王辉,宣卫芳,刘静,赵方超.飞机蒙皮用含氟聚氨酯涂层老化原因分析[J].装备环境工程,2011,8(5):43-46. WANG Hui,XUAN Wei-fang,LIU Jing,ZHAO Fang-chao.Weathering Analysis of Fluorine Containing Polyurethane Coating for Aircraft Skin[J].Equipment Environmental Engineering,2011,8(5):43-46.
飞机蒙皮用含氟聚氨酯涂层老化原因分析
Weathering Analysis of Fluorine Containing Polyurethane Coating for Aircraft Skin
投稿时间:2011-04-15  修订日期:2011-10-15
DOI:
中文关键词:  飞机蒙皮  含氟聚氨酯涂层  实验室模拟加速试验  电化学阻抗谱
英文关键词:aircraft skin  fluorinated polyurethane coating  laboratory simulated accelerated test  EIS
基金项目:
作者单位
王辉 1. 中国兵器工业第五九研究所,重庆 400039;2. 重庆市环境腐蚀与防护工程技术研究中心,重庆 400039 
宣卫芳 1. 中国兵器工业第五九研究所,重庆 400039;2. 重庆市环境腐蚀与防护工程技术研究中心,重庆 400039 
刘静 1. 中国兵器工业第五九研究所,重庆 400039;2. 重庆市环境腐蚀与防护工程技术研究中心,重庆 400039 
赵方超 1. 中国兵器工业第五九研究所,重庆 400039;2. 重庆市环境腐蚀与防护工程技术研究中心,重庆 400039 
AuthorInstitution
WANG Hui 1. No.59 Institute of China Ordnance Industry, Chongqing 400039, China;2. Chongqing Engineering Research Center for Environmental Corrosion and Protection, Chongqing 400039, China 
XUAN Wei-fang 1. No.59 Institute of China Ordnance Industry, Chongqing 400039, China;2. Chongqing Engineering Research Center for Environmental Corrosion and Protection, Chongqing 400039, China 
LIU Jing 1. No.59 Institute of China Ordnance Industry, Chongqing 400039, China;2. Chongqing Engineering Research Center for Environmental Corrosion and Protection, Chongqing 400039, China 
ZHAO Fang-chao 1. No.59 Institute of China Ordnance Industry, Chongqing 400039, China;2. Chongqing Engineering Research Center for Environmental Corrosion and Protection, Chongqing 400039, China 
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中文摘要:
      选用飞机蒙皮常用的含氟聚氨酯涂层体系为研究对象, 结合飞机服役环境的主要特点, 开展了实验室模拟加速老化试验研究, 并利用电化学阻抗谱对老化试验后的涂层进行了表征。结果表明, 紫外线仅对涂层的表面结构产生影响, 紫外试验后的涂层电阻下降较慢。在紫外-盐雾循环试验中, 紫外线引起涂层表面结构发生变化, 涂层的耐水性变差, 水更快地进入涂层内部, 引起涂层内部结构发生变化, 循环试验后的涂层电阻下降较快。紫外线和露水的综合作用是造成飞机蒙皮有机涂层出现严重老化的主要原因。
英文摘要:
      Fluorinated polyurethane coating system commonly applied in aircraft skin was selected as the research object. Laboratory accelerated test of fluorinated polyurethane coatings was carried out according to the main features of environmental factors in service area. The tested coatings were characterized by means of EIS after test. Results showed that UVA effects only on of the coating surface structure; the coating resistance drops slowly after UV test. In UV-salt spray cyclic test, the coating surface structure changes under UVA, water resistance of coatings become worse, and water permeates into the interior of coating faster, then coating internal structure changes, the coating resistance drops more rapidly after cyclic test. The main reason for organic coating of aircraft skin appearing serious aging is comprehensive effect of UV and dew.
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