effect of processing technique on the transport and mechanical properties of vapour grown carbon...
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C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7
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Effect of processing technique on the transportand mechanical properties of vapour grown carbonnanofibre/rubbery epoxy composites for electronicpackaging applications
Mohsin Ali Raza a,*, Aidan Westwood a, Chris Stirling b
a Institute for Materials Research, University of Leeds, Leeds LS2 9JT, UKb Morgan AM&T, Swansea SA6 8PP, UK
A R T I C L E I N F O
Article history:
Received 4 May 2011
Accepted 9 August 2011
Available online 16 August 2011
0008-6223/$ - see front matter � 2011 Elsevidoi:10.1016/j.carbon.2011.08.010
* Corresponding author.E-mail address: [email protected]
A B S T R A C T
Vapour grown carbon nanofibre (VGCNF)/rubbery epoxy (RE) composites were produced, by
either mechanical mixing, three-roll milling (RM) or combined ultrasonication/mechanical
mixing. Incorporation of VGCNFs resulted in significant enhancements in the thermal and
electrical conductivities of the material. Appropriate selection of processing technique and
parameters can help to maximise the potential of VGCNF additions by improving their dis-
persion in the matrix. The composites produced by RM have superior transport properties
compared with those produced by other techniques. The thermal conductivity of such
composites at 40 wt.% VGCNFs reached 1.845 W/m K, a 10-fold increase compared to RE
alone. The thermal conductivity data of VGCNF/RE composites best fits to the Hatta–Taya
model. The lowest electrical percolation threshold is at 2 wt.%, obtained for composites
produced by RM. The thermal conductivity of VGCNF/glassy epoxy (GE) composites at
12 wt.% is 10% lower than the corresponding RE composite but its electrical conductivity
is 2 orders of magnitude higher than the corresponding RE composite. VGCNFs at
40 wt.% increase the compressive strength of rubbery epoxy by �5· but the compressive
modulus of 40 wt.% VGCNF/RE composite is 12 times lower than that of 12 wt.% VGCNF/
GE composite, demonstrating highly compliant nature of RE composites.
� 2011 Elsevier Ltd. All rights reserved.
1. Introduction
Thermally and electrically conductive polymer composite
materials are of great importance for electronics packaging
applications (EPAs), such as thermal interface materials [1],
electrically conductive adhesives [2], electromagnetic inter-
ference shielding and electrostatic dissipation [3]. Multifunc-
tionality of the polymer composites depends on the size,
shape and nature of the fillers [4]. For example, not all fillers
er Ltd. All rights reserved(M.A. Raza).
can impart both thermal and electrical conductivity to poly-
mer composites; only metallic and carbon based fillers such
as carbon nanotubes (CNTs), carbon fibres and graphite flakes
can enhance both transport properties.
Vapour grown carbon nanofibres (VGCNFs) have been
studied in recent years as fillers to improve mechanical, elec-
trical and thermal properties of the polymers [5,6]. They have
high aspect ratio and are available with diameters ranging
from 50 to 200 nm and lengths of 50–100 lm. Although the
.
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C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7 85
properties of VGCNFs are inferior to those of CNT, their lower
cost and close resemblance to CNTs makes them attractive
for reinforcement in polymers [4].
VGCNFs are produced by catalytic vapour deposition from
hydrocarbons or carbon monoxide over a metal catalyst.
VGCNF consists of a tubular structure comprised of single
or double layers of stacked, truncated graphene cones which
intersect the central hollow along the fibre axis at highly ob-
lique angles [4,7]. Depending upon the cone angle and stack-
ing, various structures of the fibres are possible including
bamboo like [8] and cup-stacked [4]. The outer surface of
the carbon fibres consists of a layer of vapour-deposited car-
bon which thickens the fibres and bonds them together in
large aggregates. The exterior layer of the fibre is not as gra-
phitic as the interior layers and consists of disordered
embryonic graphene planes [7]. The graphitised VGCNF
exhibits very high electrical and thermal conductivity val-
ues. The electrical resistivity of VGCNF after graphitisation
at room temperature is therefore low, at about 5 · 10�5 O cm, which is close to the resistivity of graphite. The
thermal conductivity of as-grown VGCNF is reported to be
20 W/m K but this can exceed 1950 W/m K upon graphitisa-
tion [9]. The thermal conductivity of highly graphitic fibres
is the highest among all commercial fibres [4]. The major
drawback of VGCNFs is their poor tensile properties com-
pared to those of carbon nanotubes. This is probably due
to the weakness of the conic stacks under the shear which
is applied when the fibre is in tension in combination with
their large diameter which increases the likelihood of a flaw
being present in the section under test. Tibbetts and Beetz
[10] believe that the dependence of the fibre mechanical
properties on the diameter is also due to non-uniform car-
bon deposition rates along the length of the fibre during
growth. The large diameter fibres have lower modulus than
the small diameter fibres [4]. Patton et al. [11] estimated
the tensile modulus and tensile strength of Pyrograph-III
nanofibres (having diameter from 100 to 300 nm) to be in
the range of 88–166 GPa and 1.7–3.38 GPa, respectively. In
addition to the diameter, the tensile properties of the fibres
also depend on morphology and crystallinity.
VGCNF composites have been developed by dispersing
them in both thermoplastics [12,13] and thermosetting poly-
mers such as epoxy [5,11,14–16] as well as in elastomers
[17,18]. Two review articles [3,4] give a good overview of the
fabrication and properties of these composites. Among all
these VGCNF/polymer composites, the epoxy-based compos-
ites are the most promising for electronics packaging applica-
tions. Epoxy resins have secured a firm place in engineering
applications due to their ease of processing and application,
low viscosity (before curing), good adhesion, high strength,
low coefficient of thermal expansion, high thermal stability
and low cost [19,20]. The articles published on VGCNF/epoxy
composites to date have mainly addressed the effect of
VGCNF on the mechanical properties of the composites. Only
a few authors have addressed the thermal properties of these
composites. For example, Chen and Ting [21] developed
aligned VGCNF/epoxy composites for thermal management
applications using VGCNF mats. Beircuk et al. [22] compared
the thermal conductivities of single walled carbon nanotube
(SWCNT)/epoxy composites and VGCNF/epoxy composite at
1 wt.% loading of the filler. They found that, compared to
VGCNF, SWCNTs offer three times greater enhancement of
composite thermal conductivity. Patton et al. [11] reported
that the thermal conductivity of the composites ranges from
0.6287 to 0.8072 W/m K at 17–39 vol.% fibre, respectively.
Tibbetts et al. [3] reported the work of Lafdi and Maztex
who measured a thermal conductivity of 2.8 W/m K for a
VGCNF/epoxy composite at 20 wt.% loading, an increase of
1300% compared to the neat epoxy (0.2 W/m K). Choi et al.
