温度对2A12铝合金在模拟油箱积水环境中初期腐蚀行为的影响

doi:10.7527/S1000-6893.2013.0245

Abstract

Abstract:

Aluminum alloy corrosion in airplane tank water is a serious problem. The influence of temperature on the initial corrosion behavior of aluminum alloy 2A12 in a simulated tank water environment is studied by observing the corrosion morphology, maximum pitting corrosion depth, maximum pitting corrosion area, surface corrosion damage ratio, EIS, etc. The results indicate that pitting corrosion depth, pitting corrosion area and surface corrosion damage ratio increase with increasing temperature. In particular, at temperatures 65℃ and 75℃, corrosion speed increases dramatically. In the simulated tank water of 25, 35, 45 and 55℃, the variation in maximum pitting corrosion depth and area with time all fit well withthe power function. At temperatures 65℃ and 75℃, they both fit well with the least square polynomial fitting. In addition, EIS indicates that corrosion rate in simulated tank water of three typical temperatures (25, 55, 75℃) increases with temperature increase.

Key words: aluminum alloys, simulated tank water, pitting corrosion depth, pitting corrosion area, corrosion damage ratio

CLC Number:

V252
TG172.5

LI Chenyu, ZHU Liqun, LIU Huicong, YE Xubin, LIU Jianzhong, HUANG Yi. Influence of Temperature on Initial Corrosion Behavior of Aluminum Alloy 2A12 in Simulated Tank Water Environment[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(6): 1493-1500.

