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Article

SiO2/C Composite as a High Capacity Anode Material of LiNi0.8Co0.15Al0.05O2 Battery Derived from Coal Combustion Fly Ash

by
Arif Jumari
1,2,
Cornelius Satria Yudha
1,2,
Hendri Widiyandari
2,3,
Annisa Puji Lestari
1,2,
Rina Amelia Rosada
1,2,
Sigit Puji Santosa
4 and
Agus Purwanto
1,2,*
1
Department of Chemical Engineering, Faculty of Engineering, Universitas Sebelas Maret, Jl. Ir. Sutami 36 A, Surakarta, Central Java 57126, Indonesia
2
Centre of Excellence for Electrical Energy Storage Technology, Universitas Sebelas Maret, Jl. Slamet Riyadi, 435, Surakarta, Central Java 57146, Indonesia
3
Department of Physics, Faculty of Mathematic and Natural Science, Universitas Sebelas Maret, Jl. Ir. Sutami 36 A, Surakarta, Central Java 57126, Indonesia
4
Department of Mechanical Engineering, Institut Teknologi Bandung, Jl. Ganesha No.10, Bandung 40132, Indonesia
*
Author to whom correspondence should be addressed.
Appl. Sci. 2020, 10(23), 8428; https://doi.org/10.3390/app10238428
Submission received: 30 October 2020 / Revised: 21 November 2020 / Accepted: 25 November 2020 / Published: 26 November 2020

Abstract

:
Abundantly available SiO2 (silica) has great potential as an anode material for lithium-ion batteries because it is inexpensive and flexible. However, silicon oxide-based anode material preparation usually requires many complex steps. In this article, we report a facile method for preparing a SiO2/C composite derived from coal combustion fly ash as an anode material for Li-ion batteries. SiO2 was obtained by caustic extraction and HCl precipitation. Then, the SiO2/C composite was successfully obtained by mechanical milling followed by heat treatment. The samples were characterized by X-ray diffraction (XRD), Fourier transform infrared spectroscopy (FTIR), and scanning electron microscopy (SEM). Electrochemical properties were tested using an 18650 cylindrical cell utilizing LiNi0.8Co0.15Al0.05O2 (NCA) as the counter electrode. Based on the obtained results, the physiochemical characteristics and electrochemical performance, it was determined that SiO2/C composites were greatly affected by the temperature of heat treatment. The best result was obtained with the SiO2 content of 10% w/w, heating temperature of 500 °C, initial specific discharge capacity of 586 mAh g−1 at 0.1 C (1 C = 378 mAh g−1), and reversible capacity of 87% after 20 cycles. These results confirmed that the obtained materials had good initial discharge capacity, cyclability, high performance, and exhibited great potential as an anode material for LIBs.

