Resources / Publications
Mohammad Ghaedsharaf (1), Jean-Evrard Brunel (2), Louis Laberge Lebel (1)
Composites Part A: Applied Science and Manufacturing, 150, September 2021. DOI: 10.1016/j.compositesa.2021.106637
Thermoplastic resin; Micro-mechanics; Process modeling; CT analysis
Thermoplastic braid-trusion is a composite manufacturing process that combines braiding and pultrusion of hybrid yarns containing reinforcement and polymer fibers. During pultrusion, the melting of the polymer fibers leads to complex morphological changes at the macro, meso and micro scales. We introduce here a multiscale numerical simulation methodology to model this process. In this methodology, braided yarns are modeled as bundles of virtual discrete fibers using chains of truss elements. A thermoplastic composite braided rod was pultruded according to the simulated braid-trusion. During braid-trusion, it was observed that the braid architecture was significantly modified, which was reliably predicted by the model through macroscopic measurements of 7.6% pitch elongation, 44.0% diameter reduction, and 45.0% nominal angle reorientation. The model also predicts yarns’ cross-section area having high local fiber volume fraction of about 60% due to yarn compaction during pultrusion. These predictions of mesoscopic morphology and internal geometry are quantitatively validated using X-ray micro-computed tomography (CT) scans of the braid-truded rod. Three local fiber orientation distributions of the in-plane, out-of-plane, and with respect to the longitudinal braid axis are extracted using micro-scale analysis of virtual fibers. We found that a significant amount of fibers are oriented around specific radii ranging from 30–70% and 60–100% of the outer radius before and after pultrusion, respectively. By contrast, the local fiber orientation is uniformly distributed along the pitch length. The microscale model also shows considerable discrepancies between local and nominal braid angles.
Dragonfly was used for the segmentation, 3D visualization, and quantitative analysis of CT data.
(1) Advanced Composite and Fiber Structure Laboratory (ACFSlab), Research Center for High Performance Polymer and Composite Systems (CREPEC), Department of Mechanical Engineering, Polytechnique Montréal, 2900 Boul. Édouard-Montpetit, Campus of the University of Montreal, Montreal, H3T 1J4, Canada.
(2) Bombardier Aerospace, 1800 Boul. Marcel-Laurin, Saint-Laurent, H4R 1K2, Canada.
Return to Publications list.