Design of winding pattern of filament-wound composite pressure vessel with unequal openings based on non-geodesics

Author:

Guo Kaite1ORCID,Wen Lihua1,Xiao Jinyou1,Lei Ming1,Wang Shiyu1,Zhang Chengshuang2,Hou Xiao3

Affiliation:

1. School of Astronautics, Northwestern Polytechnical University, Xi’an, China

2. Xi’an Aerospace Composites Research Institute, Xi’an, China

3. Xi’an Institute of Aerospace Solid Propulsion Technology, Xi’an, China

Abstract

In this article, we proposed a new approach to design the winding patterns of filament-wound composite pressure vessel with unequal polar openings with non-geodesics. To ensure the continuity of winding angles between trajectories along the cylinder and the dome, the non-geodesics for cylindrical part were used. The developed winding patterns of the vessels were simulated using the MATLAB software to verify the feasibility of the acquired trajectories. To demonstrate the performance in designing the winding path for big polar ratios, we analyzed vessels with polar pole ratios of 1:2–1:4, respectively. The developed winding patterns have successfully achieved uniform fiber distributions along the mandrel without severe overlap, except for the polar pole regions. To avoid the severe overlap between filament bands, we further studied the relationship among the winding pattern, bandwidth, and the number of tangent points, and derived a suitable bandwidth based on the winding pattern. These simulated results proved the effectiveness of the developed method in design of winding pattern with unequal polar openings.

Funder

Joint Fund of Advanced Aerospace Manufacturing Technology Research

Publisher

SAGE Publications

Subject

General Materials Science

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