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不同应力幅比加载下2A12铝合金的多轴疲劳性能

陈亚军 王先超 王付胜 周剑 吴悦雷

材料工程2017,Vol.45Issue(9):136-142,7.
材料工程2017,Vol.45Issue(9):136-142,7.DOI:10.11868/j.issn.1001-4381.2016.000817

不同应力幅比加载下2A12铝合金的多轴疲劳性能

Multiaxial Fatigue Properties of 2A12 Aluminum Alloy Under Different Stress Amplitude Ratio Loadings

陈亚军 1王先超 1王付胜 1周剑 1吴悦雷1

作者信息

  • 1. 中国民航大学 中欧航空工程师学院,天津 300300
  • 折叠

摘要

Abstract

The multiaxial fatigue behavior of 2A12 aluminum alloy was studied with SDN100/1000 electro-hydraulic servo tension-torsion fatigue tester under different stress amplitude ratios, the fracture morphology and the fatigue loading curve were observed to study the failure mechanism.The results show that, under the one stage loading condition, the fatigue life prolongs with the stress amplitude ratio increasing.Under pure torsion loading, smooth and even area exists in the fracture surface.As the stress amplitude ratio increases, the number of scratch reduces, the fatigue striation and some special morphology such as the fishbone pattern, scale pattern and honeycomb pattern can be observed;under cumulative paths of different stress amplitude ratios, the variation of multiaxial fatigue life changes with first stage loading cycles;under cumulative paths of high-low stress amplitude ratio, the cycle hardening occurs obviously in the axial direction for the first stage high stress amplitude ratio loading and 2A12 alloy shows training effect.

关键词

2A12铝合金/应力幅比/多轴疲劳/失效机理/锻炼效应

Key words

2A12 aluminum alloy/stress amplitude ratio/multiaxial fatigue/failure mechanism/training effect

分类

数理科学

引用本文复制引用

陈亚军,王先超,王付胜,周剑,吴悦雷..不同应力幅比加载下2A12铝合金的多轴疲劳性能[J].材料工程,2017,45(9):136-142,7.

基金项目

国家自然科学基金项目(11502285) (11502285)

中央高校基本科研业务费中国民航大学专项资金项目(3122017112) (3122017112)

材料工程

OA北大核心CSCDCSTPCD

1001-4381

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