3.1 Microstructural Characterization
The fabricated composite specimen corresponding to maximum mechanical strength ( Al-10% SiC-4% Kaoline) was subjected to W-SEM analysis integrated with an EDS analyser. Results reveal that the conventionally sintered HMMC shows the existence of pores as shown in Fig. 5 (a). In addition to this, the formation of agglomerations along the grain boundaries was observed in the conventionally sintered composite specimen as shown in Fig. 6. These agglomerations or clusters were formed due to the existence of a large density difference between the matrix and reinforcement particles which leads to a decrease in the mechanical strength of the material. The mechanical strength of the material depends on the interfacial bonding strength between the matrix and reinforcement particles. The agglomerations and pores which were found in the conventional sintering process occupied the interface region of matrix and reinforcement and acts as barriers for the interface bonding between the matrix and reinforcement particles. These agglomerations also act as pre-existing micro-cracks that reduce the load transfer mechanism leads to early failure of composite material.
In the case of Microwave and Spark Plasma Sintered composites, SEM analysis revealed that the absence of porosities and the strong interfacial bond between the matrix and reinforcement particles (see Fig. 5 (b,c)). In addition to this, no agglomerations of particles were observed in the Microwave and Spark Plasma Sintered composites due to the faster heating rate and shorter sintering time which decelerates the chemical interactions between the matrix and reinforcement particles. EDS mapping of microwave and Spark Plasma Sintered composite shows the presence and uniform distribution of silicon (Si), Carbon (C), Oxygen (O), Magnesium (Mg), Iron (Fe), Copper (Cu) and Zinc (Zn) elements ( see Fig. 7, 8 ). The existence of these elements confirms the SiC and Kaoline (Al2O3, SiO2, Fe2O3, CaO/MgO) in the fabricated HMMC specimen.
3.2 XRD analysis
Fig 3. represents the XRD peaks for as received SiC and Kaoline reinforcements, which confirms the existence of SiC peaks in SiC reinforcement and the presence of Al
2O
3, SiO
2, CaO/MgO, TiO
2 peaks in kaoline reinforcement powder. XRD analysis of composite specimens reveals that the presence of Al
2Cu peak in the conventionally sintered composite specimen (see Fig 4). The obtained peak corresponding to Al
2Cu fairly matches with the peak identified by Gatea et al., [26]. This Al
2Cu peak in conventional sintering was formed due to the higher sintering temperature and the initiation of chemical interactions between the added reinforcements and matrix particle [27, 28]. However, these intermetallic peaks were not observed in spark plasma sintered and microwave sintered composite specimens. In the case of the conventional sintering process due to the higher exposure time at higher temperatures causes accelerated diffusion, which initiates the chemical reactions between the Al matrix and harder reinforcements. This, in turn, leads to the formation of secondary phase compounds that deteriorate the strength of the composite specimen [29].
3.3 Mechanical Characterization
Al-10% SiC-X% Kaoline (X = 0, 2, 4, 6, 8) HMMC fabricated through Conventional sintering technique. The fabricated composite specimens were subjected to mechanical testing and the results reveal that the maximum U.T.S of 263 MPa, Compession strength of 282 MPa and Hardness value of 147 VHN was obtained at Al-10% SiC-4% Kaoline HMMC specimen and the corresponding values are shown in Table 3. To investigate the effect of the sintering mechanisms on the mechanical properties, Al-10% SiC-4% Kaoline was sintered through three sintering techniques, such as Conventional Sintering, Microwave Sintering and Spark Plasma Sintering technique. Results concluded that the U.T.S and Compression strength of the composite samples which were sintered through the conventional sintering process is 6.84 % and 7.4 % lesser when compared to the HMMC fabricated through Microwave sintering and 13.3 % and 11.7 % lesser when compared to SPS techniques. This was due to the higher sintering time of green compacts in conventional sintering for achieving a good interfacial bond between matrix and reinforcements. But at higher sintering temperatures, the activation energies of matrix and reinforcement particles increases, which lead to interfacial reactions and resulting in the formation of Al2Cu brittle intermetallic compounds as shown in Fig. 4. This Al2Cu compound occupies the interfacial gap between the matrix and reinforcements and weakens the bonding strength between the adjacent particles. The existence of difference in deformation capabilities of intermetallic compound and reinforcement powders leads to generate triaxial stresses during the application of load. These internal stresses initiate the crack generation, propagation and failure of the composite specimen when the magnitude of these stresses exceeds the yield strength of the composite specimen [30].
In Microwave sintering, the heat is generated from the core part of the ceramic powder particles due to the absorption of microwaves during sintering [22] (see Fig. 9). The developed heat inside the ceramic particles was propagated to the adjacent Aluminium matrix particles. This phenomenon enhances the interfacial bonding between the composite particles and decreases the temperature gradients between the core part and surface of the composite powders [14, 31]. The lower sintering time and temperature in microwave sintering improve the grain growth and eliminate the chances of formation of intermetallic phases.
The high U.T.S and Compression strength of Spark Plasma Sintered composite were due to the generated plasma between the powder particles which enhances the bonding strength between the adjacent powder particles by breaking the impurities present on the surface of the matrix and reinforcement particles. In addition to this, this generated spark plasma generates joul heating with interface particles and electric discharge between the surrounding particles (see Fig. 10. b) [13]. Further, in the SPS process, the formation of brittle clusters was completely avoided due to the accelerated grain growth due to lesser sintering time that reduces the chemical interactions between the softer aluminium matrix and harder ceramic reinforcements [29]. The effect of sintering techniques on the variation of Hardness, U.T.S and Compression Strength of HMMC is depicted in Fig. 11 and Fig. 12 respectively. Results concluded that the U.T.S, compression strength and hardness of composites sintered by microwave sintering and SPS process can be enhanced by 6.84 %, 7.44 %, 6.12 % and 13.3 %, 11.7 % and 16.3 % respectively.
