Experimental study on the low-velocity impact and post-impact flexural properties of curved CFRP laminates reinforced by pre-hole Z-pinning (PHZ) technique

被引:11
|
作者
Teng, Xuebei [1 ]
Xu, Yingjie [1 ,2 ]
Hui, Xinyu [1 ]
Zhang, Weihong [1 ]
Dai, Haicong [3 ]
Liu, Weiwei [1 ]
Ma, Chengyan [4 ]
Li, Yujun [1 ]
机构
[1] Northwestern Polytech Univ, Sch Mech Engn, Xian, Shaanxi, Peoples R China
[2] Northwestern Polytech Univ, Shaanxi Prov Key Lab Aeronaut & Aerosp Struct Tec, Xian, Shaanxi, Peoples R China
[3] China Shanghai Aerosp Equipments Manufacturer Co, Shanghai, Peoples R China
[4] Shandong Inst Nonmetall Mat, Jinan, Shandong, Peoples R China
基金
中国国家自然科学基金;
关键词
Z-pin; CFRP laminate; low-velocity impact; residual flexural strength; MECHANICAL-PROPERTIES; FATIGUE PROPERTIES; COMPRESSION; DAMAGE; BEHAVIOR; TEMPERATURE; COMPOSITES; STRENGTH; HYBRIDIZATION; PERFORMANCE;
D O I
10.1080/15376494.2022.2077485
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper presents an experimental investigation into the effect of Z-pin on the low-velocity impact response and flexural properties after impact of the curved CFRP laminates. The Z-pinned specimens are produced using a low-damage pre-hole Z-pinning (PHZ) technique. Unpinned and Z-pinned [0/45/-45/90](4S) specimens are both subjected to low-velocity impacts. Nondestructive inspection technique is used to evaluate the internal damage after impact. Subsequently, three-point bending tests are performed to characterize the flexural properties of the impacted specimens. Experimental results indicate that Z-pinned laminate, due to the bridging traction across the delamination cracks provided by pins, can provide an efficient crack arrest mechanism both in impact and bending after impact tests. Compared with the unpinned specimens, the delamination damage projection area (DDPA) is reduced by 28.5-63.5%, depending on the diameter and volume fraction of Z-pin. In addition, Z-pin could improve the residual flexural strength significantly. The specimens with a high Z-pin volume fraction have excellent damage tolerance, leading to an 18.1-76.1% improvement in the residual flexural strength compared with unpinned specimens.
引用
收藏
页码:3479 / 3490
页数:12
相关论文
共 24 条
  • [21] Experimental and simulation study on bonded repaired low-velocity impact of carbon fiber reinforced plastic laminates for rail vehicles
    Chen, Xuanzhen
    Peng, Yong
    Wang, Kui
    Wang, Xin
    Liu, Zhixiang
    Huang, Zhiqiang
    Zhang, Honghao
    JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T, 2024, 28 : 446 - 458
  • [22] Numerical Simulating and Experimental Study on the Woven Carbon Fiber-Reinforced Composite Laminates under Low-Velocity Impact
    Liu, Hanyang
    Tang, Zhanwen
    Pan, Lingying
    Zhao, Weidong
    Sun, Baogang
    Jiang, Wenge
    VIII INTERNATIONAL CONFERENCE ON TIMES OF POLYMERS AND COMPOSITES: FROM AEROSPACE TO NANOTECHNOLOGY, 2016, 1736
  • [23] Experimental and simulation study on bonded repaired low-velocity impact of carbon fiber reinforced plastic laminates for rail vehicles
    Chen, Xuanzhen
    Peng, Yong
    Wang, Kui
    Wang, Xin
    Liu, Zhixiang
    Huang, Zhiqiang
    Zhang, Honghao
    Journal of Materials Research and Technology, 2024, 28 : 446 - 458
  • [24] Failure mechanisms in carbon fiber reinforced plastics (CFRP)/aluminum (Al) adhesive bonds subjected to low-velocity transverse pre-impact following by axial post-tension
    Liu, Xinglong
    Shao, Xuefei
    Li, Qing
    Sun, Guangyong
    COMPOSITES PART B-ENGINEERING, 2019, 172 : 339 - 351