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| Azevedo, Nuno Monteiro |
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Van Innis, Charline Van Innis
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (8/8 displayed)
- 2024Ultra tough architected joints through single manufacturing step
- 2024Ultra-tough architected adhesive joints for integrated composite processing and bondingcitations
- 2023Mechanics of PEI-expoxy interfaces
- 2023Fracture toughness of architected joints involving crack instabilities
- 2023Ultra tough architected joints through single step bonding process with tunable properties
- 2022Integrated manufacturing and toughening of composite joints using a PEI film
- 2022Composite joint toughening by multiscale architecturing through integrated manufacturing
- 2021Bonding polymer Composites with PEI film: crack trapping and enhanced fracture resitstance
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document
Composite joint toughening by multiscale architecturing through integrated manufacturing
Abstract
The intensive use of Carbon Fibre Reinforced Polymer (CFRP) Composites in aerospace is motivated by their high strength to weight ratio. However, the manufacturing of complex aeronautic structures combining metallic and composite parts requires an efficient bonding process [1]. Joints obtained through bonding with adhesives suffer from low to moderate toughness [2] and the process requires multiple steps separating the manufacturing of the composite parts and the bonding. Several strategies have been proposed to enhance the joint toughness, such as introducing a mesh or cavities in the bondline [3]. One strategy to improve the efficiency of the process is to bond the metal part to the composite panels during the curing process, without using any adhesive. On the road to the integrated bonding of hybrid metallic composite structures, the present works investigates potential toughening strategies by bonding composites via co-curing of two composites parts while relying on joint architecturing principles.