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Study on Adhesion of Carbon Fiber Resin Matrix Composite Skin Coating for Aircraft

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Abstract

By establishing a coating adhesion model, the research results can accurately control the coating process parameters of aircraft carbon fiber composite skin coating, improve the coating quality and efficiency, and provide a theoretical basis for the thermal stress analysis of laser paint removal. The research results are expected to break through the bottleneck technology of aircraft carbon fiber resin-based composite skin coating repair and provide theoretical basis and technical support for improving the quality and efficiency of aircraft carbon fiber resin-based composite skin coating repair.

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Funding

This work was supported by Scientific Research Project of Hunan Provincial Education Department in 2022 (Number: 22C1407 and entry name: Accurate and controllable laser paint removal method for aircraft carbon fiber composite skin based on three-dimensional finite element model). Authors have received research support from Scientific Research Project of Hunan Provincial Education Department. This is a phased research result.

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Authors and Affiliations

  1. Changsha Aeronautical Vocational and Technical College, Changsha, 410124, China

    Xiao Chun Fang

  2. Lingyun Technology Group Co., Ltd, Wuhan, 430040, China

    Shao Lin Fa

Authors
  1. Xiao Chun Fang
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  2. Shao Lin Fa
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Contributions

All authors contributed to the study conception and design. Material preparation, data collection and analysis were performed by XCF and SLF. The first draft of the manuscript was written by XIAO Chun fang, and all authors commented on previous versions of the manuscript. All authors read and approved the final manuscript.

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Correspondence to Xiao Chun Fang.

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Conflict of interest

Author XIAO Chun fang and SHAO Lin Fa declare they have no financial interests. The authors have no relevant financial or non-financial interests to disclose.

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Chun Fang, X., Lin Fa, S. Study on Adhesion of Carbon Fiber Resin Matrix Composite Skin Coating for Aircraft. J. Inst. Eng. India Ser. D 105, 249–254 (2024). https://doi.org/10.1007/s40033-023-00474-x

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  • DOI: https://doi.org/10.1007/s40033-023-00474-x

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