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航空航天铝合金腐蚀疲劳研究进展
引用本文:李斌,董丽虹,王海斗,周永欣,高冲. 航空航天铝合金腐蚀疲劳研究进展[J]. 表面技术, 2021, 50(7): 106-118. DOI: 10.16490/j.cnki.issn.1001-3660.2021.07.010
作者姓名:李斌  董丽虹  王海斗  周永欣  高冲
作者单位:西安理工大学 材料科学与工程学院,西安 710048;陆军装甲兵学院 装备再制造技术 国防科技重点实验室,北京 100072;陆军装甲兵学院 装备再制造技术 国防科技重点实验室,北京 100072;西安理工大学 材料科学与工程学院,西安 710048;沈阳工业大学 机械工程学院,沈阳 110870
基金项目:国家自然科学基金(51535011)
摘    要:铝合金因具有高的比强度、比模量,好的加工性能及焊接性能,在航空航天领域应用广泛.而腐蚀疲劳是造成航空航天材料失效的重要原因之一,因其危害性高、破坏性强且难以提前预测等特点,受到了广泛关注.铝合金腐蚀疲劳问题一直是飞机日历寿命研究中的重点问题,随着可重复使用航天器理念的提出,多次空天往返和地面修复过程也使腐蚀疲劳问题在可...

关 键 词:航空航天  铝合金  腐蚀疲劳  腐蚀机制  环境模拟  协同/交替试验
收稿时间:2020-07-13
修稿时间:2020-12-05

Research Progress on Corrosion Fatigue of Aerospace Aluminum Alloy
LI Bin,DONG Li-hong,WANG Hai-dou,ZHOU Yong-xin,GAO Chong. Research Progress on Corrosion Fatigue of Aerospace Aluminum Alloy[J]. Surface Technology, 2021, 50(7): 106-118. DOI: 10.16490/j.cnki.issn.1001-3660.2021.07.010
Authors:LI Bin  DONG Li-hong  WANG Hai-dou  ZHOU Yong-xin  GAO Chong
Abstract:Aluminum alloys are widely used in the aerospace field due to their high specific strength, specific modulus, good workability and welding performance. Corrosion fatigue is one of the important reasons for the failure of aerospace materials. It has attracted wide attention because of its high harmfulness, strong destructiveness and difficulty in predicting in advance. The corrosion fatigue of aluminum alloy has always been a key issue in the study of aircraft calendar life. With the concept of reusable spacecraft, multiple air-to-air round trips and ground repair processes have made corrosion fatigue problems on reusable spacecraft not to be ignored. Overviews the research status of corrosion fatigue of aerospace aluminum alloys in recent years, summarize the mechanism of corrosion fatigue crack initiation and propagation from the perspective of corrosion fatigue mechanism of aviation aluminum alloys, introduces the main laboratory corrosion fatigue test technology from two aspects of corrosion fatigue environment simulation and corrosion environment equivalent. It analyze the effects of material factors, environmental factors and mechanical factors on corrosion fatigue crack growth and life, focusing on the characteristics of fatigue life under the alternate form of corrosion fatigue. It is proposed that corrosion fatigue crack growth, damage evolution and life prediction under the combined influence of multiple factors, as well as the equivalent equivalent of accelerated corrosion environment, and the organic combination of test and simulation are important development directions for aluminum alloy corrosion fatigue in the future.
Keywords:aerospace  aluminum alloy   corrosion fatigue   corrosion mechanism   environmental simulation   pre-corrosion fatigue   alternating corrosion fatigue   collaborative/alternating test
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