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Article

Microstructure and Mechanical Property of Al6Si2Cu Alloy Subjected to Double-Solution Heat Treatment

Department of Advanced Materials Science and Engineering, Chosun University, Gwangju 501-759, Korea
*
Author to whom correspondence should be addressed.
Metals 2022, 12(1), 18; https://doi.org/10.3390/met12010018
Submission received: 8 November 2021 / Revised: 6 December 2021 / Accepted: 15 December 2021 / Published: 22 December 2021

Abstract

:
This study aims to develop the mechanical properties of the Al6Si2Cu aluminum alloy through the double-solution treatment. In addition to the Al matrix, large amounts of coarse eutectic Si, Al2Cu intermetallic, and Fe-rich phases were generated through thermo-calc simulation in agreement with the equilibrium phases. The eutectic Si phase is fragmented and spheroidized by the solution treatment as the heat treatment temperature and time increase. The Al2Cu intermetallic phase is dissolved into the Al matrix, resulting in an increase in both strength and elongation. The second-step solution temperature at 525 °C should be an optimum condition for enhancing the mechanical properties of the Al6Si2Cu aluminum alloy.

1. Introduction

Environmental problems, such as fossil fuel exhaustion, global warming, and air pollution, require specific tolerance standards for CO2 emissions or vehicle fuel consumption in the automobile industry [1,2]. There is an urgent need to study the weight reduction of automobiles that can reduce harmful gas emission and improve fuel efficiency in accordance with these social demands. Effective automobile weight reduction is more related to materials than structure design. For a long time, aluminum alloys have been studied as a lightweight material and widely applied as a substitute material. AlSiCu alloys have recently been used in cylinder blocks, cylinder heads, engine mount brackets, etc., bedue to their excellent mechanical properties and castability [3,4,5,6]. In general, the eutectic Si and Al2Cu phases of AlSiCu alloys are crystallized as coarse needles and coarse plates, respectively. When an external force is applied, a fracture can occur due to the stress concentration, which may restrict material usage [7].
Therefore, the alloy microstructure must be modified. To do this, the content of the alloying elements and the heat treatment process must be controlled. The heat treatment process technology for improving strength and elongation at the same time has yet to be well established, and many studies are needed. The single-solution heat treatment is normally limited to approximately 495 °C, since a higher temperature leads to the incipient melting of the copper-rich phase [8,9,10]. However, the single-solution heat treatment at temperatures of 495 °C or less cannot maximize the dissolution of Cu-rich phases, nor sufficiently modify the silicon particle morphology [11]. Therefore, the heat treatment duration is long, and modified elements, such as Na and Sr, must be added. These disadvantages make the AlSiCu alloys impractical for use in industry. To compensate for these disadvantages, many investigators [12,13,14] have tried to utilize a solution heat treatment temperature higher than 495 °C. Previous studies reported the double-solution heat treatment in the range of 480–495 °C for the first step and 515–530 °C for the second step in A319 and A332 alloys. The double-solution treatment process reduces the Cu-rich phase, yielding better ductility and strength compared to the single-solution heat treatment, and a better homogenization effect before aging heat treatment.
The present study investigates the microstructural and mechanical properties of Al6Si2Cu alloy that undergoes the double-solution heat treatment.