1. Introduction

In recent decades, energy shortage and environmental pollution have become serious issues along with the world population growth. Extensive research on renewable energy sources has been rapidly performed. Current renewable energy cannot be separated from energy storage systems. Lithium-ion batteries (LIBs) have become the main candidates for a wide range of applications owing to their fast charging, long lifespan, low cost, high energy density, and ability to be used repeatedly with little degradation in performance [1,2,3,4,5]. Currently, graphite is widely used as a common anode material in the industry owing to its advantage of long lifespan and low cost [6,7,8]. In addition to graphite, Li4Ti5O12 or LTO has also become a promising candidate because it has fast charging and long shelf life [9,10]. However, both of them exhibit low storage capacity (graphite = 372 mAh g−1 and LTO = 160 mAh g−1), which has become a huge obstacle to further application, especially for electric vehicles and electronic devices [1,11]. Various different anode materials with higher capacities have been studied as a candidate of the next generation of anode material. Among the various anode materials studied, Si is considered as the most promising anode material owing to its high theoretical capacity (4200 mAh g−1), moderate operating voltage (0.1–0.5 V vs. Li/Li+), and low stable plateau potential [12,13]. Unfortunately, Si anode materials experience some challenges such as low electrical conductivity, large volume expansion (>300%) during lithiation and delithiation, and an unstable solid electrolyte interphase (SEI), which leads to poor cycling performance [1,9]. Therefore, silicon suboxide or SiOx (x < 2) has been suggested as an alternative anode material. Even though SiOx has a smaller theoretical specific capacity (1961 mAh g−1) than Si, it exhibits better cycling stability, smaller volume expansion, lower cost, and eco-friendliness. SiOx also has a drawback of poor conductivity and low Coulombic efficiency at the initial charge–discharge cycle. On the other hand, it is difficult to produce SiOx owing to the partial oxidation of silicon or semi-reduction of SiO2, which require complex and convoluted synthesis steps. It is advantageous to use SiO2 as an anode material owing to its high availability and because it can be easily extracted from biomass-based waste. Similar to SiOx, SiO2 has low conductivity, which needs to be improved before being applied in full batteries [14,15].
Many approaches have been tried to overcome these problems such as inserting Li into SiO2 and modifying the size of SiO2 [14]. However, one of the most effective ways is to use composite SiO2 with carbon. The composite improves electrical conductivity and also reduces volume expansion during the charge–discharge cycling to maintain a stable electrochemical performance [16]. For example, it has been reported that the SiO2/C composite showed an impressive reversible capacity of 635.7 mAh g−1 at the discharge current of 100 mA g−1 [17]. The 3D SiO2@graphene aerogel composite shows a reversible capacity of 300 mAh g−1 at the discharge current of 500 mA g−1 [18].However, the SiO2-carbon (SiO2/C) composite preparation for anode material usually requires many complex steps such as additional process to modify the morphology, expensive silicon precursor, e.g., Tetraethyl orthosilicate (TEOS), pretreatments [18] and multiple high temperature and long heating process [17], which greatly hinders further improvement. Thus, these additional processes will directly affect the overall production cost of SiO2/C anode material. The use of cheap raw materials, especially from waste, and a simple processing method reduce the production cost in a significant amount. Hence, it is desirable to design a facile method to fabricate SiO2/C composites to realize high-performance anode materials for LIBs. In this article, we reported a facile and inexpensive method for synthesizing the SiO2/C composite from coal combustion-derived fly ash for active anode material by mechanically milling SiO2/C and heat-treating it in an inert atmosphere. The use of silica from coal fly ash is a sustainable approach to recycle, reduce, and reuse industrial waste. SiO2/C was directly used as the anode material for the LiNi0.8Co0.15Al0.05O2 battery. This approach has never been studied before.

2. Materials and Methods

2.1. Synthesize of the SiO2/C Composite from Coal Fly Ash

Coal combustion-derived fly ash was provided by PT Semen Indonesia and was stored in an oven. The chemical composition of fly ash is shown in Table 1. A total of 50 g of coal fly was extracted using 2 L of 2-M NaOH (Merck, Darmstadt, Germany). The mixture was heated at 90 °C for 4 h under stirring at 300 rpm. The separation of filtrate and solid particles was done by gravity filtration followed by the removal of the filter cake. SiO2 particles were obtained by adding 10 N HCl (Merck, Darmstadt, Germany) to the filtrate until pH 6–7. The resulted precipitates were filtered, washed using hot demineralized water three times, and dried under oven at 100 °C for 12 h. Then, the SiO2/C composite was successfully obtained through mechanical milling of SiO2-C with various SiO2 composition using a ball mill for 2 h and heating at 500 °C for 30 min under argon flow. Variations in heat treatment were applied to the optimized composite and performed at 400–600 °C under the same conditions. The overall process of SiO2/C composite synthesis can be seen in Figure 1.

2.2. Material Characterizations

The crystallographic structure of materials was studied by X-ray diffraction (XRD, Rigaku Miniflex 600 Benchtop XRD). The compositional analysis of materials was performed with Fourier transform infrared spectroscopy (FTIR, Shimadzu IRPrestige-21) and X-ray fluorescence (Bruker XRF Spectrometer, Germany). The morphologies of the materials were investigated by scanning electron microscopy (SEM, JSM-6510LA).

