期刊文献+

室温大气环境下不同时效态2A12合金的疲劳行为 被引量:5

Fatigue Behavior of 2A12 Alloy at Different Aged States in Air
下载PDF
导出
摘要 在拉-压疲劳试验机上对室温大气环境下欠时效态、峰时效态、过时效态和自然时效态2A12合金的疲劳行为进行研究,并采用扫描电镜(SEM)分析室温大气环境下不同时效态对疲劳断口形貌的影响。结果表明:在室温大气环境下,四种时效态2A12合金的疲劳断裂循环次数均随着循环应力的减小而明显增加。循环应力水平越低,疲劳寿命提高越明显;各时效态的疲劳断口均为穿晶断口。断口中均出现疲劳条纹、台阶和韧窝,并在较低循环应力下,疲劳条纹出现的区域较多;欠时效态和峰时效态断口上还可观察到轮胎花样。自然时效态表现出最好的疲劳裂纹扩展阻力,其次是欠时效态、峰时效态,过时效态的疲劳裂纹扩展阻力最低。对室温大气环境下各时效态2A12合金疲劳行为进行了讨论。 The fatigue behavior of under aged, peak-aged,over-aged and nature-aged 2A12 alloy in air at room temperature was investigated using a tension compression fatigue testing machine. The effect of air on the fatigue fractures was studied by means of scanning electron microscopy (SEM). The results showed that the cycle number of fatigue breakdown increased obviously with the cyclic stress decreasing for each aged 2A12 alloy, the lower the cyclic stress level , the more obvious increased the fatigue lifetime, in atmospheric environment with a room temperature. The fractures of every-aged state in air at room temperature are transgranulars, in which fatigue striations, steps and dimples are observed, and more areas with fatigue striations exist under lower cyclic stresses. Tyre-like patterns are observed on fatigue fractures in air for the under-aged and peak-aged. The best fatigue crack growth resistance is revealed at the natural aging state, then it is decreasing in order of the under-aged ,peakaged state and the over-aged state. The reason for the effect of air on the fatigue behavior of everyaged 2A12 alloy was discussed.
出处 《材料工程》 EI CAS CSCD 北大核心 2009年第12期67-71,共5页 Journal of Materials Engineering
基金 国家重点基础研究发展规划资助项目(G1999065005)
关键词 2A12合金 时效 空气环境 疲劳行为 2A12 alloy aged air environment fatigue behavior
  • 相关文献

参考文献7

  • 1VINOGADOV A, HASHIMOTO S, MIURA S. Fatigue crack initiation and propagation in [210] oriented copper single crystals in vacuum and in air[J]. Scripta Mat, 1996,34: 775-779.
  • 2KICHIRO ENDO, KENJIRO KOMAI. Fatigue crack propagalion in an aluminum alloy in ultra-high vacuum[J]. J Soc Mater and Sci Japan ,1977,26:143-148.
  • 3KHIREDDINE D, KHIREDDINE M H. Low cycle fatigue be havior of an aluminium alloy with small shearable precipitates[J]. Effect of Surface Coating, 2000,22 : 585- 591.
  • 4VERKIN B I, GRINBERG N M. The effect of vacuum on the fatigue behavior of metals and alloys[J]. Mater Sci Eng, 1979,41: 149-181.
  • 5WANG R, MUGHRABI H. Fatigue of copper single crystals in vacuum and in air[J]. Mater Sci Eng, 1984,65:219-243.
  • 6SLIVIK DC, BLANKENSHIP CP, STARKE JR E A, et al. Intrinsic fatigue crack growth rates for Al-Li- Cu- Mg alloys in vacuum[J]. Metal Trans,1993,22(3) :1807-1817.
  • 7亨利G 豪斯特曼D.宏观断口学及显微断口学[M].北京:机械工业出版社,1990..

共引文献17

同被引文献43

引证文献5

二级引证文献22

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部