Simulation and Analysis of Butterfly-Inspired Eclosion Deployable Structure

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Deployable structures, as an important kind of structure, have been widely used in a variety of satellite antennas and space reflectors. The research of deployable structures usually faces a series of theoretical and technical challenges because the size and mass are not only the limitations of deployable structure but also the key issues in the design process. Nevertheless, the appearance of bionic provides a new concept to develop the deployable structures. Inspired by the eclosion and development of butterfly wings, a bionic inflatable deployment structure has been presented in this paper. The whole system of emulate model is established and has a simulation analyzed with the help of dynamic analysis software. This simulation is aimed at emulating the deploying process, and calculating the stress distribution of the structure. Then some relative curve fitting is conducted on the deploying trajectory. A prototype has been fabricated and tested to be able to deploy smoothly and steadily.

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114-121

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November 2013

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] J.G. Liu, S. F Sun, A Brief Survey on Inflatable Deployment Space Structures' Research and Development. IEEE International Conference on Reconfigurable Mechanisms and Robots, Tianjin, China, 2012, 773-782.

DOI: 10.1007/978-1-4471-4141-9_69

Google Scholar

[2] Y. Xu, F.L. Guan, Structure–electronic synthesis design of deployable truss antenna, Aerospace Science and Technology. 26 (2013) 259-267.

DOI: 10.1016/j.ast.2012.05.004

Google Scholar

[3] N. Fazli, A. Abedian, Design of tensegrity structures for supporting deployable mesh antennas, Scientia Iranica. 18 (2011) 1078-1087.

DOI: 10.1016/j.scient.2011.08.006

Google Scholar

[4] Y.Q. Zhang, B.Y. Duan, T.J. Li, A controlled deployment method for flexible deployable space antennas, Acta Astronautica. 81 (2012) 19-29.

DOI: 10.1016/j.actaastro.2012.05.033

Google Scholar

[5] Q. Lin, H. Nie, J. Ren, J.B. Chen, Investigation on design and reliability analysis of a new deployable and lockable mechanism, Acta Astronautica. 73 (2012) 183-192.

DOI: 10.1016/j.actaastro.2011.12.004

Google Scholar

[6] L. Puig, A. Barton, N. Rando, A review on large deployable structures for astrophysics missions, Acta Astronautica. 67 (2010) 12-26.

DOI: 10.1016/j.actaastro.2010.02.021

Google Scholar

[7] S. Yoon, L.H. Kang, S. Jo, Development of Air Vehicle with Active Flapping and Twisting of Wing, Journal of Bionic Engineering. 8 (2011) 1-8.

DOI: 10.1016/s1672-6529(11)60007-3

Google Scholar

[8] K.S. Liu, L. Jiang, Research Progress of Bionic Structure and Function Material, Chinese Science Bulletin. 54 (2009) 2667-2681.

Google Scholar

[9] F.V. Julian, Applications - Influence of Biology on Engineering, Journal of Bionic Engineering. 3(2006) 161-177.

Google Scholar

[10] J.G. Liu, Y.C. Wang, H. Chen, X.M. Chen, Primary Research on the Bio-inspired Developable Structures in Space Application, Chinese Space Mechanical Engineering Technology Forum. Beijing, China, 2011, 189-195.

Google Scholar

[11] DSA. De Focatiis, SD. Guest, Deployable membranes designed from folding tree leaves, Philosophical Transactions of the Royal Society, Mathematical, Physical and Engineering Sciences. 360 (2002) 227-238.

DOI: 10.1098/rsta.2001.0928

Google Scholar

[12] N. Kishimoto, MC. Natori, K. Higuchi, New deployable membrane structure models inspired by morphological changes in nature, 47th Structures, Structural Dynamics, and Materials Conference: AIAA, Newport, United State, 2006, 3722-3725.

DOI: 10.2514/6.2006-1898

Google Scholar

[13] X.M. Chen, C.L. Zhou, J.Y. Shi, Ornamental Butterflies in China, first ed, China Forestry Publishing House, Beijing, 2008. (in Chinese).

Google Scholar

[14] C.G. Wang, X.W. Du, Z.M. Wan. Internal gas mass loss analysis of inflatable space antenna reflector subjected to impact, Journal of Harbin Institute of Technology. 38 (2006) 507-509.

Google Scholar