4.1. Alloy Composition
The carbon saturation level for the Sample A alloy at 1550 °C is 6.5% C. In the copper-containing Sample B alloy, the 1550 °C carbon saturation level is 4.6% C for the average EDX analysis at 10.6% Cu and 3.4% C for the bulk alloy chemistry analysis at 20.8% Cu. Thus, the alloy’s carbon solubility decreases with increasing %Cu [
27,
28]. In comparison, the bulk alloys in
Table 5 and
Table 6 display carbon levels of 3.5% C in alloy A and 1.2% C in alloy B. The importance of these numbers is that the crucible material is graphite, and despite the excessive amount of graphite carbon available for assimilation into the alloy, the carbon dissolution process is limited by fast reaction and limited alloy–graphite contact area. This effect has been demonstrated in recent work on the aluminothermic reduction of iron oxide in graphite crucibles, producing carbon steel with a carbon content of less than 0.68% [
7,
8].
The equilibrium phase chemistry of the bulk alloy compositions is displayed as cooling graphs in
Figure 6a,b.
The Sample A alloy data in
Figure 6a indicate a solidus temperature of 1093 °C and a liquidus temperature of 1171 °C. In comparison, the Sample B alloy indicates a solidus temperature of 994 °C and a liquidus temperature of 1095 °C. The closeness of the solidus and liquidus temperatures results in a narrow solidification temperature range and should lead to a rapid setting of the solid alloy composition. In addition, the low liquidus and solidus temperatures, relative to the high temperatures attained in aluminothermic reduction, which can reach 3000 °C, allowing for a longer time for the alloy beads to separate from the slag [
18]. Similarly, given the large alloy superheat, it is expected that a homogeneous alloy mass would form easily. However, the alloy Sample B bulk phase chemistry in
Figure 6b indicates that two liquid phases are stable above the liquidus temperature, with the Liquid#2 being phase-dominant.
At the liquidus temperature of 1095 °C, the liquid proportions are at 32% Liquid#2 and 68% Liquid phase. The proportion of the Liquid#2 phase then decreases rapidly as the first solid phase, HCP_A3, forms and, subsequently, large quantities of FCC_A1 and small amounts of M
5C
2 form. At 1041 °C, the Liquid#2 phase is at zero percent, and the Liquid phase remains. The liquid alloy chemistry of the two liquids above the solidus temperature is displayed in
Figure 7. It is observed that the Liquid#2 phase is a high-Mn low-Cu phase, and the Liquid phase is the opposite, a high-Cu low-Mn phase. Therefore, it is expected that the last liquid to solidify will consist of the Liquid phase and contain a high percentage of Cu and a low percentage of Mn, with the composition of 30.2% Mn, 62.9% Cu, 4.7% Al, 1.9% Si, and negligible carbon at 0.005%. The two liquids of differing compositions may explain the interdendritic high-Cu alloy observed in
Figure 4 and
Figure 5.
4.2. Slag Composition
The slag is designed to ensure adequate slag fluidity at increasing %Al
2O
3, thereby facilitating alloy–slag separation during the process and promoting the crystallisation of the water-soluble NaAlO
2 phase upon solidification. The high melting point of Al
2O
3 (2072 °C) requires extreme fluxing of the slag to maintain slag fluidity upon slag cooling.
Figure 8a,b shows the cooling curves of the target slag composition and the SEM–EDX average analysis of slag B (
Table 7). The target slag is the expected slag composition from a simple mass balance under assumption of 100% Fe and 80% Mn recovery to the alloy. As shown in
Figure 8b, the higher percentage of Al
2O
3 in slag B, 55%, leads to the formation of the spinel phase as the primary solidification phase. The slag liquidus temperature is higher at 1564 °C compared to the target slag liquidus temperature of 1373 °C. This aspect does not appear to be problematic at the high temperatures expected in aluminothermic reduction. The calculated slag viscosities of the fully liquid slags are compared in
Figure 9. It is seen that the slag viscosity values are acceptable in terms of tappable slag, typically at less than 3 Poise in viscosity [
34].
