抄録
Some attempts to get efficient membrane space structure designs using various conceptual origami models are introduced, and their basic design considerations to fit their concepts to actual space structural hardware are presented. They cover cylindrical shell elements with axially buckled patterns for inflatable tubes, and deployable flat membrane structures for light weight large aperture spacecraft including their thickness effects and their various variations driven from geometrical dual properties. Some examples of deployable concepts in nature with reference to better designs of membrane space structures are also shown, and some limitations of their origami models are discussed.
| 本文言語 | English |
|---|---|
| ホスト出版物のタイトル | Proceedings of the ASME Design Engineering Technical Conference |
| 出版社 | American Society of Mechanical Engineers |
| 巻 | 6 B |
| ISBN（印刷版） | 9780791855942 |
| DOI | |
| 出版ステータス | Published - 2013 |
| イベント | ASME 2013 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2013 - Portland, OR 継続期間: 2013 8 4 → 2013 8 7 |
Other
| Other | ASME 2013 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2013 |
|---|---|
| City | Portland, OR |
| Period | 13/8/4 → 13/8/7 |
ASJC Scopus subject areas
- 機械工学
- コンピュータ グラフィックスおよびコンピュータ支援設計
- コンピュータ サイエンスの応用
- モデリングとシミュレーション