Optimal design of laying sequence of composite gas cylinders based on impact damage

GENG Fagui; LI Qiang; SONG Xuesi; LIU Yan; LIU Peiqi; YANG Yan

doi:10.13801/j.cnki.fhclxb.20210323.001

Volume 39 Issue 2

Feb. 2022

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GENG Fagui, LI Qiang, SONG Xuesi, et al. Optimal design of laying sequence of composite gas cylinders based on impact damage[J]. Acta Materiae Compositae Sinica, 2022, 39(2): 777-787. doi: 10.13801/j.cnki.fhclxb.20210323.001

Citation:

GENG Fagui, LI Qiang, SONG Xuesi, et al. Optimal design of laying sequence of composite gas cylinders based on impact damage[J]. Acta Materiae Compositae Sinica, 2022, 39(2): 777-787. doi: 10.13801/j.cnki.fhclxb.20210323.001

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Optimal design of laying sequence of composite gas cylinders based on impact damage

doi: 10.13801/j.cnki.fhclxb.20210323.001

GENG Fagui^1
,,
LI Qiang³,
SONG Xuesi^3
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LIU Yan^3
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LIU Peiqi^{1
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YANG Yan^{2
,
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1.
School of Chemical Engineering, Dalian University of Technology, Dalian 116033, China
2.
School of Computer and Information Technology, Liaoning Normal University, Dalian 116081, China
3.
Dalian Inspection, Testing and Certification Group CO. LTD., Dalian 116013, China

Received Date: 2021-02-02
Accepted Date: 2021-03-15
Rev Recd Date: 2021-03-05

Available Online: 2021-03-25

Publish Date: 2022-02-01

Abstract

Abstract

Based on the transient dynamics theory and genetic optimization algorithm, the layup sequence of composite gas cylinder was optimized with the optimization goal of improving the resistance to impact damage. The genetic algorithm was realized by MATLAB software, and the impact damage analysis of composite gas cylinders was carried out by ANSYS. Through the information transmission between the two software, the optimized process was realized. Taking an aluminum-lined composite gas cylinder as an example for optimization, the results show that under the same impact energy, the matrix rupture area and the number of matrix rupture layers of optimized gas cylinder are greatly reduced, and the remaining burst pressure is significantly increased. When the impact energy is 60 J, the rupture matrix area on the surface reduces 8.8%, the number of rupture layers in the matrix reduces 14.3%, and the remaining burst pressure value increases 9.6%. The optimization algorithm established in this paper can be used to optimize the design of composite gas cylinders.
- composite materials,
- laying sequence,
- impact damage,
- genetic algorithm,
- burst pressure
Long Abstrsct
Innovation Points

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References(20)

References

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