孙志华,高健,王强,王志申.Al-Cu-Mg系铝合金耐环境腐蚀性能研究[J].装备环境工程,2015,12(4):27-31. SUN Zhi-hua,GAO Jian,WANG Qiang,WANG Zhi-shen.Corrosion Behavior of Al-Mg-Cu Aluminum Alloy[J].Equipment Environmental Engineering,2015,12(4):27-31.
Al-Cu-Mg系铝合金耐环境腐蚀性能研究
Corrosion Behavior of Al-Mg-Cu Aluminum Alloy
投稿时间:2015-05-11  修订日期:2015-08-15
DOI:10.7643/issn.1672-9242.2015.04.006
中文关键词:  2D12铝合金  晶间腐蚀  剥蚀  应力腐蚀
英文关键词:2D12 aluminum alloy  intergranular corrosion  exfoliation  stress corrosion cracking
基金项目:
作者单位
孙志华 中航工业北京航空材料研究院 航空材料先进腐蚀与防护航空科技重点实验室,北京 100095 
高健 中航工业北京航空材料研究院 航空材料先进腐蚀与防护航空科技重点实验室,北京 100095 
王强 中航工业北京航空材料研究院 航空材料先进腐蚀与防护航空科技重点实验室,北京 100095 
王志申 中航工业北京航空材料研究院 航空材料先进腐蚀与防护航空科技重点实验室,北京 100095 
AuthorInstitution
SUN Zhi-hua AVIC Beijing Institute of Aeronautical Materials,Aviation Key Laboratory of Science and Technology on advanced Corrosion and Protection for Aviation Material,Beijing 100095,China 
GAO Jian AVIC Beijing Institute of Aeronautical Materials,Aviation Key Laboratory of Science and Technology on advanced Corrosion and Protection for Aviation Material,Beijing 100095,China 
WANG Qiang AVIC Beijing Institute of Aeronautical Materials,Aviation Key Laboratory of Science and Technology on advanced Corrosion and Protection for Aviation Material,Beijing 100095,China 
WANG Zhi-shen AVIC Beijing Institute of Aeronautical Materials,Aviation Key Laboratory of Science and Technology on advanced Corrosion and Protection for Aviation Material,Beijing 100095,China 
摘要点击次数:
全文下载次数:
中文摘要:
      目的 研究2D12铝合金耐环境腐蚀性能。方法 对不同规格的Al-Cu-Mg系2D12铝合金的耐环境腐蚀性能包括晶间腐蚀、 剥蚀性能以及抗应力腐蚀性能, 按照标准试验方法进行测试、 分析、 评定试验数据。结果 得到了不同规格2D12铝合金晶间腐蚀深度、 剥蚀等级、 应力腐蚀断裂时间及 KISCC 等。自然时效状态 2D12 铝合金具有晶间腐蚀倾向, 最大晶间腐蚀深度为 0.18 mm。不同规格2D12铝合金抗剥落腐蚀性倾向不同, 从P级到EC级。2D12铝合金材料的拉伸应力腐蚀断裂寿命随试验应力的增加而降低, 两种薄板(δ=1.5 mm和δ=2.0 mm)和型材(EL2805)临界应力腐蚀门槛值分别为160, 140, 230 MPa。2D12铝合金在S-L和S-T方向的应力腐蚀开裂门槛应力强度因子分别为22.6 MPa·m1/2和27.1 MPa·m1/2。结论 2D12铝合金抗应力腐蚀测试结果表明,S-L方向比S-T方向的抗应力腐蚀的性能低, 其应力腐蚀开裂门槛应力强度因子与C环应力腐蚀结果一致, 断口呈现典型的沿晶断裂应力腐蚀脆性断裂特征。
英文摘要:
      Objective To study the anti-environment corrosion properties of 2D12 alloy. Methods According to the standard test methods, the corrosion tests including intergranular corrosion test, exfoliation test and stress corrosion cracking test were carried out for 2D12 Al-Mg-Cu aluminum alloys with different specifications, and the test data was analyzed and evaluated. Results The intergranular corrosion depth, exfoliation degree, stress corrosion cracking time and threshold stress intensity factor for susceptibility to stress corrosion cracking (KICC) were obtained. There was intergranular corrosion tendency for 2D12 aluminum in natural aging condition, and the maximum intergranular corrosion depth was 0.18 mm. The anti-exfoliation corrosion property of 2D12 aluminum alloys with different specifications varied from P to Ec degree. The tensile stress corrosion cracking time decreased with the increase of the test stress, and the critical stress corrosion threshold of two sheets (δ=1.5 mm and δ=2.0 mm) and EL2805 section bar were 160, 140 and 230 MPa, respectively. The KICC values of S-L and S-T orientation were 22.6 MPa·m1/2 and 27.1 MPa·m1/2, respectively. Conclusion The anti-stress corrosion test of 2D12 aluminum alloy showed that the anti-SCC property of S-L orientation was lower than that of S-T orientation, which was in accordance with the C-ring result, and the fractographies of 2D12 aluminum revealed typical intergranular fracture stress corrosion cracking characteristics.
查看全文  查看/发表评论  下载PDF阅读器
关闭

关于我们 | 联系我们 | 投诉建议 | 隐私保护 | 用户协议

您是第11968906位访问者    渝ICP备15012534号-5

版权所有:《装备环境工程》编辑部 2014 All Rights Reserved

邮编:400039     电话:023-68792835    Email: zbhjgc@163.com

视频号 公众号