Effect of layup sequence on cure deformation and accurate prediction of composite pressure vessels

被引:0
作者
Liang, Jianguo [1 ]
Miao, Chunxiang [1 ]
Li, Yinhui [2 ]
Feng, Jun [3 ]
Wu, Qi [4 ]
Zhao, Chunjiang [5 ]
Jia, Zhaotun [1 ]
Yang, Kun [1 ]
Ning, Zemin [1 ]
Xue, Yuqin [5 ]
机构
[1] Taiyuan Univ Technol, Coll Mech & Vehicle Engn, 79 Yingze West St, Taiyuan 030024, Peoples R China
[2] Taiyuan Univ Technol, Coll Informat & Comp Sci, Taiyuan, Peoples R China
[3] Nanjing Univ Sci & Technol, Natl Key Lab Transit Phys, Nanjing, Peoples R China
[4] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing, Peoples R China
[5] Taiyuan Univ Sci & Technol, Coll Mech Engn, Taiyuan, Peoples R China
基金
中国国家自然科学基金;
关键词
Composite pressure vessel; curing deformation; finite element analysis; joint modeling; layering sequence; PROCESS-INDUCED STRAIN; DIMENSIONAL VARIATIONS; SPRING-IN; DISTORTION; DESIGN;
D O I
10.1177/07316844241250186
中图分类号
TB33 [复合材料];
学科分类号
摘要
The application of composite winding pressure vessels is becoming more and more widespread, and the magnitude of deformation during curing can have a significant impact on service performance, but there are fewer studies on the accurate prediction of the numerical and experimental validation of the deformation during the curing process of pressure vessels. To accurately predict the effect of different angles of layup on the curing deformation of high-pressure hydrogen storage vessels made of T700S-12 K/4251A4B2 carbon fiber/epoxy composites in cylindrical and dome sections. In this paper, WCM-ABAQUS segmented pressure vessel accurate modeling method is proposed for the first time, using the method of converting the chemical shrinkage coefficient of epoxy resin into thermal expansion coefficient equivalently, the finite element prediction of the deformation of the pressure vessel during the curing process in different layup sequences was carried out, and the deformation values of the pressure vessel in different layup sequences were analyzed comparatively. Finally, the winding curing experiments were carried out on pressure vessels with different layup sequences, and the curing deformation values of the experimental tests on pressure vessels with different layup sequences were compared with the finite element simulation values, respectively, and the minimum error value 13.07%. It provides a reliable basis for accurately predicting the deformation value of the pressure vessel curing process, and also provides a reference for subsequent experiments to reduce the curing deformation value.
引用
收藏
页数:19
相关论文
共 52 条
[1]   Process-induced deformation in U-shaped honeycomb aerospace composite structures [J].
Al-Dhaheri, M. ;
Khan, K. A. ;
Umer, R. ;
van Liempt, F. ;
Cantwell, W. J. .
COMPOSITE STRUCTURES, 2020, 248
[2]   Spring-in and warpage of angled composite laminates [J].
Albert, C ;
Fernlund, G .
COMPOSITES SCIENCE AND TECHNOLOGY, 2002, 62 (14) :1895-1912
[3]  
ASTM Standard, 2018, D3518/D3518M-18
[4]  
test method for in-plane shear response of polymer matrix composite materials by tensile test of a 45 laminate
[5]  
ASTM Standard, 2017, D3039/D3039M-17
[6]  
test method for tensile properties of polymer matrix composite materials
[7]   Analysis of cure induced deformation of CFRP U-shaped laminates [J].
Bellini, Costanzo ;
Sorrentino, Luca .
COMPOSITE STRUCTURES, 2018, 197 :1-9
[8]   Analytical solutions for process-induced spring-in of U-shaped composite parts [J].
Chen, Junlei ;
Wang, Jihui ;
Li, Shuxin ;
Wang, Changzeng ;
Ding, Anxin .
THIN-WALLED STRUCTURES, 2021, 169
[9]   Geometrical deviation analysis of CFRP thin laminate assemblies: Numerical and experimental results [J].
Corrado, Andrea ;
Polini, Wilma ;
Sorrentino, Luca ;
Bellini, Costanzo .
COMPOSITES SCIENCE AND TECHNOLOGY, 2018, 168 :1-11
[10]   Optimization of the Winding Layer Structure of High-Pressure Composite Overwrapped Pressure Vessels [J].
Di, Chengrui ;
Zhu, Bo ;
Guo, Xiangji ;
Yu, Junwei ;
Zhao, Yanbin ;
Qiao, Kun .
MATERIALS, 2023, 16 (07)