Test on damage and mechanical property degradation of composite laminate with fastener subjected to lightning strike

被引:0
|
作者
Yin J. [1 ]
Li S. [1 ]
Yang Z. [2 ]
Yao X. [3 ]
Chang F. [1 ]
Xiao Y. [1 ]
机构
[1] Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an
[2] Department of Combat Command, Aviation University of Air Force, Changchun
[3] The State Key Laboratory of Electrical Insulation and Power Equipment, Xi'an Jiao Tong University, Xi'an
关键词
Braided composites; Composite laminate; Fastener; Lightning strike damage; Tensile mechanical property;
D O I
10.13801/j.cnki.fhclxb.20170814.001
中图分类号
学科分类号
摘要
Artificial lightning strike testing was performed on a series of carbon woven fabric/epoxy laminate with metal fastener, and damage was assessed using visual inspection, ultrasonic testing, micro X-ray inspection and high-power microscope to analyze the damage mode, damage mechanism and damage characteristic of composite laminate with metal fastener under lightning current direct effect, meanwhile, mechanical property degradation extent of composite laminate with metal fastener was also assessed using material mechanical property test system. Research results indicate that due to the lightning current distributing effect aroused by mental fastener, delamination is the mainly damage mode of composite laminate with metal fastener when subjected to lightning strike, and it is distributed along the whole thickness direction of laminate. There is a lightning current intensity threshold about whether composite laminate with metal fastener occurs lightning strike damage, and when the lightning current intensity is lower than it, composite laminate with metal fastener will not appear lightning strike damage. During the process of static tension, because lightning strike damage around fastener hole will arouse the effect of stress distribution, the tensile loading capacity of composite laminate with metal fastener with lightning strike damage increases first and then decreases with the increasing lightning peak current. © 2018, Editorial Office of Acta Materiae Compositae Sinica. All right reserved.
引用
收藏
页码:1131 / 1138
页数:7
相关论文
共 18 条
  • [1] Uman M.A., Rakov V.A., The interaction of lightning with airborne vehicles, Progress in Aerospace Sciences, 39, 1, pp. 61-81, (2003)
  • [2] Taylor R., Fiber Composite Aircraft-capability and Safety, (2008)
  • [3] Du S.Y., Guan Z.D., Strategic considerations for development of advanced composite technology for large commercial aircraft in China, Acta Materiae Compositae Sinica, 25, 1, pp. 1-10, (2008)
  • [4] Du S.Y., Advanced composite materials and aerospace engineering, Acta Materiae Compositae Sinica, 24, 1, pp. 1-12, (2007)
  • [5] Rupke E., Lightning Direct Effects Handbook, (2002)
  • [6] Hirano Y., Katsumata S., Iwahori Y., Et al., Artificial lightning testing on graphite/epoxy composite laminate, Composite Part A, 41, 10, pp. 1461-1470, (2010)
  • [7] Wang F.S., Ji Y.Y., Yu X.S., Et al., Ablation damage assessment of aircraft carbon fiber/epoxy composite and its protection structures suffered from lightning strike, Composite Structures, 145, pp. 226-241, (2016)
  • [8] Li Y.C., Li R.F., Lai H., Et al., Effect of hygrothermal aging on the damage characteristics of carbon woven fabric/epoxy laminates subjected to simulated lightning strike, Materials and Design, 99, pp. 477-489, (2016)
  • [9] Li Y.C., Li R.F., Lu L.Y., Et al., Experimental study of damage characteristics of carbon woven fabric/epoxy laminates subjected to lightning strike, Composite Part A: Applied Science and Manufacturing, 79, pp. 164-175, (2015)
  • [10] Ogasawara T., Hirano Y., Yoshimura A., Coupled thermal-electrical analysis for carbon fiber/epoxy composites exposed to simulated lighting current, Composites Part A: Applied Science and Manufacturing, 41, 8, pp. 973-981, (2010)