Amorphous Al-Ti Powders Prepared by Mechanical Alloying and Consolidated by Electrical Resistance Sintering

A novel processing method for amorphous Al50Ti50 alloy, obtained by mechanical alloying and subsequently consolidated by electrical resistance sintering, has been investigated. The characterisation of the powders and the confirmation of the presence of amorphous phase have been carried out by laser diffraction, scanning electron microscopy, X-ray diffraction, differential scanning calorimetry and transmission electron microscopy. The amorphous Al50Ti50 powders, milled for 75 h, have a high hardness and small plastic deformation capacity, not being possible to achieve green compacts for conventional sintering. Moreover, conventional sintering takes a long time, being not possible to avoid crystallisation. Amorphous powders have been consolidated by electrical resistance sintering. Electrically sintered compacts with different current intensities (7–8 kA) and processing times (0.8–1.6 s) show a porosity between 16.5 and 20%. The highest Vickers hardness of 662 HV is reached in the centre of an electrically sintered compact with 8 kA and 1.2 s from amorphous Al50Ti50 powder. The hardness results are compared with the values found in the literature.


Introduction
Al-Ti crystalline alloys are very attractive low-density materials with excellent properties at high temperatures [1]. Titanium aluminides are used for engine and airframe applications, mostly in the aerospace industry. The development of Al-Ti alloys began about 1970; however the alloys have only been used in these applications since about 2000 [2].
In general, the transformation of the crystalline phase of metallic materials to an amorphous phase can improve properties such as corrosion resistance [3], hardness [4] or mechanical strength [5]. An ideal method to obtain the amorphous phase in significant quantities is mechanical alloying.
Mechanical alloying (MA) is a peculiar grinding process that employs a high-energy ball mill in order to produce a composite metal powder with a controlled microstructure. This happens through repeated welding and fracturing of a mixture of metallic (and non-metallic) powders by the action of

