Experimental evaluation of interlaminar shear stress of CAJRAL type fibre metal laminates prepared with surface treated aluminium sheet by sobbing technique

• Autorzy: Asirvatham A.D. , Hynes N.R.J. , Selvan P. , Vignesh N.J. , Jebaraj D.J.J. , Benita B.

Identyfikatory

DOI

10.5604/01.3001.0054.4640

• Języki publikacji: EN

Abstrakty

EN

Purpose: Fiber metal laminates (FML) are a new composite, particularly the CAJRAL type laminate, consisting of aluminium and a carbon/jute/epoxy composite. The present work aims to develop low-density Fiber metal laminates (FML) with good mechanical properties for aerospace applications. Design/methodology/approach: FML combines the good characteristics of metal, such as ductility and durability, with the benefits of fibre composite materials, such as high specific strength, high specific stiffness, good corrosion resistance and fatigue resistance. The present work introduces an FML consisting of aluminium and Carbon/Jute/epoxy layers. The FML was produced by the hand lay-up technique. The aluminium sheets were surface-treated with the sobbing method. Two combinations of laminate sequencing were selected: Ca 0°/Ca 45°/Al/Ju 45° and Ca 0°/Al/Ca 0°/Al/Ju 0°. Findings: The structure characterisation after bending tests is shown and discussed. The three point-bending tests are conducted according to ASTM D 2344 standard specifications. Sample-1 (Ca 0°/Ca 45°/Al/Ju 45°/Ju 45°/Al/Ca 45°/Ca 0°) is a better result. Research limitations/implications: Preliminary studies have shown that the metal layers in the laminates and the composite carbon layer, particularly in the bend area of the laminate, significantly impact the nature of the damage. Laminate indicates the complexity of the degradation process of these materials. Practical implications: The orientation of the reinforcing fibres influences the degree of the laminate structure and affects the ability to form laminates. An important factor influencing the properties of the laminate as a whole is to provide high adhesive properties of the composite-metal connections. Originality/value: By replacing aluminium with jute. It is observed that the tensile and flexure stresses of the CAJRAL with Ca 0°/Ca 45°/Al/Ju 45°/Ju 45°/Al/Ca 45°/Ca 0° are more compared with Ca 0°/Al/Ca 0°/Al/Ju 0°/Ju 0°/Al/Ca 0°/Al/Ca 0°.

Słowa kluczowe

EN

fiber metal laminates; three-point bending test; interlaminar shear stress; laminate sequencing

PL

laminaty włókno-metal; test zginania trójpunktowego; naprężenie ścinające międzywarstwowe; sekwencjonowanie laminatów

• Wydawca: International OCSCO World Press
• Czasopismo: Archives of Materials Science and Engineering
• Rocznik: 2024
• Tom: Vol. 125, nr 1
• Strony: 15--21
• Opis fizyczny: Bibliogr. 35 poz.

Twórcy

autor

Asirvatham A.D.

• Department of Mechanical Engineering, Jayaraj Annapakiam CSI College of Engineering, Nazareth, Thoothukudi 628617, Tamil Nadu, India

autor

Hynes N.R.J.

• Faculty of Mechanical Engineering, Opole University of Technology, ul. Proszkowska 76, 45-758 Opole, Poland

• https://orcid.org/0000-0002-2679-473X

autor

Selvan P.

• Department of Mechanical Engineering, Mepco Schlenk Engineering College, Sivakasi, 626005, Tamil Nadu, India

autor

Vignesh N.J.

• Department of Mechanical Engineering, Mepco Schlenk Engineering College, Sivakasi, 626005, Tamil Nadu, India

autor

Jebaraj D.J.J.

• Department of Mechanical Engineering, Mepco Schlenk Engineering College, Sivakasi, 626005, Tamil Nadu, India

autor

Benita B.

• Department of Computer Science and Engineering, Francis Xavier Engineering College, Tirunelveli 627002, India

Bibliografia

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• [5] N.R.J. Hynes, R. Sankaranarayanan, M. Kathiresan, P. Senthamaraikannan, A. Khan, A.M. Asiri, I. Khan, Synthesis, properties, and characterization of carbon nanotube-reinforced metal matrix composites, in: A. Khan, M. Jawaid, Inamuddin, A.M. Asiri (eds), Nanocarbon and its Composites, Woodhead Publishing Series in Composites Science and Engineering, Woodhead Publishing, Sawston, Cambridge, 2019, 805-830. DOI: https://doi.org/10.1016/B978-0-08-102509-3.00027-4
• [6] J. Jerome, N.R.J. Hynes, R. Sankaranarayanan, Mechanical behavioural testing of fibre metal laminate composites, AIP Conference Proceedings 2220/1 (2020) 140035. DOI: https://doi.org/10.1063/5.0001244
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• [31] R. Sankaranarayanan, N.R.J. Hynes, D. Li, A. Chrysanthou, S.T. Amancio-Filho, Review of Research on Friction Riveting of Polymer/Metal Light Weight Multi-Material Structures, Transactions of the Indian Institute of Metals 74 (2021) 2541-2553. DOI: https://doi.org/10.1007/s12666-021-02356-w
• [32] R. Sankaranarayanan, N.R.J. Hynes, M.P. Nikolova, J.B. Królczyk, Self-Pierce Riveting: Development and Assessment for Joining Polymer - Metal Hybrid Structures in Lightweight Automotive Applications, Polymers 15/20 (2023) 4053. DOI: https://doi.org/10.3390/polym15204053
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• [34] M.K. Gurunathan, N.R.J. Hynes, O.A. Al-Khashman, M. Brykov, N. Ganesh, A. Ene, Study on the Impact and Water Absorption Performance of Prosopis juliflora and Glass Fibre Reinforced Epoxy Composite Laminates, Polymers 14/15 (2022) 2973. DOI: https://doi.org/10.3390/polym14152973
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