Optimization Forming Process of <scp>CFRP I</scp> ‐Shaped Stiffened Panel

ABSTRACT Carbon fiber reinforced polymer (CFRP) stiffened panels are widely used as primary load‐bearing structures due to their high strength‐to‐weight ratio. However, their forming process is susceptible to deformation and defects influenced by factors such as mold material, lay‐up sequence, curing temperature, and heating rate. This study presents a simulation‐based method for optimizing the forming process of CFRP I‐shaped stiffened panels. The numerical model integrates thermochemical analysis with a cure‐hardening instantaneous linear‐elastic model. Optimization of the lay‐up design, including the strategic addition of 0° plies, successfully suppressed torsional deformation in the upper flange and reduced overall panel distortion. The simulations indicate that both curing deformation and residual stress increase with higher curing temperatures and faster heating rates. Numerical and experimental results converged to identify an optimal process utilizing a rubber/stainless steel composite mold, a curing temperature of 393.15 K, and a heating rate of 2 K/min. This optimized setup reduced deformation and residual stress by 23% and 22%, respectively, compared with the baseline aluminum mold process. The proposed strategy significantly enhances the forming accuracy of CFRP stiffened panels and provides.

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Publication Details

Journal
Polymer Composites
Published
2026-03-20
DOI
https://doi.org/10.1002/pc.71021
Primary Topic
Epoxy Resin Curing Processes
Type
article
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article

Optimization Forming Process of CFRP I ‐Shaped Stiffened Panel

Yujiao Bai, J. Luo, Muhan Yan, Rongguo Wang et al.
Polymer Composites
Epoxy Resin Curing Processes
article

Optimization Forming Process of CFRP I ‐Shaped Stiffened Panel

Yujiao Bai, J. Luo, Muhan Yan, Rongguo Wang, Xinyu Zhang, Xin He, Wenzhen Qin, Guanjun Liu, Yuan Xie, Mingyu Wang, Weicheng Nie
article en

Abstract

ABSTRACT Carbon fiber reinforced polymer (CFRP) stiffened panels are widely used as primary load‐bearing structures due to their high strength‐to‐weight ratio. However, their forming process is susceptible to deformation and defects influenced by factors such as mold material, lay‐up sequence, curing temperature, and heating rate. This study presents a simulation‐based method for optimizing the forming process of CFRP I‐shaped stiffened panels. The numerical model integrates thermochemical analysis with a cure‐hardening instantaneous linear‐elastic model. Optimization of the lay‐up design, including the strategic addition of 0° plies, successfully suppressed torsional deformation in the upper flange and reduced overall panel distortion. The simulations indicate that both curing deformation and residual stress increase with higher curing temperatures and faster heating rates. Numerical and experimental results converged to identify an optimal process utilizing a rubber/stainless steel composite mold, a curing temperature of 393.15 K, and a heating rate of 2 K/min. This optimized setup reduced deformation and residual stress by 23% and 22%, respectively, compared with the baseline aluminum mold process. The proposed strategy significantly enhances the forming accuracy of CFRP stiffened panels and provides.

Polymer Composites
Aviation Industry Corporation of China (China) (CN), Beijing Institute of Technology (CN), Vaughn College of Aeronautics and Technology (US), Beijing Electronic Science and Technology Institute (CN), Harbin Institute of Technology (CN), Beijing Research Institute of Mechanical and Electrical Technology (CN), Aerospace Technology Institute (GB), Nanchang Hangkong University (CN)
Openalex Percentile: Top 13%
Epoxy Resin Curing Processes
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