Materials and Methods
Pure elemental powders of aluminum AS61 (Eckart-Werke, Eckart, Germany, purity > 99.5%) and titanium Se-Jong 4 (Se-Jong Materials, Incheon, South Korea, purity > 99.5%) were mixed to give the desired compositions of Al 50 Ti 50 . The manufacturer's chemical analysis for pure aluminum and pure titanium powders is given in Tables 1 and 2, respectively. The mixture of 72 g of Al 50 Ti 50 powder was placed in a sealed cylindrical 304 stainless steel vial, together with 304 stainless steel balls and 1.5 wt. % of ethylene bis-stearamide (EBS) wax (C 38 H 76 N 2 O 2 ), as shown in Figure 1. The wax (PCA) function is to equilibrate the particles welding and rupture processes. Powders were alloyed up to 75 h in a high-energy attritor ball mill under a purified argon Metals 2019, 9, 1140 3 of 14 atmosphere to minimize contamination (oxygen and nitrogen from air). The RBP was fixed to 50:1, the rotor speed was 500 rpm, and the dry ball mill was carried out at room temperature. The MA experiment was interrupted at desired intervals and small amounts of the alloyed mix were taken out from the vial for analysis.
Amsterdam, The Netherlands). The crystallisation process was followed by differential scanning calorimeter (DSC, Q100, TA Instruments, New Castle, DE, USA) under an argon gas flow. All the DSC results were obtained with heating rates of 40 °C/min up to a maximum temperature of 600 °C.
For the ERS process a resistance welding machine has been used (Serra Soldadura S.A., Barcelona, Spain), which provides the necessary electrical (high intensity and low voltage) and mechanical (load for compression) requirements. This adapted equipment produces the current with a one-phase transformer of 100 kVA, and the uniaxial load with a pneumatic cylinder reaching up to 14 kN. Moreover, the direct current intensity during the process is electronically controlled, and follow-up sensors record the outstanding parameters as the mobile punch displacement, the load and the effective voltage and current intensity. Once milled, powders were processed to obtain a bulk material. The 12 mm in diameter ceramic die ( Figure 2) was confined by a metallic hoop. The outlets of the die were closed with water cooled electrodes of temperature resistant copper (98.9%Cu-1%Cr-0.1%Zr), and electro-erosion resistant wafers (75.3%W-24.6%Cu) in direct contact with the powder. The amorphous powders (2 g) were placed between the wafers for sintering. Due to their low thermal conductivity, the wafers dump the heat flow from the powder mass to the electrodes.
Powders were consolidated with a compaction pressure of 80 MPa and only one electric pulse for each specimen. Several current intensities (7.0, 7.5 and 8.0 kA) and current passing times (40 to 80 cycles, with 50 cycles = 1.0 s) were tested.
Hardness tests and light micrographs were carried out on diametrical planes of the cylindrical compacts mounted in Bakelite resin. Hardness measurements distribution in the diametrical plane is shown in Figure 3. (Indentations were carried out in different positions due to the non-uniform porosity distribution, coming from the temperature gradient generated during consolidation). Indentations were carried out in the center (HVc), in the outer layer near the surface (HVo) and in the inner area (HVi) of the compact. The hardness results were compared with the values of other investigations using different sintering techniques. Size distribution and granulometric curves of the powders alloyed for different times were obtained by laser diffraction (Mastersizer 2000, Malvern Instruments, Malvern, UK). The structure and amorphisation progress of the ball milled powders were characterized by X-ray diffraction (XRD, D500, Siemens, Munich, Germany) with CuKα radiation, scanning electron microscopy (SEM, XL 30, Philips, Amsterdam, The Netherlands) and transmission electron microscopy (TEM, CM-200, Philips, Amsterdam, The Netherlands). The crystallisation process was followed by differential scanning calorimeter (DSC, Q100, TA Instruments, New Castle, DE, USA) under an argon gas flow. All the DSC results were obtained with heating rates of 40 • C/min up to a maximum temperature of 600 • C.
For the ERS process a resistance welding machine has been used (Serra Soldadura S.A., Barcelona, Spain), which provides the necessary electrical (high intensity and low voltage) and mechanical (load for compression) requirements. This adapted equipment produces the current with a one-phase transformer of 100 kVA, and the uniaxial load with a pneumatic cylinder reaching up to 14 kN. Moreover, the direct current intensity during the process is electronically controlled, and follow-up sensors record the outstanding parameters as the mobile punch displacement, the load and the effective voltage and current intensity.
Once milled, powders were processed to obtain a bulk material. The 12 mm in diameter ceramic die ( Figure 2) was confined by a metallic hoop. The outlets of the die were closed with water cooled electrodes of temperature resistant copper (98.9%Cu-1%Cr-0.1%Zr), and electro-erosion resistant wafers (75.3%W-24.6%Cu) in direct contact with the powder. The amorphous powders (2 g) were placed between the wafers for sintering. Due to their low thermal conductivity, the wafers dump the heat flow from the powder mass to the electrodes.
Powders were consolidated with a compaction pressure of 80 MPa and only one electric pulse for each specimen. Several current intensities (7.0, 7.5 and 8.0 kA) and current passing times (40 to 80 cycles, with 50 cycles = 1.0 s) were tested.
Hardness tests and light micrographs were carried out on diametrical planes of the cylindrical compacts mounted in Bakelite resin. Hardness measurements distribution in the diametrical plane is shown in Figure 3. (Indentations were carried out in different positions due to the non-uniform porosity distribution, coming from the temperature gradient generated during consolidation). Indentations were carried out in the center (HV c ), in the outer layer near the surface (HV o ) and in the inner area The structure and crystallisation progress of the compacts consolidated by ERS were characterized by XRD.

Amorphisation
In the first part of the investigation, amorphous and/or nanocrystalline powders of the Al-Ti alloy are prepared by MA. The characterisation of the powders is done for different milling times. Laser diffraction measures particles size, SEM reveals morphology and confirms particle sizes. XRD indicates whether an amorphous and/or nanocrystalline phase is present and identifies the different crystalline phases. DSC shows the crystallisation temperature of the amorphous phase and TEM identifies amorphous, nanocrystalline and/or crystalline phases.

Laser Diffraction
At the beginning of the milling process, aluminium powder has an average particle size d (0.5) of about 71.2 μm, and titanium powder of about 29.6 μm. As shown in Figure 4, the mixture of the two pure metals, in the 50/50 atomic ratio, results in an average particle size of about 41.3 μm. During the first hours of milling, when fracture processes predominate, the average particle size decreases considerably, reaching about 18.5 μm for 5 h. Between 5 and 25 h, the particle size remains stable without significant changes. However, going further of 25 h of milling, the dislocations density in the powder increases considerably, hardening it enough to make particle size to decrease to minimum values.   The structure and crystallisation progress of the compacts consolidated by ERS were characterized by XRD.