References

[1] Liang Z D. Corrosion of aluminum alloy in aircraft fuel tank compartments due to condensed water. Corrosion, 1992,48(6): 514-517.
[2] Zhu L Q, Li W P, Zhang Q, et al. Galvanic corrosion of high-strength aluminum alloys in the solution simulating the aircraft corrosion environment. Acta Aeronautica et Astronautica Sinica, 1997, 18(1): 32-37. (in Chinese) 朱立群, 李卫平, 张琦, 等. 模拟实际飞机腐蚀介质中高强铝合金材料腐蚀行为研究. 航空学报, 1997,18(1): 32-37.
[3] Zhang Y H, Lu G Z, Chen Y L. Predicting fatigue life from pre-corroded LY12-CZ aluminium test. Acta Aeronautica et Astronautica Sinica, 2005, 26(6): 779-782. (in Chinese) 张有宏, 吕国志, 陈跃良. LY12-CZ铝合金预腐蚀及疲劳损伤研究. 航空学报, 2005,26(6): 779-782.
[4] Huang Y, Liu H C, Zhu L Q, et al. Study on corrosion behavior of 30CrMnSiNi2A steels in simulated tank water environment. Journal of Materials Engineering,2012(4): 88-93. (in Chinese) 黄颐, 刘慧丛, 朱立群, 等. 30CrMnSiNi2A钢在模拟油箱积水环境中的腐蚀行为研究. 材料工程, 2012(4): 88-93.
[5] Zhang D. Corrosion and corrosion control of aircraft structure. Beijing: National Defence Industry Press, 1993: 63-71. (in Chinese) 张栋. 飞机结构的腐蚀与腐蚀控制. 北京: 国防工业出版社, 1993: 63-71.
[6] Ezuber H, El-Houd A, El-Shawesh F. A study on the corrosion behavior of aluminum alloys in seawater. Materials and Design, 2008, 29(4): 801-805.
[7] Wu X L, Liu J H, Chen X Y. Surface analysis of aluminum alloys influenced by sulfate-bacteria. Acta Metallurgica Sinica, 1999, 12(5): 867-873.
[8] Yun F L, Xu K. Effect of heavy metal ions on the corrosion of aluminum alloy 5052. Chemical Industry and Engineering, 2010, 27(2):173-176. (in Chinese) 云凤玲, 徐克. 重金属离子对5052铝合金耐蚀性能的影响. 化学工业与工程, 2010, 27(2):173-176.
[9] Khedr M G A, Lashien A M S. The role of metal cations in the corrosion and corrosion inhibition of alumimium in aqueous solutions. Corrosion Science, 1992, 33(1): 137-151.
[10] Sato F, Asakawa Y. Localized corrosion behavior of aluminum-magnesium-silicon alloy in ground water. Corrosion, 1999, 55(5): 522-529.
[11] Huang L C, Liu H C, Gu A. Failure and corrosion of coating on aluminum alloy parts used on airplanes serving in costal environment. Acta Aeronautica et Astronautica Sinica, 2009, 30(6): 1144-1149. (in Chinese) 黄领才, 刘慧丛, 谷岸. 沿海环境下服役飞机铝合金零件的表面涂层破坏与腐蚀. 航空学报, 2009, 30(6): 1144-1149.
[12] Dan Z H, Muto I, Hara N. Effects of environmental factors on atmospheric corrosion of aluminium and its alloys under constant dew point conditions. Corrosion Science, 2012, 57(1): 22-29.
[13] Grill R, Baker M A, Castle J E, et al. Corrosion behavior of a 2219 aluminium alloy treated with a chromate conversion coating exposed to a 3.5% NaCl solution. Corrosion Science, 2011,53(4): 1214-1223.
[14] Han D S, Li D. Influence of marine atmosphere humidity on initial corrosion of LY12. Journal of Chinese Society for Corrosion and Protection, 2007, 27(3): 134-136. (in Chinese) 韩德盛, 李荻. 海洋大气湿度对LY12铝合金初期腐蚀的影响. 中国腐蚀与防护学报, 2007,27(3):134-136.
[15] Han D S, Li D. Influence of temperature on initial corrosion of LY12 in marine atmosphere. Materials Protection, 2007,40(6):7-8,19. (in Chinese) 韩德盛, 李荻. 温度对LY12铝合金海洋大气初期腐蚀行为的影响. 材料保护, 2007, 40(6):7-8,19.
[16] Zhu L Q, Gu A, Liu H C, et al. Study on characters of corrosion advancing edge of typical high strength aluminum alloys. Journal of Aeronautical Materials, 2008, 28(6): 61-66. (in Chinese) 朱立群, 谷岸, 刘慧丛, 等. 典型高强铝合金材料的点腐蚀坑前缘特征的研究. 航空材料学报, 2008,28(6): 61-66.
[17] Li T, Feng H T, Li X G, et al. Corrosion behavior of 2A12 aluminum alloy in Cl^-containing solution. Materials Science and Technology, 2011, 19(3):43-48. (in Chinese) 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. 材料科学与工艺, 2011, 19(3): 43-48.
[18] Paik J K, Lee J M, Ko M J. Ultimate shear strength of plate elements with pit corrosion wastage. Thin-Walled Structures, 2004, 42(8): 1161-1176.
[19] Zhang Y H, Lu G Z, Ren K L, et al. The evolution rhythm of surface corrosion damage of LY12-CZ aluminum in varied environment. Acta Aeronautica et Astronautica Sinica, 2007, 28(1):142-145. (in Chinese) 张有宏, 吕国志, 任克亮,等. 不同环境下LY12-CZ铝合金表面腐蚀损伤演化规律研究. 航空学报, 2007, 28(1):142-145.
[20] Zhu Z T, Mu Z T, Su W G, et al. Corrosion grade evaluation of aluminum alloy based on image processing technique. Journal of Nanjing University of Aeronautics & Astronautics, 2010, 42(3): 383-386. (in Chinese) 朱做涛,穆志韬,苏维国,等. 基于图像处理技术的铝合金腐蚀等级评定方法. 南京航空航天大学学报, 2010,42(3): 383-386.
[21] Schueller G R T, Taylor S R. Electrochemical impedance analysis and interpretation. USA: ASTM Special Technical Publication 1188, 1993.
[22] Cheng Y L, Zhang Z, Cao F H, et al. A study of corrosion of aluminum alloy 2024-T3 under thin electrolyte layers. Corrosion Science, 2004, 46(7): 1649-1667.

