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手风琴式蜂窝材料等效弯曲和扭转刚度分析 被引量:3

Analysis of the Equivalent Flexural and Torsional Stiffness for Accordion Cellular Honeycomb
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摘要 手风琴式蜂窝材料因其零泊松比和大应变特性,日益受到航空界的关注。将手风琴蜂窝材料等效为均质正交各向异性薄板,提出了基于能量等效原理的手风琴蜂窝材料等效弯曲刚度和等效扭转刚度的理论分析方法,得到了等效刚度系数的解析表达式,并分析了其对胞元结构参数的敏感性。建立了手风琴蜂窝板的参数化模型,并运用数值仿真反演技术,得到了手风琴蜂窝材料的等效刚度系数。通过对比等效刚度系数的理论解与反演解,表明了该理论分析方法的可行性和正确性。 The accordion cellular honeycomb has an increasing attention in the aviation industry over the last decade, because of the zero Poisson's ratio and high-strain capability. In this paper, the accordion cellular honeycomb is equivalent to a homogeneous orthogonal anisotropic plate. A novel analytical method for solving the equivalent flexural and torsional stiffness of the accordion cellular honeycomb was proposed based on the energy equivalence principle. And the analytical expressions of the equivalent stiffness were derived. Furthermore, the influence of the base cell structure parameters on the equivalent stiffness was studied. With the parameterized model of the accordion cellular honeycomb being established, a set of inversion method based on the numerical simulation has been used to obtain the equivalent stiffness. The comparisons between the theoretical results with the inversion results show that the present analytical method is feasible and valid.
出处 《机械科学与技术》 CSCD 北大核心 2014年第10期1579-1584,共6页 Mechanical Science and Technology for Aerospace Engineering
关键词 手风琴蜂窝材料 能量等效原理 等效弯曲刚度 等效扭转刚度 accordion cellular honeycomb anisotropy aviation bending ( deformation ) boneycomb structures computer simulation degrees of freedom (mechanics) energy equivalence principle equivalent flexural stiffness equivalent torsional stiffness homogenization method inverse problems parameterization Poisson ratio schematic diagrams stiffness strain energy torsional stress
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参考文献9

  • 1Gibson L J, Ashby M F, Schajer G S, et al. The mechanics of two-dimensional cellular materials [ C ]// Proe. R. Soe. Lond. A,1982,382:25-42.
  • 2Gibson Loma J.多孔固体结构与性能[M].刘培生,译.北京:清华大学出版社,2003.
  • 3王颖坚.蜂窝结构在面内剪力作用下的变形模式[J].北京大学学报(自然科学版),1991,27(3):301-307. 被引量:19
  • 4富明慧,尹久仁.蜂窝芯层的等效弹性参数[J].力学学报,1999,31(1):113-118. 被引量:149
  • 5富明慧,刘祚秋,等.蜂窝夹层板的一种等效单层模型[J].工程力学,2001,18(A01):700-704. 被引量:7
  • 6Chen D H. Equivalent flexural and torsional rigidity of hexagonal honeycomb [ J ]. Composite Structures, 2011, 93(7) :1910-1917.
  • 7Olympio K R, Gandhi F. Zero poisson's ratio cellular honeycombs for flex skins undergoing one-dimensional morphing[ J ]. Journal of Intelligent Material Systems and Structures,2010,21 (17) : 1737-1753.
  • 8Olympio K R, Gandhi F. Flexible skins for morphing aircraft using cellular honeycomb cores [ J ]. Journal of Intelligent Material Systems and Structures, 2010, 21 (17) :1719-1735.
  • 9董文俊,孙秦.手风琴式蜂窝材料的等效弹性模量分析[J].机械科学与技术,2011,30(7):1103-1106. 被引量:6

二级参考文献16

  • 1崔光育.蜂窝夹层壳非线性静动力分析.清华大学博士学位论文[M].,1995..
  • 2蘧时胜.复合材料多层板有限元法及其参数识别.清华大学博士学位论文[M].,1996..
  • 3崔光育.蜂窝夹层壳非线性静动力分析(博士学位论文)[M].,1995..
  • 4Olympio K R, Gandhi F. Zero-v cellular honeycomb flexible skins for one-dimensional wing morphing [ A ]. 48th AIAA/ASME/ ASCE/AHS/ASC Structures, Structural Dynamics, and Ma- terials Conference [ C ], 23 - 26 April 2007, Honolulu, Hawaii.
  • 5Thill C, Etches J, Bond I, Potter K, Weaver P. Morphing skins [ J ]. Aeronautical Journal, 2008,112 : 117-139.
  • 6Reich G W, Sanders B. Development of skins for morphing aircraft applications via topology optimization [ A ]. 48th AIAA/ASME/ ASCE/AHS/ASC Structures, Structural Dynamics, and Ma- terials Coafereaee[C] , April 2007, Honolulu, Hawaii.
  • 7Gibson L J, et al. The mechanics of two-dimensional cellular mate- rials [ A ]. Proceedings of the Royal Society of London [C], 1982.
  • 8刘培生译.多孔固体结构与性能[M].清华大学出版社,2003.
  • 9吴鸿遥,合成板、夹层板与整体板的强度计算原理,1989年
  • 10团体著者,夹层板壳的弯曲、稳定和振动,1977年

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