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Thermomechanical performance of continuous carbon fibre composite materials produced by a modified 3D printer

Article dans une revue avec comité de lecture
Author
ccLE DUIGOU, Antoine
457614 Institut de Recherche Dupuy de Lôme [IRDL]
GRABOW, M.
457614 Institut de Recherche Dupuy de Lôme [IRDL]
CASTRO, M.
457614 Institut de Recherche Dupuy de Lôme [IRDL]
TOUMI, R.
457614 Institut de Recherche Dupuy de Lôme [IRDL]
UEDA, M.
481231 Nihon University
MATSUZAKI, R.
238740 Tokyo University of Science [Tokyo]
HIRANO, Y.
47050 Japan Aerospace Exploration Agency [Tokyo] [JAXA]
ccDIRRENBERGER, Justin
86289 Laboratoire Procédés et Ingénierie en Mécanique et Matériaux [PIMM]
SCARPA, F.
220393 University of Bristol [Bristol]
243745 Advanced Composites Centre for Innovation and Science [ACCIS]
D'ELIA, R.
110103 Institut Clément Ader [ICA]
LABSTIE, K.
417643 IRT Saint Exupéry - Institut de Recherche Technologique
LAFONT, U.
85250 Agence Spatiale Européenne = European Space Agency [ESA]

URI
http://hdl.handle.net/10985/23581
DOI
10.1016/j.heliyon.2023.e13581
Date
2023-02
Journal
HELIYON

Abstract

First of all, this article aimed to evidence the role of a modified printer developed for continuous carbon fibre reinforced PolyAmide (cCF/PA6-I) together with the use of a fully open slicing step on the printing quality and the longitudinal/transverse tensile and in-plane shear properties. A comprehensive assessment of the microstructure and properties with a similar material (cCF/PA6-I), but produced with a commercial printer (i.e., Markforged® MarkTwo) has been achieved. Our customised printer and the open slicer used have made possible to better control the print conditions (i.e., layer height and distance between filaments), to reduce the porosity from more than 10% to about 2% and improve the mechanical properties. Moreover, the understanding of the behaviour of these 3D printed composites with wide-ranging external temperatures is mandatory for future use in a severe environment and/or development of new thermally active 4D printed composites. The 3D printed cCF/PA6-I composites have been then thermomechanically characterised along different printing directions (0, 90 and ± 45°) from −55 to +100 °C. Unlike the longitudinal properties that hardly change with temperature, the transverse and in-plane shear stiffness and strength of these 3D printed composites were particularly sensitive to temperature variations, with decreases of 25–30% and 30–55%, respectively. This was due to the high sensitivity of the polymer matrix, the fibre/matrix and interfilament interfaces when the composites were loaded along those directions, because damages induced by internal thermal stresses. Fractography has also been carried out to reveal damage mechanisms.

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