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Bolted Joints in Three Axially Braided Carbon Fibre/Epoxy Textile Composites with Moulded-in and Drilled Fastener Holes

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Abstract

Experimental behaviour of bolted joints in triaxial braided (0°/±45°) carbon fibre/epoxy composite laminates with drilled and moulded-in fastener holes has been investigated in this paper. Braided laminates were manufactured by vacuum infusion process using 12 K T700S carbon fibres (for bias and axial tows) and Araldite LY-564 epoxy resin. Moulded-in fastener holes were formed using guide pins which were inserted in the braided structure prior to the vacuum infusion process. The damage mechanism of the specimens was investigated using ultrasonic C-Scan technique. The specimens were dimensioned to obtain a bearing mode of failure. The bearing strength of the specimens with moulded-in hole was reduced in comparison to the specimens with drilled hole, due to the increased fibre misalignment angle following the pin insertion procedure. An improvement on the bearing strength of moulded-in hole specimens might be developed if the specimen dimensions would be prepared for a net-tension mode of failure where the fibre misalignment would not have an effect as significant as in the case of bearing failure mode, but this mode should be avoided since it leads to sudden catastrophic failures.

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References

  1. Pastore C.M., Masters J.E., Foye R.L., Gowayed Y.A.: Mechanical properties of triaxially braided composites: experimental and analytical results. J. Compos. Technol. Res. 15(2), 112–122 (1993)

    Article  Google Scholar 

  2. Naik RA. Analysis of woven and braided fabric reinforced composites. (1994)

  3. Portanova M, Masters J.: Standard methods for bolt-bearing testing of textile composites. (1995)

  4. Portanova MA, Masters J.: Standard methods for open hole tension testing of textile composites. (1995)

  5. Portanova MA.: Standard methods for unnotched tension testing of textile composites. (1995)

  6. Masters JE, Portanova MA.: Standard test methods for textile composites. (1996)

  7. Potluri P.: Braiding. Wiley Encyclopedia of Composites. (2012)

  8. Fink A., Camanho P., Andrés J., Pfeiffer E., Obst A.: Hybrid CFRP/titanium bolted joints: performance assessment and application to a spacecraft payload adaptor. Compos. Sci. Technol. 70(2), 305–317 (2010)

    Article  Google Scholar 

  9. http://www.airbus.com/presscentre/corporate-information/key-documents/ Accessed 27 Nov 2015

  10. Atas A., Mohamed G., Soutis C.: Modelling delamination onset and growth in pin loaded composite laminates. Compos. Sci. Technol. 72(10), 1096–1101 (2012)

    Article  Google Scholar 

  11. Atas A., Mohamed G.F., Soutis C.: Progressive failure analysis of bolted joints in composite laminates. Plastics, Rubber and Composites. 41(4/5), 209–214 (2012)

    Article  Google Scholar 

  12. Ataş A., Soutis C.: Strength prediction of bolted joints in CFRP composite laminates using cohesive zone elements. Compos. Part B. 58, 25–34 (2014)

    Article  Google Scholar 

  13. Zitoune R., Crouzeix L., Collombet F., Tamine T., Grunevald Y.-H.: Behaviour of composite plates with drilled and moulded hole under tensile load. Compos. Struct. 93(9), 2384–2391 (2011)

    Article  Google Scholar 

  14. Chang L.-W., Yau S.-S., Chou T.-W.: Notched strength of woven fabric composites with moulded-in holes. Composites. 18(3), 233–241 (1987)

    Article  Google Scholar 

  15. Nejhad M.G., Chou T.: Compression behaviour of woven carbon fibre-reinforced epoxy composites with moulded-in and drilled holes. Composites. 21(1), 33–40 (1990)

    Article  Google Scholar 

  16. Fujita A., Maekawa Z., Hamada H., Yokoyama A.: Mechanical behavior and fracture mechanism in flat braided composites. Part 2: braided flat bar with a circular hole. J. Reinf. Plast. Compos. 11, 618–632 (1992)

    Article  Google Scholar 

  17. Fujita A., Hamada H., Maekawa Z., Ohno E., Yokoyama A.: Mechanical behavior and fracture mechanism in flat braided composites. Part 3: mechanically fastened joint in flat braided bar. J. Reinf. Plast. Compos. 13(8), 740–755 (1994)

    Article  Google Scholar 

  18. Brookstein D.S., Tsiang T.-H.: Load-deformation behavior of composite cylinders with integrally-formed braided and with machined circular holes. J. Compos. Mater. 19(5), 476–487 (1985)

    Article  Google Scholar 

  19. Wang Y.: Bearing behavior of triaxially braided flat and tubular composites. Appl. Compos. Mater. 1(3), 217–229 (1994)

    Article  Google Scholar 

  20. Gautam M, Potluri P, Ogin S, Jain P.: Necking behaviour of flattened tubular braided composites. 20th International Conference on Composite Materials, 19-24th July 2015, Copenhagen (2015)

  21. Gautam M. et al.: Hybrid composite wires for tensile armours in flexible risers: manufacturing and mechanical characterisation. Compos. Struct. 150, 73–83 (2016)

    Article  Google Scholar 

  22. Torayca T700s Datasheet, Technical Data Sheet No. CFA-005, Toray Carbon Fibers America, Inc. (2002)

  23. Lin H, Brown LP, Long AC. (eds): Modelling and simulating textile structures using TexGen. Advanced Materials Research, Trans Tech Publ (2011)

  24. ASTM D5961/D5961M: Standard Test Method for Bearing Response of Polymer Matrix Composite Laminates. ASTM International, West Conshohocken, PA, USA (2010)

    Google Scholar 

  25. Araldite LY564/Aradur 2954 Hot Curing Epoxy System Data Sheet, Huntsman Advanced Materials GmbH (2007)

  26. ASTM D3171: Standard Test Methods for Constituent Content of Composite Materials. ASTM International, West Conshohocken (1999)

    Google Scholar 

  27. Ataş A., Soutis C.: Subcritical damage mechanisms of bolted joints in CFRP composite laminates. Compos. Part B. 54, 20–27 (2013)

    Google Scholar 

  28. Fahr A., Kandeil A.Y.: Ultrasonic C-scan inspection of composite materials. Engineering Journal of Qatar University. 5, 201–222 (1992)

  29. Hasiotis T., Badogiannis E., Tsouvalis N.G.: Application of ultrasonic C-scan techniques for tracing defects in laminated composite materials. Strojniški vestnik-Journal of Mechanical Engineering. 57(3), 192–203 (2011)

    Article  Google Scholar 

  30. Argon A.: Fracture of composites. Treatise on materials science and technology. 1, 79–114 (2013)

    Article  Google Scholar 

Download references

Acknowledgments

The scientific and technological research council of Turkey (TÜBİTAK) is gratefully acknowledged for the post-doctoral scholarship granted to the first author.

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Ataş, A., Gautam, M., Soutis, C. et al. Bolted Joints in Three Axially Braided Carbon Fibre/Epoxy Textile Composites with Moulded-in and Drilled Fastener Holes. Appl Compos Mater 24, 449–460 (2017). https://doi.org/10.1007/s10443-016-9542-z

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