Effect of gap and overlap on mode Ⅱ interlaminar fracture toughness of automated fiber placement prepreg laminates

被引:0
|
作者
Fan ZHANG [1 ,2 ]
Xin LIU [1 ,2 ]
Yaoyao YE [1 ,2 ]
Qisen CHEN [1 ,2 ]
Qiang XU [1 ,2 ]
Yunbo BI [1 ,2 ]
机构
[1] China State Key Laboratory of Fluid Power and Mechatronic System, School of Mechanical Engineering,Zhejiang University
[2] Key Laboratory of Advanced Manufacturing Technology of Zhejiang Province, School of Mechanical Engineering,Zhejiang
关键词
D O I
暂无
中图分类号
V262 [飞机制造]; TB33 [复合材料];
学科分类号
摘要
Automated Fiber Placement(AFP) technology facilitates the manufacturing process of composite structures with complex geometry owing to its high efficiency and accuracy.However,the unavoidable imperfections induced by the automated layup method bring challenges to the stability of the final mechanical properties of composites.The influence of AFP-induced gaps and overlaps on the mode Ⅱ interlaminar fracture process of oven-cured laminates is experimentally investigated and explicitly revealed.End-Notched Flexure(ENF) tests were performed to measure the interlaminar fracture toughness of unidirectional laminates under three different defect configurations,namely "Gap" "Overlap" and "Gap & Overlap".A marginal decline(about-1.2% in non-precracked tests,-5.1% in precracked tests) and an obvious increase(about 15.2% in nonprecracked tests,5.2% in precracked tests) in fracture toughness were observed for the "Gap" group and the "Overlap" group,respectively.Fractographic studies which involve the metallographic observation and Scanning Electron Microscopy(SEM) observation revealed that the increases in fracture area and crack length helped improve the fracture toughness of the "Overlap" group.However,the resin-rich area with high porosity induced by gaps was detrimental to the delamination resistance.To capture the interlaminar stress distribution local to imperfections,a three-dimensional numerical model was established.Gap defects facilitate the local delamination process,and the overlap defect postpones the damage onset and the propagation.
引用
收藏
页码:390 / 401
页数:12
相关论文
共 50 条
  • [31] Effect of low temperature on mode I and mode II interlaminar fracture toughness of CFRP-steel hybrid laminates
    Koord, J.
    Voelkerink, O.
    Petersen, E.
    Huehne, C.
    COMPOSITES PART B-ENGINEERING, 2023, 262
  • [32] Influence of fiber bridging on Mode I interlaminar fracture toughness of composites
    Wang, B. (b.wang@nwpu.edu.cn), 1600, Chinese Society of Astronautics (34):
  • [34] Mode I interlaminar fracture toughness of organic fiber reinforced plastics
    Sembokuya, H
    Hojo, M
    Kemmochi, K
    ADVANCED COMPOSITES LETTERS, 1997, 6 (03) : 71 - 74
  • [35] Effect of material nonlinearity on the toughness evaluation in quasi-static mode II interlaminar fracture toughness tests of composite laminates
    Yashiro, Shigeki
    Yamasaki, Tomohiro
    Nagai, Hiroto
    Yoshimura, Akinori
    ENGINEERING FRACTURE MECHANICS, 2021, 253
  • [36] Mode I interlaminar fracture toughness of CFRP laminates reinforced with short aramid fibers
    Wang, Binhua
    Dong, Nan
    Ding, Guangzhi
    JOURNAL OF ADHESION SCIENCE AND TECHNOLOGY, 2020, 34 (23) : 2522 - 2536
  • [37] Mixed Mode I/II Interlaminar Fracture Toughness of Carbon Fiber/RTM-6 Laminates Manufactured by VARTM
    Mendonca Sales, Rita de Cassia
    Guimaraes, Fernando
    Gouvea, Ricardo Francisco
    Candido, Geraldo Mauricio
    Donadon, Mauricio Vicente
    POLYMER COMPOSITES, 2019, 40 : E1029 - E1040
  • [38] An experimental method to measure the mode-III interlaminar fracture toughness of composite laminates
    Suemasu, H
    COMPOSITES SCIENCE AND TECHNOLOGY, 1999, 59 (07) : 1015 - 1021
  • [39] Response of mode II interlaminar fracture toughness of composite laminates with carbon nanotubes interlayer
    Liu, L.
    Liang, Y. M.
    Xu, G. Y.
    INTERNATIONAL CONFERENCE ON SMART MATERIALS AND NANOTECHNOLOGY IN ENGINEERING, PTS 1-3, 2007, 6423
  • [40] Loading rate dependency of Mode I interlaminar fracture toughness for unidirectional composite laminates
    Liu, Huifang
    Nie, Hailiang
    Zhang, Chao
    Li, Yulong
    COMPOSITES SCIENCE AND TECHNOLOGY, 2018, 167 : 215 - 223