Na Chena,
Jian-Tang Jiang*a,
Cheng-Yan Xuab,
Yong Yuanc and
Liang Zhen*ab
aSchool of Materials Science and Engineering, Harbin Institute of Technology, Harbin, 150001, China. E-mail: jjtcy@hit.edu.cn; lzhen@hit.edu.cn
bMOE Key Laboratory of Micro-System and Micro-Structures Manufacturing, Harbin Institute of Technology, Harbin 150080, China
cPrecision Machinery Research Institutes of Shanghai Space Flight Academy, Shanghai 201600, China
First published on 26th October 2016
A modified Stöber method was utilized for coating SiO2 on Co microspheres with tunable thickness as a filler for electromagnetic absorbing coatings with enhanced oxidation resistance. Co microspheres with diameters of 1.5–3.5 μm were prepared using an aqueous-reduction process, and Co@SiO2 core–shell microspheres with different shell thicknesses were subsequently fabricated by a modified Stöber method using tetraethyl orthosilicate (TEOS) as a Si source. The phase, morphology, and structure of composite microspheres were characterized by X-ray diffraction (XRD), scanning electron microscopy (SEM), energy dispersive X-ray spectroscopy (EDS) and thermogravimetric analysis (TGA). Both ε and μ of Co@SiO2 microspheres increase with the increasing filling ratio. No strong eddy current effect induced by local agglomeration was observed as the presence of a SiO2 shell protects the Co particles from agglomeration and the filling ratio is up to 45 vol%. Due to the presence of the SiO2 shell, the core–shell Co@SiO2 composite microspheres exhibit better antioxidation capability than that of pure Co microspheres. The oxidation temperature of Co@SiO2 is up to 720 °C, much higher than that of Co microspheres (380 °C). The effects of SiO2 shell thicknesses and annealing treatment on microstructure evolution and on EM parameters of Co@SiO2 composites were also investigated.
Considering the requirement for isolating and protecting ferromagnetic particles from aggregation and decaying, coating ferromagnetic metal/alloy particles with an inert shell to construct composite particles with a core–shell structure has been proposed to solve the above mentioned issues.7,11,12 The various types of shell materials used include carbon materials, polymers, SnO2, SiO2, TiO2, BaTiO3, as well as graphene composites.13–17 Zhao et al. synthesized Ni@TiO2 and Ni@SiO2 composite microspheres via a solvothermal method. The EMA properties of the related coatings were significantly enhanced. Furthermore, SiO2-coated Ni core–shell composite microspheres exhibit superior oxidation resistance.18 In our previous study, SiO2 coated Co particles were prepared via a sol–gel process, protecting Co cores from oxidation and corrosion.19 Tang coated FeNi3 nanoparticles with silica shells, which effectively reduced the eddy current effect in the high frequency band.20 Che prepared CoNi@air@TiO2 yolk–shell microspheres by a sol–gel/solvothermal route,21 which is helpful to suppress the eddy current effect. These core–shell materials exhibited enhanced EMA performance and improved the oxidation/corrosion resistance as the shell isolated the ferromagnetic metal/alloy particles from aggregation and decaying.
In addition to the material selection for core/shell of the composite particles, the thickness, as well as the microstructure of shell, is also a vital factor that influences the EM properties of composite particles. Except the insulating and protecting properties, the dielectric relaxation, ferromagnetic resonance as well as the cross-particles exchange couple are all related to the composition, solidity and thickness of the shell. It is thus important to tailor the microstructures of composite particles for designing EMA materials with desired properties.
In the current study, we use a two-step process to prepare Co@SiO2 composites and investigate the microstructure and EM properties, aiming to explore the feasibility to develop highly-filled EMA coatings that can serve at a high temperature and corrosive environment. The study mainly focuses on the influences of microstructure, including the shell thicknesses and the phase composition of Co core, on EM properties. The influence of filling ratio and the oxidation resistance was also evaluated. Our work might shed insight on the design of novel microwave absorbers with high performance.
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Fig. 1 XRD patterns of Co particles (a), Co@SiO2 samples (b), and Co@SiO2 composites annealed in H2 atmosphere for 120 min (c) 500 °C; (d) 600 °C; (e) 800 °C. |
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Fig. 2 SEM images of as-prepared Co particles (a), Co@SiO2 samples (b and c), (d) EDS, and (e–g) elemental mapping of Co, Si and O of a single Co@SiO2 composite microsphere. |
EDS analysis was performed and the results are shown in Fig. 2(c)–(g). The EDS profile of an individual Co@SiO2 microsphere validates the existence of Co, Si and O. The elemental maps reveal that Co, Si and O distribute uniformly within the core–shell structures, as shown in Fig. 2(d) and (e). In particular, the annular dark spot observed in Fig. 2(e) suggests that Co concentrates in the core region, whereas the Si and O in the shell regions. Based on the EDS survey, we can infer that the unique core–shell structured with Co cores and SiO2 shells were formed through the sol–gel process.
