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自平衡单元嵌入式网壳结构的预应力优化

OPTIMIZATION OF PRESTRESS IN THE SHELL EMBEDDED OF SELF-BALANCING UNIT
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摘要 自平衡单元嵌入式网壳结构中的自平衡单元由预应力提供刚度,采用广义逆法求解平衡矩阵,编制含线性不等式约束及线性等式约束的线性优化程序并结合整体可行预应力的概念来确定初始预应力的分布。对杂交结构平衡矩阵的形成、广义逆求解、线性约束优化方法的数学模型、约束矩阵的集成等关键技术给予详细的推导说明;同时,根据理论推导编写出相应的程序用于求解预应力值,并利用非线性有限元软件对分析结果进行验证。 It is the prestress that provides stiffness in shell embedded of self-balancing unit. By using generalized inverse matrix theory method, equilibrium matrix can be solved and self-stress mode be gotten. Program has been developed based on linear restriction prestress optimal design mothod by the help of the concept of total feasible prestress. The formation of balance matrix of shell-tensegrity hybrid structure, the generalized inverse matrix method,the model of optimization and the integration of constrained condition matrix are described in detail to optimize the distribution of prestress in shell embedded of self-balancing unit. At the same time, program are developed based on this method to get the result of initial prestress. At last,shell embedded of self-balancing unit is analyzed by using this method. And the prestress result is verified by the non-linear finite element method.
出处 《钢结构》 2007年第2期1-4,47,共5页 Steel Construction
关键词 单层网壳 自平衡 平衡矩阵 广义逆阵 杂交结构 整体可行预应力 single-layer lattice shell self-balance equilibrium matrix generalized inverse matrix hybrid structure overall feasible prestress
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  • 1罗尧治,董石麟.索杆张力结构的计算机分析程序CSTS[J].空间结构,2000,6(2):56-63. 被引量:9
  • 2袁行飞,董石麟.索穹顶结构几何稳定性分析[J].空间结构,1999,5(1):3-9. 被引量:15
  • 3吴明儿,第六届空间结构学术会议论文集,1992年
  • 4Barnes M R. Form Finding and Analysis of Tension Structures by dynamic Relaxation[J].International Journal of Space Structures,1999,14(2):89~103
  • 5Sheck H J. The Force Density Method for Form Finding and Computation of General Networks[J]. Comp.Meth.Appl.Mech.Eng. 1974, 3: 115~134
  • 6Gründig L, Bahndorf J. The Design of Wide-span Roof Structures Using Micro-Computers[J]. Computer & Structures, 1988,30(3):495~501
  • 7徐芝纶.弹性力学[M].北京:人民教育出版社,1982..
  • 8TIBERT G. Deployment tensegrity structure for space applications[D]. Stockholm,Sweden:Royal institute of Technology Department of Mechanics, 2002.
  • 9PELLEGRINO S, KUKATHASAN S, TIBERT G. Small satellite deployment mechanisms[R]. Cambridge :British National Space Centre, University of Cambridge,2000.
  • 10LAI C Y, PELLEGRINO S. Non-linear finite element analysis of CRTS reflector[R]. Cambridge :European Space Agency, University of Cambridge, 2001.

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