Microstructure Changes and Improvement in the Mechanical Properties of As-Cast AlSi 7 MgCu 0 . 5 Alloy Induced by the Heat Treatment and ECAP Technique at Room Temperature

Department of Materials Engineering, Institute of Materials and Quality Engineering, Faculty of Materials, Metallurgy and Recycling, Technical University of Košice, Letná 9, 042 00 Košice, Slovakia Institute of Materials Research, Slovak Academy of Science, Watsonova 47, 040 01 Košice, Slovakia Department of Plastic Deformations and Process Simulations, Institute of Materials and Quality Engineering, Faculty of Materials, Metallurgy and Recycling, Technical University of Košice, Letná 9, 042 00 Košice, Slovakia


Introduction
Hypoeutectic aluminium-silicon alloys are well-known casting materials used in automotive industry due to their excellent castability, high strength-to-weight ratio, good mechanical properties at elevated temperature, good wear resistance, and low thermal-expansion coefficient [1].However, the low toughness and ductility of these alloys limit their wider applications, especially for engineering applications.ese limitations are as a result of heterogeneous structure of alloys that consists of α-solid solution, eutectic Si particles, and Fe-and Mn-rich intermetallic phase particles with undesirable morphology, size, and distribution that are regarded as impurities [2].
e addition of Mg and Cu to Al-Si alloys and the optimized heat treatment can improve the mechanical properties of these alloys.ose added elements allow their solid-solution hardening and precipitation hardening.e heat treatment including solution annealing, quenching, and ageing is the most widely used method to improve strength properties of these alloys due to the formation of precipitates from supersaturated solid solution during applied natural or arti cial ageing [3].During the initial stage of the arti cial ageing, the strength and hardness of alloys increases up to the maximum value.It is a result of the formation of coherent and/or semicoherent strengthening phase particles.
e decrease in strength of alloys after extended ageing time and/or at high ageing temperature is accompanied by an increase in their plasticity due to the formation of incoherent strengthening phase particles and their coarsening [4].
Besides the heat treatment of Al-Si-Mg-Cu alloys performed to improve their strength and plasticity, the techniques of severe plastic deformation (SPD) have been often used in the last decades.
ese techniques utilize deformation mechanism to re nement and homogenization of microstructure and grain-size strengthening and work or strain hardening of these alloys.Among all SPD techniques, the ECAP is widely used in the research of aluminium alloys, especially due to the production of ultra ne grained (UFG) structures of alloys and the billets of appropriate size for various structural applications [5,6].
e advantage and uniqueness of this method compared to the other methods of SPD is that pressed billets have the same initial and nal size of the cross section.In the corner of ECAP die, the UFG structure of severely deformed alloys is formed by simple shear.Moreover, in the case of alloys with heterogeneous chemical composition and microstructure, the homogenization of material occurs.However, the nal results of this technique depend above all on geometry of die, processing route, number of passes, and temperature of processing [7].
e aim of the present work is to investigate the e ect of the repetitive ECAP processing at room temperature on the microstructure and mechanical properties of overaged foundry AlSi7MgCu0.5 alloy.

