A numerical study on carbon nanotube–hybridized carbon fibre pullout

2014 ◽  
Vol 91 ◽  
pp. 38-44 ◽  
Author(s):  
Yuanyuan Jia ◽  
Zuorong Chen ◽  
Wenyi Yan
2020 ◽  
Vol 8 (1) ◽  
Author(s):  
Jyotikalpa Bora ◽  
Sushen Kirtania

Abstract A comparative study of elastic properties and mode I fracture energy has been presented between conventional carbon fibre (CF)/epoxy and advanced carbon nanotube (CNT)/epoxy laminated composite materials. The volume fraction of CNT fibres has been considered as 15%, 30%, and 60% whereas; the volume fraction of CF has been kept constant at 60%. Three stacking sequences of the laminates viz.[0/0/0/0], [0/90/0/90] and [0/30/–30/90] have been considered in the present analysis. Periodic microstructure model has been used to calculate the elastic properties of the laminated composites. It has been observed analytically that the addition of only 15% CNT in epoxy will give almost the same value of longitudinal Young’s modulus as compared to the addition of 60% CF in epoxy. Finite element (FE) analysis of double cantilever beam specimens made from laminated composite has also been performed. It has been observed from FE analysis that the addition of 15% CNT in epoxy will also give almost the same value of mode I fracture energy as compared to the addition of 60% CF in epoxy. The value of mode I fracture energy for [0/0/0/0] laminated composite is two times higher than the other two types of laminated composites.


Carbon ◽  
2020 ◽  
Vol 158 ◽  
pp. 282-290 ◽  
Author(s):  
Jinhu Chen ◽  
Agnieszka Lekawa-Raus ◽  
James Trevarthen ◽  
Tomasz Gizewski ◽  
Damian Lukawski ◽  
...  

2018 ◽  
Vol 166 ◽  
pp. 169-175 ◽  
Author(s):  
Mostafa Yourdkhani ◽  
Wenjiao Liu ◽  
Simon Baril-Gosselin ◽  
François Robitaille ◽  
Pascal Hubert

Structures ◽  
2020 ◽  
Vol 28 ◽  
pp. 2733-2751
Author(s):  
Mohammad Asad ◽  
Manicka Dhanasekar ◽  
Tatheer Zahra ◽  
David Thambiratnam

2019 ◽  
Vol 3 (1) ◽  
pp. 9 ◽  
Author(s):  
Kazuto Tanaka ◽  
Takanobu Nishikawa ◽  
Kazuhiro Aoto ◽  
Tsutao Katayama

In recent years, carbon fibre reinforced thermoplastics (CFRTP) are expected to be used as lightweight structural materials for mass-produced vehicles. CFRTP with thermoplastics as matrix allows us to weld them using melting of matrix by heating. We have been developing a direct resistance heating method, which uses carbon fibres as the resistance heating element. Carbon nanotube (CNT) is expected to be used as additive to FRP and we reported that the fibre/matrix interfacial shear strength was improved by grafting CNT on the surface of carbon fibres and tensile lap-shear strength was improved by using CNT grafted carbon fibre as the heating element for welding. For the practical use of CFRTP for structural parts, flexural strength is also necessary to be evaluated. In this study, flexural test was carried out to clarify the effect of CNT deposition time to the surface of carbon fibres on flexural strength of resistance welded CFRTP using CNT grafted carbon fibre as the heating element. The highest flexural strength was obtained when CNT10, for which CNT is grafted on the carbon fibres for deposition time of 10 min, was used for the heating element of resistance welding. In the case of CNT deposition time of 60 min, the lowest flexural strength was obtained because of the poor impregnation of the resin into the carbon fibre due to the excess CNT on the carbon fibres.


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