TY - JOUR
T1 - Rectangle preform simulation for 3-D braided composites
AU - Zhang, Mei Zhong
AU - Li, He Jun
AU - Li, Ke Zhi
PY - 2006/9
Y1 - 2006/9
N2 - It is well known that the structure of preform is one of key factors for mechanical performance of three-dimension braided composite. According to the yarn's regulation of four-step braiding pattern, a yarn unit model is presented which is of benefit to computer graphic modeling. At the same time, using Visual C++ and SolidWorks API, the software is programmed which can automatically generate the integral geometric structure of three-dimension braided performs. As a result, inputting different braided parameters, such as braided angle, fraction volume of fiber, yarn radius and different number of rows and columns, the software can automatically generate the braided entity. The three-dimension braided preforms with braided angle 22°, 33°; fraction volume of fiber 40%, 30%; number of rows and columns 2 × 2, 2 × 4, 4 × 4, 4 × 6 are simulated. The simulated results are well in correspondence with the practical preforms. It helps to investigate the microstructure in three-dimension braided preforms. And then, it is the foundation to establish the mechanical model for finite element analysis.
AB - It is well known that the structure of preform is one of key factors for mechanical performance of three-dimension braided composite. According to the yarn's regulation of four-step braiding pattern, a yarn unit model is presented which is of benefit to computer graphic modeling. At the same time, using Visual C++ and SolidWorks API, the software is programmed which can automatically generate the integral geometric structure of three-dimension braided performs. As a result, inputting different braided parameters, such as braided angle, fraction volume of fiber, yarn radius and different number of rows and columns, the software can automatically generate the braided entity. The three-dimension braided preforms with braided angle 22°, 33°; fraction volume of fiber 40%, 30%; number of rows and columns 2 × 2, 2 × 4, 4 × 4, 4 × 6 are simulated. The simulated results are well in correspondence with the practical preforms. It helps to investigate the microstructure in three-dimension braided preforms. And then, it is the foundation to establish the mechanical model for finite element analysis.
KW - Computer simulation
KW - Three-dimension braided composites
KW - Yarn unit model
UR - http://www.scopus.com/inward/record.url?scp=33846159879&partnerID=8YFLogxK
M3 - 文章
AN - SCOPUS:33846159879
SN - 1000-6893
VL - 27
SP - 985
EP - 988
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 5
ER -