Large antenna reflectors used in space have to be folded before launching. Silicone rubber is commonly used as antenna material due to its ability to maintain a shape without external supports upon deployment. However, localized vertices could appear during the folding process, which might lead to material yielding and unrecoverable deformation after deployment. In this paper, the cross folding process of a thin elastic sheet, a common folding method in packaging a reflective membrane, was studied numerically with the aim of eliminating material failure in the sheet. The deformation, stress distribution, and peak stress of the sheet and the dependency of those properties on geometrical parameters were systematically investigated. Based on these studies, two methods, i.e., central hole method and central slit method, were explored to reduce the peak stress caused by cross folding. The results showed that a central slit parallel to the first folding crease was the most effective in reducing the peak stress without causing significant damage to the antenna.
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ASME 2017 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
August 6–9, 2017
Cleveland, Ohio, USA
Conference Sponsors:
- Design Engineering Division
- Computers and Information in Engineering Division
ISBN:
978-0-7918-5818-9
PROCEEDINGS PAPER
Analysis of Cross Folding an Elastic Sheet
Zhong You
Zhong You
University of Oxford, Oxford, UK
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Degao Hou
Tianjin University, Tianjin, China
Jiayao Ma
Tianjin University, Tianjin, China
Yan Chen
Tianjin University, Tianjin, China
Zhong You
University of Oxford, Oxford, UK
Paper No:
DETC2017-67388, V05BT08A039; 8 pages
Published Online:
November 3, 2017
Citation
Hou, D, Ma, J, Chen, Y, & You, Z. "Analysis of Cross Folding an Elastic Sheet." Proceedings of the ASME 2017 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. Volume 5B: 41st Mechanisms and Robotics Conference. Cleveland, Ohio, USA. August 6–9, 2017. V05BT08A039. ASME. https://doi.org/10.1115/DETC2017-67388
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