摘要
通过对2024-T3铝合金进行不同时长条件下的预腐蚀疲劳试验,拟合得出了2024-T3铝合金DFR(Detail Fatigue Rating)随腐蚀时长的变化曲线,并通过对2024-T3铝合金预腐蚀后的疲劳断口分析,得到了2024-T3铝合金疲劳性能退化过程的一些基本特点和规律。对于掌握2024-T3铝合金的DFR退化规律,做好飞机结构的腐蚀防护有重要的参考和借鉴作用。
The degradation law of DFR of 2024-T3 aluminum alloy was determined by different pre-corrosion fatigue tests, and the fatigue fraeture of 2024-T3 aluminum alloy was analyzed by scanning electron microscope, the basic characteristics and laws of degenerate failure process of 2024-T3 aluminum alloy was studied by it. It is of great reference signifieanee for mastering the degradation law of DFR of 2024-T3 aluminum alloy and the eon＇osion protection of aircraft.
作者
陈跃良
吴省均
张勇
卞贵学
张柱柱
CHEN Yueliang;WU Xingjun;ZHANG Yong;BIAN Guixue;ZHANG Zhuzhu(Qingdao Branch of Naval Aviation University,Qingdao Shandong 266041,China)
出处
《海军航空工程学院学报》
2018年第4期376-382,422,共8页
Journal of Naval Aeronautical and Astronautical University
基金
国家自然科学基金资助项目(51375490)
