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<pubDate xmlns="http://apache.org/cocoon/i18n/2.1">Sun, 10 May 2026 01:19:40 GMT</pubDate>
<dc:date>2026-05-10T01:19:40Z</dc:date>
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<title>Bioinspired 4D Printed Tubular/Helicoidal Shape Changing Metacomposites for Programmable Structural Morphing</title>
<link>http://hdl.handle.net/10985/26081</link>
<description>Bioinspired 4D Printed Tubular/Helicoidal Shape Changing Metacomposites for Programmable Structural Morphing
LE DUIGOU, Antoine; GRABOW, M.; SCARPA, F.; DESCHAMPS, J.; COMBESCURE, C.; LABSTIE, K.; DIRRENBERGER, Justin; CASTRO, M.; LAFONT, U.
Biological structures combine passive shape‐changing with force generation through intricate composite architectures. Natural fibers, with their tubular‐like structures and responsive components, have inspired the design of pneumatic tubular soft composite actuators. However, no development of passive structural actuation is available despite the recent rise of 4D printing. In this study, a biomimicry approach is proposed with inspiration from natural fiber architecture to create a novel concept of thermally active 4D printed tubular metacomposites. These metacomposites exhibit high mechanical performance and 3D‐to‐3D shape‐changing ability triggered by changes in temperature. A rotative printer is proposed for winding a continuous carbon fibers reinforced PolyAmide 6.I composite on a PolyAmide 6.6 polymer mandrel in a similar manner to the structure of cellulose microfibrils within the polysaccharide matrix of natural fiber cell‐walls. The resulting 4D printed tubular metacomposites exhibit programmable rotation and torque in response to thermal variations thanks to the control of their mesostructure and the overall geometry. Energy density values representing a trade‐off between the rotation and the torque are comparable to shape memory alloys when normalized by stiffness. Finally, a proof of concept for an autonomous solar tracker is presented, showcasing its potential for designing autonomous assemblies for structure morphing.
</description>
<pubDate>Wed, 02 Oct 2024 00:00:00 GMT</pubDate>
<guid isPermaLink="false">http://hdl.handle.net/10985/26081</guid>
<dc:date>2024-10-02T00:00:00Z</dc:date>
<dc:creator>LE DUIGOU, Antoine</dc:creator>
<dc:creator>GRABOW, M.</dc:creator>
<dc:creator>SCARPA, F.</dc:creator>
<dc:creator>DESCHAMPS, J.</dc:creator>
<dc:creator>COMBESCURE, C.</dc:creator>
<dc:creator>LABSTIE, K.</dc:creator>
<dc:creator>DIRRENBERGER, Justin</dc:creator>
<dc:creator>CASTRO, M.</dc:creator>
<dc:creator>LAFONT, U.</dc:creator>
<dc:description>Biological structures combine passive shape‐changing with force generation through intricate composite architectures. Natural fibers, with their tubular‐like structures and responsive components, have inspired the design of pneumatic tubular soft composite actuators. However, no development of passive structural actuation is available despite the recent rise of 4D printing. In this study, a biomimicry approach is proposed with inspiration from natural fiber architecture to create a novel concept of thermally active 4D printed tubular metacomposites. These metacomposites exhibit high mechanical performance and 3D‐to‐3D shape‐changing ability triggered by changes in temperature. A rotative printer is proposed for winding a continuous carbon fibers reinforced PolyAmide 6.I composite on a PolyAmide 6.6 polymer mandrel in a similar manner to the structure of cellulose microfibrils within the polysaccharide matrix of natural fiber cell‐walls. The resulting 4D printed tubular metacomposites exhibit programmable rotation and torque in response to thermal variations thanks to the control of their mesostructure and the overall geometry. Energy density values representing a trade‐off between the rotation and the torque are comparable to shape memory alloys when normalized by stiffness. Finally, a proof of concept for an autonomous solar tracker is presented, showcasing its potential for designing autonomous assemblies for structure morphing.</dc:description>
</item>
<item>
<title>Thermomechanical performance of continuous carbon fibre composite materials produced by a modified 3D printer</title>
<link>http://hdl.handle.net/10985/23581</link>
<description>Thermomechanical performance of continuous carbon fibre composite materials produced by a modified 3D printer
LE DUIGOU, Antoine; GRABOW, M.; CASTRO, M.; TOUMI, R.; UEDA, M.; MATSUZAKI, R.; HIRANO, Y.; DIRRENBERGER, Justin; SCARPA, F.; D'ELIA, R.; LABSTIE, K.; LAFONT, U.
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.&#13;
&#13;
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.&#13;
&#13;
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.
</description>
<pubDate>Wed, 01 Feb 2023 00:00:00 GMT</pubDate>
<guid isPermaLink="false">http://hdl.handle.net/10985/23581</guid>
<dc:date>2023-02-01T00:00:00Z</dc:date>
<dc:creator>LE DUIGOU, Antoine</dc:creator>
<dc:creator>GRABOW, M.</dc:creator>
<dc:creator>CASTRO, M.</dc:creator>
<dc:creator>TOUMI, R.</dc:creator>
<dc:creator>UEDA, M.</dc:creator>
<dc:creator>MATSUZAKI, R.</dc:creator>
<dc:creator>HIRANO, Y.</dc:creator>
<dc:creator>DIRRENBERGER, Justin</dc:creator>
<dc:creator>SCARPA, F.</dc:creator>
<dc:creator>D'ELIA, R.</dc:creator>
<dc:creator>LABSTIE, K.</dc:creator>
<dc:creator>LAFONT, U.</dc:creator>
<dc:description>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.&#13;
&#13;
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.&#13;
&#13;
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.</dc:description>
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