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Study on the bolt-pin joint structure of carbon fabric composites

  • Xi'an Jiaotong University
  • Xi'an Aerospace Composites Research Institute

Research output: Contribution to journalArticlepeer-review

1 Scopus citations

Abstract

This paper presents a new composites joint structure, bolt-pin joint structure of carbon fabric composites which can provide high loading axes joint. The bear strength of fabric/epoxy composites lamination and the load of bolt-pin structure were measured. The results show that maximum bear strength of fabric/Epoxy composites laminations is 887 MPa, which exceeds 0/90 fiber lamination; bolt-pin joint structure of carbon fabric composites was advantage compared with joint of metal frame, whose forming technology is convenient and joint efficiency is high.

Original languageEnglish
Pages (from-to)473-476
Number of pages4
JournalCailiao Kexue yu Gongyi/Material Science and Technology
Volume15
Issue number4
StatePublished - Aug 2007

Keywords

  • Bear strength
  • Bolt-pin joint
  • Carbon fabric composites
  • Joint efficiency

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