F. Ghaemi*a,
R. Yunusa,
A. Ahmadianb,
F. Ismailb,
M. A. M. Salleha and
S. A. Rashida
aInstitute of Advanced Technology (ITMA), Universiti Putra Malaysia, 43400UPM, Serdang, Selangor, Malaysia. E-mail: ferialghaemi@yahoo.com; Tel: +60 1135465200
bDepartment of Mathematics, Faculty of Science, Universiti Putra Malaysia, 43400UPM, Serdang, Selangor, Malaysia
First published on 17th September 2015
In the current study, we investigated the influences of chemical vapor deposition parameters on the formation of uniform structures of few- and multi-layer graphene (FLG and MLG) as a coating phase on carbon fiber (CF). To this end, the process conditions of the chemical vapor deposition method, such as catalyst concentration, reaction temperature and time, and also carbon source flow rate, were optimized. The resulting FLG and MLG with high yields led to the modification of the CF surface by improving its properties. By applying scanning electronic microscopy, transmission electron microscopy and Raman spectroscopy, the surface morphology and structural information of the G–CF were analyzed. It was observed that under different conditions the FLG–CF and MLG–CF were obtained with 54%, 58% yields and also 10.21 m2 g−1, 8.78 m2 g−1 BET surface areas, respectively. Besides that, the FLG–CF and MLG–CF were used as fillers in the polypropylene (PP) composite and the effects of the number of graphene layers on the mechanical and thermal properties of the composite were analyzed. It is noteworthy to mention, composites based on the CF coated with G with only a few layers presented the highest surface area, strength and thermal resistance compared to those based on multi layers.
Besides that, modifying the surface of the CF is an important issue to improve the efficiency of this material in the industry. So, the modifications of the CF structure, by carbon nanomaterials, have made a big difference in improving the properties of the CF. The utilization of the nanomaterials for the modification of the carbon fiber surface to form thermally stable coatings6 and/or for the improvement of the fiber/matrix interfacial adhesion has been recently appraised.7–9 Graphene/polymer nanocomposites have been introduced as a new class of polymer composites with superior properties that can be applied in many fields of sciences and industries.10
Graphene (G) is one of the nanomaterials with a two-dimensional sheet of sp2, which has been grown on the CF to improve the CF properties.11
Its extended honeycomb network is the basic building block of other important allotropes; it can be stacked to form 3D graphite, rolled to form 1D nanotubes, and wrapped to form 0D fullerenes.12 Long-range π-conjugation in graphene yields extraordinary thermal, mechanical, and electrical properties, which have long been the interest of many theoretical studies and more recently have become an exciting area for experimentalists.12,13 Graphene sheets are divided into various types based on the number of layers such as few-layer graphene (4–10 layers) and multi-layer graphene (<10 layers).14,15 A variation of the number of graphene layers may result in a striking change in their properties.16 Accordingly, it is very important to explore the production of graphene with a selected number of layers in large quantities for their further fundamental studies and extensive applications.
In order to determine the number of graphene layers, Raman spectroscopy must be used. Raman spectroscopy is a non-invasive technique, which has been widely used to characterize the structural properties of carbon-based nanomaterials.14 Besides that, this technique has been used to determine the number of graphene layers.14,15
There are several techniques to synthesize graphene sheets including mechanical exfoliation and cleavage,17–19 chemical reduction of GO,17 thermal decomposition on SiC,20,21 liquid exfoliation22,23 and chemical vapor deposition (CVD).24–27 Synthesis of graphene through thermal chemical vapor deposition (CVD) is quite new. CVD growth has been reported as the most popular method for large-scale production of graphene layers.
To the best of our knowledge, modifying the CF by growing different types of graphene (FLG and MLG) with high surface areas and high yields by CVD has not been reported.