2.3. Electrochemical Measurements

Electrochemical measurements were performed using a cylindrical cell (18650) assembled in an argon-filled glove box. LiNi0.8Co0.15Al0.05O2/NCA (MTI, CA, USA) was used as the counter electrode; monolayer polypropylene film (Celgard 2400) was used as the separator, and 1-mol/L LiPF6 dissolved in a mixture of ethylene carbonate and diethyl carbonate (EC/DEC = 1:1, v/v) was used as the electrolyte. The working electrode was prepared with active materials, acetylene black, carboxymethyl cellulose (CMC), and styrene–butadiene rubber (SBR) obtained from MTI, CA, USA with the weight ratio of 93:1:1:5 in deionized water. The mixture was stirred for 5 h at room temperature; then, it was coated onto both side of copper foil using the doctor blade method. The copper foil was dried at 80 °C for 30 min in a vacuum oven. The load mass of active material was approximately 18 mg/cm2. The overall assembly process of cylindrical Li-ion cells is described elsewhere [19,20]. The electrochemical performance of materials was studied by galvanostatic charge–discharge cycling tests using a battery testing system (Neware BTS 6000, Neware Electronic Co., Shenzen, China) at various current rates (1 C = 372 mAh g−1) and room temperature (25 °C).

3. Results

3.1. SiO2 Characterization

Figure 2 shows the as-prepared SiO2 powder obtained from fly ash characterization by XRD (Figure 2a), FTIR (Figure 2b), SEM (Figure 2c), and XRF (Figure 2d). Based on the XRD pattern, the widening peak is detected at 15–35° of 2 theta; thus, it can be concluded that the samples exhibit amorphous properties. The impurity peaks (31° and 45°) of sodium chloride (NaCl) are detected in the sample. The presence of impurities can be caused by an unfinished cleaning process or salt entrapment in silica matrices. In addition to the impurity peak, all peaks from all samples are well indexed to ICSD Card no. 061662. Based on the FTIR spectra, the absorption peaks at 3400, 1630, and 950 cm−1 are attributed to the stretch vibration of –OH from silicanol (Si–OH) or H2O and Si–O from siloxane (Si–O–Si). The peak at 790 cm−1 is attributed to symmetrical Si–O from Si–O–Si stretching vibration. Based on the XRD and FTIR result, SiO2 is successfully obtained by caustic fusion and precipitation through following reactions [21].
SiO2(s) + 2NaOH(aq) → Na2SiO3(aq) + H2O(l)
Na2SiO3(aq) + 2HCl(aq) → H2SiO3(aq) + 2NaCl(aq)
H2SiO3(aq) + H2O(aq) → Si(OH)4(s)
Si(OH)4(s) → SiO2(s) + 2H2O(g)
SEM images (Figure 2c) confirm that there are two types of particles, i.e., primary and secondary. The secondary particle has a diameter of ~7.5 µm, which consists of clustering sub-micron-sized primary particles and small adherents on the surface. These adherents or aggregates enhanced the overall surface area of silica, which resulted in good ionic transfer during Li insertion. The XRF result shows that mostly silicon was obtained, while there are also small sodium impurities (6%), which is confirmed by the XRD result. The NaCl impurities is still detected due to the entrapment of NaCl during the silica precipitation process and exist even after multiple washing steps.
The as-obtained SiO2 powder was directly applied as anode in a NCA/SiO2 battery. Figure 3 shows the electrochemical performance of the cell. The theoretical capacity of SiO2 is adapted from a study by Liu et al. (1965 mAh/g), while the theoretical capacity of NCA is estimated at 200 mAh/g. In the final cell assembly, the SiO2 anode was selected as the limiting reactant; therefore, the specific capacity was referred to as the specific capacity of SiO2. Figure 2a shows that the specific charge and discharge capacity of SiO2 is approximately 1396 mAh/g and 1188 mAh/g, respectively. The discharge capacity was maintained for 10 cycles. Even though SiO2 has a considerably lower specific capacity than its theoretical capacity, the capacity was stable at 1/10 C. At increasing rate, as shown in Figure 2b, SiO2 exhibits an inferior rate performance and high level of irreversibility. This can be caused by the formation of electrochemically inactive lithiated SiO2 at high rate (>0.5 C). Previous studies claimed that the reaction mechanism between Li-ion and SiO2 was not been completely understood yet; however, most studies showed a significant irreversible capacity loss during initial cycling [16]. This phenomenon directly indicates the importance of compositing SiO2 with a more stable and highly conductive material such as artificial graphite or Mesocarbon microbeads (MCMB) [17,22].

