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AA2524-T34铝合金的微观结构与疲劳裂纹萌生机制
引用本文:李棠,;王清远. AA2524-T34铝合金的微观结构与疲劳裂纹萌生机制[J]. 四川建材学院学报, 2009, 0(3): 23-26
作者姓名:李棠,  王清远
作者单位:[1]西南科技大学土木工程与建筑学院,四川绵阳621010; [2]四川大学力学科学工程系,四川成都610065
基金项目:西南科技大学博士基金项目(08ZX0108).致谢:本文的全部实验工作在美国肯塔基大学化学与材料工程系完成,感谢Dr.Zhai研究小组的支持与帮助,同时感谢西南科技大学博士基金(08ZX0108)项目的资助.
摘    要:通过对新型铝合金AA2524-T34的四点弯曲疲劳实验,结合光学显微镜和电子扫描电镜(SEM),对疲劳试样表面和疲劳断口进行了微观观测,研究了材料的微观结构及在不同相对湿度下材料的疲劳裂纹萌生机制。实验应力比0.1,加载频率15Hz,实验相对湿度15%和95%。结果显示实验材料呈现了完全再结晶的层状晶粒结构,晶粒沿着轧制方向被拉长,并较为平坦。不同相对湿度下,多数疲劳裂纹萌生于材料中含Fe的粗大的β相粒子,同时伴有少量的滑移带裂纹形核、材料缺陷裂纹形核等;高相对湿度下,可见裂纹沿晶界启裂。

关 键 词:铝合金  微观结构  疲劳裂纹  裂纹萌生  相对湿度

The Microstructure and Fatigue Initiation of an AA2524 -T34 Aluminum Alloy
Affiliation:LI Tang, WANG Qing-yuan ( 1. School of Civil Engineering and Architecture, Southwest University of Science and Technology, Mianyang 621010, Sichuan, China ; 2. Department of Engineering Mechanics, Sichuan University, Chengdu 610065, Sichuan , China)
Abstract:The micro structure and mechanism of fatigue initiation of an AA2524 AI alloy was investigated at the present paper. Four-point bend fatigue tests were conducted on the test alloy along the roiling direction at room temperature and frequency of 15 Hz, R =0.1, in relative humidity 15% and 95% air, combining with optical microscopy and electronic scanning microscopy (SEM) to observe the surface and fracture surface of tested samples. It was found that the flat grain was elongated along the rolling direction, showing the layer grain structure. At different relative humidity, the majority of fatigue cracks were initiated on the coarse β phase second particle, containing Fe, a few of them were formed on sites of material defects or slip bands. At high relative humidity, it could be observed the fatigue crack formed at grain boundary.
Keywords:Aluminum alloy  Micro structure  Fatigue crack  Crack initiation  Relative humidity
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