Additionally, the resulting FLG–CF and MLG–CF are used as fillers in a polypropylene matrix and analysis of their effects on the polymer composite properties. Therefore, the polymer composites based on graphene have been fabricated with improved properties.28,29 The properties of the nanocomposite depend on the types of nanomaterials with high surface areas and excellent properties. So, the presence of graphene in the polymer matrix leads to a robust structure in the composites. The presence of G–CF in the polymer matrix has been studied to improve the composite properties.30–32 Besides that, the number of graphene layers (few or multi) has a different impact on the polymer composite properties,33 which will be discussed in this paper.
The chemical vapor deposition method was employed to grow the FLG and MLG on the CF at atmospheric pressure at different temperatures from 950 °C to 1050 °C. This process was fulfilled by the decomposition of acetylene on the catalyst surface with different flow rates (25, 50 and 100 standard cubic centimeters per minute (sccm)) on a catalyst surface under a flow of H2/N2 (50, 100 sccm) in the reactor for different reaction times (10, 30 and 50 min). Finally, the C2H2 flow was stopped, the heater was turned off and then the reactor was cooled under the flow of N2.
To analyze the structural information, morphology and surface area of the G–CF, Raman spectroscopy, the electron microscopes (SEM, TEM), and BET surface area analyzer were applied, respectively.
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Besides that, a thermogravimetric analysis (TGA) was used to analyse the thermal resistance of the polymer composite.37 The heating program was performed from 25 °C to 800 °C under a flow of nitrogen.
The catalyst concentration had two effects in this research; first, the effect on the number of graphene layers and second, on the coating phase grown on the CF surface. Based on this, the optimum catalyst concentration with a uniform and completed coating of graphene on the CF with a minimum graphene layer was required.
In the Raman spectra of the graphene, three major bands are significant: the D band, positioned at about 1340–1350 cm−1, the G band at 1580–1590 cm−1, and the 2D band at 2690 cm−1.
The G band is characteristic of all the graphitic sp2-type structures. The D band is related to the number of structural defects within the graphitic layers, and its intensity increases with the number of layers. The 2D band is sensitive to the number of layers, and it is used to determine the number of graphitic layers.38 The observed 2D band Raman peak intensity decreased with increasing the number of graphene layers.39 The ratio of intensity of the D peak and G peak and also the ration of the intensity of the 2D peak and G peak are often used for estimating the degree of graphitization, number and size of the sp2 cluster of carbonic structures. By decreasing the ID/IG, the formation of the carbon structure was proved with high graphitization. Besides that, the I2D/IG ratio of the samples increased when graphene flakes were present in the fewer layers.
Raman analysis indicates that the height of the 2D band decreased in the following order: 50 mM > 100 mM > 150 mM with different ID/IG ratios of 0.8, 0.81 and 0.69 and also I2D/IG ratios of 0.85, 0.68 and 0.61, respectively. As it can be seen in the Raman spectra, by increasing the catalyst concentration the number of graphene sheets increased.
Additionally, the BET surface area, yield and catalyst activity for all three-produced G–CF have been reported in Table 1. The total surface area of the G–CF decreased with increasing the bimetal catalyst concentration. From this result, it can be concluded that increasing the catalyst concentration leads to an increase in the amount and layers of the graphene sheet. So, there is a challenge between the amount and number of layers of the graphene sheet. A high amount of graphene causes the covering of the CF surface completely and then leads to an increase in the yield. Contrarily, increasing the number of graphene layers leads to a decreasing of the surface area of the coated CF.
Catalyst content (mM) | BET surface area (m2 g−1) | PM–CM (g) | CDE (%) |
---|---|---|---|
50 | 8.79 | 0.12 | 24 |
100 | 9.74 | 0.22 | 44 |
150 | 8.84 | 0.25 | 50 |
According to the BET surface area analysis, it was found that the 100 mM catalyst concentration produced few layers of graphene and high yields of graphene on the CF and was selected as an optimum catalyst concentration for FLG synthesis. Besides that, for growing MLG, the 150 mM catalyst concentration was used.