Amorphisation
In the first part of the investigation, amorphous and/or nanocrystalline powders of the Al-Ti alloy are prepared by MA. The characterisation of the powders is done for different milling times. Laser diffraction measures particles size, SEM reveals morphology and confirms particle sizes. XRD indicates whether an amorphous and/or nanocrystalline phase is present and identifies the different crystalline phases. DSC shows the crystallisation temperature of the amorphous phase and TEM identifies amorphous, nanocrystalline and/or crystalline phases.

Laser Diffraction
At the beginning of the milling process, aluminium powder has an average particle size d (0.5) of about 71.2 μm, and titanium powder of about 29.6 μm. As shown in Figure 4, the mixture of the two pure metals, in the 50/50 atomic ratio, results in an average particle size of about 41.3 μm. During the first hours of milling, when fracture processes predominate, the average particle size decreases considerably, reaching about 18.5 μm for 5 h. Between 5 and 25 h, the particle size remains stable without significant changes. However, going further of 25 h of milling, the dislocations density in the powder increases considerably, hardening it enough to make particle size to decrease to minimum values.

Amorphisation
In the first part of the investigation, amorphous and/or nanocrystalline powders of the Al-Ti alloy are prepared by MA. The characterisation of the powders is done for different milling times. Laser diffraction measures particles size, SEM reveals morphology and confirms particle sizes. XRD indicates whether an amorphous and/or nanocrystalline phase is present and identifies the different crystalline phases. DSC shows the crystallisation temperature of the amorphous phase and TEM identifies amorphous, nanocrystalline and/or crystalline phases.

Laser Diffraction
At the beginning of the milling process, aluminium powder has an average particle size d (0.5) of about 71.2 µm, and titanium powder of about 29.6 µm. As shown in Figure 4, the mixture of the two pure metals, in the 50/50 atomic ratio, results in an average particle size of about 41.3 µm.
During the first hours of milling, when fracture processes predominate, the average particle size decreases considerably, reaching about 18.5 µm for 5 h. Between 5 and 25 h, the particle size remains stable without significant changes. However, going further of 25 h of milling, the dislocations density in the powder increases considerably, hardening it enough to make particle size to decrease to minimum values.

X-ray Diffraction
The initial study of the milled powders has been completed by XRD analysis (Figure 6). It is observed that for the first 5 h of milling, the intensity of the diffraction peaks of Al and Ti decreases as time increases. At the same time, the width of the peaks increases considerably as a result of the decrease in crystallite size. After 12 h of milling, the formation of a nanocrystalline/amorphous phase begins by atomic diffusion between Al and Ti. Thus, after 25 h, independent peaks of Al and Ti cannot at all be observed and a characteristic wide peak of the amorphous phases appears with the maximum around 2Θ = 39 • . The percentage of amorphous phase increases with milling time, as evidenced by the widening of the halo.

X-ray Diffraction
The initial study of the milled powders has been completed by XRD analysis (Figure 6). It is observed that for the first 5 h of milling, the intensity of the diffraction peaks of Al and Ti decreases as time increases. At the same time, the width of the peaks increases considerably as a result of the decrease in crystallite size. After 12 h of milling, the formation of a nanocrystalline/amorphous phase begins by atomic diffusion between Al and Ti. Thus, after 25 h, independent peaks of Al and Ti cannot at all be observed and a characteristic wide peak of the amorphous phases appears with the maximum around 2Θ = 39°. The percentage of amorphous phase increases with milling time, as evidenced by the widening of the halo.

Differential Scanning Calorimetry
Amorphisation can also be verified by using DSC (Figure 7). For the powder milled for 12 and 25 h, the appearance of an exothermic peak from 500 °C is observed, probably corresponding to the nanocrystals growth, and partial crystallisation of the amorphous phase formed during MA. After 50 h, with a powder completely amorphous, there is a change in the shape of the curves obtained. An endothermic peak appears at about 400-550 °C, possibly reflecting the heat flow anomaly characteristic of the glass transition (difficult to find for lower milling times because of the lower amount of amorphous phase). This endothermic peak could hide the exothermic peak corresponding to the crystallisation of the amorphous phase, or maybe crystallization is retarded to higher temperatures, forming titanium aluminides (AlTi, Al3Ti and AlTi3), which again must take place above 500 °C. According to these results, in order to maintain the amorphous structure these powders could have a maximum temperature for consolidation, using conventional techniques, bellow 500 °C.

