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| Study on inland area accelerated test method for high strength aluminum alloy |
| Cui Tengfei1, Zhang Xiaojuan1, Liu Daoxin2, Yu Qing1 |
1. General Technology Department, China Helicopter Research and Development Institute, Jingdezhen 333000, China;
2. Corrosion and Protection Research Laboratory, Northwestern Polytechnical University, Xi'an 710072, China |
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Abstract In order to establishthetest method for accelerated corrosion of high strength aluminum alloys in an inland area, 7B04-T6 aluminum alloys was used for laboratory accelerated corrosion test and atmospheric environment exposure corrosion test canwhile the fatigue propeties the tested were compaluated. Through the comparative the average corrosion rate test of the samples, the corrosion morphology observation and fatigue fracture characteristics ahalysis corrosion mechanism and fatigue lifewere tested and compared. The results show that: the corrosion mode of 7B04-T6 aluminum alloy that undergone accelerated corrosion in laboratory and exposure atmospheric environmental is same. The corrosion mechanism and fatigue damage characteristics had no different. So, the accelerated environmental spectra and test methods can be used as an accelerated test method for high strength aluminum alloy to simulation inland area climate damage. The accelerated multiple is 97.64.
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| 1 ] 李玉海,刘文珽,贾国荣. 军用飞机结构日历寿命体系评定
应用范例[ M ]. 北京:航空工业出版社,2005.
[ 2 ] Hosni Ezuber, A El-Houd, F El-Shawesh. A study on the corrosion behavior of aluminum alloys in seawater [ J ]. Materials and Design
2008, 29 ( 5 ): 801 - 805.
[ 3 ] Prasanta Kumar Rout, M M Ghosh, K S Ghosh. Effect of solution pH on electrochemical and stress corrosion cracking behavior of a7150 Al-Zn-Mg-Cu alloy[ J ]. Materials Science & Engineering A, 2014, 604 ( 4 ): 156 - 165.
[ 4 ] 杨洪源,刘文珽. 民机结构外露关键部位涂层加速腐蚀环境谱研究[ J ]. 航空学报,2007( 1 ):90 - 93.
[ 5 ] 蒋祖国,田丁栓,周占廷. 飞机结构载荷/环境谱[ M ]. 北京:电子工业出版社,2012.
[ 6 ] 张 勇,陈跃良,樊伟杰,等. ×飞机半封闭部位局部环境谱当量加速关系研究[ J ]. 装备环境工程,2017( 1 ):24 - 29.
[ 7 ] 邓 斌,易丹青,杨 胜,等. 2E12铝合金加速腐蚀环境谱下的疲劳裂纹扩展[ J ]. 材料科学与工程学报,2009( 5 ):770 - 773.
[ 8 ] 张晓云,孙志华,刘明辉,等. 环境对高强度铝合金应力腐蚀行为的影响[ J ]. 中国腐蚀与防护学报,2007,26( 6 ):354 - 362.
[ 9 ] 崔继红,蔡建平,贾成厂. 盐雾环境下高强度铝合金的点蚀行为[ J ]. 中国腐蚀防护学报,2010,30( 3 ):197 - 202.
[ 10 ] S.A. Barter,L. Molent. Fatigue cracking from a corrosion pit in an aircraft bulkhead [ J ]. Engineering Failure Analysis, 2014, 39( 3 ): 155 - 163.
[ 11 ] Zhenhua Dan,Izumi Muto,Nobuyoshi Hara. Effects of environ-
mental factors on atmospheric corrosion of aluminium and its alloys under constant dew point conditions [ J ]. Corrosion Science 2012, 57 ( 1 ):22 - 29.
[ 12 ] 蔡 剑,刘道新,叶作彦,等. 腐蚀与交变载荷循环作用对2A12-T4铝合金疲劳寿命的影响[ J ]. 中国腐蚀与防护学报, 2015( 1 ):61 - 68.
[ 13 ] 李 涛,李晓刚,董超芳. Cl-含量对2A12 铝合金初期腐蚀行为的影响[ J ]. 北京科技大学学报,2009,31( 12 ):1 576 - 1 582.
[ 14 ] 蔡健平,刘 明,罗振华,等. 航空铝合金大气腐蚀加速试验研[ J ]. 材料工程. 2004,12:8 - 12.
[ 15 ] 毋 玲,孙 秦,郭英男. 高强度铝合金盐雾加速腐蚀试验研究[ J ]. 机械强度, 2006,28( 1 ):138-140.
[ 16 ] 李劲风,张 昭,郑子樵. 拉应力对 7075 铝合金的剥蚀 及其电化学阻抗谱的影响[ J ]. 腐蚀科学与防护技术,2005,17( 2 ):79 - 82
[ 17 ] 何建平,陈文理,许 玮,等. 恒温剥蚀对LC4CS铝合金结构和力学性能的影响[ J ]. 南京航空航天大学学报,1999,31( 5 ):575.
[ 18 ] 张正贵,周兆元,刘长勇. 高强度铝合金构件腐蚀疲劳失效分析[ J ]. 中国腐蚀与防护学报,2008,28( 1 ):48 - 52.
[ 19 ] 李 涛,冯海涛,李晓刚,等. 2A12 铝合金在含Cl- 环境中的腐蚀行为和规律研究[ J ]. 材料科学与工艺,2011, 19( 3 ):43 - 48. |
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