Quantification of structural response and edge orientation of Chopped Tape Thermoplastic Composites in net-shaped specimens

Journal Article (2023)
Author(s)

D.E. Gulmez (TU Delft - Aerospace Manufacturing Technologies)

Jesus Maldonado (University of Applied Sciences and Arts Northwestern Switzerland)

Kunal Masania (TU Delft - Aerospace Manufacturing Technologies)

J. Sinke (TU Delft - Aerospace Manufacturing Technologies)

C. A. Dransfeld (TU Delft - Aerospace Manufacturing Technologies)

Research Group
Aerospace Manufacturing Technologies
Copyright
© 2023 D.E. Gülmez, Jesus Maldonado, K. Masania, J. Sinke, C.A. Dransfeld
DOI related publication
https://doi.org/10.1016/j.compstruct.2023.117302
More Info
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Publication Year
2023
Language
English
Copyright
© 2023 D.E. Gülmez, Jesus Maldonado, K. Masania, J. Sinke, C.A. Dransfeld
Research Group
Aerospace Manufacturing Technologies
Volume number
321
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Abstract

Chopped Tape Thermoplastic Composites (CTTCs) offer high formability and performance for complex-shaped components in the aerospace and automotive industries. However, the mesoscopic discontinuity leads to spatial variabilities and correspondingly high scatter in the elastic properties of CTTCs due to the random orientations of chopped tapes and chopped tape-cavity edge interactions. Here we propose a new approach to investigate the effect of mould cavity edges on chopped tape orientation and hence the mechanical properties of CTTCs. Based on this approach, a Set Voronoi tessellation was implemented to represent the variability of local Young's Modulus and chopped tape-cavity edge interactions occurring during the manufacturing process. It was confirmed that the chopped tapes align along the edges, and progressively transition to a random orientation towards the middle of the specimen. The results were validated on moulded specimens and demonstrated the ability to deconvolute the edge interaction.