[1] Jia Y H, He J W. Modern aircraft manufacturing technology. Beijing: Beihang University Press, 2010: 135. (in Chinese) 贾玉红, 何景武. 现代飞行器制造工艺学. 北京: 北京航空航天大学出版社, 2010: 135.
[2] Zhao Q Y, Liu F L, Liu H D. Development of advanced aerospace fastener. Aeronautical Manufacturing Technology, 2009(3): 54-56. (in Chinese) 赵庆云, 刘风雷, 刘华东. 世界先进航空紧固件进展.航空制造技术, 2009(3): 54-56.
[3] Cao Z Q. Exploration of electromagnetic riveting application in large aircraft manufacturing. Acta Aeronautica et Astronautica Sinica, 2008, 29(3): 716-720. (in Chinese) 曹增强.电磁铆接技术在大飞机制造中的应用初探. 航空学报, 2008, 29 (3): 716-720.
[4] Ren C, Liu F L, Zhao Q Y, et al. Manufacturing technology of British system light-weight titanium alloy bolt. Aeronautical Manufacturing Technology, 2010(23): 79-81. (in Chinese) 任翀, 刘风雷, 赵庆云, 等. 轻型英制钛合金高锁螺栓制造工艺技术. 航空制造技术, 2010(23): 79-81.
[5] Furfari D, Ohrloff N, Schmidt G. Finite element analysis for advanced repair solutions: a stress analysis study of fastened and bonded fuselage skin repairs. 50th Structures, Structural Dynamics, and Materials Conference, Palm Springs: AIAA/ASME/ ASCE/AHS/ASC, 2009: 1-20.
[6] Ярковец А И. Long life bolted joining and riveting technology in aircraft structures. Zhang G L, translated. Beijing: Aviation Industry Press, 1991: 95-110. (in Chinese) 雅可维茨.飞机长寿命螺栓连接和铆接技术. 张国梁,译. 北京: 航空工业出版社, 1991: 95-110.
[7] Chakherlou T N, Mirzajanzadeh M, Abazadeh B, et al. An investigation about interference fit effect on improving fatigue life of a holed single plate in joints. European Journal of Mechanics-A/Solids, 2010, 29(4): 675-682.
[8] Mirzajanzadeh M, Chakherlou T N, Vogwell J. The effect of interference-fit on fretting fatigue crack initiation and ΔK of a single pinned plate in 7075 Al-alloy. Engineering Fracture Mechanics, 2011, 78(6): 1233-1246.
[9] Brady B G. Cracking during the installation of interference fit fasteners and bucked rivets in 7050-T7XXX machined aluminum parts. Proceedings of IMECE2006, Chicago: ASME, 2006: 1-7.
[10] Atre A, Johnson W S. Analysis of the effects of interference and sealant on riveted lap joints. Journal of Aircraft, 2007, 44(2): 353-364.
[11] Chakherlou T N, Abazadeh B. Experimental and numerical investigations about the combined effect of interference fit and bolt clamping on the fatigue behavior of Al 2024-T3 double shear lap joints. Materials and Design, 2012, 33:425-435.
[12] Xu B Y. Plastic mechanics. Beijing: Higher Education Press, 1988: 148-168. (in Chinese) 徐秉业. 塑性力学. 北京: 高等教育出版社, 1988: 148-168.
[13] Pu L G. Mechanical design. 8th ed. Beijing: Higher Education Press, 2009: 68-70. (in Chinese) 濮良贵. 机械设计. 第八版. 北京: 高等教育出版社, 2009: 68-70.
[14] An J R. Handbook of Chinese and foreign metal materials. Xi'an: Shaanxi Science and Technology Press, 2007: 325, 456. (in Chinese) 安继儒. 中外金属材料手册. 西安: 陕西科学技术出版社, 2007: 325, 456.
[15] Zhao T L. ABAQUS6.6 application in mechanical engineering. Beijing: China WaterPower Press, 2007: 270-277. (in Chinese) 赵腾伦. ABAQUS6.6在机械工程中的应用. 北京: 中国水利水电出版社, 2007: 270-277. |