Materials and Methods
e commercial AlSi7MgCu0.5 alloy casting, with a chemical composition shown in Table 1, was used for the investigation.
e optimal character of as-cast structure was achieved by the melt modi cation with Sr and inoculation with commercial Al-Ti-B grain re ner.e samples cut from the casting surface in the depth of 10 mm were used as an initial as-cast state.e cylindrical billets of the as-cast alloy state with the dimensions of 10 mm in diameter and 100 mm long were solution annealed at 823 K for 4 hours, subsequently water-quenched and arti cially aged at 573 K for 5 hours to obtain overaged alloy state.After this pre-ECAP heat treatment, the experimental billets were severely deformed by the ECAP technique at room temperature by 4 passes through the die with the angle between channels Φ 90 °and angle on outer corner of die Ψ 37 °. e billets were processed using route A in ECAP die, where the billets were not rotated between individual passes.e repetitive billet passing by this route is the most e ective in re nement and homogenization of as-cast structure of Al-Si alloys [8].
e microstructure of as-cast, overaged, and ECAPed alloy state was observed by using the light microscope (LM) and scanning electron microscope (SEM).Metallographic samples were prepared by grinding, polishing, etching in the solution of 0.5% HF in distilled water, and/or deep etching in the solution of 7% hydrochloric acid, 13% nitric acid, and 80% acetic acid.After ECAP processing, the microstructure and substructure of alloy were studied in the X-plane (perpendicular plane to the pressing direction), as shown in Figure 1.
e substructure of alloy was observed by the transmission electron microscopy (TEM) on the nally thinned foils in a solution of 33% nitric acid and 67% methanol at a temperature of 238 K and voltage of 16 V. e phase analysis of alloy states was realized by hard X-ray di raction (XRD) at P02.1 beamline at PETRA III storage ring at Deutsches Elektronen-Synchrotron (DESY) in Hamburg.
e tensile test of alloy states was carried out on short cylindrical samples at an initial strain rate of 2.5 × 10 −4 •s −1 at room temperature.e gauge length of short test samples of 5 mm diameter was 10 mm. e tensile strength characteristics (R p0.2 : yield strength; R m : tensile strength) and ductility characteristics (A: tensile elongation; A g : uniform tensile elongation; Z: reduction of area) were determined.Vickers microhardness measurements were made on the X-plane of samples at a load of 200 g and a loading time of 30 seconds.

Microstructure of As-Cast Alloy State.
e microstructure of as-cast AlSi7MgCu0.5 alloy state (Figure 2(a)) was dendritic and heterogeneous.It consists of α(Al) solid solution dendrites, interdendritic networks of eutectic silicon particles, and α-solid solution and particles of intermetallic phases.Figure 2(b) shows the eutectic and intermetallic phase particles in the microstructure of deep-etched alloy.
e morphology of eutectic Si particles was brous and coral-like.e particles of intermetallic phases were rod-like and of irregular script morphology.e phase analysis by hard XRD showed that the α(Al) solid solution and eutectic Si particles were predominant phases in as-cast alloy state (Figure 3(a)).
e presence of π(Al 8 FeMg 3 Si 6 ), β(Mg 2 Si), Q-Al 4 Mg 8 Si 7 Cu 2 and α-Al 12 (Fe,Mn) 3 Si, and/or α-Al 15 (Fe, Mn) 3 Si 2 phases was also detected by di raction analysis  e positions of α-Al 12 (Fe,Mn) 3 Si and α-Al 15 (Fe,Mn) 3 Si 2 maximum intensities responded to the same angle 2θ in the di raction patterns in comparison with the measured di raction data with minor deviations.e presence of phase with both stoichiometries in the as-cast alloy state is possible.

