A Novel Approach for Fabrication of Reaction Bonded Silicon Carbide (Rbsc) Composites N. Frage, S. Aroati, M.Cafri, H.Dilman and M.P.Dariel Department of Materials Engineering, Ben-Gurion University, P.O.Box 653, Beer-Sheva 84105, Israel ABSTRACT RBSC composites are fully dense materials fabricated by pressure-less infiltration of molten silicon into compacted mixtures of silcon carbide and carbon. Free carbon is formed as a result of the pyrolysis of an organic resin, (the carbon source) and reacts with molten silicon to form secondary SiC grains that precipitate on the original SiC particles. Non-reacted residual silicon fills the free areas between the SiC grains. The presence of the residual silicon decreases the mechanical properties of the composites; moreover, the pyrolysis process is environmentally unfriendly. In the present study, boron carbide powder was used as an alternative carbon source, leading to reduced fraction of the residual silicon. In addition, the volume available for the infiltrated silicon was reduced by using mixtures of multimodal silicon and boron carbides powders and thereby obtaining a relative density of about 80% in the compacted body. The final composites fabricated by infiltration with molten silicon, that has optimal composition display a relatively low fraction of residual silicon and improved mechanical properties (hardness 1960±300HV, elastic modulus 365±2GPa, flexural strength 271±15 MPa). It is also noteworthy that the suggested approach is environmentally friendly. INTRODUCTION RBSC is an attractive material for light armor applications. A conventional approach of RBSC fabrication involves infiltrating a compacted SiC/carbon mixture with molten Si. The reaction between molten silicon and free carbon leads to the formation of silicon carbide grains, which precipitated on the initial SiC particles, interconnect them, and provide continuous ceramic skeleton. The typical microstructure of RBSC composites consists of the about 85% inter-connected silicon carbide phase and residual silicon1. The main advantage of the RBSC fabrication process is it’s relatively low temperature (~1500°C) in comparison with pressure-less or hot pressing densification. On the other hand, RBSC composites have two main problems. The first one is the presence of the residual silicon that leads to lowering mechanical properties of the final composites and the second one is related to using carbon containing organics (resins) as a source of free carbon, which is formed as a result of a pyrolisis process. This process takes place at elevated temperatures and accompanied with releasing toxic gases and is strongly environmentally unfriendly. In order to reduce the amount of the residual silicon in reaction bonded composites it was suggested to use powder mixture with appropriate particles size distribution2. This approach allows to fabricate compacts with green density of about 20vol. % and to reduce significantly the amount of the residual silicon (<10vol. %). In our previous work was also established that boron carbide directly reacts with liquid silicon and serves as carbon source in the reaction 1-163 bonded boron carbide composites3. In the present work we have combined these two features in order to fabricate RBSC composites with decreased amount of the residual silicon and using boron carbide as an alternative source of free carbon instead carbon containing organics. EXPERIMENTAL PROCEDURE Fabrication of the Composites A commercial coarse (~120m) silicon carbide powder was grinded and sieved in order to obtain requested particle size distribution in the powders mixtures. Some of the fractions in the SiC powders mixtures were replaced by boron carbide powders with different particle size. Boron carbide powder (~1m, grade HS) was supplied by H.C. Starck, and B4C powders with average particle size of 13µm was supplied by "Modan Jang" a Chinese Company. 5 mixtures of silicon and boron carbides powders were prepared and each mixture corresponds to the desired particle size distribution (Table 1). Table 1. The powder compositions and particle size distribution that were used at this work Vol. % of different powders RB-1 RB-2 RB-3 RB-4 RB-5 53 53 53 53 53 106 10 10 10 10 10 50 SiC 18 18 12 7 2 13 19 4 0 0 0 3 0 0 0 0 0 106 0 0 0 0 0 50 B4 C 0 0 6 11 16 13 0 15 19 19 19 3 24 24 23 23 21 Porosity of green compact , %Vol. Particle size, D50 ,µm The mixtures were dry mixed in a planetary mixer for 8 hours. 