Transmission Electron Microscopy
In order to confirm the presence of the amorphous phase, TEM of milled powders for 5, 25 and 75 h is shown in Figure 8. A crystalline/nanocrystalline structure can be found for 5 h of milling. After

Differential Scanning Calorimetry
Amorphisation can also be verified by using DSC (Figure 7). For the powder milled for 12 and 25 h, the appearance of an exothermic peak from 500 • C is observed, probably corresponding to the nanocrystals growth, and partial crystallisation of the amorphous phase formed during MA. After 50 h, with a powder completely amorphous, there is a change in the shape of the curves obtained. An endothermic peak appears at about 400-550 • C, possibly reflecting the heat flow anomaly characteristic of the glass transition (difficult to find for lower milling times because of the lower amount of amorphous phase). This endothermic peak could hide the exothermic peak corresponding to the crystallisation of the amorphous phase, or maybe crystallization is retarded to higher temperatures, forming titanium aluminides (AlTi, Al 3 Ti and AlTi 3 ), which again must take place above 500 • C. According to these results, in order to maintain the amorphous structure these powders could have a maximum temperature for consolidation, using conventional techniques, bellow 500 • C.

Transmission Electron Microscopy
In order to confirm the presence of the amorphous phase, TEM of milled powders for 5, 25 and 75 h is shown in Figure 8. A crystalline/nanocrystalline structure can be found for 5 h of milling. After

X-ray Diffraction after Heat Treatment
The study of the milled powders for 75 h has been completed with XRD analyses after heating at various temperatures. Samples have been heated to 300, 500, 650 and 850 °C at 10 °C/min and maintained at temperature for 1 h, and after cooling, XRD have been performed at room temperature. As expected, up to 300 °C (Figure 9a,b) XRD does not show any significant structural change and no evidence of crystallisation is found. Between 500 and 650 °C (Figure 9c,d) the amorphous phase begins to crystallise giving rise to titanium aluminides such as AlTi, Al3Ti and AlTi3 (Figure 9d), although the presence of Al crystals is also possible. This transformation of the amorphous to the crystalline phase can be confirmed in the diffraction pattern at 850 °C (Figure 9e), where all the main peaks are already well differentiated from each other.

X-ray Diffraction after Heat Treatment
The study of the milled powders for 75 h has been completed with XRD analyses after heating at various temperatures. Samples have been heated to 300, 500, 650 and 850 °C at 10 °C/min and maintained at temperature for 1 h, and after cooling, XRD have been performed at room temperature. As expected, up to 300 °C (Figure 9a,b) XRD does not show any significant structural change and no evidence of crystallisation is found. Between 500 and 650 °C (Figure 9c,d) the amorphous phase begins to crystallise giving rise to titanium aluminides such as AlTi, Al3Ti and AlTi3 (Figure 9d), although the presence of Al crystals is also possible. This transformation of the amorphous to the crystalline phase can be confirmed in the diffraction pattern at 850 °C (Figure 9e), where all the main peaks are already well differentiated from each other.

X-ray Diffraction after Heat Treatment
The study of the milled powders for 75 h has been completed with XRD analyses after heating at various temperatures. Samples have been heated to 300, 500, 650 and 850 • C at 10 • C/min and maintained at temperature for 1 h, and after cooling, XRD have been performed at room temperature. As expected, up to 300 • C (Figure 9a,b) XRD does not show any significant structural change and no evidence of crystallisation is found. Between 500 and 650 • C (Figure 9c,d) the amorphous phase begins to crystallise giving rise to titanium aluminides such as AlTi, Al 3 Ti and AlTi 3 (Figure 9d), although the presence of Al crystals is also possible. This transformation of the amorphous to the crystalline phase can be confirmed in the diffraction pattern at 850 • C (Figure 9e), where all the main peaks are already well differentiated from each other.