Microstructure of Overaged Alloy State.
e microstructure of the pre-ECAP heat-treated alloy state (after solution annealing, quenching, and arti cial ageing) is shown in Figure 4(a).Morphology of particular phases in the microstructure of alloy is visible in Figure 4(b).
e application of heat treatment did not change the heterogeneous    e comparison of overaged (Figure 4(a)) and ECAPed (Figure 7(a)) alloy microstructure shows that the dendritic structure of the alloy was e ectively homogenized through the fragmentation and redistribution of eutectic Si particles, intermetallic phases particles, and precipitates.After ECAP technique, the change of eutectic Si-particles morphology did not occur; however, their uneven arrangement in solid solution was changed to a line in the X and Y planes of pressed billet.In the Z-plane the homogenization of Siparticles, distribution in the matrix was negligible, due to deformation character of pressed billets by route A.
e fragmentation of particles present in the alloy structure was con rmed by evaluation of their average size (d) and number per unit area (n) in the X-plane of pressed billet, as shown in Table 2. ECAP led to the decrease of average size and the increase of number per unit area of Si particles, intermetallic phase particles, and precipitates in  Phase identi cation of ECAPed AlSi7MgCu0.5 alloy by XRD showed the presence of major and minor phases in its structure.It results from the X-ray di raction patterns of alloy in Figures 8(a) and 8(b).Al-solid solution and Si-particles were major phases in the analysed alloy state, and Q-Al 4 Mg 8 Si 7 Cu 2 , β(Mg 2 Si), α-Al 12 (Fe,Mn) 3 Si, and/or α-Al 15 (Fe,Mn) 3 Si 2 were minor phases, as well as in the overaged alloy state (Figure 5). Figure 9 shows the dependence between intensity of (111) re ection of α(Al) solid solution of ECAPed alloy and azimuthal angle of the Debye-Scherrer ring.It is possible to observe a strong preferred orientation of solid solution grains.
e ECAP processing of AlSi7MgCu0.5 alloy led to the formation of ultra ne grains of the solid solution.Substructure of 4 times pressed alloy consisted of elongated grains and/or subgrains with nonequilibrium, wavy and curved boundaries, and a high density of dislocations, both within the subgrains and in the zone of the subgrain boundaries, as illustrated in Figures 7(b   e presence of these equiaxed grains, with average size of 0.6 µm in the deformed structure of alloy, was a result of higher intensity of plastic deformation in areas close to eutectic Si particles.ese particles supported the formation of deformed areas.EBSD map shows that these areas were associated with the formation of HAGBs.

Mechanical Properties of Alloy.
e tensile test at room temperature determined the strength and ductile characteristics for as-cast, overaged, and ECAPed AlSi7MgCu0.5 alloy state.e values of mechanical properties obtained by the tensile test are given in Table 3 and obtained stress-strain (R-e) curves for states of analysed alloy are shown in Figure 12.  6 Advances in Materials Science and Engineering e low characteristics of strength (yield strength and ultimate tensile strength) and ductility (elongation and reduction in area) resulted from the tensile test of as-cast alloy state.e e ect of ECAP technique on mechanical properties of the heattreated alloy is clear from the curves.In comparison with ascast alloy state, the yield strength (R p0.2 ) value of overaged alloy state slightly increased from 127 to 136 MPa, and tensile strength (R m ) of alloy decreased from 219 to 208 MPa.Pre-ECAP heat treatment to overaged alloy state also led to the increase of ductile characteristics in comparison with as-cast alloy state.e value of tensile elongation (A) increased from 10.1% in the as-cast alloy state to 17.1% in overaged alloy state and the value of reduction of area (Z) increased nearly twice from 14.6 to 28.2%.e increase in the yield strength value at 135% and tensile strength value at 60% of analysed alloy was achieved in comparison with overaged alloy state by ECAP processing at room temperature.e slight decrease occurred in tensile elongation (to 14.5%) and reduction of area (to 21.5%).However, signi cant decrease of uniform tensile elongation (A g ) occurred from 7.6 to 1.8%.e AlSi7MgCu0.5 alloy in the as-cast state indicated microhardness HV0.2 of 72.2. e heat treatment of analysed alloy to overaged state led to the slight decrease in microhardness to 69.9 and after 4 ECAP passes, the alloy showed value of 110.7 that was of 53% higher value than ascast alloy state.