[14], Prasse et al. [16] and Kotaki et al. [23] investigated the
electrical properties of such composites. The transport prop-
erties of the composites depend strongly on the processing
methods and conditions because these effect the filler disper-
sion, distribution and aspect ratio [4]. Therefore, it is
important to select appropriate processing routes and condi-
tions to produce VGCNF/polymer composites for different
applications.
Epoxy resins, despite their good properties, have some
drawbacks. Most of the epoxy-based composites reported in
the literature or used for engineering applications are highly
crosslinked materials, have high modulus and lack the con-
formability [24] which, for example, is required for thermal
interface applications. These highly crosslinked epoxy resins
are known as ‘‘glassy epoxy’’. The high modulus and brittle-
ness of glassy epoxy does not allow internal stresses to dissi-
pate which leads to delamination and thermal fatigue when
they are used as adhesives [2]. The addition of filler into such
epoxy resins generally further increases the modulus and re-
duces conformability. Therefore, it is highly desirable to pro-
duce composites for EPAs using a lower modulus matrix.
Although it is possible to decrease the modulus of the epoxy
resin by addition of flexibilisers [25], there is a commercially
available type of epoxy resin, namely rubbery epoxy, which
may be used as an alternative to state of the art glassy epoxy
resins to fabricate superior composites for EPAs. Rubbery
epoxy has a glass transition temperature (ca. 238 K) which is
below ambient temperature and it has a very low modulus
compared to glassy epoxy [18,26]. It is not a true elastomer
but its mechanical properties resemble those of an elastomer
to some extent. There is only one report of VGCNF/rubbery
epoxy composites and this has its emphasis on the mechan-
ical properties [18].
The main focus of this research was to produce VGCNF/
rubbery epoxy composites and to explore their potential for
EPAs. The transport and mechanical properties of the
VGCNF/rubbery epoxy composites are also compared with
those of corresponding composites produced using glassy
epoxy. The issue of fibre dispersion in the matrix was also
studied so as to determine the optimum production condi-
tions for these composites. Composites have been produced
via three different processing routes, namely conventional
mechanical mixing, 3-roll mill mixing and combined ultra-
sonication and mechanical mixing, in order to study the ef-
fect of mixing route on the dispersion and distribution of
the VGCNF filler and on the transport and mechanical proper-
ties of the resulting composites.
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86 C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7
2. Experimental
2.1. Materials used
VGCNFs (Pyrograf III, PS and HT grade) were purchased from
Applied Sciences Inc. These fibres have diameters in the
range of 70–200 nm and lengths about 50–100 lm. These fibres
were used as-received in fabrication of composites.
Epoxy resin, EPIKOTETM EP828, was kindly supplied by
Hexion Specialty Chemicals and two aliphatic polyether-
amine curing agents, Jeffamine D2000 and Jeffamine T403
(ex Huntsman Corporation) were used in this work.
EP828 is an undiluted clear difunctional epoxy bisphenol
A/epicholorhydrin-derived liquid epoxy resin. Jeffamine
D2000 polyetheramine is characterised by repeating
oxypropylene units in the backbone. It is a difunctional pri-
mary amine with a molecular weight of about 2000. Jeffamine
T403 polyetheramine is a trifunctional primary amine having
a molecular weight of about 440. The chemical structures of
EP 828, Jeffamine D2000 and Jeffamine T403 are shown in
Fig. 1.
Rubbery and glassy epoxies were used as matrices for
VGCNF/epoxy composites. Rubbery epoxy (RE), so-called be-
cause (after curing) it has a glass transition temperature be-
low ambient temperature, was produced by mixing epoxy
resin, Epon 828, and curing agent, Jeffamine D2000, at a
weight ratio of 25:75, respectively. The rubbery nature of the
epoxy is attributed to the moderate cross-linking developed
by the Jeffamine D2000. Glassy epoxy (GE) matrix, so-called
because (after curing) it has a glass transition temperature,
Tg, of �80 �C [26], was produced by mixing Epon 828 and
Jeffamine T403, at a weight ratio of 100:42, respectively. The
glassy nature of the resultant epoxy develops due to the
extensive cross-linking of the epoxy resin by the Jeffamine
T403.
2.2. Fabrication of composites
The VGCNF/epoxy composites were prepared by three differ-
ent mixing techniques. These are described in the following
section.
2.2.1. Conventional mechanical mixing (MM)When preparing samples with minimum dimensions of
40 · 25 · 10 mm3, 40–50 g batches were prepared by mixing
Fig. 1 – (a) Chemical structure of EPIKOTETM 828 (b) Chemical stru
T403.
VGCNFs and epoxy. All of the composite dispersions were pre-
pared at room temperature. VGCNFs were dried in an oven at
80 �C for a prolonged period to remove any moisture adsorbed
on their surface. The dried VGCNFs were then mixed at
appropriate percentages with rubbery epoxy by using a
conventional mechanical mixer with a high-speed motor at-
tached to a shaft with a propeller. This was rotated in the
mixture at 4500 rpm for 15 min. These parameters had been
‘‘optimised’’ (i.e. providing material with the highest electrical
conductivity without unduly prolonged mixing). After mixing,
the batch was degassed under vacuum to remove any trapped
air and was poured into a custom-made aluminium mould.
The filled mould was again degassed for half an hour to com-
pletely remove any trapped air. The VGCNF/RE composites
were prepared with a loading of 2–15 wt.% of VGCNFs. It
was not feasible to incorporate VGCNFs at loadings higher
than 15 wt.% by MM due to the high viscosity of the resulting
dispersion. The temperature of the dispersions increased to
60 �C during mixing. This temperature is safe for the rubbery
epoxy as it does not start to cure even after prolonged treat-
ment at 80 �C. VGCNF/GE composite was prepared in the same
way using 12 wt.% of VGCNFs. Both VGCNF/RE and VGCNF/GE
were cured at 80 �C for 2 h and 120 �C for additional 3 h. Sam-
ples of ‘‘neat’’ RE and GE were also produced by the MM
method.
2.2.2. Combined sonication and mechanical mixing (CSM)In this method, VGCNFs were first ultrasonicated in acetone
at concentration of 1.5 g/100 ml for 1, 5 and 10 h to deagglom-
erate the fibres so as to achieve better dispersion in the epoxy.
After sonication, curing agent (Jeffamine D2000) was added at
an appropriate percentage into the VGCNF/acetone disper-
sion. This dispersion was kept stirring on a hot plate at
80 �C until evaporation of the acetone was complete. Once
the acetone had been completely eliminated, resin (Epon
828) was added and mixed by the MM method at 4500 rpm
for 15 min. The rest of the procedure for fabrication of com-
posites was same as described for composites produced by
MM. VGCNF/RE composites were produced at 10 wt.% fibre
loading by the CSM method.
