Study on the low-velocity impact response of the repaired carbon fiber-reinforced plastic laminates: Bonded versus scarf repair

被引:4
作者
Chen, Xuanzhen [1 ,2 ]
Peng, Yong [1 ,2 ]
Wang, Kui [1 ,2 ]
Wang, Xin [1 ,2 ]
Liu, Zhixiang [1 ,2 ]
Huang, Zhiqiang [1 ,2 ]
Zhang, Honghao [3 ]
机构
[1] Cent South Univ, Key Lab Traff Safety Track, Minist Educ, Changsha, Peoples R China
[2] Cent South Univ, Joint Int Res Lab Key Technol Rail Traff Safety, Changsha, Peoples R China
[3] Shandong Univ, Sch Mech Engn, Key Lab High Efficiency & Clean Mech Manufacture, Minist Educ, Jinan, Peoples R China
基金
中国国家自然科学基金;
关键词
CFRP laminates; failure mechanism; finite element analysis (FEA); low-velocity impact; PROGRESSIVE FAILURE; COMPOSITE; DAMAGE; PATCH; SIMULATION; PERFORMANCE; BEHAVIOR;
D O I
10.1002/pc.28128
中图分类号
TB33 [复合材料];
学科分类号
摘要
Experimental and simulation studies of the response of bonded-repaired and scarf-repaired carbon fiber-reinforced polymer laminates under the low-velocity impact (LVI) were carried out. The center- and eccentric-repaired laminates were prepared for experiments. The experimental results verify the validity of the finite element model in terms of the force response and different modes of damage. The effect of impact energy and the variation of repair position on the impact response of the laminate was investigated based on the benchmark model. The bonded repaired laminates have higher peak impact forces and lower energy absorption than the scarf-repaired laminates; the damage of the bonded repaired laminate is mainly intralaminar damage and delamination damage of the patch; the adhesive of the scarf repair is prone to failure, leading to poor impact resistance. The relative positions of the impact point and the patch determine the impact response of a laminate repaired at different locations. The impact point at the edge of the patch has a detrimental effect on the repaired laminate. The impact point vertical position near the bottom hole edge of the parent plate in the scarf-repaired case harms the impact resistance of the laminate.Highlights The low-velocity impact response of bonded versus scarf-repaired laminates was compared. Bonding repairs provide superior impact resistance to damaged laminates than scarf repairs. The risk of adhesive failure in scarf repair is significantly higher than in bonded repair. The relative position of the damage (repair) to the impact point critically influences the impact response. Impacts near the edge of the initial damage hole can cause severe damage to scarf-repaired laminates.
引用
收藏
页码:5300 / 5319
页数:20
相关论文
共 38 条
[1]   Progress of novel techniques for lightweight automobile applications through innovative eco-friendly composite materials: A review [J].
Agarwal, Jyoti ;
Sahoo, Swarnalata ;
Mohanty, Smita ;
Nayak, Sanjay K. .
JOURNAL OF THERMOPLASTIC COMPOSITE MATERIALS, 2020, 33 (07) :978-1013
[2]  
ASTM D3518/D3518M-13, 2008, STANDARD TEST METHOD
[3]   Cohesive law estimation of adhesive joints in mode II condition [J].
Azevedo, J. C. S. ;
Campilho, R. D. S. G. ;
da Silva, F. J. G. ;
Faneco, T. M. S. ;
Lopes, R. M. .
THEORETICAL AND APPLIED FRACTURE MECHANICS, 2015, 80 :143-154
[4]   Potential repair techniques for automotive composites: A review [J].
Balakrishnan, Venkateswaran Santhanakrishnan ;
Seidlitz, Holger .
COMPOSITES PART B-ENGINEERING, 2018, 145 :28-38
[5]   Review and benchmark study on the analysis of low-velocity impact on composite laminates [J].
Bogenfeld, Raffael ;
Kreikemeier, Janko ;
Wille, Tobias .
ENGINEERING FAILURE ANALYSIS, 2018, 86 :72-99
[6]   An analytical scaling approach for low-velocity impact on composite structures [J].
Bogenfeld, Raffael ;
Kreikemeier, Janko ;
Wille, Tobias .
COMPOSITE STRUCTURES, 2018, 187 :71-84
[7]  
Camanho P.P., 2002, Mixed-Mode Decohesion Finite Elements for the Simulation of Delamination in Composite Materials
[8]   3D printed continuous fiber reinforced composite lightweight structures: A review and outlook [J].
Cheng, Ping ;
Peng, Yong ;
Li, Shixian ;
Rao, Yanni ;
Le Duigou, Antoine ;
Wang, Kui ;
Ahzi, Said .
COMPOSITES PART B-ENGINEERING, 2023, 250
[9]   Low-velocity impact performance and effect factor analysis of scarf-repaired composite laminates [J].
Cheng, Xiaoquan ;
Zhang, Jie ;
Bao, Jianwen ;
Zeng, Benyin ;
Cheng, Yujia ;
Hu, Renwei .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2018, 111 :85-93
[10]   Effects of stacking sequence and rotation angle of patch on low velocity impact performance of scarf repaired laminates [J].
Cheng, Xiaoquan ;
Du, Xiaoyuan ;
Zhang, Jie ;
Zhang, Jikui ;
Guo, Xin ;
Bao, Jianwen .
COMPOSITES PART B-ENGINEERING, 2018, 133 :78-85