• CN:11-2187/TH
  • ISSN:0577-6686

机械工程学报 ›› 2020, Vol. 56 ›› Issue (16): 33-43.doi: 10.3901/JME.2020.16.033

• 材料科学与工程 • 上一篇    下一篇

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拉扭应力幅比对LZ50钢短裂纹行为的影响

杨冰, 代胜, 廖贞, 孟飞, 肖守讷, 阳光武, 朱涛   

  1. 西南交通大学牵引动力国家重点实验室 成都 610031
  • 收稿日期:2019-12-11 修回日期:2020-03-23 出版日期:2020-08-20 发布日期:2020-10-19
  • 作者简介:杨冰,男,1979年出生,博士,研究员,博士研究生导师。主要研究方向为结构强度理论与可靠性、材料疲劳与断裂。E-mail:yb@swjtu.edu.cn
  • 基金资助:
    国家自然科学基金(51675446)和牵引动力国家重点实验室自主课题(2019TPL-13)资助项目。

Influence of Tension-torsion Stress Amplitude Ratio on Short Fatigue Crack Behaviour of LZ50 Steel

YANG Bing, DAI Sheng, LIAO Zhen, MENG Fei, XIAO Shoune, YANG Guangwu, ZHU Tao   

  1. State Key Laboratory of Traction Power, Southwest Jiaotong University, Chengdu 610031
  • Received:2019-12-11 Revised:2020-03-23 Online:2020-08-20 Published:2020-10-19

摘要: 在保持等效应力幅一致的前提下,开展LZ50钢在7种不同拉扭应力幅比(λ)载荷作用下的疲劳短裂纹复型试验。结果表明,拉扭应力幅比的变化未改变短裂纹萌生与扩展总体规律。裂纹均萌生于铁素体晶粒内部或晶界处,在微观短裂纹阶段受铁素体晶界和珠光体带状结构边界阻碍,扩展速率出现两次较明显下降;进入物理短裂纹阶段后,微观结构对裂纹扩展影响减弱,扩展速率持续上升。同时,随着拉扭应力幅比减小,相同短裂纹尺度下的扩展速率下降,断裂面与试样轴向的夹角逐渐减小,裂纹由单源萌生逐渐过渡为多源萌生,试样疲劳寿命呈增加趋势。此外,通过构建拉扭应力幅比—寿命曲线方程,证明相同等效应力幅条件下,轴向拉压载荷对材料的疲劳损伤贡献大于扭转载荷,且随着拉扭应力幅比的减小,试样疲劳寿命提高的程度不断增强。

关键词: 疲劳短裂纹, 拉扭载荷, 应力幅比, LZ50钢

Abstract: Short fatigue crack replica tests of LZ50 axle steel were carried out under seven different tension-torsion stress ratios, λ, at the same equivalent stress amplitude. The results show that, the change of tension-torsion stress ratio does not change the general trend of the short fatigue crack initiation and growth. The short fatigue cracks mostly initiate in the inner or at the boundary of the ferrite grains. At the microstructurally short crack(MSC) stage, there are two obvious drops of crack growth rate due to the inhibition of ferrite grain boundary and pearlite banded structure, while at the physically short crack(PSC) stage, the microstructure of the material has a less effect on crack growth and the growth rate increases continuously. Meanwhile, with the decrease of the stress amplitude ratio, both the crack growth rate at the same crack size and the angle between the fatigue fracture surface and the specimen axial direction gradually decrease. The initiation of the crack transforms from a single-crack-source mode to a multi-crack-source mode, and the fatigue life is increasing. Furthermore, by constructing a stress amplitude ratio and fatigue life curve equation, it is proved that with the same equivalent stress amplitude, the axial tensile-compression load contributes more to the fatigue damage of the material than the torsion load. As the stress amplitude ratio decreases, the increasing trend of the fatigue life increases.

Key words: short fatigue crack, tension-torsion load, stress amplitude ratio, LZ50 steel

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