2.2.3. Three-roll mill mixing (RM)A three-roll mill (EXAKT GmbH) was used for fabrication of
the composites. The roll mill has the ability to achieve good
filler dispersion by extremely high shearing force resulting
cture of Jeffamine D2000 (c) Chemical structure of Jeffamine
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C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7 87
from different roller speeds and filler deagglomeration using
the crushing force of the rollers. VGCNF/RE dispersions were
first prepared by MM at 1000 rpm for 2 min. This dispersion
was poured between the feed (n1) and central rollers (n2) as
shown in Fig. 2. The mixture was transported between the
n2 and n3 rollers where it was dispersed to desired degree of
fineness. The scraper system removes the finished product
from the (n3) apron roller. The VGCNF/RE dispersions were
passed through the rolls three times in gap mode operation
and two times in force mode operation at a speed of
200 rpm. In gap mode, the rollers were operated in the first
pass with gaps of 120 and 40 lm between n1/n2 rollers and
n2/n3 rollers, respectively. This gap was reduced in the second
and third passes to 60/20 lm and 15/5 lm, respectively. In
force mode operation, the gap between the rollers was kept
at less than 5/<1 lm so that rollers could apply force (approx.
2 N/mm2) on the filler to break the agglomerates. After the
fifth pass, the VGCNF/RE dispersion was collected directly
into the custom-made aluminium mould. The remaining pro-
cedure for the fabrication of the composites was same as de-
scribed for composites produced by MM. VGCNFs were
dispersed at 2–40 wt.% in RE to form composites. There was
no significant temperature increase observed for dispersions
produced by RM due not only to the low speed of the rollers
but also to their acting as heat-sinks.
2.3. Calculation of volume fraction of fibres
The volume fraction of fibres can be calculated from weight
fractions according to following equation [27]:
Vf ¼qmWf
qf Wm þ qmWfð1Þ
and
Vm ¼ 1� Vf ð2Þ
In Eqs. (1) and (2), Vf and Vm are the volume fraction of the
VGCNF and matrix, respectively, Wf and Wm are the weight
fraction of the VGCNF and matrix, respectively and qf and
qm are the densities of the VGCNF (1.95 g/cm3) and rubbery
epoxy matrix (1.025 g/cm3), respectively.
Fig. 2 – Schematic of exact 3-roll mill (http://www.exakt.de).
2.4. Characterisation
2.4.1. Electron microscopyThe morphology of the composites was observed using a LEO
1530 field emission gun scanning electron microscope (FEG-
SEM). The images were obtained using secondary electrons
at 3 kV with a working distance of 3 mm. The samples for
SEM analysis were prepared by cooling strips of the compos-
ites in liquid nitrogen and then brittle-fracturing them. The
fractured surface of the sample was sputter-coated with a
thin layer (5 nm) of Pt/Pd alloy prior to the SEM analysis. All
of the samples studied by SEM were sectioned in such a man-
ner that a surface parallel to the direction of gravity (during
moulding) was exposed for the analysis. TEM images of
VGCNF were obtained using an FEI CM200 FEGTEM with Gatan
GIF 200 Imaging filter running at 197 kV. Samples were pre-
pared by dispersing in methanol, with a drop placed on a
holey carbon-coated copper grid.
2.4.2. Thermal conductivityThe thermal conductivity of the neat epoxy resin and com-
posites was measured by the hot disk thermal constant ana-
lyser method (Hot Disk� AB), which is a transient plane
source technique [28]. The sensor, which acts both as heat
source and temperature recorder, with a radius of 3.180 mm,
was sandwiched between the two halves of each sample.
For measurement, each sample half was prepared so as to
be 8–10 mm thick (in the direction of gravity that applied dur-
ing curing in the mould, i.e. the measurement direction) and
�20 · 20 mm in the other directions, with a flat surface. The
measurements were made by applying a heating power of
0.1–0.2 W for between 10 and 80 s, depending on the thermal
conductivity of the sample. The temperature increase of the
sample as a function of time was recorded to compute the
thermal conductivity of the sample, based on solution of
the transient heat conduction equation.
2.4.3. Electrical conductivityFor electrical conductivity measurement, approximately
cuboidal samples (�5 · 5 · 2 mm) of the composites were
placed between two copper electrodes having dimensions
slightly greater than that of the sample. The electrodes were
connected to an Agilent mulitmeter (34401A) which measured
the resistance of the sample according to the two probe meth-
od. To ensure good contact between the sample and the
copper electrodes, the samples were slightly compressed
between the electrodes. To observe the effect of orientation
of the VGCNFs in the composites, the electrical conductivity,
r, was measured through the sample, designated rz (in the
direction of gravity that applied during curing in the mould),
and along the sample, designated rx and ry, as shown in Fig. 3.
2.4.4. Compression and hardness testingCompression testing of the neat epoxy and composites was
carried out an Instron universal testing system (Model No.
3382 with a 100 kN load cell). Cuboidal samples (�10 · 10 ·8 mm3) were compressed at a strain rate of 0.5 mm min�1.
The compression tests were performed on the samples so
that compression occurred parallel to the direction of gravity
in the original curing moulds (z-direction in Fig. 3). A typical
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Fig. 3 – Schematic of electrical conductivity measurement
set up.
88 C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7
compression test was carried out until the sample fractured.
Hardness testing of the samples was carried out using a shore
hardness tester (Zwick) and values were measured on scale A.
3. Results and discussion
3.1. Morphology
TEM images of the VGCNFs used in this work are shown in
Fig. 4(a) and (b). It can be seen that the fibre walls consist of
stacked graphitic planes in one or two distinct layers and
have cup-stacked (Fig. 4(a and b)) or bamboo-like (Fig. 4(k))
morphology.
The SEM micrographs of the 12 wt.% VGCNF/RE compos-
ites produced by MM and RM are presented in Fig. 4(c and d)
and Fig. 4(e and f), respectively. The dispersion quality of
the fibres in the rubbery epoxy composite produced by MM
is relatively poor compared to that in the composite produced
by RM. Clusters of agglomerated fibres (indicated by arrows in
Fig 4(c)) and some regions of the matrix without fibres can be
seen in the SEM image of the composite produced by MM. On
the other hand, the SEM image of the composite produced by
RM (Fig. 4(e and f)) showed no significant agglomerates but
uniform dispersion of the fibres in the matrix. In the compos-
ites produced by RM at 25 and 40 wt.% loading, the fibres
seem to be homogeneously dispersed in the matrix as shown
in Fig. 4(i–k). A few voids can be observed in the SEM images
of the composites produced by RM at 40 wt.% loading. These
voids arose due to the slightly higher viscosity of the disper-
sions at such high loading, which did not allow the matrix
to completely homogenise during the curing of the compos-
ite. However, it is believed that these voids can be easily
avoided either by introducing the dispersion into the mould
under pressure or by compression moulding of the compos-
ites. In contrast, the high viscosity of the VGCNF/GE compos-
ites, even at modest fibre loadings, results in a high void
content in these composites as can be seen from SEM images
(Fig. 4(g and h)). In all cases, it appears that there is little or no
orientation effect of the VGCNFs in the matrix and that the fi-
bres are randomly orientated in the matrix at loadings of 12,
25 and 40 wt.% to form isotropic composites. RM processing
also decreased the length of fibres significantly as observed
by SEM imaging (Fig. 4(l)) of processed VGCNFs (obtained after
dissolving the uncured 40 wt.% VGCNF/RE dispersion in ace-
tone and then evaporating the solution on an aluminium
SEM stub). Examination of the SEM image showed that the fi-
bre length after RM processing is as low as 5 lm but averages
about 20 lm.