The difference between the average SEM–EDX slag analyses to the bulk slag analyses (
Table 7) indicates that some alloy entrapment occurred in both Samples A and B, as represented by the 2.4% FeO content in the bulk slag compositions. Due to the highly reducing conditions in aluminothermic smelting, it is expected that all of the Fe oxide in the feed mixture will ultimately be reduced to Fe metal in the alloy. Similarly, the 2.9% Cu
2O in the bulk slag analysis represent an entrapped alloy in the slag since Cu is more inert to oxidation than Fe. The mass balance calculation numbers are summarised
Table 8. The calculations are made as the difference between the input masses and the output masses of slag and alloy and indicate the alloy mass in the slag and the overall alloy recovery percentages. A comparison of the numbers for Sample A versus Sample B at 43% versus 57% alloy yield indicates an improvement in alloy yield with Cu added as the collector metal.
The element accounting percentages shown in
Table 9 indicate a good accounting of Fe and Cu, with some loss of Mn, Si, and Al to the gas. At an industrial scale, various methods of gas-cleaning and particulate-capturing equipment can be applied, for example, a reaction chamber hood with a positive off-gas pressure. Such methods counter volatilisation and capture fumes for recycling [
11]. The differences between the SEM–EDX slag analyses and the target slag analysis in
Table 7 are lower percentages of CaO and Na
2O and higher levels of Al
2O
3, obtained in the experimental results. The composition differences between the experimentally attained slags and the target slag can be overcome by adding Na
2O flux to the post-tapped slag to increase the proportion of the water-soluble NaAlO
2 phase. As discussed in [
9], the high-residual-heat content remains after the aluminothermic reaction, and this heat should be utilised to incorporate more Na
2O Flux into the tapped slag.
4.3. Gas–Slag–Metal Equilibrium Thermochemistry
The gas–slag–metal equilibrium for the feed mixture inputs was calculated at temperatures of 1650 °C–1900 °C. The calculated equilibrium end-point alloy and slag analyses for Samples A and B are compared to the experimentally determined values, as shown in
Figure 10a–d.
The alloy composition data in
Figure 10a,b show that the Sample A carbon content line at 3.5% C crosses the equilibrium curve at 1650–1700 °C, even though the equilibrium %C range is broad (0.5–3.9% C at 1650 °C–1900 °C). The Sample B carbon content line at 1.2% C crosses the equilibrium curve at 1700 °C–1750 °C and the carbon range is narrower (0.2–2.1% C) compared to the %C range in Sample A (0.5–3.9% C). Therefore, it appears that the Cu collector metal modulates the alloy’s carbon content. This is expected, as the solubility of carbon in copper is zero at temperatures up to 2000 °C [
27,
28]. The solubility of carbon in manganese is lowered with the addition of copper to manganese [
35].
The Sample A silicon content line at 1.4% Si crosses the equilibrium curve at 1650–1700 °C, in agreement with the carbon equilibrium temperature. The %Si for the Sample B alloy at 1.2% Si crosses the equilibrium curve at 1700 °C. Both %C and %Si equilibrium contents vary broadly across the temperature range of 1650 °C–1900 °C. In particular, the %Si range is wide, spanning from 1.1% Si to 6.4% Si in Sample A and from 1.5% Si to 4.6% Si in Sample B. The %Al in the alloy is under-predicted for both Sample A and B alloys, with 0.4% Al in alloy A compared to only 0.02–0.12% Al predicted over the 1650–1900 °C temperature range. The %Al in the Sample B alloy is significantly higher than in the Sample A alloy at 2.6% Al, compared to the equilibrium range of 0.03–0.17% Al. These numbers indicate that the equilibrium calculation does not correspond to the experimental observations regarding the extent of Al reaction. However, the %C and %Si levels appear to be indicators of the trends, as there is an overlap of values, and these are all undersaturated in carbon.
