Citation: | ZOU Peng, QU Fan. Damage mechanism of composite sleeve-type bolt interference fit structure during the installation process[J]. Acta Materiae Compositae Sinica, 2022, 39(5): 2449-2459. doi: 10.13801/j.cnki.fhclxb.20210616.007 |
[1] |
ZOU P, CHEN X, CHEN H, et al. Damage propagation and strength prediction of a single-lap interference-fit lami-nate structure[J]. Frontiers of Mechanical Engineering,2020,15(4):558-570. doi: 10.1007/s11465-020-0591-5
|
[2] |
ZHANG K F, HU J S, ZOU P, et al. Effect of secondary bending and bolt load on damage and strength of composite single-lap interference-fit bolted structures[J]. Journal of Composite Materials,2019,53(28/30):4385-4398.
|
[3] |
CAO Z, CARDEW-HALL M. Interference-fit riveting technique in fiber composite laminates[J]. Aerospace Science and Technology,2006,10(4):327-330. doi: 10.1016/j.ast.2005.11.003
|
[4] |
ZOU P, LI Y, ZHANG K, et al. Influence of interference-fit percentage on stress and damage mechanism in hi-lock pin installation process of CFRP[J]. Journal of Composite Materials,2017,51(25):3525-3538. doi: 10.1177/0021998316689601
|
[5] |
LI J, LI Y, ZHANG K, et al. Interface damage behaviour during interference-fit bolt installation process for CFRP/Ti alloy joining structure[J]. Fatigue & Fracture of Engi-neering Materials & Structures,2015,38(11):1359-1371.
|
[6] |
ZOU P, LI Y, ZHANG K, et al. Mode I delamination mecha-nism analysis on CFRP interference-fit during the installation process[J]. Materials & Design,2017,116:268-277.
|
[7] |
中国航空科学技术研究院. 飞机结构抗疲劳断裂强化设计手册[M]. 北京: 航空工业出版社, 1993.
China Academy of Civil Aviation Science and Technology. The structure fatigue–Fracture strengthening technology handbook[M]. Beijing: Aviation Industry Press, 1993(in Chinese).
|
[8] |
RAJU K P, BODJONA K, LIM G H, et al. Improving load sharing in hybrid bonded/bolted composite joints using an interference-fit bolt[J]. Composite Structures,2016,149:329-338. doi: 10.1016/j.compstruct.2016.04.025
|
[9] |
MULAZIMOGLU H, HAYLOCK L. Recent developments in techniques to minimize lightning current arcing between fasteners and composite structure[R]. UK: International Conference on Lightning and Static Electricity, 2011.
|
[10] |
刘风雷, 刘丹, 刘健光. 复合材料结构干涉安装控制及应用技术[J]. 航空精密制造技术, 2011, 47(6):36-38. doi: 10.3969/j.issn.1003-5451.2011.06.010
LIU Fenglei, LIU Dan, LIU Jianguang. Control and application technology of interference installation for composite materials[J]. Aviation Precision Manufacturing Technology,2011,47(6):36-38(in Chinese). doi: 10.3969/j.issn.1003-5451.2011.06.010
|
[11] |
刘风雷. 用于复合材料干涉结构的多功能紧固系统[J]. 航空制造技术, 2007(3):98-101. doi: 10.3969/j.issn.1671-833X.2007.03.019
LIU Fenglei. Multifunctional fastening system for compo-site interference structures[J]. Aeronautical Manufac-turing Technology,2007(3):98-101(in Chinese). doi: 10.3969/j.issn.1671-833X.2007.03.019
|
[12] |
陈坤, 舒茂盛, 胡仁伟, 等. 带衬套沉头螺栓复合材料/金属接头拉伸性能[J]. 北京航空航天大学学报, 2019, 45(3):633-640.
CHEN Kun, SHU Maosheng, HU Renwei, et al. Tensile properties of composite/metal joints with bushed countersunk head bolts[J]. Journal of Beijing University of Aeronautics and Astronautics,2019,45(3):633-640(in Chinese).
|
[13] |
YUAN X, YUE Z F, WEN S F, et al. Numerical and experimental investigation of the cold expansion process with split sleeve in titanium alloy TC4[J]. International Journal of Fatigue,2015,77:78-85. doi: 10.1016/j.ijfatigue.2015.03.014
|
[14] |
American Society for Testing and Materials. Standard test method for bearing response of polymer matrix: D5961/D5961M[S]. US: American Society for Testing and Materials, 2013.
|
[15] |
HOU G, ZHANG K, FAN X, et al. Analysis of exit-ply temperature characteristics and their effects on occurrence of exit-ply damages during UD CFRP drilling[J]. Composite Structures,2020,231:111456. doi: 10.1016/j.compstruct.2019.111456
|
[16] |
HOU G, LUO B, ZHANG K, et al. Investigation of high temperature effect on CFRP cutting mechanism based on a temperature controlled orthogonal cutting experiment[J]. Composite Structures,2021,268:113967. doi: 10.1016/j.compstruct.2021.113967
|
[17] |
XU G, CHENG H, ZHANG K, et al. Modeling of damage behavior of carbon fiber reinforced plastic composites interference bolting with sleeve[J]. Materials & Design,2020,194:108904. doi: 10.1016/j.matdes.2020.108904
|
[18] |
CHANG F K, CHANG K Y. Post-failure analysis of bolted composite joints in tension or shear-out mode failure[J]. Journal of Composite Materials,1987,21(9):809-833. doi: 10.1177/002199838702100903
|
[19] |
CAMANHO P P, MATTHEWS F L. A progressive damage model for mechanically fastened joints in composite laminates[J]. Journal of Composite Materials,1999,33(24):2248-2280. doi: 10.1177/002199839903302402
|
[20] |
TSERPES K I, LABEAS G, PAPANIKOS P, et al. Strength prediction of bolted joints in graphite/epoxy composite laminates[J]. Composites Part B:Engineering,2002,33(7):522-529.
|
[21] |
MI Y, CRISFIELD M A, DAVIES G A O, et al. Progressive delamination using interface elements[J]. Delamination Behaviour of Composites,1998,32(14):367-386.
|
[22] |
BENZEGGAGH M L, KENANE M. Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus[J]. Composites Science & Technology,1996,56(4):439-449.
|
[23] |
REEDER J R, CREWS J. Mixed-mode bending method for delamination testing[J]. AIAA Journal, 1990, 28(7): 1270-1276.
|
[24] |
贾利勇, 贺高, 把余炜. 三维渐进失效模型在层压板失效分析中的应用[C]. 北京: 第17届全国复合材料学术会议, 2012: 129-135.
JIA Liyong, HE Gao, BA Yuwei. Application of 3D progres-sive failure model in laminate failure analysis[C]. Beijing: Proceedings of the 17th National Composites Academic Conference, 2012: 129-135(in Chinese).
|
[25] |
LI J, ZHANG K, LI Y, et al. Influence of interference-fit size on bearing fatigue response of single-lap carbon fiber reinforced polymer/Ti alloy bolted joints[J]. Tribology International,2016,93:151-162. doi: 10.1016/j.triboint.2015.08.044
|