SEM observation was performed to examine the effects of annealing on the morphology of Co@SiO2; the SEM images of the annealed products are shown in Fig. 3. Compared with the as-prepared product, the annealed products remain spherical morphology as no apparent changes in the size can be observed, as shown in Fig. 3. In our previous study, the particles' morphology cannot be retained and occurrence of migration and fusion cross over particles leads to merging during high temperature annealing.22 This reveals that the introduced SiO2 layer can effectively separate and isolate Co microspheres from contacting to each other, which can suppress the cross-particle diffusion and aggregation.
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Fig. 3 SEM images of Co@SiO2 samples annealed in an H2 atmosphere for 120 min at different temperatures: (a) 500 °C; (b) 600 °C; (c) 800 °C. |
Stöber process was repeated for 1, 3 and 5 times to explore the method to fabricate a SiO2 shell with different thicknesses. Fig. 4 shows the SEM and TEM images of the Co@SiO2 samples with different shell thicknesses. The magnified SEM images indicate that the roughness of the spherical surface increases with increasing coating times from one to five. To compare with the as-prepared particles, no apparent change in microsphere except for the increase of surface roughness, as shown in Fig. 4(a) and (b). Some composite microspheres were partially broken when coated the three times, as shown in Fig. 4(d) and (e). The phenomenon becomes much more common when coating times further increase to five as some fragment shape up between particles, as seen in Fig. 4(g) and (h). The energy dispersive X-ray spectroscopy (EDS) as well as elemental maps of a single broken Co@SiO2 composite microsphere coated for three times confirmed (Fig. S1, ESI†) that the peeling layer was SiO2. The core–shell structure of the composite particles was further examined by TEM. The TEM images in Fig. 4(c), (f) and (i) show that the morphology of products is consistent with SEM observation. The TEM images show that the composite microspheres possess a unique core–shell structure, with a dark sphere encapsulated in a gray shell. The thicknesses of SiO2 shell are observed to increase from around 22 nm to 64 nm, then to 98 nm, as the coating times increase from 1 to 3 and 5. The shell thickness increases for around 22 nm for each time of coating. Based on the observations, we can conclude that the core–shell composite is composed of a Co core and an outer SiO2 shell. Moreover, it is clear that changing coating times is an effective way to tailor the thickness of SiO2 shell.
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Fig. 4 SEM and TEM images of Co@SiO2 particles with different coating times: (a–c) one; (d–f) three; (g–i) five. |
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Fig. 5 Magnetic properties of (a) as-prepared Co and Co@SiO2 particles, (b) Co@SiO2 samples annealed at different temperatures for 120 min in H2 atmosphere. |
Comparison between samples of different hydrogen-thermal treatment temperatures suggests that Ms of annealed products increased obviously. Ms increased to 160 emu g−1 after the hydrogen heat treatment at a high temperature, as shown in Fig. 5(b) and Table 1. The enhancement of Ms for annealed Co@SiO2 composite microspheres is primarily ascribed to the improved crystallinity as well as reduced defects during the hydrogen-thermal treatment process.
Samples | Hc (Oe) | Ms (emu g−1) |
---|---|---|
Co | 124.0 | 157.9 |
Co–SiO2 (one time) | 112.2 | 153.2 |
Co–SiO2(three times) | 98.3 | 149.3 |
Co–SiO2 (five times) | 89.3 | 132.5 |
500 °C | 83.6 | 160.6 |
600 °C | 56.3 | 160.9 |
800 °C | 73.3 | 159.4 |
It is well known that coercivity (Hc) is a vital parameter for assessing magnetic properties, and a high-frequency resonance of the absorbent may be achieved with a high Hc.15,31 In the current research, pristine Co spheres exhibit higher coercivity (124.0 Oe) compared with bulk cobalt (10 Oe).32 After coating the Co spheres with an SiO2 layer, a decreased Hc was observed. Hc gradually decrease from 112.2 Oe to 98.3 Oe then to 89.3 Oe with the increase of SiO2 layer thickness, as shown in Table 1. It considerably decreases to around 83.6 Oe and 56.3 Oe, after hydrogen-thermal treatment at 500 °C and 600 °C. However, the decrease did not continue further, an increase of Hc was observed when annealed at 800 °C.
