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7A04铝合金应力腐蚀过程中裂纹萌生和扩展规律研究
引用本文:方艺斌,杜娟,陈翘楚,田辉.7A04铝合金应力腐蚀过程中裂纹萌生和扩展规律研究[J].材料科学与工艺,2017,25(5):86-92.
作者姓名:方艺斌  杜娟  陈翘楚  田辉
作者单位:中国民航大学 中欧航空工程师学院,天津,300300
摘    要:为了研究不同拉伸速率对应力腐蚀敏感性及应力腐蚀过程(SCC)中裂纹萌生与扩展规律的影响,本文选用7A04铝合金在3.5%wt NaCl溶液中进行慢应变速率拉伸实验(SSRT),采用扫描电子显微镜(SEM)、体式显微镜、电化学方法、高分辨透射电子显微镜(HRTEM)等方法进行研究;提出一种原位预测裂纹萌生和扩张的新方法即相移与电化学阻抗谱相结合的方法来系统研究应力腐蚀过程(SCC)中裂纹萌生和扩展规律.结果表明:当拉伸速率为3.0 um/min时,在3 h附近裂纹开始萌生,在8 h附近裂纹发生明显扩展;通过高分辨透射电子显微镜(HRTEM)对裂纹萌生和扩展机理进行研究,验证了新方法的可行性,推测裂纹的萌生和扩展机理可能是由晶界出产生的析出物引起的.

关 键 词:金属材料  应力腐蚀敏感性  电化学阻抗谱  7A04铝合金
收稿时间:2016/10/27 0:00:00

Research on crack initiation and propagation of 7A04 aluminium alloy during the stress corrosion crack
FANG Yibin,DU Juan,CHEN Qiaochu and TIAN Hui.Research on crack initiation and propagation of 7A04 aluminium alloy during the stress corrosion crack[J].Materials Science and Technology,2017,25(5):86-92.
Authors:FANG Yibin  DU Juan  CHEN Qiaochu and TIAN Hui
Affiliation:Sino-European Institute of Aviation Engineering,Civil Aviation University of China, Tianjin, 300300, China,Sino-European Institute of Aviation Engineering,Civil Aviation University of China, Tianjin, 300300, China,Sino-European Institute of Aviation Engineering,Civil Aviation University of China, Tianjin, 300300, China and Sino-European Institute of Aviation Engineering,Civil Aviation University of China, Tianjin, 300300, China
Abstract:To investigate the effect of different tensile rates on stress corrosion sensitivity and the crack initiation and propagation during the stress corrosion crack ( SCC) , the slow strain rate test ( SSRT) of 7A04 aluminum alloy in 3.5%wt NaCl solution was conducted and scanning electron microscope ( SEM ) , stereomicroscope, electrochemical method and high resolution transmission electron microscope ( HRTEM ) were used for this research. Meanwhile, a new method for the combination of phase shift and electrochemical impedance spectroscopy was proposed to study the crack initiation and propagation during SCC. The results showed that the crack initiated in the vicinity of 3 h and propagated at near 8 h with the tensile rate of 3.0 um/min;the feasibility of the new method was also verified by studying mechanism of crack initiation and propagation using high resolution transmission electron microscopy ( HRTEM ) and it ' s speculated that the mechanism of crack initiation and propagation may be caused by the precipitates produced at grain boundaries.
Keywords:metallic materials  stress corrosion sensitivity  electrochemical impendance spectroscopy  7A04 aluminum alloy
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