20mm diameter and 5mm high performs were uniaxially compacted under 180MPa. The compacts were infiltrated with liquid silicon (98.4%, Alfa Aesar) at 14800C for 15 min under vacuum 10-4 torr. Characterization Microstructure and composition The microstructure of the samples was studied using optical microscope (OM, Zeiss Axiovert 25) and scanning electron microscopy (SEM, JEOL-35) accompanied with an energy dispersive spectrometer (EDS). The samples for the microstructure characterization were prepared using standard metallographic procedure that includes a last stage of polishing by 2.5μm diamond paste. Image analysis using the Thixomet software was applied in order to determine the amount of the residual silicon in the 1-164 composites. The phase composition was determined qualitative by x-ray diffraction (XRD). Mechanical properties Micro-hardness values were determined by Vickers hardness (Buehler-Micromet 2100) with 2000gr load. Flexural strength was measured with LRX plus LLOYD machine (Lloyd Instruments, Fareham Hants, U.K.) using 1.5x2x20mm3 samples. The elastic modulus of the composite was derived from ultrasonic sound velocity measurements according to the "Pulse Echo" method. Density of the infiltrated composites was measured using Archimedes principle. RESULTS AND DISCUSSIONS Microstructure The microstructure of the composite (Fig.1) fabricated with addition of 35%vol. boron carbide powders consists of B12(C, Si)3, SiC and the residual silicon. The presence of the B12(B,C,Si)3 grains with a gray color slightly lighter than a color of SiC particles are clearly observed. It is very important to point out that B12(B,C,Si)3 grains connect ceramic particles and provide continuous ceramic skeleton, similar to that for the composites fabricated with free carbon additions and its formation is in a good agreement with the reported previously our results for reaction bonded boron carbide composites3. Fig.1. Optical microscope images of the composites microstructure with 35% Vol. B4C particles (the whole B4C original particles converted to rim) 1-165 1000 a - SiC - 35Vol.% B4C powders mixture before infiltration b - SiC - 35Vol.% B4C infiltrtaed composite Counts. b SiC B12(C,Si,B)3 500 a B4C 0 35.0 35.5 36.0 36.5 37.0 37.5 38.0 2 Fig.2. XRD pattern of the composites. According to XRD analysis (Error! Reference source not found.) the initial boron carbide particles (curve a) were completely converted to the ternary B12(B,C,Si)3 phase (curve b). It was established in our previous work that in the reaction bonded boron carbide composites fabricated without free carbon additions the secondary SiC phase displays plate-like morphology4. In contrast, for the reaction bonded SiC, fabricated with boron carbide as the carbon source, the presence of secondary SiC phase with plate-like morphology was not observed. This difference may be attributed to the fact that surface of the initial SiC particles, serves as a preferred site for heterogeneous SiC nucleation. The presence of a thick secondary SiC layer indicates that boron carbide particles serve as an effective source of carbon. Fig.3. SEM images (SE) of the composites microstructure with 35%Vol. B4C particles addition Mechanical Properties 1-166 The mechanical and the physical properties of the composites that were fabricated with different fraction of B4C were summarized in Table 2. Table 2. Properties of the infiltrated composites RBSC* RB-1 RB-2 RB-3 Density , 2.85-3.10 2.92 2.89 2.89 gr/cm3 Young’s 320-340 344 343 345 Modulus, GPa ±3 Flexural 190-250 204 255 256 strength , MPa ±18 Hardness, Hv 1500-2200 1534±202 1673±262 1835±262 Residual Si, 15-35 23.4 19.4 15.6 vol. % *Range of the composites properties reported in literature1,5,6 . RB-4 RB-5 2.83 2.83 351 353 237 270 1928±307 1963±331 12.0 10.6 According to the results presented in Table 2 the density of the composites decreasing with the added amount of boron carbide. The enhanced amount of SiC and the reduced amount of the residual silicon stand behind the increased hardness values. As was expected the values of Young modulus do not depend on the particle size of added boron carbide and increases with boron carbide volume fraction. In order to estimate the reliability of the composites, Weibull modulus (m) for flexural strength was calculated according to equation: 1 * ln ln( ) m ln max m ln 0 1 P i 0.5 Where, P , “i” is the specimen number from N samples, max is the flexural N * strength of specimen i and 0 is mean value of the flexural strength. 1-167 b 1.5 1.0 ln(ln(1/1-P)) 0.5 0.0 SiC-Hy-5-FP Linear fitting y = 16.10x - 90.65 2 R = 0.95 Weibull modulus : 16.10 -0.5 -1.0 -1.5 -2.0 -2.5 -3.0 5.40 5.45 5.50 5.55 5.60 5.65 5.70 ln() Fig.4. Weibull plots for flexural strength of composites fabricated with 35% vol. B4C The outcome of the experimental results treatment for the composites with 35vol. % carbide particles is presented in Error! Reference source not found.. The higher value of Weibull modulus for the composites fabricated by using B4C powder reflects high level of the microstructure homogeneity. CONCLUSIONS RBSC composites were fabricated using various fractions of boron carbide as an alternative source of carbon. The composites with B4C addition display high reliability and slightly better mechanical properties than the composites fabricated by conventional approaches. The suggested approach is environmentally friendly and allows avoiding the formation of carbon containing organic materials. REFERENCES 1 M.K. Aghajanian, J. Mears and R. A. Wolffe, "A New family of reaction bonded ceramics for armor applications", Ceramic Armor Materials by Design, Edited by J.W. McCauley, A. 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