3407 離散構造要素を用いた多段階統合設計法 : 人工衛星のたおればねを対象とした場合(OS7-2 システム最適化)

概要

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This paper presents an advanced multi-step optimal design method using function oriented elements for the development of the development of the leaning spring for artificial satellite. For the sake of the efficient design, the appropriate methodology must be selected in each design phase. In this research, the topology optimization method and the shape optimization method are used in the conceptual design phase and the detailed design phase respectively. Frame elements are used for both phases as the function oriented element. In addition, the numerical example of based on the actual analysis model of leaning spring part are provided to show the utility of the methodology presented here.
一般社団法人日本機械学会の論文
2007-10-30