Single-walled carbon nanotube-epoxy composites for structural and conductive aerospace adhesives

被引:125
作者
Jakubinek, Michael B. [1 ]
Ashrafi, Behnam [3 ]
Zhang, Yunfa [2 ]
Martinez-Rubi, Yadienka [1 ]
Kingston, Christopher T. [1 ]
Johnston, Andrew [2 ]
Simard, Benoit [1 ]
机构
[1] Natl Res Council Canada, Div Emerging Technol, Secur & Disrupt Technol Portfolio, Ottawa, ON K1A 0R6, Canada
[2] Natl Res Council Canada, Div Engn, Aerosp Portfolio, Ottawa, ON K1A 0R6, Canada
[3] Natl Res Council Canada, Div Engn, Aerosp Portfolio, Montreal, PQ H3T 2B2, Canada
关键词
Nano-structures; Polymer-matrix composites; Electrical properties; Joints/joining; Conductive adhesives; STRENGTH; JOINTS;
D O I
10.1016/j.compositesb.2014.09.022
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Single-walled carbon nanotubes (SWCNTs) were incorporated at low loading (up to similar to 1 wt%) into an unfilled aerospace-grade epoxy system, to impart electrical conductivity while maintaining structural bonding capability, as a route for development of a structural and conductive adhesive. At these low SWCNT loadings the tensile properties were maintained or improved, while strength decreased in a higher loading case. The structural bonding performance of composite-to-composite joints, evaluated in lap-shear and peel tests, was reasonably maintained for adhesives containing 0.5 wt% or I wt% SWCNTs. In the case of the 0.5 wt% SWCNT-adhesive, peel and lap-shear strength were unchanged while the addition of 1 wt% resulted in 30% increase of peel strength but the lap-shear strength was reduced by 10-15%. For 1 wt% SWCNT-adhesives, conductivities as high as 10(-1) S m(-1) and typically similar to 10(-3) S m-1 were achieved. Joint electrical resistance measured between aluminum adherends was larger than predicted by the bulk conductivity, but was reduced by a post-treatment step resulting in apparent joint conductivities within one order of magnitude of the bulk samples. (C) 2014 Published by Elsevier Ltd.
引用
收藏
页码:87 / 93
页数:7
相关论文
共 20 条
[1]  
Ashrafi B, 2012, INT SAMPE TECHN C P
[2]  
Bishopp J., 2011, HDB ADHESIVES SURFAC, P301
[3]  
Brauhofer W., 2008, COMPOS SCI TECHNOL, V69, P1486
[4]  
EBNESAJJAD S, 2011, PDL HANDB SER, P259
[5]   Enhanced bonded aircraft repair using nano-modified adhesives [J].
Gkikas, G. ;
Sioulas, D. ;
Lekatou, A. ;
Barkoula, N. M. ;
Paipetis, A. S. .
MATERIALS & DESIGN, 2012, 41 :394-402
[6]   Mode-I adhesive fracture energy of carbon fibre composite joints with nanoreinforced epoxy adhesives [J].
Gude, M. R. ;
Prolongo, S. G. ;
Gomez-del Rio, T. ;
Urena, A. .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2011, 31 (07) :695-703
[7]   Use of epoxy/multiwalled carbon nanotubes as adhesives to join graphite fibre reinforced polymer composites [J].
Hsiao, KT ;
Alms, J ;
Advani, SG .
NANOTECHNOLOGY, 2003, 14 (07) :791-793
[8]   Efficient laser synthesis of single-walled carbon nanotubes through laser heating of the condensing vaporization plume [J].
Kingston, CT ;
Jakubek, ZJ ;
Dénommée, S ;
Simard, B .
CARBON, 2004, 42 (8-9) :1657-1664
[9]  
Li J, 2007, IEEE AER C, DOI [10.1109/AERO.2007.352642., DOI 10.1109/AERO.2007.352642]
[10]   Aspect Ratio and Loading Effects of Multiwall Carbon Nanotubes in Epoxy for Electrically Conductive Adhesives [J].
Li, Jing ;
Lumpp, Janet K. ;
Andrews, Rodney ;
Jacques, David .
JOURNAL OF ADHESION SCIENCE AND TECHNOLOGY, 2008, 22 (14) :1659-1671