Abstract
Deployable structures are widely used in space applications such as solar arrays and an- tennas. Recently, inspired by origami, more deployable structures have been developed. This paper outlined a novel design scheme for deployable structures by taking a plane linkage as an origami unit with a large deployable ratio. The mountain and valley (M-V) crease assignment and kinematics of the plane linkage were analyzed. Physical interfer- ence in the folding progress was discovered geometrically and resolved by the split-vertex technique. Finally, tessellation of the derived pattern was successfully used to create a large-deployable-ratio structure, which was found to exhibit considerable potential in fu- ture space applications.
| Original language | English |
|---|---|
| Article number | 103605 |
| Number of pages | 15 |
| Journal | Mechanism and Machine Theory |
| Volume | 142 |
| Early online date | 3 Sept 2019 |
| DOIs | |
| Publication status | Published - 1 Dec 2019 |
| Externally published | Yes |
Keywords
- Deployable structure
- Origami
- Plane linkage
- Tessellation
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