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Title: Numerical simulation of multi-layered textile composite reinforcement forming

Journal Article · · AIP Conference Proceedings
DOI:https://doi.org/10.1063/1.3589633· OSTI ID:21516787
; ;  [1]
  1. University of Lyon, INSA-Lyon, LaMCos, CNRS UMR 5259, F-69621 (France)

One important perspective in aeronautics is to produce large, thick or/and complex structural composite parts. The forming stage presents an important role during the whole manufacturing process, especially for LCM processes (Liquid Composites Moulding) or CFRTP (Continuous Fibre Reinforcements and Thermoplastic resin). Numerical simulations corresponding to multi-layered composite forming allow the prediction for a successful process to produce the thick parts, and importantly, the positions of the fibres after forming to be known. This paper details a set of simulation examples carried out by using a semi-discrete shell finite element made up of unit woven cells. The internal virtual work is applied on all woven cells of the element taking into account tensions, in-plane shear and bending effects. As one key problem, the contact behaviours of tool/ply and ply/ply are described in the numerical model. The simulation results not only improve our understanding of the multi-layered composite forming process but also point out the importance of the fibre orientation and inter-ply friction during formability.

OSTI ID:
21516787
Journal Information:
AIP Conference Proceedings, Vol. 1353, Issue 1; Conference: ESAFORM 2011: 14. international ESAFORM conference on material forming, Belfast, Northern Ireland (United Kingdom), 27-29 Apr 2011; Other Information: DOI: 10.1063/1.3589633; (c) 2011 American Institute of Physics; ISSN 0094-243X
Country of Publication:
United States
Language:
English