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一种新型组合蜂窝结构的轴向承载性能研究 被引量:5

RESEARCH ON AXIAL LOAD CARRYING CAPACITY OF A NEW TYPE OF SUPERCELL HONEYCOMB STRUCTURE
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摘要 轴向承载力是蜂窝结构重要的力学性能指标。提出一种基本胞元由菱形和圆形构成的新型组合蜂窝结构,围绕其轴向结构稳定性、整体刚度和强度三个方面展开研究。首先运用线性特征值屈曲分析方法,通过有限元数值模拟,实现了新型组合蜂窝的结构稳定性分析过程,并与菱形、正六边形、正八边形蜂窝结构的屈曲分析结果进行了比较;同时,以某型号电动车底盘中部甲板为例,验证了新型组合蜂窝夹芯结构在轴向载荷作用下的整体强度和刚度,并分析了不同胞元壁厚对夹芯整体强度和刚度的影响。结果表明,新型组合蜂窝具有良好的轴向结构稳定性,且其夹芯层整体刚性和强度较好,轴向承载力强,是综合力学性能较优的创新构型。 Axial load carrying capacity is one of the most important mechanical property indexes of honeycomb structure. A new type of supercell honeycomb structure was put forward in which rhombus and circle were combined into the basic cell,and research was focused on its structural stability,overall strength and stiffness. By helps of finite element numerical simulation,the method of eigenvalue buckling analysis was used to realize the process of structural stability analysis of the supercell honeycomb,and the analysis result was also compared with those of rhombus,regular hexagon and regular octagon honeycomb structure.Meanwhile,a type of chassis deck of electrical motorcycle was taken as an example to testify the overall strength and stiffness of the new type of honeycomb sandwich structure's core under axial load and analyze the influence on strength and stiffness of the core with different wall thickness of its cell. The results show that the new type of supercell honeycomb is an innovative configuration with good comprehensive mechanical properties such as better axial structural stability,high strength and overall stiffness of honeycomb sandwich structure's core,and axial load-bearing capacity.
作者 何彬 李响
出处 《机械强度》 CAS CSCD 北大核心 2016年第2期328-332,共5页 Journal of Mechanical Strength
基金 国家自然科学基金项目(51305232) 湖北理工学院校级重点项目(13xjz04A)资助~~
关键词 组合蜂窝 胞元 结构稳定性 轴向承载力 Supercell honeycomb Cell Structural stability Axial load carrying capacity
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  • 1刘书田,曹先凡.零膨胀材料设计与模拟验证[J].复合材料学报,2005,22(1):126-132. 被引量:21
  • 2李庆明.蜂窝材料应力平台区的塑性屈曲变形模式[J].复合材料学报,1994,11(4):89-94. 被引量:1
  • 3Tarnai T. Buckling Patterns of Shells and Spherical Honeycomb Structures[J]. Computers and Mathematics with Applications; 1989, 17 (4-6) : 639-652.
  • 4Lu Lixin, Sun Yaping, Wang Zhiwei. Critical Buckling Load of Paper Honeycomb under out-of-Plane Pressure[J], Packaging Technology and Science, 2005, 18(3) : 141-150.
  • 5Allen H G, Bulson P S. Background to Buckling [M]. London: MCGRAW-HILL Book Company (UK) Limited, 1980.511-563.
  • 6Allen H G. Analysis and design of structural sandwich panels [M]. Oxford: Pergamon Press,1969. 56-89.
  • 7Papka S D, Kyriakides S. Biaxial crushing of honeycombⅠ: Experiments [J]. International Journal of Solids and Structures, 1999,36(29):4367-4396.
  • 8Papka S D, Kyriakides S. In-plane biaxial crushing of honeycombs Ⅱ: Analysis [J]. International Journal of Solids and Structures, 1999,36(29):4397-4423.
  • 9Chung Jaeung, Waas A M. Compressive response of circular cell polycarbonate honeycombs under inplane biaxial static and dynamic loading Ⅰ: Experiments [J]. International Journal of Impact Engineering, 2002, 27(7): 729-754.
  • 10Chung Jaeung, Waas A M. Compressive response of circular cell polycarbonate honeycombs under inplane biaxial static and dynamic loading Ⅱ: Simulations [J]. International Journal of Impact Engineering, 2002, 27(10): 1015-1047.

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