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林业科学 ›› 2025, Vol. 61 ›› Issue (9): 173-183.doi: 10.11707/j.1001-7488.LYKX20250038

• 研究论文 • 上一篇    

竹集成材格栅夹芯板轴心受压性能

王智丰1,4,汤舒畅1,彭熙之1,王达1,4,张仲凤2,4,李贤军3,4,*()   

  1. 1. 中南林业科技大学土木工程学院 长沙 410004
    2. 中南林业科技大学家居与艺术设计学院 长沙 410004
    3. 中南林业科技大学材料与能源学院 长沙 410004
    4. 中南林业科技大学现代木结构工程材制造及应用技术湖南省工程实验室 长沙 410004
  • 收稿日期:2025-01-20 出版日期:2025-09-25 发布日期:2025-10-10
  • 通讯作者: 李贤军 E-mail:lxjmu@163.com
  • 基金资助:
    国家自然科学基金面上项目(32471984);湖南省自然科学基金面上项目(2024JJ5631);湖南省教育厅优青项目(23B0236);湖南省大学生创新训练计划项目(S202410538085)。

Axial Compression Performance of Laminated Bamboo Grid Sandwich Panels

Zhifeng Wang1,4,Shuchang Tang1,Xizhi Peng1,Da Wang1,4,Zhongfeng Zhang2,4,Xianjun Li3,4,*()   

  1. 1. School of Civil Engineering, Central South University of Forestry and Technology Changsha 410004
    2. School of Furnishings and Art Design, Central South University of Forestry and Technology Changsha 410004
    3. School of Materials and Energy, Central South University of Forestry and Technology Changsha 410004
    4. Hunan Provincial Engineering Laboratory of Engineering Material of Modern Wood Structure Manufacturing and Application Technology, Central South University of Forestry and Technology Changsha 410004
  • Received:2025-01-20 Online:2025-09-25 Published:2025-10-10
  • Contact: Xianjun Li E-mail:lxjmu@163.com

摘要:

目的: 探究竹集成材格栅夹芯板的轴心受压性能,提出其轴心受压承载能力计算公式,为竹集成材格栅夹芯板在工程领域的应用提供技术参考和理论依据。方法: 以竹集成材为原材料,采用隔断法制备了4种不同长宽比的格栅夹芯板。在两端铰接的边界条件下,对试件进行面内轴向压缩试验,研究长宽比对试件承载能力、纵向应变、侧向位移的影响规律,并探讨不同长宽比试件的破坏形态和破坏机理;基于有限元仿真模拟验证试验结果,并通过参数化扩展分析明确理论计算公式的适用性边界。结果: 竹集成材格栅夹芯板的轴压受力过程主要分为:弹性阶段、弹塑性阶段和破坏阶段;长宽比为1、2、3的试件破坏模式为局部屈曲破坏,长宽比为4的试件破坏模式为整体屈曲破坏;相较于长宽比为1的试件,长宽比为2、3、4的试件承载力分别下降了7.92%、12.18%、18.27%;考虑材料各向异性和芯材剪切变形影响得到的夹芯板屈曲承载力计算公式具有较高的准确性,局部屈曲承载力计算值与试验值偏差在0.86%~2.83%,整体屈曲承载力计算值与试验值误差在8%以内;参数化分析表明,理论计算公式在长宽比1~7范围内具有较高计算精度,公式计算值与试验值、有限元模拟值的相对误差控制在10%以内。结论: 随着长宽比的增加,竹集成材格栅夹芯板的承载力有所降低,破坏模式由局部屈曲破坏转变为整体屈曲破坏;竹集成材格栅夹芯板的受压性能理论计算较为准确,能够为其工程应用提供可靠的理论支撑。

关键词: 竹集成材, 格栅夹芯板, 轴心受压, 长宽比, 承载力

Abstract:

Objective: This study aims to explore the axial compression performance of laminated bamboo grid sandwich panels, and propose a calculation formula for axial compression bearing capacity, so as to provide technical reference and theoretical basis for the application of laminated bamboo grid sandwich panels in engineering fields. Method: Four types of laminated bamboo grid sandwich panels with different aspect ratios were fabricated with laminated bamboo as raw material by partition method. In-plane axial compression tests were conducted on the specimens with hinged boundary conditions at both ends. The influence of aspect ratios on the bearing capacity, longitudinal strain, and lateral displacement of the specimens was investigated. Additionally, the failure modes and mechanisms of the specimens with different aspect ratios were examined. The reliability of the experimental results was validated through finite element simulation, and the applicability boundaries of the theoretical calculation formula were systematically delineated via parametric extension analysis. Result: The axial compression process of the laminated bamboo grid sandwich panels was categorized into three stages: elastic stage, elastic-plastic stage, and failure stage. The failure mode of specimens with aspect ratios of 1, 2, and 3 experienced local buckling, while those with an aspect ratio of 4 failed due to global buckling. Compared to the specimen with an aspect ratio of 1, the bearing capacity of specimens with aspect ratios of 2, 3, and 4 decreased by 7.92%, 12.18%, and 18.27%, respectively. The critical load calculation formulas for local and global buckling of sandwich panels, considering the effects of material anisotropy and core shear deformation, demonstrated excellent accuracy. The deviation between the calculated and experimental values of local buckling bearing capacity ranged from 0.86% to 2.83%, while the error between the calculated and experimental values of global buckling bearing capacity was within 8%. Parametric analysis demonstrated that the theoretical calculation formula exhibited high computational accuracy within the aspect ratio range of 1 to 7. The relative errors between the calculated values from the formula, the experimental values, and the finite element simulation values were controlled within 10%. Conclusion: As the aspect ratio increases, the bearing capacity of laminated bamboo grid sandwich panels decreases, and the failure mode changes from local buckling to global buckling. The theoretical calculations for the compressive behavior of laminated bamboo grid sandwich panels demonstrate high accuracy, providing reliable theoretical support for their engineering applications.

Key words: laminated bamboo, grid sandwich panels, axial compression, aspect ratio, bearing capacity

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