Influences of adhesive film on bonded-bolted hybrid single-lap joints’ performance

Abstract

Abstract: A 3D model of bonded-bolted hybrid single -lap joints contending is established based on ABAQUS, damage criteria and stiffness attenuation criterion are added in order to achieve progressive damage analysis. The model is used to analyze the influences on the structure while the thickness and ductility was altered. Results indicate that applied with brittle adhesive film, thicknessincrease can improve the bearing performance of the structure. Varying degrees of ductile adhesive film could provide similar improvement to the bearing performance of the structure. The proposed calculating methods and conclusions could provide reference to composite structure design.

Key words: , composites, adhesive film, hybrid single-lap joints, cumulative damage

CLC Number:

V250
TB33

XU Chen, SUN Y ongbo. Influences of adhesive film on bonded-bolted hybrid single-lap joints’ performance[J]. Journal of Civil Aviation University of China, 2021, 39(2): 61-64.

References 8

[1]	KIM K S, YI Y M, CHO G R, et al. Failure prediction and strength improvement of uni-directional compositesingle lap bonded joints[J]. CompositeStructures, 2008, 82(4): 513-520.
[2]	LEE Y H, LIM D W, CHOI J H, et al. Failure load evaluation and prediction of hybrid composite double lap joints[J]. Composite Structures, 2010, 92(12): 2916-2926.
[3]	XIAO Y, ISHIKAWA T. Bearing strength and failure behavior of boltedcomposite joints (part II：Modeling and simulation）[J]. Composites Science and Technology, 2005, 65(7/8): 1032-1043.
[4]	KALLMEYER A R, STEPHENS R I. A finite element model for predicting time-dependent deformations and damage accumulation in laminated composite bolted joints[J]. Journal of Composite Materials, 1999, 33(9): 794-826.
[5]	REIFSNIDER K. The mechanics of composite strength evolution[J].Composites Science and Technology, 2000, 60(12/13): 2539-2546.
[6]	KIM Y W, HONG C S. Progressive failure model for the analysis of laminated composites based on finite element approach[J]. Journal of Reinforced Plastics and Composites, 1992, 11(10): 1078-1092.
[7]	CHANG F K, SPRINGER G S. The strengths of fiber reinforced composite bends[J]. Journal of Composite Materials, 1986, 20(1): 30-45.
[8]	SONG M G, KWEON J H, CHOI J H, et al. Effect of manufacturingmethods on the shear strength of composite single-lap bonded joints[J]. Composite Structures, 2010, 92(9): 2194-2202.

[1]	CAI Jinga , LIU Hanlei a , HUO Haifenga , ZHI Yanfei b , REN Yanlongb. Fatigue damage pattern and microstructure study of ECC [J]. Journal of Civil Aviation University of China, 2024, 42(1): 59-64.
[2]	WANG Hui , ZHANG Wenjie , LIU jie , CHEN Linfeng , LI Zenan. Flight delay prediction model based on CART algorithm [J]. Journal of Civil Aviation University of China, 2022, 40(3): 35-40.
[3]	ZHANG Peng , BAI Yanhui. Static source error correction of civil aircraft based on stepwise regression analysis [J]. Journal of Civil Aviation University of China, 2022, 40(2): 1-5.
[4]	ZHAI Wenpeng, LIU Runnan, ZHU Chengyuan. Optimization of taxiway based on improved Dijkstra algorithm [J]. Journal of Civil Aviation University of China, 2022, 40(1): 1-6.
[5]	ZHAO Fangran, ZHOU Shengliang, HUO Haifeng. Experimental study on hydrophobic ice suppression performance of modified emulsified asphalt [J]. Journal of Civil Aviation University of China, 2021, 39(6): 49-53.
[6]	JU Chenyang , FENG Wengang , HE Xiaochun. Research on information sharing model of civil aviation security based on blockchain [J]. Journal of Civil Aviation University of China, 2021, 39(6): 43-48.
[7]	QU Jingyi , CHEN Xuyang , JU Peng , LIU Fang , ZHANG Xiongwei . Flight delay visualization system based on ES-Redis [J]. Journal of Civil Aviation University of China, 2021, 39(6): 20-27.
[8]	YANG Lin , LI Chunzhu , ZHANG Nan , LU Tingting. Research on Departure Flight Schedule Optimization of Pudong Airport Based on Capacity Flow Matching [J]. Journal of Civil Aviation University of China, 2021, 39(5): 7-10.
[9]	YANG Jianzhong, LIU Ming, CHEN Xiyuan. Fault simulation of electro-hydrostatic actuator system of aircraft considering nonlinear factors [J]. Journal of Civil Aviation University of China, 2021, 39(4): 54-59.
[10]	TIAN Jing, HU Hexiang. Fault diagnosis of aero-engine gas path based on GA-LSSVM [J]. Journal of Civil Aviation University of China, 2021, 39(3): 29-33.
[11]	YANG Yonggang , SONG Wei . Flight control and simulation of quad-rotor UAV under wind field disturbance [J]. Journal of Civil Aviation University of China, 2021, 39(3): 16-21.
[12]	WANG Li, Lei. High-precision position solution method for airport scene monitoring [J]. Journal of Civil Aviation University of China, 2021, 39(2): 21-25.
[13]	ZHENG Fengmin, AN Y an. Calculation of maximum failure speed of military aircraft [J]. Journal of Civil Aviation University of China, 2021, 39(2): 7-11.
[14]	WANG Fei. Stationarity and nonlinearity test of air traffic flow time series [J]. Journal of Civil Aviation University of China, 2021, 39(2): 1-6.
[15]	SU Jingxin, ZHAO Wenhao, CHEN Dong, LU Pengcheng. Flexural properties of repaired composite laminate structure under hygrothermal conditions [J]. Journal of Civil Aviation University of China, 2020, 38(2): 60-64.