Discussion
e as-cast alloy state with heterogeneous dendritic structure was an initial state for the evaluation of the e ect of the ECAP technique on the structure and mechanical properties of AlSi7MgCu0.5 alloy.e as-cast structure consisted of the solid solution dendrites, eutectic Si-particles, and the particles of intermetallic phases that are typical for silumines of this chemical composition [3].e analyses of phases in the alloy as-cast structure, realized by hard X-ray di raction, con rmed the presence of major phases Al (α-solid solution) and Si (eutectic particles) and minor phases intermetallic Q-Al 4 Mg 8 Si 7 Cu 2 , π(Al 8 FeMg 3 Si 6 ), β(Mg 2 Si), and α-Al 12 (Fe, Mn) 3 Si and/or α-Al 15 (Fe,Mn) 3 Si 2 phases.e position of the maximum intensities of α-Al 12 (Fe,Mn) 3 Si and α-Al 15 (Fe, Mn) 3 Si 2 phases corresponded to the same di raction angle 2θ in the di raction patterns compared to the measured di raction data with the slight deviations.ese small deviations were induced by the change in the lattice parameter through the substitution of Fe and Mn atoms in the lattice of above mentioned phases [10].e Q-Al 4 Mg 8 Si 7 Cu 2 phase corresponded to the Q-Al 4 Mg 5 Si 4 Cu and also to the Q-Al 5 Mg 8 Si 6 Cu 2 phase that often occur in the microstructure of this type of alloys [11][12][13], but the Q-Al 4 Mg 8 Si 7 Cu 2 phase was clearly con rmed in the structure of analysed alloy.e average size of eutectic Si particles in the as-cast alloy state was relatively low (d 0.5 μm), and the value of their number per unit area was high (n 21.3 × 10 4 mm −2 ).
e eutectic Si particles in this alloy state were brous and had coral-like morphology common for hypoeutectic modi ed silumines [14,15].e intermetallic Q-Al 4 Mg 8 Si 7 Cu 2 phase particles of plate-like morphology, π(Al 8 FeMg 3 Si 6 ) and β(Mg 2 Si) phases of script-like morphology, and α-Al 12 (Fe,Mn) 3 Si and/or α-Al 15 (Fe,Mn) 3 Si 2 rod-like morphology present in microstructure of alloy were also observed in the works of many authors [13,16].e average size of intermetallic particles was 1.9 μm, and their number per unit area was 0.31 × 10 4 mm −2 .e particles of intermetallic phases enriched with Fe and/or Mn in the structure of Al-Si alloys are considered as impurities, and their increased content in the structure reduces the values of strength characteristics, ductility, and toughness of these alloys [3,17].e e ect of the as-cast heterogeneous structure of this type alloy and unfavourable morphology of the particles of intermetallic phases on the level of their strength, ductility, and hardness was also investigated by others [18,19].
Subsequently, the as-cast alloy was heat treated before application of the ECAP technique to increase its plasticity.Increased alloy plasticity enabled pressing the alloy billets by maximum number of their passes through channels of ECAP die and thus maximizing the level of their mechanical properties.e analysed alloy was heat treated to overaged state through the combination of optimized solution annealing at 823 K for 4 hours, water-quenching, and optimized arti cial ageing at 573 K for 5 hours.
e spheroidization and signi cant coarsening of eutectic Si particles which occurred during solution annealing and moreover dissolution of the intermetallic phase particles and their morphology changes were also observed by many authors Advances in Materials Science and Engineering [3,13,18].Alloy annealing process led to the dissolution and/or fragmentation of rod-like Si particles into smaller segments due to reduction of the surface tension of these particles that subsequently spheroidized and through the effect of annealing temperature coarsened by diffuse growth [3,19].e average size of eutectic Si particles increased six times up to 3.0 µm and their number per unit area decreased from 21.3 to 1.0 × 10 4 mm −2 during heat treatment of analysed alloy before ECAP.e comparison of X-ray diffraction patterns of overaged and as-cast alloy state showed that the dissolution of intermetallic π(Al 8 FeMg 3 Si 6 ) phase particles and slight increase in content of intermetallic α-Al 12 (Fe, Mn) 3 Si or α-Al 15 (Fe,Mn) 3 Si 2 phase particles occurred during solution annealing and artificial ageing of alloy.ere was no change in the average size of intermetallic phase particles (2.0 µm) in comparison with as-cast alloy state, yet the value of number per unit area significantly decreased by about 70% to 0.09 × 10 4 mm −2 .e significant increase in content of Q-Al 4 Mg 8 Si 7 Cu 2 phase and slight increase of β(Mg 2 Si) phase in comparison with as-cast alloy state was observed from X-ray diffraction patterns.e presence of these phases in the overaged alloy structure was also confirmed in the work of Farkoosh et al. [13].However, it is possible to assume that both these phases were dissolved during the solution annealing of alloy and then during artificial ageing, they precipitated from solid solution as incoherent particles [13,20].e selected area electron diffraction confirmed that the precipitation of incoherent particles of β(Mg 2 Si), Q-Al 4 Mg 5 Si 4 Cu, Al x Fe y Si z , and Si from solid solution occurred during the artificial ageing of analysed alloy.eir average size was 114 nm, and number per unit area was 3.5 × 10 6 mm −2 .
ese particles were evenly distributed in solid solution of the analysed alloy.e d-spacing values of Q-Al 4 Mg 5 Si 4 Cu phase confirmed by SAED and of Q-Al 4 Mg 8 Si 7 Cu 2 phase confirmed by X-ray diffraction were coincided with tolerance of 0.001 nm, but more precise analysis confirmed the presence of Q-Al 4 Mg 5 Si 4 Cu.e phase of Al x Fe y Si z analysed by SAED can be regarded as the intermetallic phase of Al 12 (Fe,Mn) 3 Si and/or α-Al 15 (Fe,Mn) 3 Si 2 , and the presence of which was confirmed by X-ray diffraction.e significant increase in the plasticity of alloy occurred after application of heat treatment which was also investigated in the work of Moradi et al. [18].
e tensile elongation of alloy in the overaged state was increased 1.7 times (to 17.1%) in comparison with the as-cast alloy state, and furthermore, the strength of alloy did not decrease.e increase of ductility occurred due to the removal of unfavourable morphology of particles in the alloy structure by spheroidization of eutectic Si particles and dissolution of intermetallic phase particles.e uniform precipitation of fine incoherent particles from alloy solid solution during the artificial ageing compensated the decline of strengthening of alloy caused by coarsening of eutectic Si particles and provided almost the same level of alloy yield strength and tensile strength (the change in the range of 10 MPa) in comparison with the as-cast alloy state.
After the application of pre-ECAP heat treatment, the severe plastic deformation of alloy by ECAP at room temperature was carried out.Correctly chosen conditions of severe plastic deformation had a very favourable effect on the mechanical properties of foundry alloys, as mentioned in the work of others [8,[21][22][23].e experiments, which were the subject of this work, confirmed these findings for AlSi7MgCu0.5 alloy and additionally demonstrated the importance of the pre-ECAP heat treatment before severe plastic deformation.Severe plastic deformation of analysed alloy by the ECAP technique at room temperature after heat treatment of alloy significantly changed the character of its microstructure.e fragmentation and redistribution of the eutectic Si particles, particles of intermetallic phases, and particles of precipitates to homogeneous form occurred.Moreover, ultrafine grained alloy structure was formed, which led to increase in strength and plasticity of alloy, as it was reported in works [18,23].
e redistribution of Si particles, confirmed by analyses of microstructure of alloy, was result of repetitive severe plastic deformation by simple shear of billet in the corner of ECAP die channels.e heterogeneous dendritic structure was successfully removed in the X-plane and Y-plane of the pressed billet, yet the significant heterogeneity of arrangement of Si-particles was retained in the Z-plane of the billet.is difference in the billet planes was a result of the mechanism of deformation by the chosen route A, as discussed in detail in many works [8,23].e fragmentation of eutectic Si particles induced by a high degree of deformation reflected in a slight decrease in the average size of Si particles evaluated in the X-plane (from 3.0 to 2.5 μm) and a slight increase in the number per unit area at a half in comparison with overaged alloy state.e decrease in average size of intermetallic phase particles in the structure of alloy after ECAP (from 2.0 to 1.6 μm) and double increase in their number per unit area, decrease in average size of precipitated particles (from 114 to 77 nm), and double increase of their number per unit area in comparison with overaged alloy state were also results of the fragmentation.e fragmentation of the particles present in the structure of Al-Si alloys after their ECAP processing was also reported in many works [18,21,[23][24][25][26]. Analyses of phases in the microstructure of alloy after ECAP by X-ray diffraction confirmed the presence of minor phase of the same chemical composition as in overaged alloy state before ECAP.In the deformed alloy microstructure, the minor α-Al 15 (Fe,Mn) 3 Si 2 and/or α-Al 12 (Fe,Mn) 3 Si, β(Mg 2 Si) and Q-Al 4 Mg 8 Si 7 Cu 2 phases were confirmed.In the solid solution of the analysed alloy after ECAP, the strong preferred orientation of the matrix was observed through the dependence between intensity of (111) reflection of α(Al) solid solution of ECAPed alloy and azimuthal angle of the Debye-Scherrer ring.Preferential orientation was also observed in the case of AlSi7 alloy after ECAP in the work of García-Infanta et al. [8].e application of ECAP led to the formation of ultrafine grained structure of solid solution of alloy.
e elongated grains and/or subgrains with high dislocation density were observed by TEM, and grains and/or subgrains were separated mainly by nonequilibrium, wavy, and curved boundaries, as observed in the works of others [24,26].ese grains and/or subgrains of alloy solid solution were separated by HAGBs and LAGBs with a significant degree of texture, what was confirmed by SAED.

