Chinese Journal of Mechanical Engineering >

2018 , Vol. 31 >Issue 6: 112 - 112

DOI: https://doi.org/10.1186/s10033-018-0305-7

Mechanism and Robotics

Effect of Cycling Low Velocity Impact on Mechanical and Wear Properties of CFRP Laminate Composites

  • Yang Sun ,
  • Zhen-Bing Cai ,
  • Song-Bo Wu ,
  • Jian-Hua Liu ,
  • Jia-Xin Yu
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  • 1. Tribology Research Institute, Key Lab of Advanced Technologies of Materials, Southwest Jiaotong University, Chengdu 610031, China;
    2. Key Laboratory of Testing Technology for Manufacturing Process of Ministry of Education, Southwest University of Science and Technology, Mianyang 621010, China

收稿日期: 2018-02-03

  网络出版日期: 2019-07-23

基金资助

Supported by National Natural Science Foundation of China (Grant Nos. U1530136, 51627806), Young Scientifc Innovation Team of Science and Technology of Sichuan Province of China (Grant No. 2017TD0017), and Opening Project of Key Laboratory of Testing Technology for Manufacturing Process of China (Grant Nos. 2016-01, Southwest University of Science and Technology)

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Effect of Cycling Low Velocity Impact on Mechanical and Wear Properties of CFRP Laminate Composites

  • Yang Sun ,
  • Zhen-Bing Cai ,
  • Song-Bo Wu ,
  • Jian-Hua Liu ,
  • Jia-Xin Yu
Expand
  • 1. Tribology Research Institute, Key Lab of Advanced Technologies of Materials, Southwest Jiaotong University, Chengdu 610031, China;
    2. Key Laboratory of Testing Technology for Manufacturing Process of Ministry of Education, Southwest University of Science and Technology, Mianyang 621010, China

Received date: 2018-02-03

  Online published: 2019-07-23

Supported by

Supported by National Natural Science Foundation of China (Grant Nos. U1530136, 51627806), Young Scientifc Innovation Team of Science and Technology of Sichuan Province of China (Grant No. 2017TD0017), and Opening Project of Key Laboratory of Testing Technology for Manufacturing Process of China (Grant Nos. 2016-01, Southwest University of Science and Technology)

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摘要

The mechanical and wear properties of CFRP laminate were investigated using a method of cycling low velocity impact, to study the trend and mechanism of impact resistance of the CFRP laminate under repeated impact during its service process. The interface responses of CFRP laminate under different impact kinetic energy during the cycling impact process were studied were studied experimentally, such as impact contact duration, deformation and energy absorption. The worn surface morphologies were observed through optical microscopy and a 3-D surface profiler and the cross-sectional morphologies were observed through SEM to investigate the mechanism of impact material damage. Based on a single-degree-of-freedom damping vibration model, the normal contact stiffness and contact damping of the material in different wear stages were calculated. It shows the failure process of CFRP laminate damaged by accumulated absorption energy under the cycling impact of different initial kinetic energy. The results indicate that the stiffness and damping coefficients will change at different impact velocities or cycle numbers. The damage mechanism of CFRP laminates under cycling low kinetic energy is delamination. After repeated experiments, it was found that there was a threshold value for the accumulated absorption energy before the failure of the CFRP laminate.

关键词： CFRP laminate; Low velocity impact; Impact resistance; Accumulated absorption energy threshold; Delamination

本文引用格式

Yang Sun , Zhen-Bing Cai , Song-Bo Wu , Jian-Hua Liu , Jia-Xin Yu . Effect of Cycling Low Velocity Impact on Mechanical and Wear Properties of CFRP Laminate Composites[J]. Chinese Journal of Mechanical Engineering, 2018 , 31(6) : 112 -112 . DOI: 10.1186/s10033-018-0305-7

Abstract

The mechanical and wear properties of CFRP laminate were investigated using a method of cycling low velocity impact, to study the trend and mechanism of impact resistance of the CFRP laminate under repeated impact during its service process. The interface responses of CFRP laminate under different impact kinetic energy during the cycling impact process were studied were studied experimentally, such as impact contact duration, deformation and energy absorption. The worn surface morphologies were observed through optical microscopy and a 3-D surface profiler and the cross-sectional morphologies were observed through SEM to investigate the mechanism of impact material damage. Based on a single-degree-of-freedom damping vibration model, the normal contact stiffness and contact damping of the material in different wear stages were calculated. It shows the failure process of CFRP laminate damaged by accumulated absorption energy under the cycling impact of different initial kinetic energy. The results indicate that the stiffness and damping coefficients will change at different impact velocities or cycle numbers. The damage mechanism of CFRP laminates under cycling low kinetic energy is delamination. After repeated experiments, it was found that there was a threshold value for the accumulated absorption energy before the failure of the CFRP laminate.

Key words： CFRP laminate; Low velocity impact; Impact resistance; Accumulated absorption energy threshold; Delamination

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