TY - JOUR
T1 - 热塑性预浸料赋形褶皱缺陷的全局灵敏度分析
AU - Zhang, Jiachen
AU - Guo, Yuan
AU - Lyu, Bingyi
AU - Xiao, Jinyou
AU - Wen, Lihua
AU - Hou, Xiao
N1 - Publisher Copyright:
© 2024 Beijing University of Aeronautics and Astronautics (BUAA). All rights reserved.
PY - 2024
Y1 - 2024
N2 - Wrinkles are easily produced during the forming process of complex composite structures, which affect the forming quality and load-bearing performance of the components. It is urgent to establish the quantitative mapping relationship between forming process parameters and prepreg wrinkles to support the low-defect forming manufacturing of components. In this paper, a global sensitivity analysis method for wrinkled defects in thermoplastic prepregs coupled with multiple process parameters is proposed. A finite element simulation method based on a non-orthogonal constitutive model is developed for the wide temperature domain deformation of thermoplastic prepreg. Combining the distance between the prepreg and the mold and the curvature of the out of plane bending of the prepreg improves the reliability of quantitative characterization of crease defects. Finally, a global sensitivity analysis method was established using the Sobol global sensitivity index based on variance, which can quantitatively calculate the impact of forming process parameters on wrinkle defects. It is verified through the typical carbon fiber/polycarbonate (CF/PC) material single dome forming process. The results show that in the temperature range of 200-250℃ and the pressure range of 0.2-2.0 kPa, the influence of temperature on the wrinkling defects of CF/PC prepreg is greater than that of pressure, and there is a dual parameter coupling effect of temperature and pressure during the forming process.
AB - Wrinkles are easily produced during the forming process of complex composite structures, which affect the forming quality and load-bearing performance of the components. It is urgent to establish the quantitative mapping relationship between forming process parameters and prepreg wrinkles to support the low-defect forming manufacturing of components. In this paper, a global sensitivity analysis method for wrinkled defects in thermoplastic prepregs coupled with multiple process parameters is proposed. A finite element simulation method based on a non-orthogonal constitutive model is developed for the wide temperature domain deformation of thermoplastic prepreg. Combining the distance between the prepreg and the mold and the curvature of the out of plane bending of the prepreg improves the reliability of quantitative characterization of crease defects. Finally, a global sensitivity analysis method was established using the Sobol global sensitivity index based on variance, which can quantitatively calculate the impact of forming process parameters on wrinkle defects. It is verified through the typical carbon fiber/polycarbonate (CF/PC) material single dome forming process. The results show that in the temperature range of 200-250℃ and the pressure range of 0.2-2.0 kPa, the influence of temperature on the wrinkling defects of CF/PC prepreg is greater than that of pressure, and there is a dual parameter coupling effect of temperature and pressure during the forming process.
KW - finite element analysis (FEA)
KW - global sensitivity analysis
KW - quantitative analysis
KW - thermoplastic prepreg
KW - wrinkle defect
UR - http://www.scopus.com/inward/record.url?scp=85194941463&partnerID=8YFLogxK
U2 - 10.13801/j.cnki.fhclxb.20230920.003
DO - 10.13801/j.cnki.fhclxb.20230920.003
M3 - 文章
AN - SCOPUS:85194941463
SN - 1000-3851
VL - 41
SP - 1070
EP - 1079
JO - Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica
JF - Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica
IS - 2
ER -