复合材料科学与工程 ›› 2026, Vol. 0 ›› Issue (9): 99-106.DOI: 10.19936/j.cnki.2096-8000.20260928.011

• 设计与工艺 • 上一篇    下一篇

船用编织复合材料夹芯结构极限强度渐进失效仿真方法研究

胡涛1, 秦恺2, 王玮1, 汤云溪1*   

  1. 1.水上载运装备安全研究院(宁波)有限公司 工业软件业务部,宁波 315000;
    2.武汉理工大学 船海与能源动力工程学院,武汉 430060
  • 收稿日期:2026-04-16 出版日期:2026-09-28 发布日期:2026-09-23
  • 通讯作者: 汤云溪(1984—),男,学士,高级工程师,研究方向为复合材料船舶,yxtang@imtes.cn。
  • 作者简介:胡涛(1983—),男,硕士,高级工程师,研究方向为船海领域安全与可靠性。
  • 基金资助:
    轻量化材料与结构的表征理论方法及适配技术研究(2022YFB4300102)

Research on the simulation method for ultimate strength and progressive failure of marine braided composite sandwich structures

HU Tao1, QIN Kai2, WANG Wei1, TANG Yunxi1*   

  1. 1. Industrial Software Business Department,Institute for Maritime Transport Equipment Safety, Ningbo 315000, China;
    2. School of Naval Architecture Ocean and Energy Power Engineering, Wuhan University of Technology, Wuhan 430060, China
  • Received:2026-04-16 Online:2026-09-28 Published:2026-09-23

摘要: 为解决船用大中型夹芯复合材料结构极限强度分析中三维精细化建模计算成本过高的问题,本文提出并验证了一种高效的“壳-实耦合”有限元简化模型。本文将三维渐进损伤破坏准则降维适配至二维壳单元,并以典型L形加强筋连接结构为对象,对比评估了芯材实体/蒙皮壳单元耦合(方法一)与夹芯板整体壳单元等效(方法二)两种简化策略。结果表明:方法二的简化策略在基础结构刚度预测上有较大偏差;而方法一结合在关键区域(如帽形加强筋)划分不少于6个单元的网格策略,能在还原非线性破坏模式并将极限载荷预测误差控制在7%以内的前提下,实现近百倍的计算效率提升。

关键词: 夹芯复合材料, 编织复合材料, 极限强度, 渐进失效

Abstract: To address the issue of excessively high computational costs associated with 3D refined modeling in the ultimate strength analysis of large and medium-sized marine sandwich composite structures, an efficient “shell-solid coupling” simplified finite element model was proposed and validated. The 3D progressive damage failure criteria were dimensionally reduced and adapted to 2D shell elements. Taking a typical L-shaped stiffener connection structure as the research object, two simplified modeling strategies were comparatively evaluated: the coupling of solid elements for the core and shell elements for the skin (Method 1), and the equivalent overall shell element modeling for the entire sandwich panel (Method 2). The results indicated that Method 2 yielded significant deviations in predicting the basic structural stiffness. In contrast, Method 1, combined with a meshing strategy that allocates no less than 6 elements in critical regions (such as hat-shaped stiffeners), achieved a nearly hundredfold increase in computational efficiency while accurately reproducing nonlinear failure modes and keeping the ultimate load prediction error within 7%.

Key words: sandwich composite, braided composite, ultimate strength, progressive failure

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