3.2. Effect of SiO2 Composition in the SiO2/C Composite on Its Structure and Coulombic Capacity

As-prepared SiO2 was mechanically milled with MCMB and heated at 500 °C for 30 min under flowing argon. Figure 4 shows the XRD analysis of the SiO2/C composite with various SiO2 wt%. Because as-obtained SiO2 is in an amorphous form, the diffraction peaks of graphite are dominant in all samples, and the SiO2 peak is not detected; however, there is an increase in the peak width, specifically at 2 theta of 27°, which may be caused by an increase in the amount of amorphous silica (SiO2).
The initial charge/discharge curves of the samples at different SiO2 content at 1/10 C are shown in Figure 5a. It is easily observed that the specific capacity of the SiO2/C composite depends on the SiO2 content in the composite. It is observed that the first capacity of the SiO2/C composite considerably increased with an increase in the SiO2 content. However, when the content of SiO2 was greater than 10%, the capacity was insignificantly increased.
Table 2 shows that all samples have greater capacity than batteries that contain carbon materials (340 mAh g−1) (0.1 V vs. Li/Li+) [1]. Increased capacity occurs because SiO2 (1961 mAh g−1) acts as an active material in composites and is responsible for increasing battery capacity. The increased capacity also indicates that SiO2 used in the composite exhibits electrochemical activity [16,17,18]. Based on previous reports, the small amount of NaCl within silica matrices can potentially enhance the electrochemical performance of LIBs. Borong Wu et.al. claimed that 1% NaCl in electrolyte of Li-Graphite cell can improve the SEI formation on graphite surface which enhance the cycling performance. Study by Ikhsanudin et al. had stated that NaCl can improve the capacity of NCA cathode. Since the specific discharge capacity listed in Table 2 exceeds the capacity of pure graphite, we can conclude that the effect of a small amount of NaCl is still insignificant compared to the effect of silica composite on the graphite anode. However, the effect of NaCl additive on NCA/Graphite cell can be furtherly studied in future research [23,24].
However, an increase in the SiO2 content in the anode material will also result in a decrease in battery stability (cyclability). Figure 5c shows that the reversible capacity of SiO2/C 30% remains at 51% after 15 cycles. This is mostly due to the unstable solid electrolyte interphase (SEI) on the surface of Si [25], which causes lithium to be trapped in the active surface of Si and results in the rapid loss of irreversible capacity and low initial Coulombic efficiency (CE) [16,17,18]. These reactions that occur in the process can be summarized as follows:
2SiO2 + 4Li+ + 4e → Li4SiO4 + Si
SiO2 + 2Li+ + 2e → Li2O + Si
Si + xLi + xe → Li4Si
Reactions (2) and (3) result in the generation of irreversible capacity, which leads to capacity loss. In addition, Li4SiO4 compounds are reported to be electrochemically inactivated. However, Li4SiO4 and Li2O act as buffer components and accommodate volume expansion that occurs in LixSi during lithiation and delithiation. This occurs because Li4SiO4 (2.39 g cm−3) and Li2O (2.02 g cm−3) are denser materials than LixSi. The presence of oxide compounds shows a significant decrease in the volume expansion compared to when the material is homogeneous LixSi [16,26,27].
The rate performance of the SiO2/C 10% composite was further examined, and the results are shown in Figure 5d; the samples tested at the discharge current of 0.1, 0.5, and 1 C provided the best performance. It is clearly observed that the sample still has a high specific capacity of approximately 395 mAh g−1 at the current rate of 1 C. Figure 5c also shows that the reversible capacity slowly increased from 541 mAh g−1 to 601 mAh g−1 after 3 cycles and was stable after the first 15 cycles. The latest studies explain that an increase in reversible capacity is due to SiO2, which is not fully active at the beginning of cycling and will be active in the next cycling [9,10,24]. Figure 5d shows that the sample has high stability. It was possible to obtain the reversible capacity at 87% after 31 cycles at 1 C and CE was always above 98%. These results confirm that the SiO2/C composite with 10 wt% SiO2 exhibited the best performance owing to its excellent specific capacity, good cyclability, and high performance, and showed considerable potential as an anode material for LIBs.

