Study on temperature gradient of ultra-thick foam sandwich composite structure during curing
This paper conducts numerical simulations and experimental measurements on the temperature distribution of ultra-thick foam sandwich composite structure with varying ply thicknesses, aiming to investigate the influence of prepreg ply thickness on the temperature gradient of foam sandwich structure....
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Published in | Case studies in thermal engineering Vol. 65; p. 105552 |
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Main Authors | , , , , , , |
Format | Journal Article |
Language | English |
Published |
Elsevier Ltd
01.01.2025
Elsevier |
Subjects | |
Online Access | Get full text |
ISSN | 2214-157X 2214-157X |
DOI | 10.1016/j.csite.2024.105552 |
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Abstract | This paper conducts numerical simulations and experimental measurements on the temperature distribution of ultra-thick foam sandwich composite structure with varying ply thicknesses, aiming to investigate the influence of prepreg ply thickness on the temperature gradient of foam sandwich structure. Firstly, the curing kinetic of CYCOM970/T300 prepreg was studied using non-isothermal differential scanning calorimetry (DSC). Then, thermal analysis of foam sandwich composite structure with different ply thicknesses was conducted using ABAQUS software combined with user subroutines. Subsequently, thermocouple sensors were used to measure the curing temperature of foam sandwich structure. The results indicate that the prepreg ply thickness has a significant impact on the temperature gradient during the curing process of foam sandwich structure. When there are a larger number of prepreg plies, overheating of the prepreg on the foam upper layer occurs, resulting in a significant temperature gradient in the thickness direction of the structure. In this case, reducing the heating rate of the autoclave curing process can effectively reduce the temperature overshoot of the prepreg on the foam upper layer. |
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AbstractList | This paper conducts numerical simulations and experimental measurements on the temperature distribution of ultra-thick foam sandwich composite structure with varying ply thicknesses, aiming to investigate the influence of prepreg ply thickness on the temperature gradient of foam sandwich structure. Firstly, the curing kinetic of CYCOM970/T300 prepreg was studied using non-isothermal differential scanning calorimetry (DSC). Then, thermal analysis of foam sandwich composite structure with different ply thicknesses was conducted using ABAQUS software combined with user subroutines. Subsequently, thermocouple sensors were used to measure the curing temperature of foam sandwich structure. The results indicate that the prepreg ply thickness has a significant impact on the temperature gradient during the curing process of foam sandwich structure. When there are a larger number of prepreg plies, overheating of the prepreg on the foam upper layer occurs, resulting in a significant temperature gradient in the thickness direction of the structure. In this case, reducing the heating rate of the autoclave curing process can effectively reduce the temperature overshoot of the prepreg on the foam upper layer. |
ArticleNumber | 105552 |
Author | Gao, Xiao-Chu Xu, Si-Si Zhao, Xue-Ying Li, Pei-Zhi Wang, Yu-Kui Zhao, Hai-Tao Sun, Yi |
Author_xml | – sequence: 1 givenname: Yi surname: Sun fullname: Sun, Yi organization: School of Mechatronics Engineering, Harbin Institute of Technology, Harbin, Heilongjiang, 150006, China – sequence: 2 givenname: Xue-Ying surname: Zhao fullname: Zhao, Xue-Ying organization: Harbin Aircraft Industry Group Co., Ltd, Harbin, Heilongjiang, 150066, China – sequence: 3 givenname: Yu-Kui surname: Wang fullname: Wang, Yu-Kui organization: School of Mechatronics Engineering, Harbin Institute of Technology, Harbin, Heilongjiang, 150006, China – sequence: 4 givenname: Hai-Tao surname: Zhao fullname: Zhao, Hai-Tao email: wangyukui@hit.edu.cn organization: School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai, 200240, China – sequence: 5 givenname: Si-Si surname: Xu fullname: Xu, Si-Si organization: Harbin Aircraft Industry Group Co., Ltd, Harbin, Heilongjiang, 150066, China – sequence: 6 givenname: Pei-Zhi surname: Li fullname: Li, Pei-Zhi organization: School of Mechatronics Engineering, Harbin Institute of Technology, Harbin, Heilongjiang, 150006, China – sequence: 7 givenname: Xiao-Chu surname: Gao fullname: Gao, Xiao-Chu organization: School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai, 200240, China |
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Cites_doi | 10.1155/2023/7110987 10.1016/j.csite.2023.103336 10.1177/002199839202600502 10.1177/0954008317693291 10.1016/j.aml.2020.106226 10.1088/1402-4896/ad13dd 10.1016/S0168-874X(03)00119-7 10.1007/s10973-012-2892-3 10.1007/s13272-011-0028-2 10.1016/j.compstruct.2018.05.038 10.3390/ma12020259 10.1016/j.ijmecsci.2021.107033 10.1038/s41598-024-64198-y 10.1177/0021998302036001300 10.1016/j.compstruct.2020.112822 10.1007/s10999-012-9205-7 10.1007/s10443-022-10086-5 10.1177/0021998317699868 10.1088/2053-1591/ac0518 10.1016/j.compstruct.2019.01.041 10.1002/pc.26252 10.1177/002199839102500302 10.1007/s00289-023-04713-9 10.1002/adem.201800036 10.1177/0021998302036021712 10.1016/j.procir.2018.04.042 10.1002/app.40566 10.1016/j.compscitech.2023.110149 10.1002/pat.6066 |
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Keywords | Foam sandwich structure Composite materials Finite element analysis Cure Temperature gradient |
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Snippet | This paper conducts numerical simulations and experimental measurements on the temperature distribution of ultra-thick foam sandwich composite structure with... |
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SubjectTerms | Composite materials Cure Finite element analysis Foam sandwich structure Temperature gradient |
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Title | Study on temperature gradient of ultra-thick foam sandwich composite structure during curing |
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