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Advances in Materials Science and Engineering e average width of grains and/or subgrains was on level of 0.2 µm and length of 0.65 µm.ese values respond to average width and length of grains and/or subgrains (0.23 µm and 0.58 µm, resp.) of ECAPed AlSi7 alloy evaluated in the work of Gutierrez-Urrutia et al. [24].Based on EBSD results, it is clear that the size of deformed grains and/or subgrains was different due to the presence of eutectic Si particles in the structure of alloy.e elongated subgrains of solid solution were observed away from eutectic Si particles.e subgrains analysed using TEM and SAED confirmed that they were separated by LAGBs.
e equiaxed grains of deformed solid solution with HAGBs were identified by SAED in the areas close to eutectic Si particles, which are also observed in ECAPed silumines in the works of others [18,22,24,25].e average size of the fine equiaxed grains of alloy solid solution after ECAP was 0.6 µm.
eir size corresponds to the average length of elongated subgrains of solid solution in the areas away from Si particles.ese grains of solid solution close to Si particles acquired the equiaxed shape due to the higher degree of the plastic deformation in these areas in comparison with the areas of solid solution away from Si particles.e higher intensity of deformation led to cumulation of dislocation around coarse Si particles and the process of dynamic recovery of structure in these areas [19,25].
us, the submicroscopic heterogeneity of the distribution of the eutectic Si particles led to a heterogeneous refinement of solid solution, which consists of the formation of deformation areas with elongated grains and/or subgrains and areas with equiaxed grains.e application of the ECAP technique led to the significant increase in the strength of overaged alloy.e increase in the yield strength of analysed alloy was more significant than the increase in its tensile strength.e yield strength of the alloy increased by about 135% (to 319 MPa), and the tensile strength increased by about 60% (to 332 MPa).After ECAP, the values of tensile elongation and the area decreased in comparison with overaged alloy state, but were still higher than in the as-cast alloy state.From Figure 12, the change of character of stress-strain curves of alloy after ECAP is clear.is curve shape is typical for aluminium alloys after severe plastic deformation [27].e alloy processed by ECAP at room temperature was characterized by a low value of the uniform tensile elongation A g � 1.8% (compared to the 8.9% and 7.6% in as-cast and overaged state of alloy, resp.) and a high value of the ratio R p0.2 /R m � 0.96, what was a result of strain hardening of severely deformed solid solution of alloy at room temperature.e overall increase in the strength and plasticity of alloy after ECAP was a result of strain hardening of solid solution, hardening of grains and/or subgrains boundaries, redistribution, homogenization and fragmentation of eutectic Si-particles, particles of intermetallic phases, and precipitates in solid solution of analysed alloy [22][23][24]28].