The Raman spectroscopy results are shown in Fig. 2. By increasing the temperature from 950 °C to 1050 °C, the ratio of ID/IG decreased from 0.96 to 0.53 and also I2D/IG increased from 0.65 to 0.82, respectively, which reveals the increment of the graphitization (decreased D peak and an increased G peak). Additionally, the increasing of the 2D peak at 1050 °C, states the presence of the few layers of the graphene. Therefore, when the temperature increased, the number of graphene layers decreased as well (Table 2).
Temperature (°C) | BET surface area (m2 g−1) | PM–CM (g) | Carbon deposition efficiency (%) |
---|---|---|---|
950 | 6.32 | 0.16 | 32 |
1000 | 9.74 | 0.22 | 44 |
1050 | 10.21 | 0.27 | 54 |
The total surface area of the G–CF increased with increasing the reaction temperature. From this result, it can be understood that the reaction-temperature increment leads to an increase in the amount of the thin layers of the graphene nanoparticles as well as the surface area of the resulting G–CF. Moreover, the carbon deposition efficiency also increases with the temperature rise.
The Raman spectra of the graphene layers grown on the surface of the CF showed that the 2D and D peaks of the spectra changed significantly with the growth time (Fig. 3). By increasing the growth time, the D peak increased and 2D peak decreased. So, the ratios of ID/IG were about 0.94, 0.57 and 0.78 and the ratio of I2D/IG were 0.97, 0.82 and 0.65 for 10, 30 and 50 min, respectively. It means that by increasing the synthesis time, the coating of the graphene on the CF increased and covered the CF surface completely. On the other hand, increasing the time led to an increase in the number of graphene layers.
This is evidenced from the intensity of the 2D peak in the Raman spectra, which reveals that the presence of a few layers of graphene coated on the CF was low as reflected by the height of the D peak in the Raman spectra. On the other hand, by increasing the time to 50 min, the catalyst was no longer active, thus a greater number of graphene layers were formed on the CF surface, which caused the decrease in the 2D peak.
Moreover, the surface area results reported in Table 3 state that the G sheet on the CF at 30 min has the highest surface area, whereas, the reaction time of 10 min is insufficient to grow graphene completely on the CF so the surface area is low. By increasing the time to 30 min, the surface area of the G–CF increased. Contrarily, by increasing the duration to 50 min, the number of graphene layers increased; so, the minimum effect of graphene growth was observed.
Time (min) | BET surface area (m2 g−1) | PM–CM (g) | Carbon deposition efficiency (%) |
---|---|---|---|
10 | 8.07 | 0.10 | 20 |
30 | 10.21 | 0.27 | 54 |
50 | 9.96 | 0.30 | 60 |
A similar trend was observed on the yield, it was increased significantly as the reaction time increased from 10 to 30 minutes. For the samples synthesized at 30 and 50 minutes, no major differences are observed in the yield, purity, and thermal decomposition temperatures, thus it was concluded that the reaction time of 30 min was the optimum for the FLG growth and 50 min was suitable for the MLG synthesis.
The Raman analysis (Fig. 4) for the Ni/Cu at different C2H2 flow rates indicates that the ratios of ID/IG were 0.82, 0.56 and 0.94 and also the ratios of I2D/IG were 0.74, 0.82 and 0.69 for 25, 50 and the 100 sccm flow rate which are related to the presence of fewer layers of graphene in the 50 sccm flow rate and amorphous carbon at 25 and 100 sccm flow rate. This could be a consequence of the increase in the flow rate of C2H2—a fact confirmed also by the N2 adsorption–desorption isothermal. Although the 25 sccm flow rate had the potential to grow a single layer graphene sheet but the sheet was incomplete, so the highest surface area of G–CF was at the 50 sccm flow rate. By increasing the flow rate to 100 sccm, the surface area decreased (Table 4).