The %Mn and %Fe equilibrium values at 1900 °C are the closest to the experimental values for both alloys. The equilibrium value range is from 68% Mn to 76% Mn compared to 66% in the Sample A alloy, and the equilibrium range is from 54% Mn to 66% Mn compared to 54% Mn in Sample B alloy. The alloy B copper content at 1900 °C equilibrium is 20% Cu compared to 21% Cu analysed in the alloy. The discrepancy in the best fit equilibrium temperatures of from 1650 to 1700 °C for %C and %Si vs. 1900 °C for the closest values in %Mn and %Fe for Sample A indicates that complete equilibrium is not attained in the short reaction time of the aluminothermic reaction applied in this work. In particular, the %Al is predicted to be close to zero at equilibrium, whilst this is not the case in the produced alloy.
Figure 10c,d displays the slag compositions in comparison to the equilibrium lines at 1650–1900 °C. The equilibrium lines for Sample A and Sample B slag are the same since the copper metal added in Sample B is inert with respect to the slag components. It is seen that the %Al
2O
3 in slag A and slag B are the same at 52%, compared to the higher values predicted for equilibrium at 56–59% Al
2O
3. This discrepancy arises from the complete oxidation of Al predicted in the equilibrium calculations, compared to some Al remaining in reserve in the alloy. Higher levels of MnO in the slags at 22.7% MnO in slag A and 19.4% MnO in slag B, compared to the equilibrium values of 8%–13%, indicate lower Mn recovery in the experiments. The slag A and slag B %CaO are lower than the equilibrium values, possibly due to the incomplete incorporation of CaO into the melt. The SiO
2 and Na
2O contents in the slags correspond to the equilibrium values at temperatures ranging from 1700 to 1750 °C. The equilibrium gas compositions for Samples A and B are similar, as displayed in
Figure 10e. The gas consists of CO, Na, Mn, and H
2. Little Cu is present in the Sample B gas composition, indicating a high distribution of Cu to the alloy as found experimentally.
The FactSage-calculated gas–slag–metal mass distribution of the elements Mn, Si, Al, and Cu for Sample B is summarised in
Figure 11a–d as a function of temperature, and the element distribution of Mn, Si, and Al for Sample A are shown in
Figure 12a–c. It is observed that losses of Mn and Cu to the gas phase increase with increasing temperature. Manganese has a high vapour pressure and is expected to easily enter the gas phase, as confirmed in
Figure 10e. Interestingly, this trend is not seen in the case of Al, although one may expect the same behaviour from both Cu and Al, since these metals both have similar vapour pressures, even though it is orders of magnitude less than that of Mn [
36,
37]. Instead, Al is fully reacted in the aluminothermic reaction of MnO and SiO
2 to form Al
2O
3.
Copper distribution to the alloy is high, being 100% at 1650 °C and 96% at 1900 °C, with an increased loss to the gas phase as the temperature increases. Since Cu is inert to oxidation, there is no oxidation loss to the slag phase. Comparing
Figure 11a to
Figure 12a reveals increased the Mn recovery of 2–6% to the alloy in Sample B with added Cu. Comparing
Figure 11b to
Figure 12b shows a higher distribution of Si to the alloy in Sample B (by 3–5%) at 1650 °C compared to 1700 °C.
The only difference between the Sample A and B inputs is the addition of the Cu collector metal. The output slag analyses are similar. Therefore, the effect of Cu on the activity of the Mn alloy is considered.
Figure 13a,b shows the equilibrium activities in the bulk alloy products. The main difference is the lowered activity of Mn in Sample B due to the addition of Cu. According to Le Chatelier’s principle, lowering the Mn activity will increase the driving force of reaction (2) towards completion [
11]. At the start of the aluminothermic reduction process, the activity differences in Mn in the alloy of Sample A and Sample B would be greater because the initial alloy formation consists of much Cu and little Mn in Sample B, compared to mostly Mn in Sample A alloy.