Conclusions
Severe plastic deformation by the ECAP technique at room temperature in combination with pre-ECAP heat treatment of foundry heat-treatable AlSi7MgCu0.5 alloy led to a significant improvement of its mechanical properties through the homogenization and refinement of structure.Realized experiments and analyses and their evaluation and discussion with a knowledge from the technical literature led to these conclusions: (1) e α(Al) solid solution in dendritic form and eutecticum in form of eutectic Si particles and solid solution were the major phases in the as-cast alloy structure, and intermetallic phases of Q(Al (3) e application of pre-ECAP heat treatment to overaged alloy state led to the significant increase in plasticity of the alloy without decrease in the alloy strength.(4) e ECAP at room temperature of analysed alloy led to the homogenization of its microstructure through the fragmentation and the redistribution of eutectic Si particles, intermetallic phases and particles of precipitates, and formed ultrafine grained structure of alloy.e elongated grains and/or subgrains of solid solution (width of 0.2 µm, length of 0.65 µm) were formed in the areas distant from eutectic Si particles, and due to a higher degree of plastic deformation in areas close to Si-particles, the formation of equiaxed grains (0.6 µm) of solid solution occurred separated mostly by HAGBs.(5) e ECAP at room temperature led to the significant increase in strength and ductility of alloy in comparison with the as-cast state.e yield strength and tensile strength of alloy increased to 319 MPa and 332 MPa, respectively.e tensile elongation and reduction of area increased to 14.5% and 21.5%, respectively.e alloy microhardness HV0.2 increased to 110.7.e above-mentioned strengthening and improvement of the ductility were achieved due to the positive changes of microstructure after heat treatment and ECAP processing of alloy at room temperature.

