Crash simulation of wound composite tubes based on multi-level modelling

被引:4
作者
Berger, A. [1 ,2 ]
Pyttel, T. [3 ]
Duddeck, F. [2 ,4 ]
机构
[1] ESI Gmbh, Neu Isenburg, Germany
[2] Queen Mary Univ London, Sch Engn & Mat Sci, London, England
[3] Tech Hsch Mittelhessen, Dept Mech Engn, Friedberg, Germany
[4] Tech Univ Munich, Dept Civil Geo & Environm Engn, D-80290 Munich, Germany
关键词
crushing tubes; filament winding; virtual manufacturing; finite element method; crash simulation; FILAMENT; STRENGTH; OPTIMIZATION; DESIGN;
D O I
10.1080/13588265.2014.984487
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Fibre reinforced plastics are widely used for energy absorbing parts. Due to their superior strength to density ratio they provide a high performance and are ideal for lightweight design for crashworthiness. For this, it is essential that the mechanical behaviour of fibre reinforced composites be predicted correctly by simulation. However, due to the complex inner structure, this is still a challenging task, in particular in case of highly nonlinear crash loading. In order to provide an alternative in this paper a virtual manufacturing simulation chain is proposed to gather detailed geometrical information about the roving structure of a filament wound tube on meso-scale. In addition effective material properties, based on calibrated models of the individual constituents, for the filament-matrix interaction are derived by micro-scale calculations. Both, combined with a USER MATERIAL model for the roving structure finally provide a complete finite element model which is used for the crash simulation of the filament wound tube. By comparing the numerical results to experimental data, the potential of the approach is shown and occurring differences are discussed as well as possible subsequent investigations are proposed.
引用
收藏
页码:151 / 164
页数:14
相关论文
共 24 条
[1]   Influence of filament winding parameters on composite vessel quality and strength [J].
Cohen, D .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 1997, 28 (12) :1035-1047
[2]   The effect of fiber volume fraction on filament wound composite pressure vessel strength [J].
Cohen, D ;
Mantell, SC ;
Zhao, LY .
COMPOSITES PART B-ENGINEERING, 2001, 32 (05) :411-427
[3]   The predictive capability of failure mode concept-based strength criteria for multidirectional laminates [J].
Cuntze, RG ;
Freund, A .
COMPOSITES SCIENCE AND TECHNOLOGY, 2004, 64 (3-4) :343-377
[4]   OPTIMIZATION OF FILAMENT-WOUND PARTS BASED ON NON-GEODESIC WINDING [J].
DECARVALHO, J ;
LOSSIE, M ;
VANDEPITTE, D ;
VANBRUSSEL, H .
COMPOSITES MANUFACTURING, 1995, 6 (02) :79-84
[5]  
Feindler N., 2012, THESIS TU MUNCHEN GE
[6]   EFFECTS OF BAND WEAVING ON FIBER STRENGTH IN FILAMENT-WOUND COMPOSITE STRUCTURES [J].
GRAMOLL, K ;
RAMAPRASAD, S .
COMPOSITES ENGINEERING, 1995, 5 (04) :363-373
[7]   Experimental testing and phenomenological modelling of the fragmentation process of braided carbon/epoxy composite tubes under axial and oblique impact [J].
Greve, L. ;
Pickett, A. K. ;
Payen, F. .
COMPOSITES PART B-ENGINEERING, 2008, 39 (7-8) :1221-1232
[8]   Effect of fiber waviness on stiffness and strength reduction of unidirectional composites under compressive loading [J].
Hsiao, HM ;
Daniel, IM .
COMPOSITES SCIENCE AND TECHNOLOGY, 1996, 56 (05) :581-593
[9]   Optimal design of filament wound structures under internal pressure based on the semi-geodesic path algorithm [J].
Kim, CU ;
Kang, JH ;
Hong, CS ;
Kim, CG .
COMPOSITE STRUCTURES, 2005, 67 (04) :443-452
[10]   Filament winding: kinematics, collision control and process optimisation through application of dynamic programming [J].
Koussios, S. ;
Bergsma, O. K. ;
Beukers, A. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2006, 37 (11) :2088-2104