Influence of Temperature on Initial Corrosion Behavior of Aluminum Alloy 2A12 in Simulated Tank Water Environment

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	ZHANG Teng, HE Yuting, GAO Chao, LI Changfan, SHAO Qing. Damage rule of 2A12-T4 aluminum alloy with long-term atmospheric corrosion [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(2): 661-671.
[2]	TU Jilin, WANG Yongjun, ZHANG Jichun, WU Jianjun, WEI Shengmin. Analysis and Experiment on Buckling of Rubber Bladder Forming of Thin Aluminum Alloy Plate Parts [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(8): 2341-2347.
[3]	ZHANG Mulin, ZHU Liqun, LIU Huicong, YE Xubin, LIU Jianzhong. Corrosion Behavior of 300M Ultra-high Strength Steel in Simulated Gap Water Environment [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(4): 954-962.
[4]	Wang Huiting;Gao Lin;Shen Xiaohui;Li Shuanggao. Hydromechanical Deep Drawing of Aluminum Alloy 2A12O Assisted by Augmented Radial Pressure [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(6): 1266-1271.
[5]	Hu Jialin;Chen Yueliang;Zhang Ding;Yang Maosheng. Analysis of Corrosion Damage and Fatigue Life Based on Corrosion Image [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(1): 131-135.
[6]	Xie Ruoze;Lu Zixing;Chen Chengjun;Zhang Fangju;Zhao Yabin. Measurement of Dynamic Compressive Behavior of Aluminum-alloy Foams by Polycarbonate SHPB System [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(8): 1435-1439.
[7]	Wang Hui;Lu Guozhi;Wang Le;Zhang Youhong. Cellular Automaton Simulations of Surface Corrosion Damage Evolution [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2008, 30(6): 1490-1496.
[8]	LIU Yan\\|li;ZHONG Qun peng;ZHANG Zheng . PREDICTIVE MODEL BASED ON ARTIFICIAL NEURAL NET FOR FATIGUE PERFORMANCES OF PRIOR-CORRODED ALUMINUM ALLOYS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2001, 22(2): 135-139.
[9]	WAN Min;ZHOU Xian bin;LI Xiao xing;WU Hui. PROCESS PARAMETERS IN STRETCH FORMING OF MIRROR SKINS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1999, 20(4): 39-43.
[10]	Xie Weijie;Li di;Hu Yanling;Guo Baolan. STATISTICAL STUDY OF CORROSION KINETICS LAW FOR LY12CZ AND 7075T7351 ALUMINUM ALLOY IN EXCO SOLUTION [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1999, 20(1): 34-38.
[11]	Zhang Hong;Tang Yaxin;Yu Chengye;Zhang Yongkang;Guo Dahao;Wu Hongxing. EXPERIMENTAL STUDY ON SURFACE STRENGTHENING OF ALUMINUM ALLOY BY LASER SHOCKING [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(2): 248-251.
[12]	Ding Chuanfu;Ou Yanghui;Luo Anmin;Yue Junwen. A STUDY OF STRAIN FATIGUE MECHANICS BEHAVIOUR [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(3): 373-378.
[13]	Zheng Peng;Zheng Yuzhen;Wei Hui;Qian Yourong. CHARACTERISTICS AND EFFECTS OF RESIDUAL STRESS DISTRIBUTED ALONG THE THICKNESS IN 2324 ALUMINUM ALLOY PLATE [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(3): 330-336.
[14]	Jian Zengun;Yang Gencang;zhou Yaohe. UNDERCOOLING AND STRUCTURE OF Al-4.5%Cu Alloy [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(1): 51-54.
[15]	Xu Yongli;Ji Daoxing;Chen Changqi. MICROSTRUCTURE AND MORPHOLOGY OF RAPIOLY COOLED Al-Cu ALLOYS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1994, 15(7): 887-890.