[1] 胡建军, 陈跃良, 刘军. 飞机结构搭接件腐蚀试验研究[J]. 强度与环境, 2011, 38(4):49-53. HU J J, CHEN Y L, LIU J. Investigation on lap-joints material corrosion test of aircraft structure[J]. Structure & Environment Engineering, 2011, 38(4):49-53(in Chinese).
[2] 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 H P, LIU H C, ZHU L Q, 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(in Chinese).
[3] 刘文珽, 李玉梅, 陈群志, 等. 飞机结构腐蚀部位涂层加速试验环境谱研究[J]. 北京航空航天大学学报, 2002, 28(1):109-112. LIU W T, LI Y M, CHEN Q Z, et al. Accelerated corrosion environmental spectrums for testing surface coatings of critical areas of flight aircraft structures[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(1):109-112(in Chinese).
[4] 陈跃良, 段成美, 金平. 飞机结构局部环境加速腐蚀当量谱[J]. 南京航空航天大学学报, 1999, 31(3):338-341. CHEN Y L, DUAN C M, JIN P. Local environment and accelerating corrosion equivalent spectrums of aircraft structure[J]. Journal of Nanjing University of Aeronautics and Astronautics, 1999, 31(3):338-341(in Chinese).
[5] 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 C Y, ZHU L Q, LIU H C, 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(in Chinese).
[6] WANG B B, WANG Z Y, HAN W, et al. Effects of magnesium chloride-based multicomponent salts on atmospheric corrosion of aluminum alloy 2024[J]. Transactions of Nonferrous Metals Society of China, 2013, 23(4):1199-1208.
[7] DAN Z, MUTO I, HARA N. Effects of environmental factors on atmospheric corrosion of aluminum and its alloy under constant dew point conditions[J]. Corrosion Science, 2012, 57(4):22-29.
[8] 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 H W, HE Y T, FAN C H, 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(in Chinese).
[9] 宋恩鹏, 刘文珽, 杨旭. 飞机内部腐蚀关键部位加速试验环境谱研究[J]. 航空学报, 2006, 27(4):646-649. SONG E P, LIU W T, YANG X. Study on accelerated corrosion test environment spectrum for internal aircraft structure[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(4):646-649(in Chinese).
[10] 张丹峰, 陈跃良. 当量加速试验条件下铝合金腐蚀形态演化规律[J]. 南京航空航天大学学报, 2010, 42(3):340-342. ZHANG D F, CHEN Y L. Corrosion damage evolvement rule of aluminum alloy under equivalent accelerated condition[J]. Journal of Nanjing University of Aeronautics and Astronautics, 2010, 42(3):340-342(in Chinese).
[11] 张有宏, 吕国志, 陈跃良. LY12-CZ铝合金预腐蚀及疲劳损伤研究[J]. 航空学报, 2005, 26(6):779-782. ZHANG Y H, LV G Z, CHEN Y L. Predicting fatigue life from pre-corroded LY12-CZ aluminum test[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(6):779-782(in Chinese).
[12] 刘文珽. 飞机结构腐蚀/老化控制与日历延寿技术[M]. 北京:国防工业出版社, 2010:80-81. LIU W T. Corrosion/aging control and prolonging the calendar life technology of aircraft structure[M]. Beijing:National Defence Industry Press, 2010:80-81(in Chinese).
[13] 陈跃良, 段成美. 海军飞机环境谱加速腐蚀当量折算研究[R]. 青岛:海军航空技术学院, 1995. CHEN Y L, DUAN C M. Study on equivalent of accelerated corrosion of naval aircraft environment spectrums[R]. Qingdao:Naval Aeronautics & Astronautics Institute, 1995(in Chinese).
[14] 刘文珽. 飞机结构日历寿命体系评定技术[M]. 北京:航空工业出版社, 2004:110-111. LIU W T. The evaluation technique of calendar life for aircraft structure[M]. Beijing:Aviation Industry Press, 2004:110-111(in Chinese).
[15] 董超芳, 生海, 安英辉, 等. Cl-作用下2A12铝合金在大气环境中腐蚀初期的微区电化学行为[J]. 北京科技大学学报, 2009, 31(7):878-883. DONG C F, SHENG H, AN Y H, et al. Local electrochemical behavior of 2A12 aluminum alloy in the initial stage of atmospheric corrosion under Cl- conditions[J]. Journal of University Science and Technology Beijing, 2009, 31(7):878-883(in Chinese).
[16] 张睿, 张慧霞, 贾瑞灵. 钛及其合金的腐蚀[J]. 材料开发与应用, 2013, 28(4):96-103. ZHANG R, ZHANG H X, JIA R L. The corrosion resistance of titanium and its alloy[J]. Development andApplication of Materials, 2013, 28(4):96-103(in Chinese).
[17] JARFALL L. Verification of the damage tolerance of a fighter aircraft[J]. Fatigue, 1994, 16(1):67-74.
[18] DURET N. Titanium for damage tolerance application on A380[C]//The 10th Conference on Titanium. Hamburg:TMS, 2003, 2667-2671.
[19] CHANG H Y, PARK Y S, HWANG W S. Initial modeling of crevice corrosion in 316L stainless steels[J]. Materials Processing Technology, 1998, 103(2):206-217.
[20] 姜应律, 吴荫顺. 用极化曲线研究钛合金在水、醇中腐蚀机理的差异[J]. 腐蚀科学与防护技术, 2005, 17(3):154-158. JIANG Y L, WU Y S. Study of mechanism of electrochemical reaction for titanium alloy TC4 in 3% NaCl solution and ethanol by polarization curve[J]. Corrosion Science and Protection Technology, 2005, 17(3):154-158(in Chinese).
[21] 王玲, 宣卫芳, 牟献良. 2A11铝合金/碳钢偶接件在强化自然环境条件下的腐蚀特性[J]. 表面技术, 2011, 40(5):1-4. WANG L, XUAN W F, MOU X L. Corrosion performance of 2A11 aluminum alloy coupled with carbon steel in accelerated natural environmental condition[J]. Surface Technology, 2011, 40(5):1-4(in Chinese).
[22] 李金桂. 腐蚀控制系统工程学概论[M]. 北京:化学工业出版社, 2009:55-57. LI J G. An introduction to system engineering science for corrosion control[M]. Beijing:Chemical Industry Press, 2009:55-57(in Chinese). |