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Impact of Assembly Method on the Strength of Single-Lap Joints of Aircraft Aluminum Alloy Sheets

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Języki publikacji
EN
Abstrakty
EN
The paper presents a comparative analysis of the strength properties of single-lap assembly joints. Single-lap joints are commonly used in various structures because of their strength properties. Three types of joints, widely used in modern structures, were prepared and tested: adhesive, rivet, and hybrid adhesive-rivet joints. The experiments were carried out using aluminum alloy EN AW-2024, a structural material used in aviation. In the adhesive joints, the substrates were joined using a two-component epoxy adhesive composed of Epidian 53 epoxy resin and polymide curing agent (PAC) – Epidian 53/PAC/100:80. The rivet joints were formed using steel-aluminum blind rivets. The rivets were arranged in four different configurations. One of the very important structural factors considered when designing single-lap assembly joints is overlap length. In the present study, two overlap lengths were tested: 12 mm and 20 mm. The assembly joints were subjected to strength tests. Tensile-shear strength was determined. The results were analyzed statistically.
Twórcy
  • Faculty of Mechanical Engineering, Lublin University of Technology, Nadbystrzycka 36, 20-618 Lublin, Poland
Bibliografia
  • 1. Arenas J.M., Narbón J.J., Alía C. Optimum adhesive thickness in structural adhesives joints using statistical techniques based on Weibull distribution. International Journal of Adhesion and Adhesives, (3)30, 2010, 160–165.
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  • 10. Marques E.A.S., da Silva L.F.M., Banea M.D., Carbas R.J.C. Adhesive Joints for Low- and High- Temperature Use: An Overview. The Journal of Adhesion. (91)7, 2015, 556–585.
  • 11. Miturska I., Rudawska A. Mechanical properties of selected epoxy adhesives. Informatyka, Automatyka, Pomiary w Gospodarce i Ochronie Środowiska, 7(4), 2017, 88–91.
  • 12. Rudawska A. Influence of the Thickness of Joined Elements on Lap Length of Aluminium Alloy Sheet Bonded Joints. Advances in Science and Technology Research Journal, 9, 2015, 35–44.
  • 13. Sadowski T. Zarzeka-Raczkowska E. Hybrid Adhesive Bonded and Riveted Joints – Influence of Rivet Geometrical Layout on Strength of Joints / Połączenia Hybrydowe Klejowo-Nitowe – Wpływ Geometrii Rozmieszczenia Nitów Na Wytrzymałość Połączeń. Archives of Metallurgy and Materials, 57(4), 2012, 1127–1135.
  • 14. Seth A., Vance J.M., Oliver J.H. Virtual reality for assembly methods prototyping: a review. Virtual Reality, 15(1), 2011, 5–20.
  • 15. Silva L.F.M., Öchsner A. Modeling of adhesively bonded joints. Springer, 2008.
  • 16. Silva L.F.M., Pirondi, A. Hybrid adhesive joints. Springer, 2011.
  • 17. Taib A.A., Boukhili R., Achiou S., Gordon S., Boukehili H. Bonded joints with composite adherends. Part I. Effect of specimen configuration, adhesive thickness, spew fillet and adherend stiffness on fracture. International Journal of Adhesion and Adhesives. 26(4), 2006, 226–236.
  • 18. BS EN 4400–2:2019 standard – Aerospace series. Aluminium and aluminium- and magnesium- alloys. Technical specification. Aluminium and aluminium alloy sheet and strip.
  • 19. http://www.aerospacemetals.com/aluminum-distributor.html [access date: 12.12.2019]
  • 20. PN-EN 573–1:2006 standard – Aluminium and aluminium alloys – Chemical composition and types of plasticised products.
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-b4f493bc-fec8-4746-97c4-a4d0d61d243e
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