Porosity
At the beginning of the ERS process (pressing stage, at 80 MPa), the powder mass porosity decreases very little, both because of the high hardness of the amorphous powders and the low applied pressure. In general, after the whole process, amorphous powders milled for 75 h and ERS with low intensity still have a high porosity ( Figure 10). For higher current intensities, the densification capacity increases. The increase in processing time (in cycles in Figure 10) acts in similar way. No satisfactory experiments were carried out with current intensities lower than 7 kA or higher than 8 kA. For low current intensities, the high electrical resistivity of the powder mass makes sintering difficult. For high current intensities, sintered compacts stick and cannot be separated of the

Porosity
At the beginning of the ERS process (pressing stage, at 80 MPa), the powder mass porosity decreases very little, both because of the high hardness of the amorphous powders and the low applied pressure. In general, after the whole process, amorphous powders milled for 75 h and ERS with low intensity still have a high porosity ( Figure 10). For higher current intensities, the densification capacity increases. The increase in processing time (in cycles in Figure 10) acts in similar way.

Porosity
At the beginning of the ERS process (pressing stage, at 80 MPa), the powder mass porosity decreases very little, both because of the high hardness of the amorphous powders and the low applied pressure. In general, after the whole process, amorphous powders milled for 75 h and ERS with low intensity still have a high porosity ( Figure 10). For higher current intensities, the densification capacity increases. The increase in processing time (in cycles in Figure 10) acts in similar way. No satisfactory experiments were carried out with current intensities lower than 7 kA or higher than 8 kA. For low current intensities, the high electrical resistivity of the powder mass makes sintering difficult. For high current intensities, sintered compacts stick and cannot be separated of the No satisfactory experiments were carried out with current intensities lower than 7 kA or higher than 8 kA. For low current intensities, the high electrical resistivity of the powder mass makes sintering difficult. For high current intensities, sintered compacts stick and cannot be separated of the wafers. As expected, it results difficult to remove the porosity of hardened amorphous powders after MA, however, this is not the case for softer unmilled crystalline powders. The porosity of ERS compacts made from pure Ti powders is much lower and can reach values of up to 4% even with lower current intensities ( Figure 11). Metals 2019, 9, x FOR PEER REVIEW 9 of 14 wafers. As expected, it results difficult to remove the porosity of hardened amorphous powders after MA, however, this is not the case for softer unmilled crystalline powders. The porosity of ERS compacts made from pure Ti powders is much lower and can reach values of up to 4% even with lower current intensities ( Figure 11). As observed in the trend lines in Figures 10 and 11, the slope for pure Ti compacts is smaller than in the case of milled Al50Ti50 compacts. Therefore, for ductile powders, the increase in sintering time does not affect the decrease in porosity as much as in the case of very hard powders. The high-porosity ERS 7/40 Al-Ti compact (sintered with intensity of 7 kA and 40 cycles) has been selected to show the effect of ERS on the microstructure ( Figure 12). The uniform porosity distribution generally found in conventionally sintered compacts differs from the non-uniform distribution after ERS. Electrically sintered compacts have a more porous outer layer with a width of about 2 mm (Figure 12a,c) and a densified centre (Figure 12b,d). The ERS 7/40 compact has an average porosity of about 20.1%, however, the porosity in the outer layer is about 32.8% and in the centre about 8.5%. The porosity variation is caused by the unequal temperature distribution in the compact, consequence of the preferential electric paths inside the compact and the heat sink through the die walls. Temperature rises less and decreases faster near the wall of the ceramic die.

X-ray Diffraction of Compacts after Heat Treatment
An additional and important issue to consider is the effect of the sintering process on the microstructure. Although the sintering process is very quick, the temperature variation inside the compact could affect, as shown next, the stability of the amorphous phase. Also, the effect of additional exposure to high temperatures on the microstructure is of interest, because of the typical use of Al-Ti alloys [1].
The amorphous phase stability with temperature in the ERS 7/40 compact has been evaluated by XRD carried out at different temperatures (Figure 13). At room temperature (Figure 13a), after the ERS process, a small wide peak appears, due to the partial transformation of the amorphous phase into nanocrystals. Nanocrystals could probably be of Al, or some of the intermetallic compounds AlTi, Al3Ti and AlTi3. If the compact is heated to 300 °C (Figure 13b), the main peak (at 39°) starts growing, as a result of the increase of the crystalline phase. The peak still shows a significant width, typical of a small crystallite size. Although the temperature is not very high, the effect of time at this temperature (heating rate of 10 °C/min and 0.5 h at temperature) makes the amorphous structure to dissipate as compared with the sintered compact. At higher temperatures of 500 and 650 °C ( Figure  13c,d) there is not a big difference between the main peaks, resulting a stable structure. As observed in the trend lines in Figures 10 and 11, the slope for pure Ti compacts is smaller than in the case of milled Al 50 Ti 50 compacts. Therefore, for ductile powders, the increase in sintering time does not affect the decrease in porosity as much as in the case of very hard powders.
The high-porosity ERS 7/40 Al-Ti compact (sintered with intensity of 7 kA and 40 cycles) has been selected to show the effect of ERS on the microstructure ( Figure 12). The uniform porosity distribution generally found in conventionally sintered compacts differs from the non-uniform distribution after ERS. Electrically sintered compacts have a more porous outer layer with a width of about 2 mm (Figure 12a,c) and a densified centre (Figure 12b,d). The ERS 7/40 compact has an average porosity of about 20.1%, however, the porosity in the outer layer is about 32.8% and in the centre about 8.5%. The porosity variation is caused by the unequal temperature distribution in the compact, consequence of the preferential electric paths inside the compact and the heat sink through the die walls. Temperature rises less and decreases faster near the wall of the ceramic die.