2. Materials and Methods

The investigated Al6Si2Cu alloys were prepared by gravity cast into ingots (670 mm × 100 mm × 40 mm) to evaluate their microstructure and mechanical properties before and after heat treatment. The alloy composition was analyzed through inductively coupled plasma mass spectrometry (ICP-MS) (OPTIMA 4300 DV, Perkin Elmer, Wellesley, MA, USA). The chemical composition was 6.01Si, 2.09Cu, 1.03Fe, 0.19Mn, and Al balance. Table 1 presents the first and second-step solution heat treatments applied to the Al6Si2Cu alloys. The solution temperature was carefully set to avoid the initial melting of the Al2Cu phase. The first-step solution temperature was 495 °C below the melting temperature of the Al2Cu phase. The second-step solution was heat-treated to 515 °C and 525 °C above the melting temperature of the Al2Cu phase to prevent incipient melting.
For the microstructure analysis, the specimens were observed using an optical microscope (OM) (AXIO, ZEISS, Oberkochen, Land Baden-Württemberg, Germany) after etching using Keller’s solution (1.25 mL nitric acid + 0.75 mL hydrochloric acid + 0.5 mL hydrofluoric acid + 47.5 mL distilled water). For a more precise investigation, several phases in the matrix were observed and analyzed through scanning electron microscopy (SEM) (DE/SUPRA 40VP, ZEISS, Oberkochen, Land Baden-Württemberg, Germany), energy-dispersive spectroscopy (EDS) (Apollo SDD, EDAX, Mahwah, NJ, USA), and electron probe micro analysis (EPMA) (Shimadzu, EPMA-1600, Kyoto, Japan). X-ray diffraction (XRD) (Rigaku, SmartLab X-ray diffractometer, Tokyo, Japan) was performed for the crystal structure analysis. The 2θ analysis was conducted from 30° to 50° using CuKα. The step size was 0.01°, and the scan step time was 1 s. The hardness test for the evaluation of the mechanical properties was performed using a microhardness tester (Micro Vickers hardness Tester) (Shimadzu, HMV-G 21ST, Kyoto, Japan), and measured 20 times for each specimen at 5 s holding time with 1 kg load. The tensile test specimens were prepared in the form of a plate with a parallel portion 16.5 mm length, 5 mm width, and 3 mm thickness. A tensile tester (Table-top precision universal tester) (Shimadzu, AGS-20kNX, Kyoto, Japan) was used at 1 mm/min strain rate at room temperature.

