新型船用复合材料夹芯夹筋板力学试验研究

Experimental investigation on mechanical properties of new type of marine composite plate with reinforcing ribs and core material in the middle

  • 摘要: 【目的】:面向复合材料实船应用广阔前景,设计了一种泡沫填充的复合材料夹芯夹筋结构(组合厚板)。【方法】针对组合厚板各向异性特点,对组合厚板顺筋方向和垂直筋方向分别进行三点弯曲试验和拉伸试验,对比了该结构不同方向上的强度和模量,重点分析了组合厚板在两个方向弯曲荷载下的破坏模式及其失效机制,讨论了试件中心位置、胞元筋板数量对其力学性能的影响。【结果】组合厚板各向异性显著,相较于顺筋方向,结构垂直筋方向弯曲强度提高82%,拉伸模量提高22%。弯曲荷载下,结构发生初次破坏后,承载力大幅降低;垂直筋方向初始破坏模式为下面板局部脱粘,顺筋方向初始破坏模式为筋板剪切破坏。【结论】胞元筋板数量和中心位置对组合厚板弯曲强度影响显著,对其拉伸模量影响较小。弯曲荷载下,结构初始破坏模式与胞元筋板数量、弯曲中心位置无关;初始破坏时,纤维未出现明显屈曲、断裂现象,面板、筋板和泡沫之间的粘接强度一定程度上决定了结构的弯曲强度;初始破坏后,试件的损伤过程有所不同。对组合厚板开展力学试验,为后续复合材料夹芯夹筋板在船海主承力结构上的推广应用提供技术参考。

     

    Abstract: Objectives Due to the broad application prospect of composite materials in ships, a composite sandwich structure filled with foam and ribs(combined thick plate) is designed.Methods Based on the anisotropic characteristics of combined thick plate, three-point bending and tensile tests on combined thick plate along the direction of the reinforcing ribs and perpendicular to the direction of the reinforcing ribs are conducted, the strength and modulus of the structure in different directions are compared. The failure modes and failure mechanisms of combined thick plate under bending loads in two directions are analyzed, and the effects of the center position of the specimen and the number of cell reinforced plates on their mechanical properties are discussed. Results The anisotropy of combined thick plate is significant. Compared to the longitudinal direction, the bending strength of the structure in the vertical direction of the reinforcement is increased by 82%, and the tensile modulus is increased by 22%. The results show that under bending load, the bearing capacity of the structure decreases significantly after the initial failure. The initial failure mode for the plate with perpendicular to the direction of the reinforcing bars is partial debonding of the lower panel, while the initial failure mode for the plate with along the direction of the reinforcing bars is failure of the reinforced panel due to shear.Conclusions The number of ribs in the cell and center position has a significant impact on the bending strength of the combined thick plate, but has a small impact on its tensile modulus. Under bending load, the initial failure mode of the structure is independent of the number of ribs in the cell and the position of the bending center. At the initial failure, there is no obvious buckling and fracture of the fiber, and the bending strength of the structure is determined to some extent by the adhesive strength between the panel, rib and foam. After initial failure, the damage process of the specimen varies. The results can provide technical reference for the promotion and application of composite sandwich reinforcement plates in the main load-bearing structures of ships and seas in the future.

     

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