A Numerical Simulation Method for the One-Step Compression-Stamping Process of Continuous Fiber Reinforced Thermoplastic Composites

被引:8
作者
Chen, Lu [1 ]
Deng, Tianzhengxiong [1 ]
Zhou, Helezi [1 ]
Huang, Zhigao [1 ]
Peng, Xiongqi [2 ]
Zhou, Huamin [1 ]
机构
[1] Huazhong Univ Sci & Technol, Sch Mat Sci & Engn, State Key Lab Mat Proc & & Mould Technol, Wuhan 430074, Peoples R China
[2] Shanghai Jiao Tong Univ, Sch Mat Sci & Engn, Shanghai 200030, Peoples R China
基金
中国国家自然科学基金;
关键词
CFRTP; compression molding; stamping forming; FEM; ALE; FSI; MESH QUALITY IMPROVEMENT; FILLING STAGE; INJECTION; ORIENTATION;
D O I
10.3390/polym13193237
中图分类号
O63 [高分子化学(高聚物)];
学科分类号
070305 ; 080501 ; 081704 ;
摘要
Continuous fiber reinforced thermoplastic (CFRTP) composites have many advantages, such as high strength, high stiffness, shorter cycle, time and enabling the part consolidation of structural components. However, the mass production of the CFRTP parts is still challenging in industry and simulations can be used to better understand internal molding mechanisms. This paper proposes a three-dimensional simulation method for a one-step compression-stamping process which can conduct thermoplastic compression molding and continuous fiber reinforced thermoplastic composite stamping forming in one single mold, simultaneously. To overcome the strongly coupled non-isothermal moving boundary between the polymer and the composites, arbitrary Lagrangian-Eulerian based Navier-Stokes equations were applied to solve the thermoplastic compression, and a fiber rotation based objective stress rate model was used to solve for the composite stamping. Meanwhile, a strongly coupled fluid structure interaction framework with dual mesh technology is proposed to address the non-isothermal moving boundary issue between the polymer and the composites. This simulation method was compared against the experimental results to verify its accuracy. The polymer flow fronts were measured at different molding stages and the error between simulation and experiment was within 3.5%. The final composites' in-plane deformation error was less than 2.5%. The experiment shows that this work can accurately simulate the actual molding process.
引用
收藏
页数:19
相关论文
共 24 条
[1]  
Arnold D.N., 1985, CALCOLO, V21, P337, DOI [10.1007/bf02576171, DOI 10.1007/BF02576171]
[2]   Rate constitutive equations for computational analyses of textile composite reinforcement mechanical behaviour during forming [J].
Badel, P. ;
Gauthier, S. ;
Vidal-Salle, E. ;
Boisse, P. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2009, 40 (08) :997-1007
[3]  
Bathe K.-J., 2006, FINITE ELEMENT PROCE, P148
[4]   FIBER ORIENTATION IN SIMPLE INJECTION MOLDINGS .1. THEORY AND NUMERICAL-METHODS [J].
BAY, RS ;
TUCKER, CL .
POLYMER COMPOSITES, 1992, 13 (04) :317-331
[5]  
Belytschko T., 2013, NONLINEAR FINITE ELE, V2nd, P55
[6]  
Donea JAH., 2004, Encyclopedia of Computational Mechanics Second Edition, V1, P14, DOI DOI 10.1002/0170091355.ECM009
[7]  
HIEBER CA, 1978, ISRAEL J TECHNOL, V16, P248
[8]  
Kennedy P., 2013, FLOW ANAL INJECTION, V2nd, P38
[9]   A multiobjective mesh optimization framework for mesh quality improvement and mesh untangling [J].
Kim, Jibum ;
Panitanarak, Thap ;
Shontz, Suzanne M. .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 2013, 94 (01) :20-42
[10]   Fixed-point fluid-structure interaction solvers with dynamic relaxation [J].
Kuettler, Ulrich ;
Wall, Wolfgang A. .
COMPUTATIONAL MECHANICS, 2008, 43 (01) :61-72