SEM analysis of the composites therefore demonstrates
that the ability of the RM to deagglomerate the fibres and dis-
perse them uniformly is far superior to that of conventional
mixing (MM). This capability is also evidenced by the fact that
RM enabled the dispersion of VGCNFs in the matrix even at a
loading of 40 wt.%, which could not be achieved by any other
means. Indeed, this composition could also be coated easily
onto a substrate prior to curing, suggesting that the fibres
were well wetted with the resin. In contrast, it was observed
that it was difficult to produce the VGCNF/RE composite at
loadings as low as 15 wt.% of fibres by MM because the high
viscosity of the dispersion hindered processing.
3.2. Thermal conductivity and its correlation withprocessing of composites
The thermal conductivities at room temperature of the
VGCNF/RE and VGCNF/GE composites as a function of wt.%
of VGCNFs are presented in Fig. 5. The thermal conductivity
of the VGCNF/RE composites increases (approximately) line-
arly with increasing fibre loading. The thermal conductivity
of the VGCNF/RE produced by RM is proportional to the vol-
ume fraction of fibre according to the equation obtained by
linear fitting of measured thermal conductivity data versus
volume fraction of fibres: k = 6.69 Vf + 0.21 (where k is the
thermal conductivity of the composites and Vf is the volume
fraction of the fibre). The thermal conductivity of the neat
RE is 0.1769 W/m K (approximately consistent with the afore-
mentioned equation). The composite produced by RM at
15 wt.% loading has a thermal conductivity of 0.811 W/m K
which is a �4.5-fold increase cf. neat RE. The thermal conduc-
tivity of the composites with 25 wt.% (15 vol.%) of VGCNFs
reached 1.31 W/m K, representing a 7-fold increase, and at
40 wt.% (26 vol.%) reached 1.85 W/m K, representing a 10-fold
increase over neat RE.
Compared with the composites produced by MM, the ther-
mal conductivities of the corresponding composites produced
by RM are 11–38% higher, depending upon the wt.% of
VGCNFs incorporated (up to 12 wt.%). This increase can be
attributed to the improved distribution and dispersion of
VGCNF in the matrix achieved by RM, as observed by SEM
analysis. However, at 15 wt.% of VGCNFs the thermal conduc-
tivity of the composite produced by RM is only 8% higher than
the corresponding composite produced by MM. It is possible
that the intensity of shearing by MM increased due to the ob-
served high viscosity of the 15 wt.% VGCNF/RE dispersion and
that this resulted in much more deagglomeration of the fibres
and improved their dispersion in the matrix. However this
does not undermine the advantage of producing VGCNF com-
posites by RM because RM not only offers somewhat superior
dispersion of the filler in the matrix but also allows a higher
loading of the filler in the matrix to be processed without
compromising the uniform dispersion of the filler. In this
way, RM enabled production of composites with very high
thermal conductivities at 25 and 40 wt.% loading of VGCNFs.
These thermal conductivities are not only comparable to
those of many of the commercially available thermal inter-
face materials used for thermal management in EPAs but
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Fig. 4 – TEM images of (a and b) single and double layer VGCNF, SEM images of (c and d) 12 wt.% VGCNF/RE produced by MM
(arrows pointing towards agglomerates), (e and f) 12 wt.% VGCNF/RE produced by RM, (g and h) 12 wt.% VGCNF/GE produced
by MM (arrows pointing toward voids) (i) 25 wt.% VGCNF/RE produced by RM, (j and k) 40 wt.% VGCNF/RE produced by RM
(arrow pointing towards bamboo-shaped VGCNF). Some voids in (i–k) are due to fibre pull-out during fracture (l) solvent-
extracted VGCNFs, showing evidence of fibre shortening to an average length of ca. 20 lm by roll milling.
C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7 89
were also obtained at 20–30 wt.% lower loading of the filler
[1,29].
Patton et al. [11] reported that the thermal conductivity of
VGCNF/epoxy (using Pygrograf III fibres) increases linearly
with the increase of volume fraction of fibre. This is in agree-
ment with our work. However, they reported very low thermal
conductivity values for these composites, finding that com-
posites with VGCNF loadings of 30 and 39.2 vol.% had thermal
conductivities of only 0.6587 W/m K and 0.8072 W/m K,
respectively. In contrast to their work, similar thermal con-
ductivity values were achieved in this work at much lower
loadings (6–9 vol.%) of the fibres. This is attributed to more
intense shearing of the mixtures by RM, resulting in good
dispersion of the fibres in the matrix.
In view of the simplicity and common availability of the
conventional MM technique, the present study did neverthe-
less investigate the effect of the propeller’s mixing speed
and duration on the thermal conductivity of VGCNF/RE
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Fig. 5 – Thermal conductivities of the VGCNF/epoxy
composites as a function of wt.% of VGCNFs.
90 C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7
composites. The results for the 12 wt.% VGCNF/RE composite
produced by MM are presented in Fig. 6. It can be seen that the
thermal conductivity of the composite increases with
increasing mixing speed and time. One interpretation is that
both higher speed and longer mixing time contribute to
deagglomeration of the fibres and subsequently to their good
dispersion in the matrix. The thermal conductivity of 12 wt.%
VGCNF/RE produced by MM at 4500 rpm for 15 min is almost
the same (0.561 W/m K) as was obtained by RM (0.540 W/
m K). In addition, the thermal conductivity of the composite
produced at 4500 rpm for 60 min has 14% higher thermal con-
ductivity than the corresponding composite produced by RM.
These results clearly show that, at lower filler loading, the
conventional mixing technique is equally capable of produc-
ing composites with higher thermal conductivities, provided
that the time and speed of mixing are carefully selected.
On the other hand, the thermal conductivity (0.483 W/m K)
of the 10 wt.% VGCNF/RE composite produced by CSM is al-
most the same as that of the corresponding composite pro-
Fig. 6 – Effect of mixing speed (mixing time is 15 min.) and
time (mixing speed is 4500 rpm) on the thermal
conductivity of the 12 wt.% VGCNF/RE composite produced
by MM.
duced by MM (0.459 W/m K), as shown in Fig. 5. Thus there
is no clear benefit from sonication in this case. The effect of
sonication time on the thermal conductivity of the 10 wt.%
VGCNF/RE composite produced by CSM is shown in Fig. 7.