Table 3. Mechanical properties of fabricated Al- SiC-Kaoline HMMC
|
U.T.S (MPa)
|
Compression Strength (MPa)
|
Hardness (VHN)
|
Al
|
150
|
171
|
98
|
Al- 10% SiC
|
184
|
203
|
111
|
Al- 10% SiC-2% Kaoline
|
202
|
248
|
122
|
Al- 10% SiC-4% Kaoline
|
263
|
282
|
147
|
Al- 10% SiC-6% Kaoline
|
229
|
252
|
137
|
Al- 10% SiC-8% Kaoline
|
193
|
221
|
136
|
3.4 Effect of Sintering mechanisms on Porosity of the HMMC
The percentage of voids present in the given specimen is referred as porosity. Porosity present in the material degrades the mechanical properties of the material. Pores generate the weak interfaces between the matrix and reinforcement particles that act as obstacles for the propagation of heat during the sintering. The existence of thermal mismatch between the matrix and reinforcements causes the differences in the deformation capabilities of softer aluminium matrix and harder reinforcements that create the pores at the interface regions. In the case of spark plasma sintering due to the simultaneous application of pressure and heat over a short time period and the presence of vacuum during the SPS process, the likelihood of pore formation was minimized and causes an efficient diffusion process between the particles. During the compaction process, it was observed that the compressibility of hybrid composite powders decreases with an increase in harder ceramic reinforcement particles. At the low compaction pressure rates (i.e., Quasi-static condition) the powder particles are having sufficient time to rearrangement and fill the interfacial gaps and produce the densified green compacted composite specimen. But at dynamic compaction pressure conditions, the powder particles don't have time to rearrangement such that interlocking occurs about their mean positions and undergone plastic deformation during compaction. This causes very few chances to fill the interfacial gaps that cause high porosity in the composite specimens that degrade the mechanical strength of the fabricated samples [30]. In this experiment higher porosity levels of 4.5443% was obtained for conventionally sintered composite. The SPS and microwave sintered composite specimens showed porosity levels of 1.9523 % and 3.1013 % respectively as shown in Fig. 13. In the case of the Spark Plasma Sintering technique, porosity negatively affects the sintering process. Porosities present in the composite acts as electrical resistance and causes acute diversion of electric currents at the junctions of Al- SiC- Al particles (see Fig. 10.b), which prone to decreasing joul heating regions and reduces the densification of material [13]. To eradicate this defect, the reinforcement particles must be dispersed uniformly throughout the matrix which can be achieved by an appropriate selection of process parameters during the ball milling process.
3.5 Impact Energy
The energy absorbed by the material before fracture is termed impact energy. Figure 14 Indicates that there was an enhancement of 59.3% and 75.58% impact energy for microwave and Spark Plasma Sintered HMMC when compared to Conventional sintered HMMC. The lower impact energy of conventional sintered composite was due to the presence of brittle Al2Cu intermetallic compound which was formed as a result of chemical interactions between matrix and reinforcement particles [26]. The brittle intermetallics reduces the energy absorption capability of the material [32, 33]. In addition to this, the presence of higher porosity levels and microcracks in conventional sintered composites is the key factor for the lesser impact energy of HMMC [34]. In the case of Microwave and Spark Plasma Sintered HMMC’s, the presence of shorter sintering time and temperature makes the specimens free from agglomerations and causes a strong interfacial bond which makes the large plastic deformation at high-stress concentration areas before the fracture [35]. The high impact energy of Microwave and Spark Plasma Sintered HMMC leads to ductile fracture under the application of load.
3.6 Fractography
Fracture in the tensile specimen is classified into the brittle fracture and ductile fracture. The distribution of reinforcement particles in the matrix material, interfacial bonding between the particles and the agglomerations which are formed due to the chemical interactions between the adjacent particles are the essential factors that affect the type of fracture in tensile specimens. The non-uniform dispersion of reinforcements leads to variation in a strain carrying potentiality between the softer aluminium matrix and harder ceramic reinforcements (SiC, Kaoline). The presence of clusters weakens the interfacial bond which promotes the early stage failure of the composite under the application of load.
Fractured tensile specimens are subjected to SEM analysis to know the fractured patterns like Dimple and cleavage facts. The formation of Dimples was generally formed on the fracture surface of the ductile specimen with large plastic deformation and localized stresses [36, 37]. Transgranular cleavages occur on the brittle fracture which enhances the propagation of crack through the intergranular grain boundaries [32, 33, 38, 39]. Figure 15(a-c) represents the SEM micrographs for the tensile fractured surfaces. The presence of harder reinforcements and the formation of Al2Cu intermetallic compound due to the large sintering time of conventional sintering promotes cleavage facts on the fractured surface as shown in Fig. 14(a). In the case of microwave and Spark Plasma Sintering, as the composite specimens are sintered in less time brittle agglomerations was not found in XRD patterns of SPS and Microwave Sintering. Figure 14 (b,c) reveals the presence of dimples due to the absence of Al2Cu intermetallic compound which causes ductile failure and enhances the elastic nature of composite specimens [40].