复合材料蜂窝芯子结构设计与节点剪切性能研究

Structural design and node shear properties of composite honeycomb cores

  • 摘要: 蜂窝结构作为一种源于自然界的多孔仿生结构,因其优异的力学特性而备受关注。复合材料蜂窝芯子作为蜂窝夹层结构的关键组成部分,直接决定了整体结构的可靠性与稳定性。传统蜂窝芯子胞元之间缺乏连续纤维连接,存在结构缺陷。现有研究多聚焦于蜂窝夹层复合材料整体性能,针对蜂窝芯子本身的结构设计与工艺参数调控的研究存在空白,尤其缺乏对蜂窝芯子节点剪切性能的有效测试与表征方法。针对上述问题,本文设计了两种蜂窝芯子胞元之间具有连续纤维连接的层间交织结构,提出了相应的节点剪切性能测试方法,系统研究了纤维结构对节点剪切性能的影响。结果表明,缝合蜂窝芯子缝合针距为3.0 mm时,节点剪切强度最优,强度可达13.40 MPa。整体机织蜂窝芯子,组织点密度为70 cm−2时节点剪切性能最优,强度可达18.05 MPa。本研究为高性能复合材料蜂窝芯子的结构设计与节点性能优化提供了关键实验依据。

     

    Abstract: As porous biomimetic structures derived from nature, honeycomb structures have attracted considerable attention due to their excellent mechanical properties. Composite honeycomb cores, as key components of sandwich structures, directly determine the reliability and stability of the overall structure. Traditional honeycomb cores lack continuous fiber connections between adjacent cells, resulting in structural weaknesses. Current research has primarily focused on the overall performance of honeycomb sandwich composite structures, leaving a gap in studies on the structural design and process parameter control of the honeycomb core itself, particularly regarding effective testing and characterization methods for its node shear performance. To address these issues, this paper designs two types of layer-to-layer interlocked structures with continuous fiber connections between honeycomb core cells, proposes corresponding test methods for node shear performance, and systematically investigates the influence of fiber architecture on node shear performance. The results show that the stitched honeycomb core exhibits an optimal node shear strength of 13.40 MPa at a stitching distance of 3.0 mm. For the integrally woven honeycomb core, optimal node shear performance is achieved at an interlacing density of 70/cm2, with a strength of 18.05 MPa. This study provides key experimental evidence for the structural design and node shear performance optimization of high-performance composite honeycomb cores.

     

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