Prediction of the mechanical behavior of fiber-reinforced composite structure considering its shear angle distribution generated during thermo-compression molding process

2019 ◽  
Vol 220 ◽  
pp. 441-450 ◽  
Author(s):  
Dug-Joong Kim ◽  
Myeong-Hyeon Yu ◽  
Jaeyoung Lim ◽  
Byeunggun Nam ◽  
Hak-Sung Kim
2007 ◽  
Vol 2007 (0) ◽  
pp. 413-414
Author(s):  
Keisuke HAYABUSA ◽  
Dai KUDO ◽  
Toshihiro OHTANI ◽  
Shigeru MORINAGA ◽  
Masaki Ohmiya ◽  
...  

2016 ◽  
Vol 1133 ◽  
pp. 121-125
Author(s):  
Hanif Muqsit ◽  
Ali Nawaz Mengal ◽  
Saravanan Karupannan

In this study, the focus was on the optimum design of laminate stacking sequences (LSS) of basalt fiber reinforced composite (BFRP) structure. Eleven rectangular composite panels with different stacking sequences and fiber orientations were analyzed. A three-point flexural test according to ASTM D790 was carried out in ANSYS to simulate the basalt fiber reinforced composite layup flexural strength. From the results, it was found that the composite structure layup of [0/0/45/0/0]s has the highest strength among all samples.


2013 ◽  
Vol 554-557 ◽  
pp. 507-511
Author(s):  
Hong Ling Yin ◽  
Xiong Qi Peng ◽  
Tong Liang Du ◽  
Jun Chen

By combining carbon woven fabric with thermoplastics grains, a thermo-stamping process is proposed for forming parts with complex double curvatures in one step, to implement the affordable application of fiber reinforced composites in high volume merchandises such as automotive industry. In the proposed thermo-stamping process, laminated carbon woven fabrics with thermoplastic grains are heated, and then transferred rapidly to a preheated mould for thermo-stamping, and cooled down to form the carbon fiber reinforced composite part. Various thermoplastics such as PP, PA6 and ABS are used as matrix material in the composite part. Experimental results including shear angle distribution in the fabric, deformed boundary profile of fabric with different original fiber orientation and forming defects are presented. It is demonstrated that high quality parts can be obtained with the proposed forming process, and defects are controllable. By using the proposed process and laminated structures, it is feasible to implement the high-volume and low-cost manufacturing of fiber reinforced composite parts.


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