SiC Conversion Coating Prepared from Silica-Graphite Reaction

The β-SiC conversion coatings were successfully synthesized by the SiO(v)-graphite(s) reaction between silica powder and graphite specimen. This paper is to describe the effects on the characteristics of the SiC conversion coatings, fabricated according to two different reaction conditions. FE-SEM, FE-TEMmicrostructuralmorphologies, XRDpatterns, pore size distribution, and oxidation behavior of the SiC-coated graphite were investigated. In the XRD pattern and SAD pattern, the coating layers showed cubic SiC peak as well as hexagonal SiC peak. The SiC coatings showed somewhat different characteristics with the reaction conditions according to the position arrangement of the graphite samples. The SiC coating on graphite, prepared in reaction zone (2), shows higher intensity of beta-SiC main peak (111) in XRD pattern as well as rather lower porosity and smaller main pore size peak under 1 μm.


Introduction
Graphite is attractive material for high temperature applications due to its high strength, high modulus, excellent thermal shock resistance, light weight, and ease in machining.It has been used as the engineering materials, like heaters, electrical contacts, high temperature heat exchangers, rocket nozzles and leading edges of aircraft wings, and so forth [1,2].A serious disadvantage to the use of graphite is that it begins to oxidize to a gaseous phase at temperatures of 500 ∘ C with a consequent loss of material.Thus the use of graphite material has been greatly restricted due to the poor oxidation resistance at high temperature in an oxidizing atmosphere.Good oxidation resistance is necessary in their high temperature applications [3].
A silicon carbide (SiC) coating is effective in developing the oxidation resistance and the wear resistance of graphite materials and C/C composites, because silicon carbide has good oxidation wear resistance and high hardness.Thus it has been used as several mechanical components and ceramic engine parts, aerospace and aircraft applications, Si-wafer pot, gas turbine component, and nozzle materials [4].
To prevent a severe oxidation behavior of graphite, it is necessary to form a protective SiC coating of the surface of the graphite.There have been several efforts to develop such SiC coating processes for the graphite.The previous studies were mainly concerned with the formation of SiC coatings on graphite substrates using RF sputtering with a sintered SiC target [5].Chemical vapor deposition (CVD) method has been widely utilized in fabricating coating.However, the SiC coating layers for complex shape components can be easily formed by chemical vapor reaction method [6,7].The SiC conversion layer obtained by such solid-vapor reaction has good adherence with graphite matrix.The conversion coating process is based on carbothermal reduction, in which silica reduction is carried out with carbon source.This process is independent of the molar ratio of silica to carbon; in the end, silica reduction with SiC source is excluded in overall process (SiO 2 + 3C → SiC + 2CO) [6].Of particular importance to SiC phase nucleation is SiO generation from silica-carbon reaction [8].With the formation of SiO, CO vapor (SiO 2 + C → SiO + CO), the SiC polycrystalline phase on the surface of graphite is coated through such reduction behavior between SiO and carbon source (SiO + 2C → SiC + CO) [9][10][11][12][13].Generally, the SiC crystal phase, produced from the SiO vapor and graphite at high temperature over 1500 ∘ C, shows mainly cubic structure of 3C type with hexagonal SiC phase [13].During heat treatment or annealing at high temperature, the cubic SiC phase might be transformed into hexagonal SiC phase through solid-state transformation such as closepacked layer (111) shift or spreading of stacking faults [14,15].
In this study, the SiC conversion coatings were formed on the graphite substrates by conversion reaction method through the carbothermal reduction process of the silica powder and graphite.The crystal phase analysis and microstructure observation for the conversion layer on graphite were performed.Oxidation behavior and pore size distribution of the SiC conversion coating layers, formed over graphite, were investigated.

Experimental
In this work, silica (SiO 2 ) powder (average particle size: 3 m, NOA Technology, USA) and finely ground graphite were used to form the SiC conversion layers.Silica powder and graphite substrate (IG-11, density: 1.77 g/cm 3 , Toyo Tanso Co., Japan) were placed in a graphite crucible and then heated to 1750 ∘ C. The outside of the graphite crucible was controlled with constant Ar gas flow.The reaction conditions and the SiO and CO partial pressures during the conversion process were controlled with the graphite architecture designed (Figure 1).The inside of the graphite crucible was coated with spraycoated BN and covered with graphite foil to prevent reaction with the silica melt.The conversion coatings were fabricated in two different reaction zones (Figure 1).The specimens in reaction zone (1) were placed on the gas-permeable carbon foil brides fixed to graphite crucible wall and reaction zone (2) was confined with silica melt.
SiC conversion layers on the graphite were analyzed using an X-ray diffractometer (X'Pert Pro, Phillips).Surface morphologies of the SiC conversion layer were observed by FE-SEM (Hitachi S-4800, Japan).The oxidation behavior of the SiC coating layer formed on the graphite was investigated by DSC/TGA (differential scanning calorimetry/thermogravimetric analysis) and differential scanning calorimeter (DSC SDT Q600, TA instruments).The SiC-coated graphite in the DSC/TGA instrument was heated to 700 ∘ C under flowing Ar gas; the specimens were exposed at this temperature over 2 hrs, blowing air at a rate of 100 mL/min.The pore size distribution of the SiC coating was analyzed by mercury intrusion porosimetry (AutoPore IV 9500 Micromeritics Instrument).Microstructure and diffraction patterns of the fragment samples separated from coating layer were analyzed by 200 kV FE-TEM (Field Emission Transmission Electron Microscope, Tecnai G2 F20).