However, since the standard deviations in the thermal con-
ductivity data are high and overlap each other, it is not possi-
ble to draw any conclusion regarding the effect of sonication
on the thermal conductivity of the composites.
Neat glassy epoxy (GE) has 27% higher thermal conductiv-
ity than the rubbery epoxy (RE) but the thermal conductivity
of 12 wt.% VGCNF/GE produced by MM (0.51 W/m K) is 10%
lower than that of the 12 wt.% VGCNF/RE composite produced
by MM; the increase in thermal conductivity of the GE com-
posite upon loading with 12 wt.% of VGCNFs is 85% lower
than that for the RE composite. GE is a highly cross-linked
polymer and this imparts a higher thermal conductivity than
that of the lightly cross-linked RE polymer. It might therefore
be expected that, upon incorporation of VGCNFs, the resulting
GE composite should have a higher thermal conductivity than
the corresponding RE composite due to GE’s inherent higher
cross-linking density. However, this is not the case for two
reasons: (i) GE has a higher viscosity than RE which inhibits
uniform dispersion of VGCNFs in GE and (ii) air trapped in this
dispersion during mixing due to this higher viscosity results
in excessive void formation in the final GE composite. It was
also observed that the maximum possible loading of VGCNFs
in GE by MM could not exceed 12 wt.% due to the high viscos-
ity of GE. The heat generated by working the high viscosity
12 wt.% VGCNF/GE dispersion increased the temperature to
above 70 �C and if mixing was prolonged this would be hot en-
ough to initiate curing of the GE which might hinder the dis-
persion of VGCNFs. Therefore, for production of VGCNF/GE
composite at higher filler loadings steps must be taken to en-
sure that the temperature does not exceed a safe limit (e.g.
50 �C). In contrast, RE overcomes the problems associated
with GE since RE not only has a low modulus in its cured state
but its lower viscosity before curing (643 cP at a shear rate of
15 s�1) allows higher loading of the filler and poses no risk of
curing initiation due to heat of working. The final RE compos-
ite also contains fewer voids compared to GE composites.
These advantages make RE more attractive than GE for mak-
ing composites with higher loadings of fillers.
Fig. 7 – Effect of sonication time on the thermal conductivity
of the 10 wt.% VGCNF/RE composite produced by CSM.
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C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7 91
3.2.1. Theoretical models for thermal conductivityThe thermal conductivity of VGCNF/RE composites can be
predicted by various theoretical models. However, the estima-
tion of thermal conductivity by these models depends mainly
on using the correct thermal conductivity values for the fill-
ers. Although the theoretical values of thermal conductivities
of individual VGCNFs and carbon nanotubes are very high, in
reality the values are 2–3 orders of magnitude lower due
imperfections in the structure [30]. In polymer composites, a
large fraction of the filler is dispersed in the matrix resulting
in contacts between the filler particles to form conducting
networks. The contacts between the fillers also exhibit ther-
mal contact resistance which affects the overall thermal con-
ductivity of the composites. Yu et al. [30] calculated the
thermal conductivity of carbon nanofibres (grown on silicon
wafers) from thermal contact resistance measurements to
be about 14 W/m K. The structure of these fibres is same as
that of Pyrograf-III (used in this work) with diameters of
�50 nm. Patton et al. [11] estimated the thermal conductivity
of Pyrograf-I fibres having diameter in the range of 1–100 lm
to be about 20 W/m K. Therefore, the thermal conductivity
of VGCNFs used in this work was assumed to be about
20 W/m K and this value was used for the prediction of com-
posite thermal conductivity.
The thermal conductivity of VGCNF/RE composites pre-
dicted according to various models is presented in Fig. 8.
The rule of mixtures (Eq. (3)) gave overestimated values of
thermal conductivity of VGCNF/RE composites and the paral-
lel electric circuit model (Eq. (4)) gave underestimated values
[31].
Kc ¼ Vf Kf þ VmKm ð3Þ
Kc ¼KmKf
Vf Km þ VmKfð4Þ
In Eqs. (3) and (4), Kc is the thermal conductivity of the
composite, Vf and Vm are the volume fraction of the VGCNF
and matrix, respectively and Kf and Km are the thermal
Fig. 8 – Theoretically predicted and experimentally
determined thermal conductivities of VGCNF/RE composites
vs. volume fraction of the fibres.
conductivities of the VGCNF (20 W/m K) and the matrix
(0.1769 W/m K), respectively.
The former assumes that fillers are able to form conduc-
tive networks in the matrix and ignores any effect of filler as-
pect ratio. The latter model assumes that the fillers are
homogeneously dispersed and are completely isolated in
the matrix. Consequently, phonons would be damped in the
insulating matrix and will not propagate from one particle
to another. The assumption of the parallel electric circuit
model cannot be envisaged as realistic because it is not pos-
sible to produce polymer composites without filler–filler con-
tacts at high filler loadings. Hence, both models are unable to
predict accurately the thermal transport behaviour of the
VGCNF/RE composites.
A more realistic model for 3-dimensional randomly ori-
ented short fibre reinforced composites was developed by
Hatta et al. [32] based on the Eshelby’s equivalent inclusion
model [33] (Eq. (5)) and is known as the Hatta–Taya model.
This model takes into account the aspect ratio of the fibres,
which is one of the key parameters governing the thermal
transport properties of the fibre based composites.
Kc ¼½1þ VffðKf � KmÞð2S33 þ S11Þ þ 2Kmg� � Km
Jð5Þ
where,
J ¼ 3ð1 � Vf ÞðKf � KmÞS11S33 þ Kmf3ðS11 þ S33Þ � Vf ð2S11 þ S33Þgþ3K2
mðKf�KmÞ, S11 and S33 are the tensors for thermal conduction, a
function of fibre’s aspect ratio g.
S11 ¼g
2ðg2 � 1Þ32
fgðg2 � 1Þ12 � cos h�1gg
S33 ¼ 1� 2S11
g ¼ LD, where L is the length and D is the diameter of the fibre.