3.3. Effect of Heat Treatment on the SiO2/C Composite

Figure 6a shows the FTIR spectra of SiO2 in the composite after heat treatment at 400, 500, and 600 °C. The FTIR spectra of SiO2/C show similar results at various heat treatment temperatures. The peaks at 3432, 3434, and 3433 cm−1 are assigned to the –OH stretching in SiO2/C heat-treated at 400, 500, and 600 °C, respectively. Furthermore, the peak at approximately 1600 cm−1 indicates the presence of an –OH bending band. This hydroxide group indicates the presence of water molecules [15]. It is observed that an increase in the heat treatment temperature will decrease the water content in SiO2/C (Figure 6b). The presence of SiO2 is detected as the Si–O–Si stretching vibration of the sharp peak at approximately 1100 cm−1 [28,29]. SiO2/C heat-treated at 600 °C shows smaller transmittance than SiO2/C heat-treated at 400 and 500 °C, specifically for the peak at approximately 1100 cm−1. On the other hand, SiO2/C heat-treated at 600 °C has better transmittance than SiO2/C heat-treated at 400 and 500 °C for the peak at approximately 400 cm−1. It can be concluded that heat treatment affects the SiO2 surface chemistry. The FTIR spectra of graphite also show peaks at approximately 3400 and 1600 cm−1, which indicates the presence of water molecules in graphite, as previously described.
Figure 7 shows the XRD patterns of SiO2/C at various heat treatment temperatures. Based on the figure, all samples exhibit a graphite structure (JCPDS PDF 75-2078) owing to low content and crystallinity of silica compared to that of artificial graphite. The crystallite size of the samples, which is determined by the Scherer equation [19,30], is affected by the heat treatment temperature; it increased along with an increase in temperature, although heat treatment was performed for only 30 min.
The SEM characterization of artificial graphite and SiO2/C composite heated at various temperatures is shown in Figure 8. Most graphite particles have a spherical shape with ~27-μm size. Flakes of carbon were observed between spherical particles. The abovementioned figure shows that SiO2/C has rough surface morphology, owing to the presence of 10% of SiO2 aggregates. SiO2 secondary particles break into micron-sized primary particles during the ball milling process. The average primary particle size of SiO2 on the graphite surface heated at 400, 500, and 600 °C is 344, 399, and 450 nm, respectively. Moreover, with an increase in temperature, the average particle size of SiO2/C increases, owing to the agglomeration of particles [9,31].
Table 3 shows that all samples have greater specific capacity than batteries using carbon materials. Compared to graphite, all samples have higher initial discharge capacity with an increase in temperature. Thus far, it can be concluded that with an addition of SiO2 and increase in the heat treatment temperature, all of our samples exhibit high initial capacity; this improvement is achieved using an easy and simple method.
The initial charge/discharge curve of the samples at different heat treatment temperature of SiO2/C is shown in Figure 9a. Based on the cyclability and rate ability of the cell, 500 °C is the optimum temperature to obtain the SiO2/C composite. It is predicted that at higher temperature, the SiO2/C composite is agglomerated into larger sizes, which lowers the diffusion kinetics of Li-ion during the charge–discharge process. At low temperature, the composite process did not completely occur.
The rate performance of the SiO2/C composite depending on heat treatment variation is shown in Figure 9c. The samples were tested at the charge and discharge current of 0.1, 0.5, and 1 C. It is clearly observed that the samples treated at various temperatures have a high specific capacity of approximately 410 mAh g−1 at the current rate of 1 C. Figure 9c also shows that the reversible capacity increases from 581 mAh g−1 to 595 mAh g−1 after two cycles at the heat treatment temperature of 500 °C. The latest research explains that an increase in reversible capacity owing to SiO2 is not fully active at the beginning of cycling and will be active during next cycling [14,16,17]. The obtained results confirm that the SiO2/C composite heat-treated at 500 °C produces the best results, owing to its excellent specific capacity, good cyclability, and high performance as anodes for LIBs [18,32,33]. Based on Table 4, the overall result is considered good since the starting material is far more inexpensive and the process is simple compared to previous reports.