The coercivity of magnetic material is related to the magnetocrystalline anisotropy as well as defects in the materials.33,34 The high Hc of as-prepared Co spheres may be related to the high density of defects that developed during the preparation. The decreased Hc during annealing is mainly attributed to elimination of defects. The slight increase of coercivity observed after annealed at 800 °C may be related to the conversion from amorphous to crystalline Co as amorphous Co usually possess lower coercivity. The Co@SiO2 composite microspheres with high saturation magnetization and coercivity should possess better microwave absorbing ability.
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Fig. 6 Electromagnetic properties of the Co@SiO2/paraffin composite materials with different coating times: (a) complex permittivity; (b) complex permeability. |
Fig. 6(b) shows the μ′ and μ′′ of all Co@SiO2 composite microspheres in the frequency range of 2–18 GHz. It can be seen that the μ′ and μ′′ slightly decrease with the increasing thickness of SiO2. The natural resonance of all samples occurs at below 2 GHz, and the presence of SiO2 shell would not influence the natural resonance behavior. In addition, no obvious eddy current effect is observed in all the samples. The permeability of ferromagnetic particles mainly depends on the Ms and the eddy current effect. The eddy current effect was quite weak since the bare Co particles prepared through solution chemistry process possess high resistivity. In addition, the bare as well as the clad particles are very fine and well dispersed, which is not favorable to induce local eddy current by particles aggregation. Thus, the decrease of the permeability is attributed to the variations of Ms, which is ascribed to the introduction of non-ferromagnetic SiO2 shells.
In conclusion, the introduction as well as the thickness of SiO2 shell has no significant influence on the electromagnetic properties of Co particles, which is beneficial for the preparation and design of the stealth coatings.
Fig. 7 depicts the complex permittivity and permeability of the Co@SiO2 microspheres with different filling ratios. As seen in Fig. 7(a), the ε′ enhances obviously with the increase of filling ratio. For example, the ε′ of Co@SiO2 microspheres increases from 4.1 to 7.2 and 10.9 at 8 GHz, when the filling ratio increases from 15 vol% to 25 vol% and 45 vol%, respectively. The dielectric relaxation is relatively weak, and the relaxation frequency remains at about 14 GHz. In the present study, the enhancement in permittivity is attributed to the enhanced surface charge polarization. The relaxation intensity is related to the total interface areas of conductor/isolator. The increased filling ratio yields more interface and thus contributes to enhanced dielectric relaxation. On the other hand, the filling ratio has little effect on the relaxation frequency as the relaxation frequency almost remains unchanged when filling ratio increases.
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Fig. 7 Electromagnetic properties of the Co@SiO2/paraffin composite materials with different volume of Co@SiO2 particles: (a) complex permittivity; (b) complex permeability. |
The complex permeability of Co@SiO2 samples, for both μ′ and μ′′, obviously increases with the increasing filling ratio as presented in Fig. 7(b), indicating that permeability of the composite materials is highly dependent on the content of Co@SiO2 microspheres. Moreover, the frequency of natural ferromagnetic resonance is found to shift to a higher frequency when the filling ratio increases, suggesting that the filling ratio has significant influence on the frequency and intensity of natural resonance. In addition, when the filling ratio is up to 45 vol%, no strong eddy current effect, induced by local agglomeration, is observed as the presence of SiO2 shell protects the Co particles from agglomeration.
In order to investigate the effect of annealed temperature on the EM wave absorption of Co@SiO2 composite, the EM parameters were also measured in the frequency range from 2 to 18 GHz. Fig. 8 shows the complex permittivity and permeability of annealed Co@SiO2 composite. When the annealing temperature was below 600 °C, ε′ gradually increases with the increase of annealing temperature; however, the ε′′ almost remained unchanged. When the annealing temperature increased to 800 °C, the Co@SiO2 composite spheres present great change in ε′ and ε′′. A peak on the curve of ε′′ in 6.2 GHz is observed, illustrating an intense dielectric relaxation, as shown in Fig. 8(a). In this study, the conductivity of Co@SiO2 composite particles increased after annealing in H2, leading to the increase of permittivity. Nevertheless, the significant increase in conductivity and the emergence of dielectric relaxation resulted in the highest permittivity when the particles annealed at 800 °C.
The effects of annealing temperature on the complex permeability are shown in Fig. 8(b). After annealed at different temperatures, the permeability of Co@SiO2 composite particles does not change obviously. The permeability of the Co@SiO2 composite particles is related to the Ms. Since the variation in Ms is very slight, the permeability remains unchanged.
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Fig. 9 TG patterns of as-prepared Co and Co@SiO2 composite microspheres with different coating times. |
Footnote |
† Electronic supplementary information (ESI) available. See DOI: 10.1039/c6ra24519f |
This journal is © The Royal Society of Chemistry 2016 |