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Mechanics of Composite Materials

, Volume 55, Issue 5, pp 655–666 | Cite as

Static and Fatigue Characteristics of Pinned Metal-Composite Joints

  • G. Beketova
  • M. Shevtsova
  • V. SymonovEmail author
Article
  • 18 Downloads

Metal-composite joining methods currently rely almost exclusively on the adhesive bonding, the application of mechanical fasteners or a combination of the methods, the pros and cons of which are well known. In this article, a manufacturing-oriented solution for increasing the static and fatigue characteristics of metal composite bolted T-joints loaded in the out-of-plane direction by reinforcing the composite basement with a thin metal plate having die cut pins is proposed. Static load–displacement and fatigue life curves were obtained experimentally for different types of joints. The results obtained showed that, for a fiberglass/epoxy laminate, the solution proposed increased its static and fatigue failure loads by 64 and 50% respectively. It was also found that pinned adhesive joints were more effective than the conventional bolted ones at high-cycle loadings (the number of cycles exceeded 104).

Keywords

pinned metal-composite joints out-of-plane loading interlaminar static and fatigue strengths,pullouttest 

Notes

Acknowledgements

This work was performed with the financial support FP7 KhAI-ERA project “Integrating the National Aerospace University “KhAI” into ERA” (GA No 294311) and NETME Centre built in the frame NETME Centre project “New Technologies for Mechanical Engineering” (Reg. No. CZ.1.05/2.1.00/01.0002) with the financial support from the Operational Program Research and Development for Innovations of Czech Republic.

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Copyright information

© Springer Science+Business Media, LLC, part of Springer Nature 2019

Authors and Affiliations

  1. 1.National Aerospace University - “Kharkiv Aviation Institute”KharkivUkraine
  2. 2.Brno University of TechnologyFaculty of Mechanical EngineeringBrnoCzech Republic

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