It was observed by SEM that VGCNF/RE composites contain
randomly oriented VGCNFs and therefore, the thermal con-
ductivity of the composites is assumed to be isotropic at all
loadings. The average length and diameter of the fibres were
determined from SEM analysis of VGCNF/RE composites pro-
duced by RM and were about 20 lm and 116 nm (Fig. 4(l)),
respectively, i.e., the aspect ratio (g) is 172. Using the value
of g = 172 and assuming the thermal conductivity of VGCNF
is 20 W/m K, our thermal conductivity data for VGCNF/RE
composites produced by RM correlates well to the Hatta–Taya
model. It can be seen from Fig. 8 that by assuming a fibre
length, L = 1 lm (i.e., g = 9), the thermal conductivity of the
resulting composites would be significantly lower than for
composites having our observed fibre length, L = 20 lm (i.e.,
g = 172). However, it was also observed that when the value
of g was set to be >200 (e.g. g = 1030, L = 120 lm and
D = 116 nm) this had no significant effect on the thermal con-
ductivity of the resulting composites compared to the case for
g = 172. This shows that the Hatta–Taya model is valid only for
a randomly oriented short fibre composite (i.e. the present
case) when the aspect ratio is below a certain value [33].
3.3. Electrical conductivity
The electrical conductivities (measured in the direction paral-
lel to that of gravity during curing of the resin, rz) of the
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92 C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7
VGCNF/epoxy composites produced by various techniques as
a function of wt.% of VGCNFs are presented in Fig. 9. As
observed for the thermal conductivity, the highest increase
in electrical conductivity with VGCNF loading is observed
for the composites produced by the RM and lowest increase
is observed for composites produced by CSM. The percolation
threshold (Pc), defined as the filler content required to achieve
a conductivity of P10�6 S.m�1 [31], for VGCNF/RE composites
produced by RM was found to be just less than 2 wt.%. On the
other hand, Pc may be as high as 4 wt.% for composites pro-
duced by MM since the electrical conductivity of 2 wt.%
VGCNF/RE composite produced by MM was not detectable
by the instrument used (which can detect resistance up to
100 MO).
In contrast to the thermal conductivity behaviour of the
composites produced by MM, increasing the mixing time at
4500 rpm caused no significant increase in the electrical con-
ductivity of the 12 wt.% VGCNF/RE composite produced by
MM. This was the main reason that all of the composites pro-
duced by MM used a speed of 4500 rpm (for no more than
15 min.). However, it should be noted that unlike thermal con-
ductivity, the electrical conductivity of 12 wt.% VGCNF/RE
composite produced by RM is an order of magnitude higher
than that of the corresponding composite produced by MM.
Hence, the lower Pc obtained for the composites produced
by RM and higher electrical conductivity indicates that the
RM not only dispersed the VGCNFs in the matrix well but also
distributed them uniformly. The good distribution of these fi-
bres in the matrix decreases their separation by the polymer
matrix which increases the probability of electron tunneling
and hence increases the electrical conductivity of the result-
ing composite.
Fig. 9 – Electrical conductivities of VGCNF/RE composites produce
inset shows the fit of RM-derived VGCNF/RE composites’ data to
The electrical conductivity of 10 wt.% VGCNF/RE composite
produced by CSM is one order of magnitude lower than the cor-
responding composite produced by MM. This is thought to be
due to a decrease in aspect ratio of the fibres or breaking of car-
bon bridges between the fibres during the sonication process
[18]. It was also observed for 10 wt.% VGCNF/RE composite pro-
duced by CSM that longer sonication times (up to 10 h) caused
no increase in electrical conductivity and this is similar to what
is observed for its thermal conductivity.
The electrical conductivities of the VGCNF/RE composites
were measured in different directions through samples (as
shown in Fig. 3) to study the effect of fibre orientation on
the electrical conductivity and these are plotted in Fig. 10 as
a function of wt.% of VGCNF.
The electrical conductivities of VGCNF/RE composites pro-
duced by RM are almost the same in every direction at all
loadings of VGCNFs. This clearly indicates that the compos-
ites produced by RM have no preferred orientation of the
VGCNFs, which is thus oriented randomly in the matrix.
Hence, all of the composites produced by RM are isotropic.
On the other hand, the composites produced by MM have
slightly higher electrical conductivities in the x or y direction
than in the z-direction. This indicates that fibres are slightly
more oriented in the x or y directions at VGCNF loadings of
up to 15 wt.%. These results show that the composites pro-
duced by RM are more isotropic than those produced by MM.
The electrical conductivity comparison between 12 wt.%
VGCNF/GE composite produced by MM and the corresponding
RE composite is also shown in Fig. 10. The GE composite has
an electrical conductivity which is 2 orders of magnitude
higher (in the z-direction) than for the RE composite. The
electrical conductivities of GE composites are almost the
d by various techniques as a function of wt.% of VGCNF. The
the power law.
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Fig. 10 – Electrical conductivities of VGCNF/RE composites as a function of wt.% of VGCNF produced by RM and MM measured
in different directions. The electrical conductivity of VGCNF/GE composite is also presented for comparison.
C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7 93
same in all directions unlike RE composites, and the GE com-
posite produced by MM at 12 wt.% of VGCNFs is highly isotro-
pic in nature. The higher electrical conductivity of the VGCNF/
GE composite is attributed to the inherent high electrical con-
ductivity (6.3 · 10�9 S.cm�1) and high cross-linking density of
GE compared to RE [2]. The extensive cross-linking of GE
brings the molecular chains of epoxy close to each other
and, compared to RE, this could decrease the gap between
the fibres allowing more electrons to tunnel/transport be-
tween the fibres and through the thin layer of GE.
At the percolation threshold composites undergo a transi-
tion from insulator to conductor due to the ability of the fillers
to form conductive networks. The current–voltage behaviour
of the composites below the percolation threshold results in
a straight line according to Ohm’s law which indicates that
particle–particle contact is the dominant mechanism of con-
duction. Electrical conductivity of the composites thus in-
creases by several orders of magnitude compared to the
neat polymer. However, above Pc the current–voltage relation-
ship of the composites does not follow a linear relationship
[4]. This indicates that electron tunneling between filler parti-
cles is the dominant conduction mechanism. The behaviour
of such composites above Pc can be described with a percola-
tion-like power law (Eq. 6) [34].
r / ðP� PcÞt ð6Þ
Where, r is electrical conductivity of the composite, P is the
volume fraction of the VGCNFs, Pc is the volume fraction of
the VGCNFs at the percolation threshold and t is the critical
exponent which depends on the structure of the conductive
networks.
