郑洪,彭涛,舒畅,杨燕,王辉.铝合金化学氧化膜盐雾试验后腐蚀点评定方法研究[J].装备环境工程,2021,18(4):70-76. ZHENG Hong,PENG Tao,SHU Chang,YANG Yan,WANG Hui.Corrosion Evaluation Method of Aluminum alloy Chemical Oxidation Film after Salt Spray Test[J].Equipment Environmental Engineering,2021,18(4):70-76.
铝合金化学氧化膜盐雾试验后腐蚀点评定方法研究
Corrosion Evaluation Method of Aluminum alloy Chemical Oxidation Film after Salt Spray Test
投稿时间:2020-10-12  修订日期:2021-01-04
DOI:10.7643/issn.1672-9242.2021.04.010
中文关键词:  铝合金  化学氧化膜  阿洛丁1200S  腐蚀点  评定方法中图分类号:TG172 文献标识码:A 文章编号:1672-9242(2021)04-0070-07
英文关键词:aluminum alloy  chemical oxidation film  Alodine-1200S  corrosion pitting  evaluation method
基金项目:
作者单位
郑洪 航空工业成都飞机工业集团有限责任公司,成都 610091 
彭涛 航空工业成都飞机工业集团有限责任公司,成都 610091 
舒畅 西南技术工程研究所,重庆 400039 
杨燕 航空工业成都飞机工业集团有限责任公司,成都 610091 
王辉 西南技术工程研究所,重庆 400039 
AuthorInstitution
ZHENG Hong Chengdu Aircraft Industry Group Co.,Ltd., Chengdu 610091, China 
PENG Tao Chengdu Aircraft Industry Group Co.,Ltd., Chengdu 610091, China 
SHU Chang Southwest Technology and Engineering Research Institute, Chongqing 400039, China 
YANG Yan Chengdu Aircraft Industry Group Co.,Ltd., Chengdu 610091, China 
WANG Hui Southwest Technology and Engineering Research Institute, Chongqing 400039, China 
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中文摘要:
      目的 制定飞机用2024铝合金表面阿洛丁1200S化学氧化膜盐雾试验后腐蚀点的评定依据。方法 通过开展铝合金化学氧化膜盐雾试验,分别利用目视、SEM微观、能谱分析和电化学阻抗测试等手段,表征盐雾试验后的腐蚀形貌及特征。结果 试验后样品表面出现的典型腐蚀特征尺寸大于或等于0.15 mm时,正常视力的检测人员均能目视可见。目视可见的黑点、典型彗星状拖尾或只有彗星尾巴等形貌处的化学转化膜和基材已腐蚀,局部有腐蚀点的膜层,其耐蚀性大幅下降,失去对侵蚀性介质的阻挡能力。结论 仅出现不符合目视可见和基体腐蚀特征,不能判定为腐蚀点。当出现肉眼可见的黑点,典型彗星状拖尾或只有彗星尾巴等形貌,可判定为腐蚀点。在实际生产检验检测过程中,可采取类似方法研究腐蚀点的评判方法,建立铝合金表面处理盐雾试验后腐蚀图谱和腐蚀点评定准则。
英文摘要:
      The evaluation basis of corrosion point on surface of 2024 aluminum alloy for aircraft after salt spray test of alodine 1200S chemical oxide film is established.The corrosion morphology and characteristics of aluminum alloy chemical oxide film after salt spray test are characterized by visual, SEM microscopic, energy spectrum analysis and electrochemical impedance test. After the test, when the size of typical corrosion characteristics on the surface of the sample is greater than or equal to 0.15 mm, all the inspectors with normal vision can visually see it. The visible black spots, the typical cometary tail or only the comet tail and other morphologies of the chemical transformation film and substrate have been corroded, and the corrosion resistance of the film layer with local corrosion points has decreased significantly, losing the ability to block the corrosive medium. The corrosion point can not be determined as only the non-compliance with the visible and matrix corrosion characteristics. When black spots are visible to the naked eye, the typical cometary tail or only the comet tail can be judged as corrosion spots. Similar methods can be adopted to study the evaluation method of corrosion spots in the actual production inspection and test, and the corrosion maps and evaluation criteria of corrosion spots after the salt spray test of aluminum alloy surface treatment can be established.
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