史洪微,崔常京,韦涛,陈群志,刘福春,韩恩厚.严酷环境下飞机典型结构异种材料电偶腐蚀特点与防护对策[J].装备环境工程,2020,17(5):52-57. SHI Hong-wei,CUI Chang-jing,WEI Tao,CHEN Qun-zhi,LIU Fu-chun,HAN En-hou.Behaviours and Protective Measures of Galvanic Corrosion on Dissimilar Materials of Typical Aircraft Structure in Harsh Environment[J].Equipment Environmental Engineering,2020,17(5):52-57.
严酷环境下飞机典型结构异种材料电偶腐蚀特点与防护对策
Behaviours and Protective Measures of Galvanic Corrosion on Dissimilar Materials of Typical Aircraft Structure in Harsh Environment
投稿时间:2019-05-20  修订日期:2019-06-20
DOI:10.7643/issn.1672-9242.2020.05.008
中文关键词:  电偶腐蚀  电偶电流  铝合金  防护措施
英文关键词:galvanic corrosion  galvanic current  aluminium alloy  protective measure
基金项目:国家自然科学基金(51571202)
作者单位
史洪微 中国科学院金属研究所 中国科学院核用材料与安全评价重点实验室,沈阳 110016 
崔常京 北京航空工程技术研究中心,北京 100076 
韦涛 中国科学院金属研究所 中国科学院核用材料与安全评价重点实验室,沈阳 110016 
陈群志 北京航空工程技术研究中心,北京 100076 
刘福春 中国科学院金属研究所 中国科学院核用材料与安全评价重点实验室,沈阳 110016 
韩恩厚 中国科学院金属研究所 中国科学院核用材料与安全评价重点实验室,沈阳 110016 
AuthorInstitution
SHI Hong-wei Key Laboratory of Nuclear Materials and Safety Assessment, Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China 
CUI Chang-jing Beijing Aeronautical Technology Research Center, Beijing 100076, China 
WEI Tao Key Laboratory of Nuclear Materials and Safety Assessment, Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China 
CHEN Qun-zhi Beijing Aeronautical Technology Research Center, Beijing 100076, China 
LIU Fu-chun Key Laboratory of Nuclear Materials and Safety Assessment, Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China 
HAN En-hou Key Laboratory of Nuclear Materials and Safety Assessment, Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China 
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中文摘要:
      介绍了电偶腐蚀的原理,以飞机结构上容易出现的三种电偶腐蚀(碳纤维增强环氧复合材料-铝合金、钛合金-铝合金、铝合金-不锈钢)为例,对目前关于这三种电偶腐蚀的研究进行了综述,分析了电偶腐蚀的环境影响因素,综述了耦合材料的失效特点和形式,探讨了利用阻隔、涂层和缓蚀剂等手段减缓和防止电偶的防护措施,指出利用微区测试技术、联合多种研究手段和复合环境因素在研究电偶腐蚀方面的重要性。在多因素条件下,设计模拟耦合件的试验,有利于模拟实际工况的特征。
英文摘要:
      This paper introduced the mechanism of galvanic corrosion. The study on three typical types of galvanic corrosion prone to happen in aircraft structure (carbon fiber reinforced epoxy composite-aluminium alloy, titanium alloy-aluminium alloy, aluminium alloy-stainless steel) was reviewed. The influence of environmental factors on galvanic corrosion was analyzed and the failure characteristics and behaviors of coupling materials were given. The protective measures for mitigation of galvanic corrosion, such as separation, coatings and inhibitors were reviewed. The use of micro-zone techniques, the combination of multi-methods and the consideration of environmental factors are important to research galvanic corrosion. Under multi-factors, the design of simulated galvanic components is beneficial to simulate the actual working conditions.
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