4. Conclusions

In this study, a high-performance SiO2/C composite was obtained by extracting SiO2 from coal fly ash, mechanical milling of SiO2-C at various SiO2 content, and heating SiO2-C composites at 400–600 °C. SiO2/C composites exhibit specific gravity that is higher than that of carbon materials, which confirms that SiO2 from fly ash acts as an active material and exhibits electrochemical activity. SiO2/C composites with 10% of SiO2 and heat treatment temperature of 500 °C shows the best result with the initial specific capacity of 586 mAh g−1 at 0.1 C and the reversible capacity of 87% after 20 cycles. This method is advantageous for mass production owing to its low cost. Furthermore, the obtained SiO2-C composites exhibit excellent reversible capacity, high initial specific capacity, good cyclability, and high performance of the anode. Based on these results, SiO2 from coal fly ash is a great candidate for the anode material for LIBs.

Author Contributions

Conceptualization, H.W., S.P.S. and A.J.; data curation, A.P.L., R.A.R.; formal analysis, H.W., C.S.Y.; investigation, A.J., A.P. and H.W.; methodology, A.J., A.P.L., R.A.R.; project administration, A.P.; supervision, A.P.; validation, S.P.S., A.J. and A.P.; visualization, C.S.Y.; writing—original draft, A.J. and C.S.Y.; writing—review and editing, A.P. All authors have read and agreed to the published version of the manuscript.

Funding

This research is financially supported by the Indonesian Ministry of Education and Culture through World Class Research scheme with contract No. 112/UN27.21/HK/2020. This research is also partially funded by the Indonesian Ministry of Research and Technology/National Agency for Research and Innovation, and Indonesian Ministry of Education and Culture under World Class University Program managed by Institut Teknologi Bandung (contract No: 1534/C5/KB.07.02/2019).

Acknowledgments

We acknowledge PT. Semen Indonesia for providing the fly ash.

