宫玉辉,刘铭,张坤,等.不同腐蚀环境对7475-T7351铝合金疲劳性能及裂纹扩展速率的影响[J].材料工程,2010, (9):71-73.GONG Yu-hui, LIU Ming, ZHANG Kun, et al. Effects of different corrosion environments on fatigue property and crack growth rate in 7475-T7351 aluminum alloy[J].Journal of Materials Engineering, 2010, (9): 71-73.
[2]
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 Hui-cong, ZHU Li-qun,et al. Scalling of 2524 aluminum alloy with cladding in simulate fuel tank water environment and influence to corrosion behavior[J].Journal of Materials Engineering, 2013, (5):11-15.
[3]
鲍蕊,张建宇,费斌军.潮湿空气环境对2024-T3铝合金疲劳性能的影响[J],材料研究学报,2007,21(5):547-550.BAO Rui, ZHANG Jian-yu, FEI Bin-jun. The influence on fatigue performance of 2024-T3 aluminum alloy in damp air environment [J]. Journal of Materials Research, 2007, 21(5): 547-550.
[4]
KIMBERLI J, SACHIN R S, PAUL N C,et al. Effect of prior corrosion on short crack behavior in 2024-T3 aluminum[J]. Corrosion Science,2008,50(9):2588-2595.
[5]
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.
[6]
DUQUESNAY D L, UNDERHILL P R, BRITT H J. Fatigue crack growth from corrosion damage in 7075-T6511 aluminium alloy under aircraft loading[J].International Journal of Fatigue,2003,25(5):371-377.
任三元,曹鹏钧,刘海涛.预腐蚀典型铆接结构疲劳寿命特性研究[J].装备环境工程,2009,6(1):27-29. REN San-yuan, CAO Peng-jun, LIU Hai-tao. Research on fatigue life characteristics of pre-corroded typical riveted structure [J]. Equipment Environmental Engineering, 2009,6(1):27-29.
[9]
高镇同,蒋新桐,熊峻江.疲劳性能试验设计和数据处理——直升机金属材料疲劳性能可靠性手册[M].北京:北京航空航天大学出版社,1999.173-177. GAO Zhen-tong, JIANG Xin-tong, XIONG Jun-jiang. Fatigue Performance Test Design and Data Processing-The Fatigue Performance Reliability Manual of Metal Material Used on Helicopter[M].Beijing:Beihang University Press, 1999.173-177.
[10]
郑晓玲.民机结构耐久性与损伤容限设计手册(下册)[M].北京:航空工业出版社,2003. ZHENG Xiao-ling. Handbook of Civil Aircraft Structures Durability and Damage Tolerance Design[M]. Beijing: Aviation Industry Press,2003.
[11]
蒋祖国.飞机结构腐蚀疲劳[M].北京:航空工业出版社,1992. 39-43.JIANG Zu-guo. Corrosion Fatigue of Plane Structure[M]. Beijing: Aviation Industry Press, 1992.39-43.
[12]
陈跃良,卞贵学,郁大照,等. 腐蚀环境下飞机结构疲劳全寿命评估模型[J].机械强度, 2012,34(1):137-143.CHEN Yue-liang,BIAN Gui-xue, YU Da-zhao,et al. Fatigue holistic life assessment model of aircraft structure under corrosive environment[J].Journal of Mechanical Strength, 2012, 34(1): 137-143.
[13]
耿德平,宋庆功.航空材料腐蚀疲劳研究进展[J].腐蚀与防护,2011,32(3):206-209.GENG De-ping, SONG Qing-gong. Development of corrosion fatigue theory for aeronautical materials[J].Corrosion & Protection, 2011,32(3):206-209.
[14]
张有宏.飞机结构的腐蚀损伤及其对寿命的影响[D].西安:西北工业大学,2007.ZHANG You-hong. The corrosion damage and its effect on life of aircraft structure[D]. Xi'an: Northwestern Polytechnical University, 2007.
[15]
包俊成,赵捷,王志奇,等.钛合金BT20焊接接头腐蚀疲劳性能的实验研究[J].中国腐蚀与防护学报,2010,3(4):313-316.BAO Jun-cheng, ZHAO Jie, WANG Zhi-qi, et al. Experimental research on fatigue property of welded joints of BT20 titanium alloy in corrosion environment[J]. Journal of Chinese Society for Corrosion and Protection,2010,3(4):313-316.