Design of continuous transition line pattern between layers of composite pressure vessel

• Published in: Journal of reinforced plastics and composites 2024-01
• Main Authors: Liang, Jianguo, Xue, Yuqin, Li, Yinhui, Zhao, Chunjiang, Liu, Jianglin, Zhao, Xiaodong, Zu, Lei
• Format: Article
• Language: English
• ISSN: 0731-6844; 1530-7964
• DOI: 10.1177/07316844241226548

To realize efficient and stable continuous transition between different winding process layers of composite pressure vessels. This article uses the non-geodesic winding equation to propose a transition layer design method for composite pressure vessel shells with circular cross-section core molds and ellipsoidal heads. Firstly, the fourth-order Runge–Kutta method is used to solve the non-geodesic stabilized winding pattern and then analyze different regions’ transition ability. Established a calculation model to determine the corresponding transition winding trajectory according to the known core mold shape and fiber position and carried out computer image simulation of different modes of transition layer patterns, and finally carried out experimental verification of 35 MPa composite pressure vessel based on the simulation. The results show that different regions of the core mold have different abilities to change different starting winding angles, and the design of the transition process layer based on this law can save the area needed for transition. This method realizes the smooth transition of different process layers; the fiber of the transition layer does not slip in the actual winding process, and the actual pattern of the winding is consistent with the simulation results, which saves 20.8% of the winding time, and effectively improves the automation of the composite pressure vessel winding process.