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7055铝合金T型型材的应力腐蚀行为研究
引用本文:滕奎,罗先甫,李红萍,查小琴. 7055铝合金T型型材的应力腐蚀行为研究[J]. 材料开发与应用, 2021, 36(4): 44-50
作者姓名:滕奎  罗先甫  李红萍  查小琴
作者单位:1. 上海飞机设计研究院, 上海 201210;
摘    要:通过拉伸性能测试、C环应力腐蚀试验、金相分析、扫描电镜和透射电镜观察等研究了7055铝合金T型型材的应力腐蚀开裂(SCC)行为.结果表明:7055铝合金T型型材纵向试样的抗拉强度、屈服强度、伸长率及断面收缩率均大于横向试样的;在间浸腐蚀和恒温恒湿环境下,纵向C环试样的开裂时间均长于横向试样的.型材纵向截面晶粒变形特征明...

关 键 词:7055铝合金  C环应力腐蚀  应力腐蚀开裂
收稿时间:2021-02-10

Study on Stress Corrosion Cracking Behavior of T Profiles of 7055 Aluminum Alloy
TENG Kui,LUO Xianfu,LI Hongping,ZHA Xiaoqin. Study on Stress Corrosion Cracking Behavior of T Profiles of 7055 Aluminum Alloy[J]. Development and Application of Materials, 2021, 36(4): 44-50
Authors:TENG Kui  LUO Xianfu  LI Hongping  ZHA Xiaoqin
Affiliation:1. Shanghai Aircraft Design and Research Institute, Shanghai 201210, China;2. Luoyang Ship Material Research Institute, Luoyang 471023, China;3. Henan Key Laboratory of Technology and Application of Structural Materials for Ships and Marine Equipments, Luoyang 471023, China
Abstract:The stress corrosion cracking(SCC) performance of 7055 aluminum alloy were investigated by using tensile testing, C-ring stress corrosion experiment, metallographic observation, scanning electron microscope and transmission electron microscope. The results show that longitudinal test specimen of 7055 aluminum alloy had higher tensile strength, yield strength, elongation and reduction of area than those of the transverse specimen. The cracking time of longitudinal C-ring specimens was longer than that of transverse specimens under intermediate immersion and constant temperature and humidity environment. The deformation grains were mainly elongated in the longitudinal section. The crack of the transverse sample grew along the longitudinal direction. Once the crack was formed, it grew rapidly along the elongated grain boundary, the crack was straight and the cracking time short. The grains of transverse section were equiaxial, and the crack of longitudinal sample grew along the transverse direction. In the process of crack growth, deflection along the grain boundary occurred, and the cracking time was long. The stress corrosion mechanism of 7055 alloy consisted of hydrogen embrittlement and electrochemical theory. 
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