Variable-thickness design of CFRP B-pillar reinforcement considering draping

被引:4
作者
Lv, Tiantong [1 ]
Wang, Dengfeng [1 ]
机构
[1] Jilin Univ, Coll Automot Engn, State Key Lab Automot Simulat & Control, Changchun 130022, Jilin, Peoples R China
基金
中国国家自然科学基金;
关键词
Preform design; draping simulation; variable-thickness design; ply drop; GENETIC ALGORITHM; OPTIMIZATION; SIMULATION; DEFORMATION; BEHAVIOR; PREFORMS; FABRICS; MODEL;
D O I
10.1177/09544070211005572
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
An integrated optimization method that comprehensively considers draping factors such as fiber reorientations and cutting of layers is proposed for designing CFRP B-pillar reinforcement with a variable thickness. A laminate parameterization scheme, the local shared layer parameterization scheme (LSL-PS), is developed to parameterize the physical composition of laminates with variable-thickness. Kinematic draping simulations and preform designs are introduced to evaluate fiber reorientations and eliminate manufacturing defects. The optimization design of the B-pillar reinforcement is integrated with a LSL-PS, draping-simulation and preform-design, a RBF surrogate model and GA. At the same time, a comparative optimization without the consideration of draping factors is performed in parallel. The comparison results show that considering draping not only helps designers eliminate manufacturing defects but also helps to obtain a further weight reduction of 13.33% because fiber reorientations are fully utilized to improve the structural performance.
引用
收藏
页码:3157 / 3169
页数:13
相关论文
共 32 条
[1]  
Abdalla M., 2008, 49 AIAA ASME ASCE AH, P1798, DOI [10.2514/6.2008-1798, DOI 10.2514/6.2008-1798]
[2]   Genetic algorithm optimization and blending of composite laminates by locally reducing laminate thickness [J].
Adams, DB ;
Watson, LT ;
Gürdal, Z ;
Anderson-Cook, CM .
ADVANCES IN ENGINEERING SOFTWARE, 2004, 35 (01) :35-43
[3]  
[Anonymous], 2009, P 50 AIAA ASME ASCE
[4]   Textile composite structural analysis taking into account the forming process [J].
Aridhi, Abderrahmen ;
Arfaoui, Makrem ;
Mabrouki, Tarek ;
Naouar, Naim ;
Denis, Yvan ;
Zarroug, Malek ;
Boisse, Philippe .
COMPOSITES PART B-ENGINEERING, 2019, 166 :773-784
[5]   Multi-objective crashworthiness optimization of tapered thin-walled square tubes with indentations [J].
Asanjarani, A. ;
Dibajian, S. H. ;
Mandian, A. .
THIN-WALLED STRUCTURES, 2017, 116 :26-36
[6]  
Astm D., 2012, STANDARD TEST METHOD
[7]   Experimental and numerical investigations of the impact behaviour of composite frontal crash structures [J].
Boria, S. ;
Obradovic, J. ;
Belingardi, G. .
COMPOSITES PART B-ENGINEERING, 2015, 79 :20-27
[8]  
FAUX I.D., 1979, COMPUTATIONAL GEOMET
[9]   Draping simulation of carbon/epoxy plain weave fabrics with non-orthogonal constitutive model and material behavior analysis of the cured structure [J].
Han, Min-Gu ;
Chang, Seung-Hwan .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2018, 110 :172-182
[10]  
Hvejsel C., 2008, 12 AIAA ISSMO MULT A, P5897