X-ray Diffraction of Compacts after Heat Treatment
An additional and important issue to consider is the effect of the sintering process on the microstructure. Although the sintering process is very quick, the temperature variation inside the compact could affect, as shown next, the stability of the amorphous phase. Also, the effect of additional exposure to high temperatures on the microstructure is of interest, because of the typical use of Al-Ti alloys [1].
The amorphous phase stability with temperature in the ERS 7/40 compact has been evaluated by XRD carried out at different temperatures (Figure 13). At room temperature (Figure 13a), after the ERS process, a small wide peak appears, due to the partial transformation of the amorphous phase into nanocrystals. Nanocrystals could probably be of Al, or some of the intermetallic compounds AlTi, Al 3 Ti and AlTi 3 . If the compact is heated to 300 • C (Figure 13b), the main peak (at 39 • ) starts growing, as a result of the increase of the crystalline phase. The peak still shows a significant width, typical of a small crystallite size. Although the temperature is not very high, the effect of time at this temperature (heating rate of 10 • C/min and 0.5 h at temperature) makes the amorphous structure to dissipate as compared with the sintered compact. At higher temperatures of 500 and 650 • C (Figure 13c,d) there is not a big difference between the main peaks, resulting a stable structure. Metals 2019, 9, x FOR PEER REVIEW 10 of 14

Hardness of Al-Ti Alloys
The difference between the hardness of Al50Ti50 ERS compacts and that of other ones mentioned in the literature, prepared with similar procedures, has been studied. The hardness of the compacts,

Hardness of Al-Ti Alloys
The difference between the hardness of Al50Ti50 ERS compacts and that of other ones mentioned in the literature, prepared with similar procedures, has been studied. The hardness of the compacts,

