Radial compression pressure estimation of carcass layers in unbonded flexible pipes based on neural networks

被引:1
作者
Yan, Jun [1 ,2 ]
Du, Hongze [1 ]
Li, Wenbo [1 ]
Xu, Qi [1 ]
Bu, Yufeng [1 ]
Lu, Hailong [1 ]
机构
[1] Dalian Univ Technol, Dept Engn Mech, State Key Lab Struct Anal Ind Equipment, Dalian 116024, Peoples R China
[2] Dalian Univ Technol, Ningbo Res Inst, Ningbo 315016, Peoples R China
基金
中国国家自然科学基金;
关键词
Unbonded flexible pipes; Carcass layer; Radial compression pressure estimation; Neural network; Generalization performance analysis; COMPOSITE PANEL; PREDICTION; COLLAPSE;
D O I
10.1016/j.oceaneng.2023.114578
中图分类号
U6 [水路运输]; P75 [海洋工程];
学科分类号
0814 ; 081505 ; 0824 ; 082401 ;
摘要
Radial pressure resistance is a key factor in the design of unbonded flexible pipe carcass layers because it directly affects the safe installation and use of marine flexible pipes. It is challenging to evaluate the performance of radial compression because the carcass layer, which is a large-angle helical winding structure in innermost flexible pipes with a special-shaped cross section, experiences numerous contact frictions under radial pressure. In this study, a radial pressure estimation approach based on neural networks is proposed to address the aforementioned issues. This study explores the nonlinear relationship between the limited structural responses (circumferential strain) and the overall load (radial compression pressure) from the radial compression experi-mental data and estimates the radial compression pressure of carcass layers. The input variables are the struc-tural strains, and the output variable is the radial pressure. Furthermore, some examples are used to test the generalization of the method, including robustness and understanding, considering the geometric characteristics of the carcass layer. The results demonstrate that the method can accurately predict the radial pressure applied to the carcass layer and provide a theoretical framework for the design of unbonded flexible pipes in deep-sea environments.
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收藏
页数:9
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