Process-performance integrated modeling to virtually optimize parameters for preforming of multi-layer woven fabric composite prepregs

The design of manufacturing parameters is crucial to efficiently produce woven fabric composite parts using automatic manufacturing process. To optimize blank geometry and stacking sequence in prepreg compression molding (PCM) for minimum material waste and maximum final product performance, a virtual design method based on process-performance integrated modeling was developed for woven fabric composite preforming. This design method starts with the preforming modeling realized via a non-orthogonal material model that can continuously trace warp and weft yarn directions. Experimental validation indicates that the prediction error of the preforming modeling for multi-layer woven fabric composites is less than 3 % in profiles of the produced parts and within 4 % in yarn angles. With the preforming modeling, the blank geometry represented by finite element mesh was virtually modified through design iterations, so as to obtain the ideal blank geometry that could yield the smallest amount of material in the binder region to be trimmed. Then, the ideal blank geometry was applied in real preforming, and the results proved that the material waste caused by trimming could be controlled to 9 %∼14 % with this modeling-based design method, much lower than the 30 %∼50 % value in current industrial practice. Afterwards, various stacking sequences were input to the preforming modeling, and the predicted yarn orientations, yarn angles and part geometry from the preforming modeling were mapped to the performance analysis, so as to numerically identify the configuration for highest elastic stiffness of the final part. Experimental validation illustrates that this process-performance integrated modeling can lead to less than 4.15 % prediction error in part stiffness, and it can successfully determine the stacking sequence for highest part performance without the need for real manufacturing and performance experiments.

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Publication Details

Journal
Composites Part A Applied Science and Manufacturing
Published
2025-05-17
DOI
https://doi.org/10.1016/j.compositesa.2025.109032
Citations
3
Primary Topic
Epoxy Resin Curing Processes
Type
article
Field-Weighted Citation Impact
2.14
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article

Process-performance integrated modeling to virtually optimize parameters for preforming of multi-layer woven fabric composite prepregs

Weizhao Zhang, Wanrui Zhang, Yifeng Xiong, Rui Li et al.
3 citations
Composites Part A Applied Science and Manufacturing
Epoxy Resin Curing Processes
2.14
article

Process-performance integrated modeling to virtually optimize parameters for preforming of multi-layer woven fabric composite prepregs

Weizhao Zhang, Wanrui Zhang, Yifeng Xiong, Rui Li, Deyong Sun, Jianchao Zou, Chongrui Tang
article en
3 citations

Abstract

The design of manufacturing parameters is crucial to efficiently produce woven fabric composite parts using automatic manufacturing process. To optimize blank geometry and stacking sequence in prepreg compression molding (PCM) for minimum material waste and maximum final product performance, a virtual design method based on process-performance integrated modeling was developed for woven fabric composite preforming. This design method starts with the preforming modeling realized via a non-orthogonal material model that can continuously trace warp and weft yarn directions. Experimental validation indicates that the prediction error of the preforming modeling for multi-layer woven fabric composites is less than 3 % in profiles of the produced parts and within 4 % in yarn angles. With the preforming modeling, the blank geometry represented by finite element mesh was virtually modified through design iterations, so as to obtain the ideal blank geometry that could yield the smallest amount of material in the binder region to be trimmed. Then, the ideal blank geometry was applied in real preforming, and the results proved that the material waste caused by trimming could be controlled to 9 %∼14 % with this modeling-based design method, much lower than the 30 %∼50 % value in current industrial practice. Afterwards, various stacking sequences were input to the preforming modeling, and the predicted yarn orientations, yarn angles and part geometry from the preforming modeling were mapped to the performance analysis, so as to numerically identify the configuration for highest elastic stiffness of the final part. Experimental validation illustrates that this process-performance integrated modeling can lead to less than 4.15 % prediction error in part stiffness, and it can successfully determine the stacking sequence for highest part performance without the need for real manufacturing and performance experiments.

Composites Part A Applied Science and ManufacturingVol. 197
Northwestern Polytechnical University (CN), Chinese University of Hong Kong (HK), Chinese University of Hong Kong, Shenzhen (CN), Northwestern Polytechnic University (US)
Openalex Percentile: Top 14%
Epoxy Resin Curing Processes
2.14
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