The inset in Fig. 9 shows that the VGCNF/RE composites’
data fit to the power law, indicating that the dominant mecha-
nism is electron tunneling at Pc. The t value for VGCNF/RE com-
posites is 2.5, higher than the universal value of 2 predicted by
statistical percolation theory [35]. Values of t between 1.7 and 2
are observed for spherical fillers while the values of t > 2 ob-
served for VGCNF [16] and carbon nanotube-based composites
[36] are attributed to their high aspect ratio [4]. The Pc value for
VGCNF/RE composites found in the present work (ca. 2 wt.%)
corresponds well to that reported by Kotaki et al. [23] but is sig-
nificantly higher than that reported by others [16,37]. Allaoui
et al. [37] reported significantly lower Pc (0.064 wt.%) and t
(1.94) values for VGCNF/epoxy composites. The fibre–fibre
and fibre–matrix contacts play a significant role in controlling
the electron tunneling behavior. The tunneling phenomenon
is influenced not only by inter-particle distance (i.e. thickness
of the polymer layer between fillers) but also by the tunneling
resistivity of the polymer [37]. The higher Pc and t values in
the present work might be due to the nature of rubbery epoxy
matrix, which has lower cross-linking density and presumably
lower electrical conductivity than the epoxy used by Allaoui
et al. [37] and Prasse et al. [16]. We have already noted that
the 12 wt.% VGCNF/GE composite has 2 orders of magnitude
higher electrical conductivity than the corresponding RE com-
posite. This suggests that RE has much lower electrical conduc-
tivity than GE and hence contributes to higher Pc and t values,
as compared with those observed by others.
The relationship between electrical and thermal conductiv-
ity as a function of volume fraction of the VGCNF for VGCNF/RE
composites produced by RM is presented in Fig. 11. It can be
seen from Fig. 11 that a significant increase in both electrical
and thermal conductivity of the composites occurs above the
percolation threshold of �1.1 vol.%. This indicates that the
conducting networks formed facilitate both electrical and ther-
mal transport in these composites at Vf above Pc. The inset in
Fig. 11 also shows that the electrical conductivity increases
exponentially with the increase of thermal conductivity (at Vf
between 0.032 and 0.26). The experimental data fit best to Eq.
(7) as shown in the inset
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Fig. 11 – Thermal and electrical conductivity of VGCNF/RE composites vs. vol.% of VGCNF. The inset shows that the electrical
and thermal conductivity data of VGCNF/RE composites fit to the exponential model.
94 C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7
Y ¼ yo þA expðRoxÞ ð7Þ
Where, y is electrical conductivity and x is thermal con-
ductivity, yo is the intercept and A and Ro are constants. The
greater increase in electrical conductivity, as compared to
thermal conductivity, with increasing Vf is related to the in-
crease in electron tunneling between the fibres due to
decreasing gaps, and thus thinner layers of the polymer, be-
tween them.
VGCNF/RE composites showed significant enhancements
in electrical conductivity compared to neat RE but these val-
ues are still significantly lower than required for developing
electrically conductive adhesives for EPAs. However, the good
dispersion of the fibres in the matrix and the isotropic nature
of these composites makes them promising candidates for
electrostatic dissipation and electromagnetic interference
shielding applications.
3.4. Comparison of VGCNF/rubbery epoxy compositeswith carbon nanotube/epoxy composites
Significant efforts have been directed towards harnessing
the high thermal conductivity and electrical conductivity
of CNT in polymer matrix composites. Published data sug-
gest that incorporation of CNT offers significant improve-
ments in epoxy resin transport properties but there are
significant variations in the values of thermal conductivity
reported.
Previously, Thostenson and Chou [38] reported the thermal
conductivities of multiwalled CNT/epoxy composites pro-
duced by RM. They reported that the composites with 5 wt.%
CNT have thermal conductivities of �0.35 W/m K, i.e. �60%
higher than for epoxy alone. It is appropriate to compare the
thermal conductivity of VGCNF/rubbery epoxy composite, also
produced by RM, in this work and this comparison shows that
the incorporation of 5 wt.% VGCNF into rubbery epoxy can pro-
duce �96% enhancement in thermal conductivity. On the other
hand, Yu et al. [39] reported a thermal conductivity increase of
250% upon incorporation of purified single walled CNT in epoxy
and this increase is twice as high as that achieved by incorpora-
tion of VGCNF in rubbery epoxy at an equivalent loading of
6 wt.%. However, Yu et al. [39] reported almost same percolation
threshold (1 vol.%) and furthermore the electrical conductivity
of their 4 vol.% purified single walled CNT/epoxy composite
was the same as that measured in this work for the VGCNF/rub-
bery epoxy composite produced by RM at equivalent loading. In
contrast to the findings of Thostenson et al. and Yu et al., Gojny
et al. [31] reported only a 4% increase in thermal conductivity
upon incorporation of 1.2 wt.% of double walled CNT into epoxy.
Thus, comparison of VGCNF/rubbery epoxy composites with
CNT/epoxy composites suggests that, overall, VGCNFs and CNTs
can give comparable transport properties when used as fillers at
equivalent loadings in epoxy. Thus, the lower cost of VGCNF and
the ease with which they may be processed at higher loadings to
form composites affords them a major advantage over CNT
when producing composites for EPAs.
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Fig. 13 – Compression stress–strain diagram of neat RE, neat
GE, 12 wt.% VGCNF/RE, 12 wt.% VGCNF/GE and 40 wt.%
VGCNF/RE composites.
C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7 95
3.5. Compression testing
The uniaxial compression stress–strain curves of neat RE and
VGCNF/RE composites produced by RM at VGCNF loadings of
12, 15, 25 and 40 wt.%s are presented in Fig. 12. It can be seen
that neat RE has very low modulus (6.77 MPa at a compressive
strain of 20%) and it experiences a compressive strain of �28%
before failure. This demonstrates the conformable nature of
rubbery epoxy which resembles that of elastomers. The addi-
tion of VGCNFs in RE at loadings of 12 and 15 wt.% increases
the compressive modulus by 2· and increases the compres-
sive strength and strain to failure (at which a crack appeared
in the sample) by �3· and �1.5·, respectively. The compres-
sive modulus and failure strength of the 25 wt.% VGCNF/RE
composite increased by �3· and �4·, respectively compared
to neat RE. At 40 wt.% loading of VGCNF, the compressive
modulus, strength and strain to failure increased by �3·, 5·and 1.8·, respectively, again compared to neat RE. Overall,
the compressive modulus increased by only 2–3· with VGCNF
loadings up to 40 wt.%, demonstrating the highly compliant
nature of the RE composites. Thus, compression testing of
VGCNF/RE composites shows that VGCNF addition signifi-
cantly improves the mechanical properties of RE without
compromising the original compliant nature of RE. The
VGCNF increases the compressive strength of RE by acting
as a barrier to crack propagation. It was observed during com-
pression testing that neat RE completely crumbles into pieces
at failure. This behaviour was not observed in the case of
VGCNF/RE composites as the samples remained intact even
when a crack appeared thereby avoiding catastrophic failure.
For comparison, the compressive stress–strain diagram for
VGCNF/RE and VGCNF/GE composites produced by MM is
shown in Fig. 13. The compression stress–strain curves of neat
GE and VGCNF/GE composites show that these materials have
very high moduli compared to those of RE composites. It can be
seen from Fig. 13 that the VGCNF/GE composite has �2· lower
compressive strength at failure compared to neat GE. In con-
trast to RE composites, VGCNFs do not act as a reinforcing filler
for GE composites. The VGCNF/GE composites inherit their
high stiffness from GE and further addition of VGCNF was det-
Fig. 12 – Compression stress–strain diagram of neat RE and
VGCNF/RE composites produced by RM.
rimental to the compressive properties of GE, with the fibres
effectively acting as flaws in this case. This behaviour is the
opposite to what is observed for VGCNF/RE composites. The
compressive modulus of VGCNF/RE composites (measured at
a strain of 20%), even at a loading of 40 wt.%, is�12· lower than
for the 12 wt.% VGCNF/GE composite (Fig. 13).
