Chinese Journal of Ship Research, Volume. 19, Issue 5, 141(2024)

Optimized CFRP layering design for circumferential internal corrugated compression shell

Runze WU1...2, Jianliang SUN1,2, Xu ZHANG1,2, and Mingfang QI12 |Show fewer author(s)
Author Affiliations
  • 1School of Mechanical Engineering, Yanshan University, Qinhuangdao 066004, China
  • 2National Engineering Research Center for Equipment and Technology of Cold Rolled Strip, Yanshan University, Qinhuangdao 066004, China
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    Objective

    In order to meet the development trend of low weight and high strength in the design of compression shell structures for deep-sea submersibles, this paper proposes a structural enhancement method which involves winding a circumferential internal corrugated compression shell with a carbon fiber reinforced polymer (CFRP), then analyzes and optimizes the CFRP layering scheme.

    Method

    Finite element simulation software ABAQUS is used to change the layering parameters of the CFRP according to the stress distribution of the composite layers, and the optimal winding angle under 14 layers of CFRP is explored to obtain the best layering scheme. The relevant strength failure criteria are then combined to check the intensity.

    Results

    The results indicate that 40° is the best CFRP winding angle to enhance the circumferential internal corrugated compression shell. When the layering mode is (±40°2/±55°2/±70°2/90°2), the stress distribution between the layers is relatively uniform, meaning that the structure has a lighter weight while its strength fulfills the actual use requirements.

    Conclusion

    The proposed structure can reduce the overall weight of deep-sea compression shells and push the development of the field toward lightweight design.

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    Runze WU, Jianliang SUN, Xu ZHANG, Mingfang QI. Optimized CFRP layering design for circumferential internal corrugated compression shell[J]. Chinese Journal of Ship Research, 2024, 19(5): 141

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    Paper Information

    Category: Ship Structure and Fittings

    Received: Jul. 3, 2023

    Accepted: --

    Published Online: Mar. 14, 2025

    The Author Email:

    DOI:10.19693/j.issn.1673-3185.03438

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