Invention Grant
US08239180B2 Numerical structural analysis system based on the load-transfer-path method 失效
基于负载传递路径法的数值结构分析系统

  • Patent Title: Numerical structural analysis system based on the load-transfer-path method
  • Patent Title (中): 基于负载传递路径法的数值结构分析系统
  • Application No.: US12092571
    Application Date: 2006-11-06
  • Publication No.: US08239180B2
    Publication Date: 2012-08-07
  • Inventor: Kunihiro TakahashiToshiaki Sakurai
  • Applicant: Kunihiro TakahashiToshiaki Sakurai
  • Applicant Address: JP Tokyo
  • Assignee: Keio University
  • Current Assignee: Keio University
  • Current Assignee Address: JP Tokyo
  • Agency: patenttm.us
  • Priority: JP2005-321695 20051107
  • International Application: PCT/JP2006/322069 WO 20061106
  • International Announcement: WO2007/052784 WO 20070510
  • Main IPC: G06G7/48
  • IPC: G06G7/48
Numerical structural analysis system based on the load-transfer-path method
Abstract:
The purpose of this invention is to reduce the calculation time in the numerical structure analysis system based on load-transfer-path method.The parameters are set in the condition that the supporting point B in the objective structure is fixed and the load is applied to the specific loading point A. The FEM calculation means 2 calculates the deformation of the objective structure according to the structural stiffness matrix in the stiffness matrix holding means 1 to find the basic data such as the displacement of each point and so on. The FEM calculation means calculates each deformation to find the displacement under the condition that the specific loading point A and the supporting point B are fixed and three inspection loadings are applied to the variable loading point C. The partial stiffness matrix calculation means 3 solves the multidimensional simultaneous linear equation based upon the internal stiffness matrix of the objective structure, the load value and the displacement to find the partial stiffness matrix KAC. The stiffness parameter calculation means 8 calculates the value of the stiffness parameter U* according to the partial stiffness matrix KAC and the displacement in the basic data and so on. The value of U* of each point is calculated with changing the variable loading point C as to follow sequentially all the necessary points in the objective structure.
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