< > = solid; ( ) = liquid.
The fact that aluminium particle size strongly influences the overall aluminothermy reaction extent implies that the aluminium reduction reaction is controlled at the aluminium oxide reaction interface [
33,
38,
39]. This effect is the analogue of MnO in slag reduced by carbon, with the reaction interface area as the main unknown [
40]. The driving force for the chemical reaction is the MnO activity in the slag relative to its equilibrium value. The MnO
2 ore has few fluxing compounds (
Table 3), resulting in high MnO activity at the start of reduction via reaction (2). Similarly, the aluminium particles should be pure at the start of reduction. The formation of an Al
2O
3 product film on the surface of aluminium particles was shown in previous work, but this film was not continuous and its breakup occurred easily [
41]. In the aluminothermy of SiO
2–MnO–Fe–Al mixtures, a ferrosilicomanganese powder product was formed with some Al
2O
3 particles entrapped in the alloy phase, even though both the oxide and alloy were reported as molten [
42]. The application of fluxing agents in the current study should improve the separation of the Al
2O
3 product from the alloy, and as the fluxes dissolve Al
2O
3 at the reaction interface, the Al
2O
3 activity is lowered to drive reaction (2) towards completion. The sequence of the melting of reactants and products can influence the reaction rate. Since aluminium has a low melting point of 660 °C compared to copper at 1083 °C, manganese at 1244 °C, silicon at 1410 °C, and iron at 1535 °C, it is expected that aluminium melts before its reaction with the oxides. The reaction of liquid aluminium was observed in the reaction of aluminium with MgO, in which the reduction in MgO proceeded after the molten aluminium covered the MgO [
41]. Therefore, in addition to optimising the chemistry design to maximise reactant activities and minimise product activities, thereby driving reactions to completion according to Le Chatelier’s principle, the chemistry application may also be used to limit Al
2O
3 product layer formation at the reaction interface.
In addition to reaction (2) as the main reaction of importance, the following reactions are likely at play in the reaction system, as designed in this work. At low temperatures, the ore is decomposed to Fe
2O
3 and Mn
2O
3 according to reaction (3) at 680 °C and reaction (4) at 546 °C to 600 °C [
43,
44]. The released water and oxygen from reactions (3) and (4) can react with carbon and aluminium via reactions (5) to (8). The reaction of aluminium with the oxygen from rection (4) serves as the ignition start. The presence of reductant carbon is aimed at a reduction in Fe
2O
3 and Mn
2O
3 to FeO and MnO in reactions (9) and (10) to remove the requirement of pre-roasting, as mentioned by Bhoi et al. [
1]. CO gas is released and helps to maintain reducing conditions in the reaction volume. Aluminothermic reduction in FeO and part-reduction in SiO
2 occurs via reactions (11) and (12).
< > = solid; ( ) = liquid; [ ] = gas.
Considering the similarities between Sample A and B feed mixtures, and the only difference as the Cu collector metal added, it is clear that the increase in alloy yield from 43% to 57% in Sample A versus Sample B (
Table 8) is mainly due to the inert Cu collector metal. The increase in the Mn yield is 6%, which is a combination of the activity-lowering effect, as shown in
Figure 13a, and the collector metal effect, namely that copper droplets serve as physical collector volumes for the newly formed Mn metal via reaction (2).
In summary, this work demonstrates that a sodium-fluxed slag with high Al2O3 solubility can be utilised in the aluminothermic reduction in MnO2 ore using Cu as a collector metal and adding a minor carbon reductant quantity. The addition of a carbon reductant negates MnO2 ore pre-roasting step. The Cu collector metal increases the Mn recovery to the alloy by 6%. The feed mixture formulation yields a NaAlO2-containing slag suitable for leaching to recover aluminium for circular processing, thereby providing a feed to the Hall–Héroult electrochemical process. A medium-carbon Fe–Mn–Si–Al–Cu complex ferroalloy is formed, which is suitable as a ferroalloying additive in steelmaking.