Influence of Pre-stress Corrosion on Fatigue Life of 2A12-T4 Aluminum Alloy
摘 要
进行了两种温度三种应力水平下2A12-T4铝合金试样在EXCO溶液中不同浸泡时间的预应力腐蚀试验, 而后进行疲劳试验至试件断裂。采用多元方差分析, 确定了腐蚀温度、浸泡时间和应力水平是影响试件疲劳寿命的显著因素, 三者的共同作用会加剧试样的腐蚀, 降低试样的疲劳寿命。根据试验结果, 采用回归算法, 建立了以腐蚀温度、浸泡时间和应力水平三参数表征的剩余疲劳寿命计算模型, 理论值与试验值对比, 二者误差约为25%。通过扫描电镜观察, 分析了腐蚀温度、浸泡时间和应力水平对试件微观损伤的机理。
Abstract
Pre-stress corrosion experiments of 2A12-T4 aluminum alloy under two kinds of temperature, three kinds of stress level and different immersion times in EXCO solution were conducted, and then fatigue experiment was implemented to calculate the fatigue life. Multi-variance analysis showed that the corrosion temperature, immersion time and stress level were remarkable factors affecting the fatigue life. Corrosion is being aggravated by the three effects working together, and the fatigue life is reduced. A residual fatigue life calculation model, token with corrosion temperature, immersion time and stress level, was established by regression arithmetic based on the test results. Comparing theoretical values and experimental datas, the errors are about 25%. The fracture surface was observed by SEM, the microscopic damage mechanism of temperature, immersion time and stress level were analyzed.
中图分类号 TG172.9 V215.5+2
所属栏目 试验研究
基金项目 国家自然科学基金(50975284)
收稿日期 2012/8/15
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备注王晓光,硕士研究生,
引用该论文: WANG Xiao-guang,HE Yu-ting,ZHANG Hai-wei,JIAO Sheng-bo,FENG Yu,KANG Qing-shan. Influence of Pre-stress Corrosion on Fatigue Life of 2A12-T4 Aluminum Alloy[J]. Corrosion & Protection, 2013, 34(6): 475
被引情况:
【1】李晓虹,何宇廷,张腾,李昌范, "腐蚀/疲劳交替作用下2A12-T4铝合金的损伤特性",机械工程材料 39, 62-66(2015)
【2】张春晓,石晓磊, "腐蚀条件下基于残差修正的飞机结构寿命灰色马氏链预测",腐蚀与防护 37, 230-235(2016)
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【5】Frederic Menan,Gilbert Henaff. Synergistic action of fatigue and corrosion during crack growth in the 2024 aluminium alloy[J]. Procedia Engineering,2010,2(1):1441-1450.
【6】张有宏. 飞机结构的腐蚀损伤及其对寿命的影响[D]. 西安: 西北工业大学硕士学位论文,2007.
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【8】何建平,樊蔚勋,袁庆铭. 慢应变速率下铝合金的腐蚀行为[J]. 中国腐蚀与防护学报,2003,23(1):17-20.
【9】刘文珽, 李玉海. 飞机结构日历寿命体系评定技术[M]. 北京: 航空工业出版社, 2004.
【10】仝基斌, 饶思贤, 朱立群,等. 有/无应力下LY12CZ铝合金点蚀数据的关联规律[J]. 中国腐蚀与防护学报, 2009, 29(6): 504-508.
【11】饶思贤, 张玉波, 朱立群,等. 外加应力下的LY12CZ电化学行为[J]. 北京航空航天大学学报, 2007, 33(10): 1246-1249.
【12】Liu X D,Frankel G S. Effects of compressive stress on localized corrosion in AA20242T3[J]. Corrosion Science,2006,48(10):3309-3329.
【13】程宗辉. LY12CZ铝合金飞机构件腐蚀行为研究[D]. 哈尔滨: 哈尔滨工程大学研士学位论文, 2006.
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