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Open Access

Real-time control for autoclave curing process of CFRP composites considering tool-part interaction

Wenyuan TANGa,bLiang HEcXinyu HUIa,b( )Jianwen NIUa,bYingjie XUa,b( )Rutong YANGa,bYutong LIUa,b
State IJR Center of Aerospace Design and Additive Manufacturing, Northwestern Polytechnical University, Xi’an 710072, China
Shaanxi Engineering Laboratory of Aerospace Structure Design and Application, Northwestern Polytechnical University, Xi’an 710072, China
AVIC Xi’an Aircraft Industry (Group) Company LTD, Xi’an 710089, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

An integrated real-time control methodology is introduced to mitigate process-induced challenges, namely temperature overshoot, uneven cure, and interfacial shear stress, during the autoclave curing of Carbon Fiber-Reinforced Polymer (CFRP) composites. First, a high-fidelity Finite Element (FE) model incorporating tool-part interaction is developed to reveal the curing process of the composites, wherein the interaction is characterized by friction interface modeling with experimentally measured cure-dependent friction coefficients. The accuracy of FE model is confirmed through experimental tests on a doubly curved T-stiffened composite panel. This validated model then generates a dataset of curing temperature profile and associated defect information, which is used to train a customized Long Short-Term Memory (LSTM) neural network. We culminate in a real-time control framework that actively optimizes the curing process by integrating LSTM-based state prediction with Q-learning-driven decision logic. The optimized thermal profile demonstrates a clear performance enhancement over the traditional multi-dwell approach, achieving marked reductions in temperature difference, Degree of Cure (DoC) difference and tool-part interface shear stress, which provides more insights for intelligent composite manufacturing.

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Chinese Journal of Aeronautics

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Cite this article:
TANG W, HE L, HUI X, et al. Real-time control for autoclave curing process of CFRP composites considering tool-part interaction. Chinese Journal of Aeronautics, 2026, 39(3). https://doi.org/10.1016/j.cja.2025.103948

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Received: 15 January 2025
Revised: 05 February 2025
Accepted: 09 March 2025
Published: 14 November 2025
© 2025 The Author(s). Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).