Chinese Journal of Ship Research, Volume. 19, Issue 2, 107(2024)

Study on the impact dynamics theoretical model of bidirectional limited single-layer vibration isolation system with segmented limit stiffness

Qian CHEN1, Shaoyu XIAO2, and Guanjun ZHANG1
Author Affiliations
  • 1School of Naval Architecture, Ocean and Energy Power Engineering, Wuhan University of Technology, Wuhan 430063, China
  • 2China Ship Development and Design Center, Wuhan 430064, China
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    Objective

    To address the issue of nonlinear stiffness changes in isolation systems with limiters under impact excitation, an impact dynamics theoretical model and its anti-impact performance research are conducted.

    Methods

    First, using the idea of segmented linear equivalence, an impact dynamics theoretical model of a bidirectional limited single-layer vibration isolation system with a segmented linear stiffness limiter is established. The theoretical model is then solved using the analytical method and compared with the impact response of the finite element method under different impact conditions.

    Results

    The analytical solution of the dynamic theoretical model is highly consistent with the finite element numerical solution under different impact conditions.

    Conclusion

    Through comparative analysis, the accuracy of the impact dynamics theoretical model and solution method of the bidirectional limited single-layer vibration isolation system with segmented linear stiffness limiter is verified, providing a theoretical basis for research on the working principle and performance characteristics of vibration isolation systems with limiters.

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    Qian CHEN, Shaoyu XIAO, Guanjun ZHANG. Study on the impact dynamics theoretical model of bidirectional limited single-layer vibration isolation system with segmented limit stiffness[J]. Chinese Journal of Ship Research, 2024, 19(2): 107

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    Paper Information

    Category: Ship Structure and Fittings

    Received: Mar. 3, 2023

    Accepted: --

    Published Online: Mar. 18, 2025

    The Author Email:

    DOI:10.19693/j.issn.1673-3185.03292

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