潘峤,杨丽媛,孙志华,骆晨,刘明,高蒙,高建,汤智慧.涂漆铝合金铆接件在美济礁大气环境中初期失效行为[J].装备环境工程,2019,16(7):13-17. PAN Qiao,YANG Li-yuan,SUN Zhi-hua,LUO Chen,LIU Ming,GAO Meng,GAO Jian,TANG Zhi-hui.Degradation Behaviors of Coated Riveted Structure during the Early Stages of Exposing to Marine Atmospheric Environment at Mischief Reef[J].Equipment Environmental Engineering,2019,16(7):13-17.
涂漆铝合金铆接件在美济礁大气环境中初期失效行为
Degradation Behaviors of Coated Riveted Structure during the Early Stages of Exposing to Marine Atmospheric Environment at Mischief Reef
投稿时间:2019-02-14  修订日期:2019-07-25
DOI:10.7643/ issn.1672-9242.2019.07.003
中文关键词:  铆接结构  涂层  铆钉  电化学
英文关键词:riveted structure  coating  rivet  electrochemical
基金项目:“十三五”技术基础科研项目(JSHS2016207A002-2)
作者单位
潘峤 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
杨丽媛 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
孙志华 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
骆晨 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
刘明 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
高蒙 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
高建 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
汤智慧 中国航发北京航空材料研究院 中国航空发动机集团航空材料先进腐蚀与防护重点实验室,北京 100095 
AuthorInstitution
PAN Qiao Key Laboratory of Science and Technology on advanced Corrosion and Protection for Aviation Material, Aero Engine Corpo-ration of China Aviation, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
YANG Li-yuan Key Laboratory of Science and Technology on advanced Corrosion and Protection for Aviation Material, Aero Engine Corpo-ration of China Aviation, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
SUN Zhi-hua Key Laboratory of Science and Technology on advanced Corrosion and Protection for Aviation Material, Aero Engine Corpo-ration of China Aviation, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
LUO Chen Key Laboratory of Science and Technology on advanced Corrosion and Protection for Aviation Material, Aero Engine Corpo-ration of China Aviation, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
LIU Ming Key Laboratory of Science and Technology on advanced Corrosion and Protection for Aviation Material, Aero Engine Corpo-ration of China Aviation, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
GAO Meng Key Laboratory of Science and Technology on advanced Corrosion and Protection for Aviation Material, Aero Engine Corpo-ration of China Aviation, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
GAO Jian Key Laboratory of Science and Technology on advanced Corrosion and Protection for Aviation Material, Aero Engine Corpo-ration of China Aviation, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
TANG Zhi-hui Key Laboratory of Science and Technology on advanced Corrosion and Protection for Aviation Material, Aero Engine Corpo-ration of China Aviation, AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China 
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中文摘要:
      目的 研究铆接结构件在南海热带岛礁海洋大气环境暴露初期的失效行为。方法 通过对在热带岛礁大气环境中暴露初期的试样进行外观拍照、光泽度测试、色差测试、光学显微拍照、以及电化学阻抗测试(EIS),描述相关变化过程。结果 试样暴露1 a后,失光率和色差分别达到67.0%和10.67,平面位置呈现出沟壑状形貌特征,连接缝隙底部和铆钉顶部存在明显的涂层缺陷。平面位置0.01 Hz处的阻抗模值由初始的2.81×1010 Ω降低为8.19×108 Ω,而铆钉位置0.01 Hz处的阻抗模值由初始的1.09×109 Ω降低为2.92×106 Ω。结论 试样在热带岛礁大气环境暴露初期的外观变化主要表现为失光和变色,平面位置、连接缝隙底部及铆钉顶部均存在一定程度的微观形貌变化。随暴露时间的增加,电化学阻抗呈下降趋势,且铆钉位置的下降幅度相对更大。
英文摘要:
      Objective To study on the degradation behaviors of coated riveted structure during the early stage of exposing to marine atmospheric environment at a tropical island. Methods Relevant changes were described by analyzing relevant data of macro photos, glossiness, chromatic aberration, optical micro images and EIS of specimens in the early stage of exposing to marine atmospheric environment at a tropical island. Results It was found that the glossiness loss rate and the chromatic aberration of the specimens exposed for 1 year were 67.0% and 10.67, respectively. Some ravines- and gullies-liked patterns can be seen at flat area, while defects can be found in the coatings at rivet and crevice. Additionally, the impedance magnitude of flat area at 0.01 Hz was changed from 2.81×1010 Ω to 8.19×108 Ω. Meanwhile, that data at rivet was changed from 1.09×109 Ω to 2.92×106 Ω. Conclusion The appearance change of specimens exposed to marine atmospheric environment at a tropical island are mainly embodied on glossiness loss and color change. Certain morphology change can be found on the coatings at flat area, rivet and crevice. In addition, the impedance decreases with the increase of the exposure time. Nevertheless, it has a relatively larger decrease range at rivet compared to that at flat area.
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