Data Availability
e results of the research are discussed and compared with the results published in the reviewed articles and books listed in References.ese articles and books can be considered as data supporting results.Many of these articles are available online on journals website and expert articles databases.

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Advances in Materials Science and Engineering (Figure 3(b)).

Figure 2 :
Figure 2: As-cast microstructure of AlSi7MgCu0.5 alloy observed by (a) LM after etching and (b) SEM after deep etching.

Figure 4 :
Figure 4: Microstructure of AlSi7MgCu0.5 alloy in overaged state observed by (a) LM after etching and (b) SEM after deep etching.

3. 3 .
Microstructure of Alloy after ECAP Processing.ECAP processing led to the signi cant microstructure change of heattreated AlSi7MgCu0.5 alloy state.e microstructure of this state after 4 passes of billet through equal channel at room temperature in X, Y, and Z planes are shown in Figures 7(a), 7(c), and 7(e).
) and 7(d).e average width of the grains and/or subgrains in the X-plane of pressed billet solid solution was 0.2 µm, and the length was 0.65 µm.e SAED (Figures 7(b), 7(d), and 7(f )) indicated that elongated grains and/or subgrains with preferred orientation (texture) separated by a low angle grain boundaries (LAGBs) and/or high angle grain boundaries (HAGBs) were present in the alloy substructure.e cellular dislocation substructure of deformed AlSi7MgCu0.5 in the Zplane of pressed billet is clear from Figure7(f).Figure10shows

Figure 7 :
Figure 7: Microstructures and substructures with SAED of AlSi7MgCu0.5 alloy after ECAP observed by (a) LM in X-plane, (b) TEM in X-plane, (c) LM in Y-plane, (d) TEM in Y-plane, (e) LM in Z-plane, and (f) TEM in Z-plane.
5 21.3 × 10 4 1.9 0.31 × 10 4 --Overaged 3.0 1.0 × 10 4 2.0 0.09 × 10 4 114 3.5 × 10 6 ECAPed 2.5 1.5 × 10 4 1.6 0.18 × 10 4 77 8.1 × 10 6the character of grain and/or subgrain boundaries of solid solution.e grains and/or subgrains of solid solution, with HAGBs and LAGBs observed in ECAPed alloy state, are shown in Figure11.e size and distribution of these grains and/or subgrains were uneven due to the presence of eutectic Si particles in the structure of alloy.It is clear that elongated subgrains with LAGBs were present in the substructure of alloy in the areas distant from eutectic Si particles.On the contrary, ner equiaxed grains with HAGBs were found close to the Si particles.