Results and Discussion
The chemical conversion reaction process in formation of SiC coating on graphite substrate has been accomplished within two reaction zones having different SiO partial pressure in the graphite architecture.The SiC conversion coatings were formed on the surface of graphite substrates under two reaction zones.The surface morphologies of SiC conversion coatings formed on graphite are visible in FE-SEM images (Figure 2).Relatively dense morphology of SiC conversion coating was observed in surface images.It seemed that the graphite (coke) grains and the pitch were changed into the closely bonded-SiC grains in coating layer during the conversion process.FEM surface image of the conversion layer obtained at reaction zone (1) showed rather a porous morphology, but that of reaction zone (2) showed relatively dense microstructure.
Cross-sectional microstructure of the polished specimen, prepared by SiC coating process, is shown in Figure 3.The conversion coating layer on graphite, fabricated in reaction zone (2), showed a chemical composition (Si : C) of approximately 1 : 1.The boundary between SiC coating layer and graphite showed somewhat mixed pattern showing composition gradient of SiC phase and matrix graphite.Reaction zone (1), arranged on the carbon foil bridges, would have the reaction condition of a low SiO vapor pressure.But the SiO vapor partial pressure of reaction zone (2) would be gradually increased by the reduction reaction of silica and carbon with reaction time [11][12][13].The SiO vapor in case of reaction zone (1) was supplied from the silica-carbon reaction of reaction zone (2) and its partial pressure was estimated to be in the range of 0.8∼0.9bar.The SiO vapor partial pressure is calculated from the some data regarding carbothermal reduction process [6,16,17], while reaction zone (2) wrapped with   silica melt in graphite crucible would have rather high vapor pressure as compared to that of reaction zone (1).Therefore, it seemed that the specimen in reaction zone (2) is exposed to higher SiO vapor pressure than that of reaction zone (1).The SiO vapor pressure in the silica melt bubble (reaction zone ( 2)) would be increased to the range of approximately 1∼3 bar with increasing reaction time.After reaction process, the size of the silica bubble was enlarged by 2∼3 times of graphite specimen.Thus, in reaction zone (2), the reaction of SiO vapor and graphite would induce rapid formation of SiC coating on bare graphite.The SiO vapor is infiltrated into graphite specimen and then the reaction of SiO vapor and graphite grains creates SiC grains.
The XRD patterns of SiC conversion coating layers formed on graphite are shown in Figure 4.The XRD pattern of surface region of the specimens showed mainly cubic 3C-SiC, referred to as -SiC, crystalline phase of strong peaks corresponding to the (111), (220), and (311) planes.Particularly, the specimen (Figure 4(c)), fabricated at reaction zone (2), showed very high SiC peak intensity with small graphite peak.Although (111) peak intensity of the SiC coating on graphite prepared at reaction zone (1) was detected, very high (0001) peak of the graphite is shown (Figure 4(b)).The intensity difference of graphite peaks of Figures 4(b) and 4(c) represents different conversion reaction rate according to the SiO partial pressure in their reaction zones.The graphite in reaction zone (2), confined with silica melt at high temperature, has relatively high SiO vapor pressure; thus its conversion rate for coating formation would be rather fast when compared to the that of reaction zone (1).In addition, the coating specimen showed weak hexagonal SiC peaks of (101) (Figures 4(b) and 4(c)) as well as (103) plane (Figure 4(c)).The cubic -SiC structure has been considered to be the low-temperature polymorph of SiC.In this study, the presence of the hexagonal SiC might be explained as a result of polymorphic transformation of cubic SiC, created from the reaction between SiO vapor and graphite at high temperature.It seemed that the structure transformation from -SiC (cubic structure) to -SiC (hexagonal structure) is followed by simply a subsequent cool-down at high temperature over 1500 ∘ C under Ar atmosphere [14,15].The SiC conversion coating layers formed on graphite were analyzed by FE-TEM (Figure 5).The fine Pore size distribution of the SiC-coated graphite and bare graphite was tested (Figure 6).After formation of SiC coating on graphite, the specimen, obtained at reaction zone (1), showed major peak of 1∼2 m in diameter.The coated graphite showed the decrease of porosity compared to bare graphite.The difference in pore size distribution pattern of the coated graphite would be due to higher SiO vapor pressure.
Oxidation behavior of the SiC-coated graphite was measured by DSC/TGA instrument (Figure 7).The bare graphite (Figure 7(a)) was severely oxidized showing strong exothermic curve in the exposure condition (at 700 ∘ C) to air blowing in less than 2 hrs.While the coated graphite, obtained at reaction zone (1), showed a significant weight loss to 24.3 wt%, the specimen, coated at reaction zone (2), showed relatively low weight loss.The SiC-coated graphite (Figures 7(b) and 7(c)) showed small weight loss to air at elevated temperature in the oxidation test.The decrease in the porosity of the coated graphite would imply the densification by the formation of the conversion layer in surface region.Finally, the SiC conversion coatings could be easily formed on graphite substrate using graphite furnace through chemical vapor reaction process.

Conclusions
The crystalline SiC conversion coatings were formed over the graphite.The surface coating layers showed the XRD peaks of (111), (220), and (311) planes of cubic SiC phase and

FragmentFigure 5 :
Figure 5: FE-TEM images and diffraction patterns of SiC conversion coating.