Mohammad Ghaedsharaf (1), Jean-Evrard Brunel (2), Louis Laberge Lebel (1)
Composites Part B: Engineering, 218, April 2021. DOI: 10.1016/j.compositesb.2021.108938

Keywords

Fibers; Finite element analysis (FEA); Braiding; Micro-computed tomography (CT) scan; Digital element approach (DEA)

Abstract

This paper proposes a modeling methodology to predict the 3D and internal geometry of biaxial braids. Inspired by the digital element approach, braided yarns are modeled as a bundle of virtual fibers. Here we adopt truss elements to a virtual fiber with actual material properties instead of beam elements that have limitations due to the beam flexural rigidity. The mesoscopic morphology prediction of two common braid patterns of the diamond (1/1) and regular (2/2) are validated by a comprehensive quantitative comparison with X-ray micro-computed tomography (CT) scans of braided carbon fibers. We find that the fiber-level frictional behavior is able to explain the jammed state of braids wherein the frictional dissipation energy quickly grows, while the braid has a stable elongation, diameter, and braid angle. Parametric studies illustrate how the increase in the coefficient of friction affects the yarn cross-sectional shape, whereas it has an insignificant effect on the crimp and jammed state of braids. Models also reveal that changing a wide range of the fiber modulus of elasticity hardly impacts the mesoscopic morphology and crimp of the braids.

How Our Software Was Used

Dragonfly was used for quantitative analysis of the CT images. It was also used to tune the threshold of grayscale values to distinguish braided carbon fibers and voids in CT scans

Author Affiliation

(1) Advanced Composite and Fiber Structure Laboratory, Research Center for High Performance Polymer and Composite Systems, Department of Mechanical Engineering, Polytechnique Montréal, 2900, Boul. Édouard-Montpetit, University of Montréal Campus, Montréal, H3T 1J4, Canada.
(2) Bombardier Aerospace, 1800, Boul. Marcel-Laurin, Saint-Laurent, H4R 1K2, Canada.