C2H2 flow rate (sccm) | BET surface area (m2 g−1) | PM–CM (g) | Carbon deposition efficiency (%) |
---|---|---|---|
25 | 8.12 | 0.18 | 36 |
50 | 10.21 | 0.27 | 54 |
100 | 10.33 | 0.31 | 62 |
Regarding the aforementioned circumstances, by applying different conditions in the CVD method, few-layer graphene (FLG) and multi-layer graphene (MLG) were obtained. Therefore, by using the 100 mM catalyst condition at 1050 °C under a 50 sccm acetylene flow rate for 30 min, the FLG on the CF was produced and contrarily by usage of the 150 mM catalyst concentration at 1000 °C under the 100 sccm acetylene flow rate for 50 min, the MLG on the CF was synthesized. SEM and TEM images of FLG–CF and MLG–CF are presented in Fig. 5 and 6, respectively.
Fig. 5 and 6 illustrate the representative SEM and TEM images for the FLG–CF and MLG–CF, respectively. The SEM images demonstrated that the coating of graphene layers on the CF surface and TEM images show the structure and number of graphene layers. It is obvious that the yield and the surface area varied as the layers of graphene increased. The BET surface area and the yield were estimated at about 10.21 m2 g−1 and 54% for the FLG on the CF and 8.78 m2 g−1 and 58% for the MLG on the CF, respectively. Consequently, by increasing the graphene layers on the CF, the coating of the graphene on the CF was denser which led to an increase in the yield and decrease in the surface area. According to the TEM images, it can be seen that different conditions led to the two types of graphene morphology (FLG and MLG). The few layers are presented in the TEM images of Fig. 5 and multi layer in Fig. 6, as well. Regarding the TEM images, the G sheet in the FLG case is clearer and thinner than in the MLG form.
By comparing the FLG–CF–PP, MLG–CF–PP and CF–PP, it was realized that the presence of the G flakes in the polymer matrix was more important than the number of graphene layers as a reinforcing factor; however, the effect of the number of graphene layers also had a significant role as an interlocking operation with the matrix of the composite. Furthermore, to probe the interaction between the fibers and polymer matrix, Raman spectroscopy has been applied. Generally, such an interaction is reflected by a peak shift or peak width change. In the field of composite materials, it has been known for more than two decades that the application of the mechanical strain to fibers (in air, thus without a polymer matrix), such as carbon or Kevlar, results in the shifted frequencies of the Raman peaks (usually 2D peak), which are directly related to the interatomic force constants.40 Therefore, the peak shift or peak width change states the interaction between the fibers and the polymer matrix. So, the spectra related to the graphene nanocomposite were sharper than the neat PP matrix because of the resonance and absorbance effects.
Fig. 8(a–d) shows the Raman spectra of the PP, CF–PP, FLG–CF–PP and MLG–CF–PP samples.
The peaks of graphene in the Raman spectra are obviously observed but the peaks for the PP did not appear because of their low intensity.41 So, the presence of the graphene led to an increase in the intensity of G and 2D peaks, which was due to the enhancement of the interaction between the polymer and filler. Finally, it was found that the interaction of the FLG–CF was more than the MLG–CF with the polymer matrix.
In this research, the tensile stress and Young's modulus of pure PP were about 28 MPa and 1400 MPa, respectively.
Comparing the stiffness of the different resulting composite, illustrates a significant improvement in the tensile modulus. By adding the different fillers into the PP matrix, the tensile stress and modulus of the polymer increased. Besides that, by comparing the tensile results of the filler (CF) with the nanographene (FLG and MLG), it can be concluded that the tensile stress and Young's modulus of the CF–PP are the lowest amounts, which are related to the smooth surface. This leads to the defective flow of the polymer matrix around the CF surface that causes the CF to be easily pulled out of the matrix. The stiffness and the rigidity of the FLG–CF–PP composite were higher than the MLG–CF–PP because of the FLG presence that led to the enhancement of the interfacial adhesion between the filler and the polymer42 because of more enhancement in the surface area of the CF. On the other hand, the presence of a few layers of G with a high surface area in comparison with the multi layers of G led to not only high stress transfer but also the high rigidity of the resultant composite.
