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Open Access

A novel inflatable rings supported design and buoyancy-weight balance deformation analysis of stratosphere airships

Weinan GAOa,bJi ZHANGa,bTeng MAa,bGuochang LINa,bYuanpeng LIUa,bChangguo WANGa,bHuifeng TANa,b( )
Center for Composite Materials, Harbin Institute of Technology, Harbin 150001, China
National Key Laboratory of Science and Technology on Advanced Composites in Special Environments, Harbin Institute of Technology, Harbin 150080, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Owing to the unique advantages in flight altitude, dwelling time and wide coverage area, stratospheric airships provide permanent monitoring and surveillance for both civil and military applications. Here we propose a semi-rigid stratosphere airship design with circumferential high-pressure inflatable rings and a longitudinal carbon fiber skeleton supported inside. We perform numerical simulations to analyze the deformation characteristics during the whole ascending and descending process. An equivalent internal gradient pressure model of helium is established based on the capsule shape and buoyancy-weight equilibrium conditions. The implicit dynamic method is used to deal with the large deformation of the airship capsule under a low negative pressure condition. Deformation and load-bearing performance of the airship capsule, inflatable ring, skeleton, and suspension line are obtained under different working conditions. The results show that the airship, supported with the inflatable rings and the suspension lines, effectively maintains the shape and ensures the stiffness during the ascending, dwelling, and descending stages, especially suffering from negative pressure.

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Chinese Journal of Aeronautics
Pages 340-347

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Cite this article:
GAO W, ZHANG J, MA T, et al. A novel inflatable rings supported design and buoyancy-weight balance deformation analysis of stratosphere airships. Chinese Journal of Aeronautics, 2022, 35(1): 340-347. https://doi.org/10.1016/j.cja.2020.11.019

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Received: 12 August 2020
Revised: 09 September 2020
Accepted: 27 September 2020
Published: 09 January 2021
© 2021 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).