Friction spot joining of aluminum alloy 2024-t3 and carbon-fiber-reinforced polyphenylene sulfide composite laminate with additional pps film interlayer
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Universidade Federal de São Carlos
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Friction Spot Joining (FSpJ) is a prize-winning joining technique for hybrid
metal-polymer composite structures. This master thesis was devised to
investigate the feasibility of FSpJ of metal-composite structures with additional
film interlayer. Friction spot joints of aluminum alloy 2024-T3 and carbon-fiberreinforced
polyphenylene sulfide laminate composite with additional PPS film
interlayer were successfully produced. The highest peak temperature achieved
during the joining process was 417°C. DSC analysis demonstrated that the
degree of crystallinity decreased for the composite (from 22% to 12%) and
increased for the PPS film (from 7% to 27%) after joining. TGA analysis
indicated that no extensive thermo-mechanical degradation induced by the
joining process occurred. The main bonding mechanisms of FSp joint were
identified as macro- and micro-mechanical interlocking, as well as adhesion
forces. The process-related microstructural effects were evaluated and
correlated to the local mechanical performance of the joining parts through
micro and nanohardness. Further, mechanical grinding, sandblasting and
plasma activation surface pre-treatments were performed on the composite part
to enhance the adhesion between the joining parts. The generated surface
features due to the surface pre-treatments were correlated to the mechanical
performance of the joints. Sandblasted specimens showed the best mechanical
performance among the surface pre-treatments used in this work. The lap shear
strength of joints with interlayer (2703 ± 114 N up to 3069 ± 166 N) was up to
55% higher than the corresponding joints without film. The fatigue life of the
joints with interlayer was 4 times longer in comparison with those without
interlayer; superior fatigue strength was also observed. The durability of the
joints was evaluated through hydrothermal accelerated aging; the maximum
reduction in initial strength was 12.4% for 28 days of aging. Finally, the failure
mechanisms of the joints were discussed, demonstrating a mixture of adhesivecohesive
failure mode.
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ANDRÉ, Natália Manente. Friction spot joining of aluminum alloy 2024-t3 and carbon-fiber-reinforced polyphenylene sulfide composite laminate with additional pps film interlayer. 2015. Dissertação (Mestrado em Ciência e Engenharia de Materiais) – Universidade Federal de São Carlos, São Carlos, 2015. Disponível em: https://repositorio.ufscar.br/handle/20.500.14289/8275.