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. Process flow diagram of SiO2 and SiO2/C composite synthesis.
Figure 1. Process flow diagram of SiO2 and SiO2/C composite synthesis.
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Figure 2. Coal fly ash-derived SiO2 characterization by (a) XRD, (b) FTIR, (c) SEM, and (d) XRF.
Figure 2. Coal fly ash-derived SiO2 characterization by (a) XRD, (b) FTIR, (c) SEM, and (d) XRF.
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Figure 3. (a) Charge discharge curve and (b) ratability of SiO2 as the LiNi0.8Co0.15Al0.05O2 (NCA) battery anode.
Figure 3. (a) Charge discharge curve and (b) ratability of SiO2 as the LiNi0.8Co0.15Al0.05O2 (NCA) battery anode.
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Figure 4. Electrochemical performance of SiO2 in the NCA battery.
Figure 4. Electrochemical performance of SiO2 in the NCA battery.
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Figure 5. (a) Initial charge/discharge curve of the samples at different SiO2 content at 0.05 C; (b) magnified charge–discharge curve of the samples; (c) cycling performance of the samples at different SiO2 content; (d) rate and cycling performance of the SiO2/C 10% composite.
Figure 5. (a) Initial charge/discharge curve of the samples at different SiO2 content at 0.05 C; (b) magnified charge–discharge curve of the samples; (c) cycling performance of the samples at different SiO2 content; (d) rate and cycling performance of the SiO2/C 10% composite.
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Figure 6. (a) FTIR spectrum of composite SiO2/C 10% heated at 400, 500, and 600 °C and (b) Magnified zone at hydroxyl peak.
Figure 6. (a) FTIR spectrum of composite SiO2/C 10% heated at 400, 500, and 600 °C and (b) Magnified zone at hydroxyl peak.
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Figure 7. XRD pattern of composite SiO2/C heated at 400, 500, and 600 °C.
Figure 7. XRD pattern of composite SiO2/C heated at 400, 500, and 600 °C.
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Figure 8. SEM images (500× and 10,000× magnification) of graphite (a,b) and 10% SiO2/C composite with heat treatment at (c,d) 400 °C, (e,f) 500 °C, and (g,h) 600 °C.
Figure 8. SEM images (500× and 10,000× magnification) of graphite (a,b) and 10% SiO2/C composite with heat treatment at (c,d) 400 °C, (e,f) 500 °C, and (g,h) 600 °C.
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Figure 9. (a) Initial charge/discharge curve of the SiO2/C composite at 0.1 C; (b) cycling performance of the SiO2/C composite; (c) rate performance of the SiO2/C composite at various temperatures.
Figure 9. (a) Initial charge/discharge curve of the SiO2/C composite at 0.1 C; (b) cycling performance of the SiO2/C composite; (c) rate performance of the SiO2/C composite at various temperatures.
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Table 1. XRF analysis of coal combustion-derived fly ash from PT Semen Indonesia.
Table 1. XRF analysis of coal combustion-derived fly ash from PT Semen Indonesia.
ComponentOSiFeCaAlNaMgKSTiClPMnTrace Metals
wt%36.620.418.19.44.03.53.11.21.10.70.50.40.30.7
Table 2. Initial specific capacity of the SiO2/C composite.
Table 2. Initial specific capacity of the SiO2/C composite.
Content of SiO2
(wt%)
Initial Specific Capacity Based on the Anode
(mAh g−1)
Columbic Efficiency
(%)
034085
135683
336580
542378
1054176
3055272
Table 3. Initial specific capacity of the SiO2/C composite depending on the heat treatment temperature.
Table 3. Initial specific capacity of the SiO2/C composite depending on the heat treatment temperature.
Heat Treatment Temperature
(°C)
Initial Specific Capacity
(mAh g−1)
Columbic Efficiency
(%)
40050674
50058676
60070582
Table 4. Comparative study of SiO2 based anode electrochemical performance.
Table 4. Comparative study of SiO2 based anode electrochemical performance.
PrecursorsProductMethodsVoltage (V)Initial Specific Capacity (mAh/g)Retention CapacityRate PerformancesRef.
TEOSSiO2/Graphene AerogelHydrothermal0–3 V453 (half cell)~100% (300 cycles)103 mAh/g (5 A/g)[18]
TEOSSiO2/C Hollow spherePrecipitation0–3 V400 (half cell)421% (160 cycles)-[17]
TEOSSiO2/C nanorodsPrecipitation0–3 V498 (half cell)95% (100 cycles)345 mAh/g (1 A/g)[33]
SiO2 nanoparticleLithiated SiO2Heat treatment0–3 V1859 (half cell)70% (50 cycles)100 mAh/g (~2 A/g)[14]
Coal derived Fly ashSiO2/GraphiteBall Milling-Heat Treatment2.7–4.2 V541 (full-cell)87% (20 cycles)410 mAh/g (372 mAh/g)This Work
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Jumari, A.; Yudha, C.S.; Widiyandari, H.; Lestari, A.P.; Rosada, R.A.; Santosa, S.P.; Purwanto, A. SiO2/C Composite as a High Capacity Anode Material of LiNi0.8Co0.15Al0.05O2 Battery Derived from Coal Combustion Fly Ash. Appl. Sci. 2020, 10, 8428. https://doi.org/10.3390/app10238428

AMA Style

Jumari A, Yudha CS, Widiyandari H, Lestari AP, Rosada RA, Santosa SP, Purwanto A. SiO2/C Composite as a High Capacity Anode Material of LiNi0.8Co0.15Al0.05O2 Battery Derived from Coal Combustion Fly Ash. Applied Sciences. 2020; 10(23):8428. https://doi.org/10.3390/app10238428

Chicago/Turabian Style

Jumari, Arif, Cornelius Satria Yudha, Hendri Widiyandari, Annisa Puji Lestari, Rina Amelia Rosada, Sigit Puji Santosa, and Agus Purwanto. 2020. "SiO2/C Composite as a High Capacity Anode Material of LiNi0.8Co0.15Al0.05O2 Battery Derived from Coal Combustion Fly Ash" Applied Sciences 10, no. 23: 8428. https://doi.org/10.3390/app10238428

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