Axial energy absorption characteristics and trigger mechanism of C-channel CFRP thin-walled structures

被引:0
作者
Lv R. [1 ,2 ]
Ren Y. [1 ,2 ]
机构
[1] State Key Laboratory of Advanced Design and Manufacturing for Vehicle Body, Hunan University, Changsha
[2] College of Mechanical and Vehicle Engineering, Hunan University, Changsha
来源
Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica | 2023年 / 40卷 / 10期
基金
中国国家自然科学基金;
关键词
composite; crashworthiness; damage model; progressive failure; triggering mechanism;
D O I
10.13801/j.cnki.fhclxb.20230112.003
中图分类号
学科分类号
摘要
To improve the crashworthiness of C-channel carbon fiber reinforced polymer (CFRP) thin-walled structures, the energy absorption characteristics and failure behavior of the structures under axial crushing load were studied. Considering the delamination effect, the progressive damage model of C-channel CFRP thin-walled structure was established. The quadratic stress failure and the nonlinear damage evolution criterion based on the mixed-mode energy method were used to predict the initial interlaminar failure and damage evolution, respectively. For this structure, the hybrid-angle chamfer trigger and steeple trigger were proposed, and the effects of different trigger configurations on the crashworthiness index and failure mode of C-channel CFRP thin-walled structures were compared and analyzed. The results show that the initial peak load corresponding to the hybrid-angle chamfer trigger decreases with the increase of the hybrid angle; The initial peak load can be effectively reduced by reducing the contact area between the hybrid-angle chamfer trigger and the loading plate at the initial crushing stage; The hybrid-angle steeple trigger can improve the failure process and has a positive effect on improving the crashworthiness of the structure. © 2023 Beijing University of Aeronautics and Astronautics (BUAA). All rights reserved.
引用
收藏
页码:5947 / 5956
页数:9
相关论文
共 31 条
  • [1] XIONG Jian, LI Zhibin, LIU Huibin, Et al., Advances in aerospace lightweight composite shell structure[J], Acta Materiae Compositae Sinica, 38, 6, pp. 1629-1650, (2021)
  • [2] SONG Tao, YU Xuduo, JIANG Shengda, Et al., Axial crushing response and failure mechanism of variable stiffness carbon fiber/epoxy resin composite thin-walled tube, Acta Materiae Compositae Sinica, 38, 11, pp. 3586-3600, (2021)
  • [3] WANG Yang, WU Zhibin, LIU Fu, Crush experiment of composite cargo floor stanchions[J], Acta Materiae Compositae Sinica, 37, 9, pp. 2200-2206, (2020)
  • [4] JIANG H Y, REN Y R., Crashworthiness and failure analysis of steeple-triggered hat-shaped composite structure under the axial and oblique crushing load[J], Composite Structures, 229, (2019)
  • [5] REN Yiru, XIANG Jinwu, LUO Zhangping, Crashworthiness analysis and design of aircraft fuselage structure, Engineering Mechanics, 30, 10, pp. 296-304, (2013)
  • [6] WANG Xueqin, ZHANG Zhendong, MA Dawei, Et al., Quasi-static compression experimental study on energy absorption characteristics of multicellular structures filled with carbon fiber reinforced epoxy composite tubes[J], Acta Materiae Compositae Sinica, 38, 9, pp. 2887-2896, (2021)
  • [7] ZHUANG Weimin, LIU Yang, LIU Xiyang, Simulation on delamination failure of carbon fiber reinforced epoxy resin composite circular tube under axial crushing, Journal of Mechanical Engineering, 56, 12, pp. 107-115, (2020)
  • [8] KIM J S, YOON H J, SHIN K B., A study on crushing behaviors of composite circular tubes with different reinforcing fibers[J], International Journal of Impact Engineering, 38, 4, pp. 198-207, (2011)
  • [9] XIAO Pei, SU Xuan, MOU Haolei, Et al., Quasi-static axial compression performance tests and numerical simulation for composite corrugated plate, Journal of Vibration and Shock, 40, 15, pp. 156-164, (2021)
  • [10] ZHU G H, SUN G Y, LI G Y, Et al., Modeling for CFRP structures subjected to quasi-static crushing[J], Composite Structures, 184, pp. 41-55, (2018)