China Plastics ›› 2021, Vol. 35 ›› Issue (2): 22-28.DOI: 10.19491/j.issn.1001-9278.2021.02.004

• Materials and Properties • Previous Articles     Next Articles

Study on Three⁃point Bending Properties of Foam Sandwich Composites under Different Reinforcement Methods

HE Peixi1, LAI Jiamei1(), WAN Yibiao1, ZHAO Chenxu1, HUANG Zhichao2   

  1. 1.Polymer Processing Research Lab,School of Mechanical and Electric Engineering,Nanchang University,Nanchang 330031,China
    2.Key Laboratory for Conveyance and Equipment of the Ministry of Education,East China Jiaotong University,Nanchang 330013,China
  • Received:2020-08-05 Online:2021-02-26 Published:2021-02-22

Abstract:

This paper reported an investigation on the three-point bending properties of the foam sandwich composites prepared through stitching and rib reinforcement methods. A three-point bending experiment was carried out with a universal testing machine for the seamed and unstitched carbon fiber, glass fiber, and glass-carbon hybrid fiber foam sandwich composites, with the corresponding load-deflection curves presented in the paper. The flexural properties of the seamed carbon fiber foam sandwich composites were further studied by means of a reinforcing rib method. The results indicated that the performance of the glass-carbon hybrid fiber foam sandwich composites was improved in comparison with the glass fiber foam sandwich composites. The introduction of reinforcing ribs increased the bending strength of the stitched carbon fiber foam sandwich composites from 17.79 MPa to 37.47 MPa. The bending performance of the stitched carbon fiber foam sandwich composite was improved with an increase in the number of reinforcement ribs. At the same number of reinforcement ribs, the sandwich composites achieved optimum bending strength of 46.96 MPa when the reinforcement ribs were laid in parallel. Next was under the 20 ° cross-laying of the reinforcement ribs and least was under the cross-laying of the reinforcement ribs.

Key words: foam sandwich structure, fiber reinforcement, matrix rib, flexural behavior

CLC Number: