Accommodating Thickness in Origami Based Deployable Arrays1Source: Journal of Mechanical Design:;2013:;volume( 135 ):;issue: 011::page 111005Author:Zirbel, Shannon A.
,
Lang, Robert J.
,
Thomson, Mark W.
,
Sigel, Deborah A.
,
Walkemeyer, Phillip E.
,
Trease, Brian P.
,
Magleby, Spencer P.
,
Howell, Larry L.
DOI: 10.1115/1.4025372Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The purpose of this work is to develop approaches to accommodate thickness in origamibased deployable arrays with a high ratio of deployedtostowed diameter. The origami flasher model serves as a basis for demonstrating the approach. A thicknessaccommodating mathematical model is developed to describe the flasher. Practical modifications are presented for the creation of physical models and two options are proposed: allowing the panels to fold along their diagonals or applying a membrane backing with specified widths at foldlines. The mathematical model and hardware modifications are employed to create several physical models. The results are general and apply to a range of applications. An example is provided by the application that motivated the work: a deployable solar array for space applications. The model is demonstrated in hardware as a 1/20th scale prototype with a ratio of deployedtostowed diameter of 9.2 (or 1.25 m deployed outer diameter to 0.136 m stowed outer diameter).
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| contributor author | Zirbel, Shannon A. | |
| contributor author | Lang, Robert J. | |
| contributor author | Thomson, Mark W. | |
| contributor author | Sigel, Deborah A. | |
| contributor author | Walkemeyer, Phillip E. | |
| contributor author | Trease, Brian P. | |
| contributor author | Magleby, Spencer P. | |
| contributor author | Howell, Larry L. | |
| date accessioned | 2017-05-09T01:01:07Z | |
| date available | 2017-05-09T01:01:07Z | |
| date issued | 2013 | |
| identifier issn | 1050-0472 | |
| identifier other | md_135_11_111005.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/152586 | |
| description abstract | The purpose of this work is to develop approaches to accommodate thickness in origamibased deployable arrays with a high ratio of deployedtostowed diameter. The origami flasher model serves as a basis for demonstrating the approach. A thicknessaccommodating mathematical model is developed to describe the flasher. Practical modifications are presented for the creation of physical models and two options are proposed: allowing the panels to fold along their diagonals or applying a membrane backing with specified widths at foldlines. The mathematical model and hardware modifications are employed to create several physical models. The results are general and apply to a range of applications. An example is provided by the application that motivated the work: a deployable solar array for space applications. The model is demonstrated in hardware as a 1/20th scale prototype with a ratio of deployedtostowed diameter of 9.2 (or 1.25 m deployed outer diameter to 0.136 m stowed outer diameter). | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Accommodating Thickness in Origami Based Deployable Arrays1 | |
| type | Journal Paper | |
| journal volume | 135 | |
| journal issue | 11 | |
| journal title | Journal of Mechanical Design | |
| identifier doi | 10.1115/1.4025372 | |
| journal fristpage | 111005 | |
| journal lastpage | 111005 | |
| identifier eissn | 1528-9001 | |
| tree | Journal of Mechanical Design:;2013:;volume( 135 ):;issue: 011 | |
| contenttype | Fulltext |