It is also revealed in Table 5 that the modulus of FLG–CF–PP was more than MLG–CF–PP and both nanocomposites had higher modulus than the CF–PP composite. Such a significant difference may be related to the presence of graphene and also a difference in the graphene layers. The FLG–CF as the strongest filler had a high adhesion with the polymer matrix that was proved with the tensile results. Additionally, the presence of the graphene layers led to an improvement in the surface area of the CF with a tough interlocking with the PP matrix. Hence, the operative reinforcement modulus of the FLG–CF–PP was more than CF–PP (about 1155 MPa) and the MLG–CF–PP (about 380 MPa). So, it can be concluded that the effect of the presence of the graphene is more than the number of the graphene layers on the mechanical properties of the polymer composite.
Sample | Tensile stress (MPa) | Increment (%) | Tensile modulus (MPa) | Increment (%) |
---|---|---|---|---|
PP | 28 | — | 1400 | — |
CF–PP | 30.5 ± 0.5 | 8.9% | 1603.7 ± 24.5 | 14.5% |
FLG–CF–PP | 51.2 ± 0.8 | 82.8% | 2758.3 ± 49.8 | 97.0% |
MLG–CF–PP | 46.3 ± 0.4 | 65.4% | 2375.2 ± 36.5 | 69.6% |
The TGA curves of the pure PP, CF–PP, FLG–CF–PP and MLG–CF–PP composites are illustrated in Fig. 11(a). The presence of the fillers, such as the CF and G in the PP matrix caused an increase in the composite degradation temperature because of the higher heat absorption capacity. The neat PP decomposed rapidly starting at about 350 °C to 400 °C and was completely degraded at 490 °C with no residual char left. The CF–PP composite started losing weight at 420 °C, which was at a higher temperature than the pure PP.
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Fig. 11 (a) TGA and (b) DTG curves of different composites (1: neat PP, 2: CF–PP, 3: MLG–CF–PP and 4: FLG–CF–PP). |
At 500 °C, the sample started to degrade and the graphene layers oxidized. Therefore, the temperatures above 500 °C corresponded to the lost mass of the graphene while the decomposition below this temperature was related to the amorphous carbon.43 The nanocomposites (FLG–CF–PP and MLG–CF–PP) began losing their mass and ended at the temperatures around 520 °C to 600 °C and 470° to 590°, respectively. The FLG–CF–PP had more thermal resistance than the MLG–CF–PP and both of them had more stability than the CF–PP. Subsequently, by adding the G–CF to the PP matrix, the thermal stability of the polymer composite was significantly enhanced in comparison to the composites without graphene flakes. Further evidences from the DTG graphs in Fig. 11(b) show the melting temperatures of the composites. Using fillers with high thermal resistance increased the melting point of the composites. The melting point for the PP was around 470 °C and increased to 520 °C for CF–PP, 580 °C for MLG–CF–PP and 600 °C for FLG–CF–PP.
These increases can be attributed to the heterogeneous nucleation effect of the nanofillers, which facilitates the crystallization of the PP chains when the nanocomposite is cooled down from a temperature above its melting point.44 It is known that the value of the degree of super cooling, Tmax, can be employed in order to describe the crystallization behavior of the polymers. The lower value of Tmax for the nanocomposites compared to the PP shows that the induction time to crystallize is lower for the nanocomposites than that of PP.
To investigate the impacts of the different fillers on the mechanical and thermal properties of the resulting polymer composites, the tensile test and TGA/DTG were performed. Hence, the FLG–CF–PP with the highest surface area was selected as a pioneer filler in the polymer matrix to increase the mechanical properties and thermal stability properties of the polymer. The tensile stress and modulus of the FLG–CF–PP, MLG–CF–PP and CF–PP composites have increased significantly to about 98.2% and 114.2%, 65.3% and 69.6%, and 8.9% and 14.5%, respectively, compared to the neat PP. In addition, the thermal stability of the CF–PP, MLG–CF–PP and FLG–CF–PP increased from 50 °C to 125 °C, respectively, in comparison to the neat PP. Therefore, these results reveal the importance of not only the modification of the CF surface as a filler in the polymer composites but also the impact of the number of graphene layers on the polymer composite properties.
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