Confluent 3D-assembly of fibrous structures
Source abstract
Abstract
The ability to independently control fiber alignments and structural geometry is critical for design of optimal three-dimensional (3D) fibrous structures. We present a novel method to 3D-assemble carbon fiber structures, containing no seams or adhesive joints, using a confluence of several textile methodologies. A variety of complex structural shapes with tailored fiber topologies are demonstrated to be achievable. These optimized structures are shown to have unprecedented static and dynamic strength as well as damage tolerance and ductility. For example, the energy absorption capacity of a 3D-assembled carbon fiber prismatic sandwich structure is shown to be 300% greater than a high performance metallic counterpart.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Additive Manufacturing and 3D Printing Technologies · Cellular and Composite Structures · Innovations in Concrete and Construction Materials
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (27)
Show source-provided references
1. A composite matter of alignment10.1126/science.1215841 ↗
2. Nature's hierarchical materials10.1016/j.pmatsci.2007.06.001 ↗
3. Feather structure, biomechanics and biomimetics: the incredible lightness of being10.1007/s10336-013-1038-0 ↗
4. Nanomechanical properties of bird feather rachises10.1098/rsif.2014.0961 ↗
5. Chou · 1992
6. Review of applications for advanced three-dimensional fibre textile composites10.1016/S1359-835X(99)00034-2 ↗
7. Fibre damage in the manufacture of advanced three-dimensional woven composites10.1016/S1359-835X(03)00213-6 ↗
8. Effect of weaving damage on the tensile properties of three-dimensional woven composites10.1016/S0263-8223(02)00108-3 ↗
9. Fiber insertion process for improved damage tolerance in aircraft laminates
10. Review of z-pinned composite laminates10.1016/j.compositesa.2007.08.016 ↗
11. A comparative study of tensile properties of non-crimp 3D orthogonal weave and multi-layer plain weave e-glass composites10.1016/j.compositesa.2009.04.032 ↗
12. Compressive response of glass fiber composite sandwich structures10.1016/j.compositesa.2013.07.007 ↗
13. Hybrid core carbon fiber composite sandwich panels: fabrication and mechanical response10.1016/j.compstruct.2013.10.002 ↗
14. Microstructure and mechanical properties of 3D- five-directional braided composites10.1016/j.ijsolstr.2009.05.013 ↗
15. Geometrical modelling and control of a triaxial braiding machine for producing 3D preforms10.1016/S1359-835X(03)00061-7 ↗
16. Some recent advances in the fabrication and design of three-dimensional textile preforms: a review10.1016/S0266-3538(99)00093-7 ↗
17. Lord · 1973
18. TohoTenax; STS40 Datasheet. Available at: http://www.tohotenax-eu.com.
19. Nils Malmgren AB; NM Infusion 664 Datasheet.
20. DIAB Group; Divinycell H250 Datasheet.
21. Damage tolerance assessment of composite sandwich panels with localised damage10.1016/j.compscitech.2005.05.026 ↗
22. High-velocity impact behaviour of prestressed composite plates under bird strike loading10.1155/2012/372167 ↗
23. ERG Aerospace Corporation, http://www.ergaerospace.com/.
24. Improving the bending strength and energy absorbtion of corrugated sandwich composite structures10.1016/j.matdes.2013.05.018 ↗
25. Zenkert · 1997
26. Failure criteria for unidirectional fiber composites10.1115/1.3153664 ↗
27. The impulsive response of sandwich beams: analytical and numerical investigation of regimes of behaviour10.1016/j.jmps.2006.07.001 ↗