容易由大α+β晶簇或α晶粒组成的大组织域引发。分析了应力比R = -1、0.1和0.5时高周疲劳和超高周疲劳的裂纹起裂机理,结果表明:负应力比下裂纹起裂区域的微观组织演化主要由多次循环挤压过程主导,晶粒细化,断面下形成纳米晶粒;
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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