Hardness of Al-Ti Alloys
The difference between the hardness of Al 50 Ti 50 ERS compacts and that of other ones mentioned in the literature, prepared with similar procedures, has been studied. The hardness of the compacts, in general, depends mainly on two factors: the hardness of the powders that constitute the compact and the density of the resulting compact. Figure 14 shows the hardness values of some materials related to those studies.
First, the hardness values of the starting materials should be highlighted. Pure aluminium and titanium have a very low hardness compared to their alloys. Pure aluminium powder has a hardness of only 20 HV [15]. This low hardness of the aluminium powder can be increased by mechanical alloying, both because of the grains refinement and by the effect of the PCA, leading to the formation of a solid solution, thus increasing the hardness of the powder to 127 HV [16], which decreases after a short stress relieve treatment at 600 • C to 97 HV [16]. In addition, after conventional consolidation by uniaxial pressing and furnace sintering the hardness of pure aluminium can decrease to 80 HV [16], mainly because of the grain growth. It is also possible to increase the hardness of conventionally consolidated pure Al compacts to about 180 HV by milling the powder in an atmosphere of ammonia [17,18]. Apart from grain refining, ammonia causes the formation of nitrogen-rich compounds that produce dispersion hardening.
Pure titanium has a higher hardness than pure aluminium. Commercial powders can reach up to about 70 HV [15] or 160 HV [19]. This difference depends largely on the morphology and/or fabrication process of the powder. On the other hand, pure titanium compacts can reach 255 HV [20], 270 HV [21] and 290 HV [19].
In Al-Ti alloyed powder mixtures and compacts, there is a noticeable increase in hardness compared to pure Al. In general, a higher content of Ti produces a greater final hardness, because of forming an Al(Ti) solid solution after mechanical alloying and/or intermetallic compounds like Al 3 Ti, AlTi and AlTi 3 after heat treating or sintering. For instance, with the presence of only 2.88 at.% of titanium, sintered aluminium compacts increase the hardness from 80 HV to about 104 HV [22]. With the increase of titanium up to 5.58 at.%, the hardness increases to about 202 HV [15]. In addition, for the Al 50 Ti 50 alloy, the hardness increases to values between 300 and 790 HV [23][24][25][26][27][28].
Metals 2019, 9, x FOR PEER REVIEW 11 of 14 in general, depends mainly on two factors: the hardness of the powders that constitute the compact and the density of the resulting compact. Figure 14 shows the hardness values of some materials related to those studies. First, the hardness values of the starting materials should be highlighted. Pure aluminium and titanium have a very low hardness compared to their alloys. Pure aluminium powder has a hardness of only 20 HV [15]. This low hardness of the aluminium powder can be increased by mechanical alloying, both because of the grains refinement and by the effect of the PCA, leading to the formation of a solid solution, thus increasing the hardness of the powder to 127 HV [16], which decreases after a short stress relieve treatment at 600 °C to 97 HV [16]. In addition, after conventional consolidation by uniaxial pressing and furnace sintering the hardness of pure aluminium can decrease to 80 HV [16], mainly because of the grain growth. It is also possible to increase the hardness of conventionally consolidated pure Al compacts to about 180 HV by milling the powder in an atmosphere of ammonia [17,18]. Apart from grain refining, ammonia causes the formation of nitrogen-rich compounds that produce dispersion hardening.
Pure titanium has a higher hardness than pure aluminium. Commercial powders can reach up to about 70 HV [15] or 160 HV [19]. This difference depends largely on the morphology and/or fabrication process of the powder. On the other hand, pure titanium compacts can reach 255 HV [20], 270 HV [21] and 290 HV [19].
The hardness results of the ERS compacts of this work are shown in Figure 15. Independently of the initial powder microstructure (crystalline or amorphous) current intensity has a similar effect on sintered compacts, with higher intensities resulting in higher hardness. However, the effect of sintering time does not have much influence on hardness, because the effect of time is lower on the energy transferred to the compact. In all the specimens, the centre (HVc) has a greater hardness than the outer layer (HVo). The hardness measured for the inner zone (HVi) does not show much difference with the centre hardness, since the porosity gradient is not uniform. There is a wide area around the Figure 14. Hardness of aluminium, titanium and Al 50 Ti 50 alloys according to bibliographic data [15][16][17][18][19][20][21][22][23][24][25][26][27][28].
The hardness results of the ERS compacts of this work are shown in Figure 15. Independently of the initial powder microstructure (crystalline or amorphous) current intensity has a similar effect on sintered compacts, with higher intensities resulting in higher hardness. However, the effect of sintering time does not have much influence on hardness, because the effect of time is lower on the energy transferred to the compact. In all the specimens, the centre (HV c ) has a greater hardness than the outer layer (HV o ). The hardness measured for the inner zone (HV i ) does not show much difference with the centre hardness, since the porosity gradient is not uniform. There is a wide area around the compact centre with low and homogeneous porosity. Between the denser inner and the outer area, there is a sharp porosity change.
