[1]回丽,于翔,许良,等.航空铝合金腐蚀坑当量化技术[J].中国机械工程, 2015, 26(16): 2233-2236.
HUI Li, YU Xiang, XU Liang, et al. On Quantitative Techniques of Corrosion Pits of Aerial Aluminum Alloys [J]. China Mechanical Engineering, 2015, 26(16): 2233-2236.
[2]张海威,何宇廷,范超华,等.腐蚀/疲劳交替作用下飞机金属材料疲劳寿命计算方法[J].航空学报, 2013, 34(5):1114-1121.
ZHANG Haiwei,HE Yuting,FAN Chaohua, et al. Fatigue Life Prediction Method for Aircraft Metal Material under Alternative Corrosion/Fatigue Process[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(5):1114-1121.
[3]张川,姚卫星. 铝合金预腐蚀剩余寿命的分形维数预测方法[J].中国机械工程,2013,24(17):2337-2340.
ZHANG Chuan, YAO Weixing. Prediction of Residual Life of Pre-corrosion Aluminum Alloy with Fractal Dimension [J]. China Mechanical Engineering, 2013,24(17):2337-2340.
[4]GRUENBERG K M, CRAIG B A, HILLBERRY B M, et al. Predicting Fatigue Life of Pre-corroded 2024-T3 Aluminum[J]. International Journal of Fatigue, 2004, 26(6):629-640.
[5]BELLINGER N C, KOMOROWSKI J P, BENAK T J. Residual Life Predictions of Corroded Fuselage Lap Joints[J].International Journal of Fatigue,2001,23(1):349-356.
[6]SABELKIN V, PEREL V Y, MISAK H E, et al. Investigation into Crack Initiation from Corrosion Pit in 7075-T6 under Ambient Laboratory and Saltwater Environments[J]. Engineering Fracture Mechanics, 2015,134:111-123.
[7]MEDVED J J, BRETON A M, IRVING P E. Corrosion Pit Size Distributions and Fatigue Lives: a Study of the EIFS Technique for Fatigue Design in the Presence of Corrosion[J]. International Journal of Fatigue, 2004, 26:71-80.
[8]胡家林,陈跃良,张玎,等.基于图像的腐蚀损伤及疲劳寿命研究[J].航空学报, 2010,31(1):131-135.
HU Jialin, CHEN Yueliang, ZHANG Ding, et al. Analysisof Corrosion Damage and Fatigue Life Based on Corrosion Image [J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(1): 131-135.
[9]DAN Z H, MUTO I, HARA N. Effects of Environmental Factors on Atmospheric Corrosion of Aluminium and Its Alloys under Constant Dew Point Conditions [J]. Corrosion Science,2012, 57(1):22-29.
[10]徐火平,刘慧丛,朱立群,等. 盐雾环境中高强铝合金点腐蚀行为与暴露面积的关系[J].航空材料学报, 2010,30(4):59-64.
XU Huoping, LIU Huicong, ZHU Liqun, et al. Relation between Pitting Corrosion Behavior and Exposed Area of High Strength Aluminum Alloys in Neutral Salt Spray[J]. Journal of Aeronautical materials, 2010,30(4):59-64.
[11]董超芳,安英辉,李晓刚,等. 7A04铝合金在海洋大气环境中初期腐蚀的电化学特性[J].中国有色金属学报,2009, 19(2): 346-352.
DONG Chaofang, AN Yinghui, LI Xiaogang, et al. Electrochemical Performance of Initial Corrosion of 7A04 Aluminium Alloy in Marine Atmosphere[J]. The Chinese Journal of Nonferrous Metals, 2009, 19(2): 346-352.
[12]黄领才,刘慧丛,谷岸. 沿海环境下服役飞机铝合金零件的表而涂层破坏与腐蚀[J].航空学报,2009, 30(6):1144-1149.
HUANG Lingcai,LIU Huicong,GU An. Failure and Corrosion of Coating on Aluminum Alloy Parts Used on Airplanes Serving in Costal Environment[J]. Acta Aeronautics et Astronautics Sinica, 2009,30(6):1144-1149.
[13]李晨钰,朱立群,刘慧丛,等.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[J].航空学报,2013, 34(6): 1493-1500.
LI Chenyu. ZHU Liqun. LIU Huicong. et al. Influence of Temperature on Initial Corrosion Behavior of Aluminum Alloy 2A12 in Simulated Tank Water Environment[J]. Acta Aeronautica et Astronautica Sinica, 2013,34(6): 1493-1500.
[14]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[J]. Corrosion Science, 2011,53(4): 1214-1223.
[15]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[J].化学工业与工程,2010,27(2):173-176.
YUN Fengling, XU Ke. Effect of Heavy Metal Ionson the Corrosion of Aluminum Alloy 5052[J]. Chemical Industry and Engineering, 2010,27(2):173-176.
[16]管琪,刘慧丛,朱立群,等.2524铝合金包铝层在模拟油箱积水环境中结垢及其对腐蚀行为的影响[J].材料工程,2013(5):11-15.
GUAN Qi, LIU Huicong, ZHU Liqun, et al. Scaling of 2524 Aluminum Alloy with Cladding in Simulated Fuel Tank Water Environment and Influence to Corrosion Behavior[J]. Journal of Materials Engineering,2013(5):11-15.
[17]LI J F , ZHENG Z Q, JIANG N, et al. Localized Corrosion Mechanism of 2xxx-series Al Alloy Containing S(Al2CuMg) and θ′(Al2Cu) Precipitates in 4.0% NaCl Solution at pH 6.1[J]. Materials Chemistry and Physics, 2005, 91(2/3):325-329.
[18]UHILIG H H. Environmental Factors Effecting the Critical Pitting Potential of Aluminium[J]. Journal of the Electrochemical Society, 1969,116:906-914.
[19]HOAR T P, MEARS D C, ROTHWELL G P. The Relationships between Anodic Passivity, Brightening and Pitting[J]. Corrosion Science, 1965, 5(4):279-289.
[20]谭晓明,张丹峰,卞贵学,等. 腐蚀对新型高强度铝合金疲劳裂纹萌生机制及扩展行为的作用[J].机械工程学报,2014,50(22):76-83.
TAN Xiaoming, ZHANG Danfeng, BIAN Guixue, et al. Effect of Corrosion Damage on Fatigue Crack Initiation Mechanism and Growth Behavior of High Strength Aluminum Alloy[J]. Journal of Mechanical Engineering, 2014, 50(22): 76-83.
[21]JONES K, HOEPPNER D W. Prior Corrosion and Fatigue of 2024-T3 Aluminum Alloy[J].Corrosion Seience,2006, 48(10):3109-3122.
[22]张有宏,吕国志,陈跃良,等.铝合金腐蚀损伤的形态学研究[J].腐蚀科学与防护技术,2007,19(4):272-274.
ZHANG Youhong, LYU Guozhi, CHEN Yueliang, et al. Morphological Study on Corrosion Damage of Aluminum Alloy[J]. Corrosion Science and Protection Technology, 2007, 19(4):272-274. |