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A study of tensile residual strength of composite laminates under different patch-repaired series

  • M. H. Ding*
  • , S. Zhan
  • , Y. H. Tang
  • , L. Wang
  • , D. Q. Ma
  • , R. G. Wang
  • *Corresponding author for this work
  • Hafei Aviation Industry Co. Ltd.
  • Harbin Institute of Technology
  • College of Materials Science and Chemical Engineering, Harbin Engineering University

Research output: Contribution to journalConference articlepeer-review

Abstract

The tensile behavior of composite laminate structures repaired by bonding external patches was studied in the paper. Two different types of patches including wedge patches and inverted wedge patches were used and failure mechanisms, failure load and strength predictions were studied. A convenient and fast method of building 2-D finite element modeling (FEM) of laminate structure repaired was proposed and the strength of repaired laminate structures was calculated by FEM. The results showed that more than 80% tensile strength of the undamaged laminate could be recovered by bonding patch repairs. Moreover, the results indicated that the strength of inverted wedge patches repair were higher than that of wedge patches repair. FEM simulation results indicated that high stress concentration was found along the edges of invert patches and the most weakness part located in the adhesive bondline. FEM analysis results showed that the strength predicted matched well with the test strength.

Original languageEnglish
Article number012018
JournalIOP Conference Series: Materials Science and Engineering
Volume242
Issue number1
DOIs
StatePublished - 13 Oct 2017
Event2017 3rd International Conference on Applied Materials and Manufacturing Technology, ICAMMT 2017 - Changsha, China
Duration: 23 Jun 201725 Jun 2017

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