Metals 2019, 9, x FOR PEER REVIEW 12 of 14 compact centre with low and homogeneous porosity. Between the denser inner and the outer area, there is a sharp porosity change. The highest measured hardness corresponds to the centre of the compact ERS at 8 kA from amorphous powder milled for 75 h. The microstructure contains mainly nanocrystals of aluminium and Al3Ti, AlTi and AlTi3 compounds with possible amorphous phase residues. Vickers hardness reaches values between 633 and 662 HV for different sintering times.
If lower current intensity (7 kA) is applied, the hardness in the compact centre decreases slightly to values between 607 and 623 HV because of the lower densification, although a higher amount of amorphous phase remains untransformed.
The hardness in the outer layer of the compact decreases considerably for both 8 kA and 7 kA. Hardness values vary between 480 and 530 HV. The prevalence of an amorphous structure in this area because of the lower attained temperature, versus a nanocrystalline or crystalline structure development, should account for a higher hardness. However, the predominant factor is the increase in porosity, negatively affecting hardness.
After an annealing heat treatment (for 7 and 8 kA ERS compact) up to 650 °C for 1 h, the hardness decreases considerably. In the centre, the hardness reaches 503-515 HV, with values between 352-378 HV in the outer porous layer. This decrease of around 20% is due to the amorphous/nanocrystalline to crystalline phase transformation and grain growth.
For ERS compacts prepared from Al-Ti powder milled for 5 h, the hardness reaches values between 392 and 448 HV in the inner and periphery, respectively. After 5 h of milling, the powder microstructure has not reached an amorphous structure, but a supersaturated solid solution with areas of aluminium and titanium. After ERS processing with 8 kA, the microstructure will probably consist in a small percentage of intermetallic compounds together with solid solutions and pure elements.
Finally, it has been confirmed that the hardness of the ERS 6/40-80 pure Ti compacts (both in the centre and periphery) is lower than that of the compacts prepared from milled Al50Ti50 powders. Hardness ranges between 248-263 HV for the outer layer and 296-323 HV for the centre of the compact. These compacts are highly densified, but no hardening mechanism is developed for pure titanium. The highest measured hardness corresponds to the centre of the compact ERS at 8 kA from amorphous powder milled for 75 h. The microstructure contains mainly nanocrystals of aluminium and Al 3 Ti, AlTi and AlTi 3 compounds with possible amorphous phase residues. Vickers hardness reaches values between 633 and 662 HV for different sintering times.
If lower current intensity (7 kA) is applied, the hardness in the compact centre decreases slightly to values between 607 and 623 HV because of the lower densification, although a higher amount of amorphous phase remains untransformed.
The hardness in the outer layer of the compact decreases considerably for both 8 kA and 7 kA. Hardness values vary between 480 and 530 HV. The prevalence of an amorphous structure in this area because of the lower attained temperature, versus a nanocrystalline or crystalline structure development, should account for a higher hardness. However, the predominant factor is the increase in porosity, negatively affecting hardness.
After an annealing heat treatment (for 7 and 8 kA ERS compact) up to 650 • C for 1 h, the hardness decreases considerably. In the centre, the hardness reaches 503-515 HV, with values between 352-378 HV in the outer porous layer. This decrease of around 20% is due to the amorphous/nanocrystalline to crystalline phase transformation and grain growth.
For ERS compacts prepared from Al-Ti powder milled for 5 h, the hardness reaches values between 392 and 448 HV in the inner and periphery, respectively. After 5 h of milling, the powder microstructure has not reached an amorphous structure, but a supersaturated solid solution with areas of aluminium and titanium. After ERS processing with 8 kA, the microstructure will probably consist in a small percentage of intermetallic compounds together with solid solutions and pure elements.
Finally, it has been confirmed that the hardness of the ERS 6/40-80 pure Ti compacts (both in the centre and periphery) is lower than that of the compacts prepared from milled Al 50 Ti 50 powders. Hardness ranges between 248-263 HV for the outer layer and 296-323 HV for the centre of the compact. These compacts are highly densified, but no hardening mechanism is developed for pure titanium.

Conclusions
A novel method of compacts processing of the Al 50 Ti 50 alloy obtained by mechanical alloying and subsequent consolidation by ERS has been investigated. As expected, amorphous and/or nanocrystalline, powders of the Al 50 Ti 50 alloy were prepared by mechanical alloying up to 75 h. Particles size of the powders reached about 8.6 µm and showed an almost spherical shape. It has been checked that the amorphous phase crystallizes at about 500 • C, forming titanium aluminides.
Amorphous and/or nanocrystalline powders of the Al 50 Ti 50 alloy were successfully sintered by ERS with different current intensities (7-8 kA) and processing times (0.8-1.6 s). This technique avoids the difficulty of obtaining a green compact for conventional sintering because of the high hardness of these compacts. Electrically sintered compacts show non-uniform distribution of porosity with a porous outer layer and densified centre. For instance, the ERS 7/40 compact has a global porosity of about 20.1%, however, the porosity in the outer layer is about 32.8% and in the centre about 8.5%. The electrically sintered compact processed with 8 kA for 1.2 s from amorphous powders reaches a significant Vickers hardness of up to 662 HV.