The compressive stress–strain curves for 12 wt.% VGCNF/
RE composites produced by RM and MM are similar showing
no significant difference at macro-scale (Fig. 13). VGCNF/RE
composites have very low modulus and high compressive
strain to failure even at loadings of up to 40 wt.%. These re-
sults suggest that the effect of VGCNF addition on the
mechanical properties of the material mainly depends upon
the original nature of the polymer. Hence, VGCNFs are highly
effective fillers for improving the mechanical properties of RE
without sacrificing its compliant behaviour. It is believed that
the mechanical properties of VGCNF/RE can be further
enhanced by compression moulding of these composites as
this can be expected to further reduce their void content.
3.6. Hardness testing
The shore hardnesses of neat RE and VGCNF/RE composites
produced by RM and MM are presented in Fig. 14. In parallel
Fig. 14 – Shore hardnesses of neat RE and VGCNF/RE
composites produced by RM and MM.
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96 C A R B O N 5 0 ( 2 0 1 2 ) 8 4 – 9 7
to the compression behaviour, the hardness of VGCNF/RE
composites increases with the increasing wt.% of VGCNF.
The hardness of VGCNF/RE composites produced by RM at
25 and 40 wt.% loading of VGCNF increases by 22% and 28%,
respectively, compared to neat RE. The hardness of 12 wt.%
VGCNF/RE produced by MM is �10% higher than the corre-
sponding composite produced by RM and this might be due
to the presence of agglomerated fibres. The small increases
in hardness and compressive modulus upon incorporation
of VGCNF into RE clearly show that VGCNF/RE composites
are highly compliant materials.
4. Conclusions
• Variations of VGCNF concentration and processing within
the rubbery epoxy matrix have direct and appreciable
effects upon the transport and mechanical properties of
the resulting composites and this allows for the potential
of VGCNFs to be more fully exploited than previously dem-
onstrated in polymer composites.
• Composites produced by RM have much better dispersion and
distribution of VGCNFs in RE than those produced by either
MM or CSM methods. This is attributed to good shear mixing
and crushing action in the RM. The maximum possible load-
ing of VGCNFs in RE depends on the mixing technique. The
VGCNFs can be loaded conveniently into RE up to 40 wt.% by
RM and up to 12–15 wt.% by MM. SEM analysis and electrical
conductivity data show that the VGCNF/RE composites pro-
duced by RM are isotropic in nature while some anisotropy
is observed in the composites produced by MM.
• Increasing the speed and time of mixing in the MM process
significantly improves the thermal conductivities of the
resulting composites. However, increasing the mixing time
does not have an appreciable effect on the electrical con-
ductivities of the resulting composites. On the other hand,
increasing sonication time during CSM mixing deteriorates
the transport properties of the resulting composites. This is
thought to be due to a decrease in the aspect ratio of the
fibres and/or breaking of carbon bridges between the fibres.
• The composites produced by RM have 13–38% higher ther-
mal conductivities and an order of magnitude higher elec-
trical conductivities than the composites produced by MM.
However, MM is capable of producing composites with
thermal conductivities comparable to those of composites
produced by RM (at low loadings of VGCNFs) by increasing
the speed and time of mixing.
• The thermal conductivities of VGCNF/RE composites increase
linearly with increasing wt.% of VGCNF. The thermal conduc-
tivity of VGCNF/RE composites produced by RM with 15 wt.%
and 40 wt.% of VGCNF resulted in a�4-fold increase (0.811 W/
m K) and �10-fold increase (1.854 W/m K), respectively, com-
pared to RE alone (0.1769 W/m K). The thermal conductivity
data for VGCNF/RE composites (produced by RM) best fit to
the Hatta–Taya model, when assuming the thermal conduc-
tivity of VGCNF is about 20 W/m K.
• The electrical conductivity of VGCNF/RE composites also
increases with increasing wt.% of VGCNF. The lowest per-
colation threshold (2 wt.%) is obtained for composites pro-
duced by RM rather than for those produced by MM. It is
observed that above Pc, the electrical behaviour of VGCNF/RE
composites follows the percolation-like power law. A correla-
tion between electrical and thermal conductivity with
increasing wt.% of VGCNF is observed above Pc. It is also
observed that the electrical conductivity of VGCNF/RE com-
posites increases exponentially with increasing thermal con-
ductivity (i.e. with increasing wt.% of VGCNF) due to a stronger
electron tunneling effect at higher loading of VGCNF.
• The electrical conductivity of a VGCNF/RE composite was
found to be 2 orders of magnitude lower than the corre-
sponding GE composite produced by MM. This behaviour
is attributed to the inherent high electrical conductivity
and high cross-linking density of GE.
• Comparison of these VGCNF/rubbery epoxy composites
with carbon nanotube/epoxy composites indicates that
VGCNF can be used to produce composites with thermal
and electrical transport performance comparable to that
of corresponding composites based on carbon nanotubes.
• Compression testing of VGCNF/RE composites showed that
VGCNF incorporation up to 40 wt.% significantly increased
the compressive strength and strain to failure without sig-
nificant detriment to the original compliant nature of RE.
On the other hand, it was observed that VGCNF incorpora-
tion into GE was detrimental to its mechanical properties.
A VGCNF/RE composite with 40 wt.% loading of VGCNF has
a compressive modulus 12 times lower than that of the
12 wt.% VGCNF/GE composite. This shows that VGCNF/RE
composites are much more compliant materials than
VGCNF/GE composites. The shore hardness of the VGCNF/
RE composite at a loading of 40 wt.% increased by only
28% compared to that of neat RE.
• VGCNF/RE composites, with their unusual combination of
high thermal and electrical conductivities and conformable
nature (for gap filling applications) are promising candidates
for electronics packaging applications, particularly for ther-
mal interface applications. VGCNF/RE composites offer high
compliance, ease of processing (even at high filler loading),
low viscosity and long shelf-life before curing, and fewer voids
(which could act as stress concentrators) after curing. These
features make them attractive as adhesives for various EPAs.
In future work, this concept can be developed by testing the
thermal management performance of these composites in
‘‘demonstrator’’ electronic packaging assemblies which
include relevant working electronic components.
Acknowledgements
The authors thank Morgan AM&T and EPSRC for funding
M.A.R.’s Dorothy Hodgkin Postgraduate Award Scholarship.
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