3. Results and Discussion

3.1. Microstructure

Figure 1 shows the microscopic observation of the surface microstructure of the as-cast specimen. The microstructure of the cast material depicted a typical dendrite structure. The secondary dendrite arm spacing measured by an image analyzer (I-Solution) (IMT i-Solution ver.11, Vancouver, BC, Canada) was 40 µm. The Al6Si2Cu alloys had two major Fe–Si intermetallic phases: α-Al15(Fe, Mn)3Si2, which is known as the α-Fe phase, and β-Al5FeSi, which is known as the β-Fe phase. The α-Al15(Fe, Mn)3Si2 phase had a dense form and did not cause crack formation in the casting process. In addition, the composition and shape may change depending on the solution conditions. On the contrary, the β-Al5FeSi phase had a morphologically needle-shape microstructure. The β-Fe phase was brittle, and became a factor of lowering the mechanical properties of the cast material.
Figure 2 presents the backscattered electron (BSE) photographs of the gravity casting (as-cast) specimen and T44A-DS8A(first step solution heat treatment: 495 °C 4h, second step solution heat treatment: 515 °C 8 h specimen). Figure 2a,c illustrate the four phases, that is, the Chinese-script shape α-Al15(Fe, Mn)3Si2 phase, the needle-shape β-Al5FeSi phase, the plate-shape θ-Al2Cu, and the eutectic Si phase. BSEs are beam electrons reflected from the sample by elastic scattering. The BSE signal is strongly related to the atomic number (Z) of the specimen. Typically, heavier elements can more strongly deflect incident electrons compared to lighter elements due to their larger nuclei. More backscattered electrons were emitted from the sample surface; hence, heavy elements such as Cu and Fe, which had atomic numbers of Z = 29 and Z = 26, respectively, appeared bright in an SEM image compared to lighter elements, such as aluminum (Z = 13) and silicon (Z = 14). The EDS analysis of each phase was then performed. Table 2 presents the results, which were consistent with those of the α-Al15(Fe, Mn)3Si2 and β-Al5FeSi EDS analyses reported by Ceschini et al. [15]. Figure 2b,d depict enlarged images of θ-Al2Cu. In the as-cast specimens, θ-Al2Cu existed in coarse form, but segmented and dissolved after the solid solution treatment. These microstructure observations showed no evidence of incipient melting phenomena, despite the second-step solution temperature being higher than the melting temperature of the Al2Cu phase.
Figure 3 shows the morphology of the θ-Al2Cu phase for each solution treatment condition. The coarse θ-Al2Cu phase of the as-cast ingot generally incurred the incipient melting in the Al matrix when heat-treated above 520 °C. This defect was caused by the simultaneous decrease of the strength and ductility of the aluminum alloy. This study solves the abovementioned problem on heat treatment by using the double-solution heat treatment method before and after the melting point of the θ-Al2Cu phase. In the first-step solution heat treatment, many impurity elements in the microstructure were redissolved into the Al matrix, and the θ-Al2Cu phase was partially dissolved, as shown in Figure 3, contributing to the solid solution hardening effect. In the second-step heat treatment, the coarse form of the θ-Al2Cu phase became more fragmented and finer, and dissolved as the temperature and time of the solution treatment increased as shown in Figure 3d,g. Therefore, defects (e.g., pores) caused by incipient melting were not observed.
Figure 4 shows the results of the EPMA analysis of each phase of the as-cast specimen. The elemental distributions of Al, Cu, Fe, Mn, and Si in the matrix are also presented. The BSE micrographs present α-Al15(Fe, Mn)3Si2, β-Al5FeSi, θ-Al2Cu, and eutectic Si. Fe and Mn were concentrated in the Chinese-script-shaped α-Fe phase, while Fe and Si were distributed in the needle-shape β-Fe phase.
Figure 5 depicts the equilibrium phase of the Al6Si2Cu alloy by thermodynamic calculations. The thermodynamic calculation results showed that the Al15(Fe, Mn)3Si2 and β-Al5FeSi phases existed in the solution treatment temperature range. In addition, the melting temperature of θ-Al2Cu, which was the basis for the first- and second-step solution temperatures herein, was approximately 510°.
Figure 6 displays the results of the microscopic observation of the microstructure changes, such as Fe-rich phase and Si particle according to the as-cast and solution treatment conditions. In general, as the heat treatment temperature and time increased, the average area of the Si particles decreased, and the aspect ratio increased, as clearly shown in the phase micrographs. The Si particle changed its atomic position by diffusing on the surface, leaving the silicon lattice by interdiffusion, and migrating through aluminum at the Al–Si interface in the phase boundary [16,17]. These diffusions were active above 500 °C, which was consistent with the equilibrium phase diagram in Figure 5. The Si particles were spheroidized from the edge by diffusion when the heat treatment temperature was higher than 500 °C.
Table 3 shows the quantitative evaluation results of the Si phase after the solution treatment, which were measured by an image analyzer (I-Solution) (IMT i-Solution ver.11, Vancouver, BC, Canada), showing the mean area of the Si particles, aspect ratio, and increase in the aspect ratio compared with those of the as-cast sample value. The aspect ratio of silicon particles was image analyzed using the image recognition function of i-solution software(I-Solution) (IMT i-Solution ver.11, Vancouver, BC, Canada). The aspect ratio is the ratio of width to height, and the software automatically recognizes the image of dark Si particles that are distinct from the Al matrix and Fe-rich phase. The average value was measured by calculating the ratio of horizontal and vertical pixels of the recognized Si particle image. The mean area of the eutectic Si phase was decreased by the solution treatment, and depended on temperature and time. The aspect ratio of the eutectic Si particles increased by approximately 130% in T44A and T44B, compared to those in the as-cast specimen. That of DS8A increased by approximately 60% compared to that in the first-step solution treatment, while that in DS8B increased by more than 100%. The shape of the brittle Si phase in the aluminum alloy was spheroidized; thus, the elongation and the toughness of this Al6Si2Cu alloy were thought to have improved, resulting in the enhancement of both ductility and fatigue strength.

3.2. XRD Analysis

Figure 7 illustrates the diffraction peaks of Si, Al, and θ-Al2Cu. The θ-Al2Cu diffraction peaks were observed at 2θ = 42.04 (220), 2θ = 43.04 (112), and 2θ = 47.28 (310). The diffraction peaks of the (220) and (112) planes of the Al2Cu intermetallic phase in the as-cast specimen were clearly observed before the solution heat treatment. However, these diffraction peaks became weak and disappeared from the solution specimen, T44A-DS8A. The Al2Cu phase was usually dissolved into the Al matrix during the solid solution treatment (Figure 3). The Al2Cu phase dissolution in the matrix may lead to a supersaturation of the Cu atoms into the Al lattice. This is enough to deform the Al lattice, causing an increase in the mechanical strength of the Al6Si2Cu aluminum alloy.

3.3. Mechanical Properties

Figure 8 shows the results of the micro-Vickers hardness test of the heat-treated Al6Si2Cu alloy with each load (i.e., 19.61 N and 245 mN). The alloy hardness after the heat treatment increased by approximately 30% compared with that of the as-cast specimen, since the coarse θ-Al2Cu particles that precipitated in the ingot did not contribute to the precipitation hardening. It is, however, thought that the hardness increased due to the solid solution hardening effect, as the Cu atoms were dissolved in the matrix after the solution treatment. As shown in Figure 8a, the indenter size was approximately 60 µm when the load was 19.61 N. In other words, hardness depended on several intermetallic and Si phases, as well as on the Al matrix. The intermetallic and eutectic Si phases and the Al matrix were measured at the same time. The hardness of the first- and second-step solution-treated specimens was higher than that of the as-cast specimen. Figure 8b shows the measured Al matrix hardness depicting that the hardness of the first- and second-step solution-treated specimens significantly increased.
Figure 9 depicts the tensile test results obtained at various solution heat treatments showing the mechanical properties (e.g., UTS, YS, and elongation) at each solution treatment. The mechanical strength after the second-step solution heat treatment increased the ultimate tensile strength from 185 MPa to 248 MPa, the yield strength from 152 MPa to 181 MPa, and the elongation from 1.36% to 2.65% compared with the as-cast specimen. Figure 9b shows the typical flow curves of as-cast, T44A-DS8B, and T44B-DA8B samples. The tensile strength and elongation of T44B-DA8B sample is higher than that of the as-cast and T44A-DS8B samples. These results are attributed to the Cu atoms being dissolved into the Al matrix without defect by the double-solution heat treatment, which contributed to the solid solution hardening, spheroidized shape of the brittle Si phase, and improved alloy elongation and toughness.

4. Conclusions

This study presents the double-solution heat treatment on the microstructure and mechanical properties of the Al6Si2Cu alloys. The following conclusions are drawn:
1.
The microstructure of the gravity-casted Al6Si2Cu alloys was investigated. The Chinese-script shape α-Al15(Fe, Mn)3Si2, β-Al5FeSi phase, and θ-Al2Cu and eutectic Si phases were observed and analyzed in agreement with the thermodynamically calculated equilibrium phase diagram.
2.
The XRD analysis depicted that the diffraction peaks of the (220) and (112) plane of the Al2Cu phase were observed in the gravity-cast specimens, but were not found in the solution treatment due to the Al2Cu phase dissolution into the Al matrix.
3.
The double-solution heat treatment process was enough to dissolve the θ-Al2Cu phase into the Al matrix without leaving any defects (e.g., pores) caused by the incipient melting of the θ-Al2Cu phase.
4.
As the heat treatment temperature and time increased, the Si particles were spheroidized; the average area of the Si particles decreased by approximately 56%; and the aspect ratio increased by approximately 418%.
5.
The mechanical properties increased after the double-solution heat treatment. The ultimate tensile strength and elongation of the T44B-DS8B specimen increased by up to 34% and 95%, respectively.

Author Contributions

Conceptualization, C.K.; methodology, C.K., S.A., M.K. and C.H.; software, S.A. and M.K.; validation, C.K. and S.A.; formal analysis, S.A. and C.H.; investigation, C.K. and S.A.; data curation, C.H. and S.A.; writing—original draft preparation, S.A.; writing—review and editing, S.A. and C.K.; visualization, S.A. and M.K.; supervision, C.K.; project administration, C.K.; funding acquisition, C.K. This paper was prepared the contributions of all authors. All authors have read and agreed to the published version of the manuscript.

Funding

This research was funded by Chosun University (2020).

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Not applicable.

Acknowledgments

This study was supported by a research fund from Chosun University (2020).

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. Optical micrograph of the as-cast Al6Si2Cu alloy showing the typical dendrite microstructure of the gravity casting process.
Figure 1. Optical micrograph of the as-cast Al6Si2Cu alloy showing the typical dendrite microstructure of the gravity casting process.
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Figure 2. Microstructural observation of the Al6Si2Cu alloy: (a) BSE(backscatter electron) micrograph showing various as-cast phases; (b) BSE micrograph showing the Al2Cu and Si phases of as-cast; (c) BSE micrograph showing various T44A-DS8A phases; and (d) BSE micrograph showing the Al2Cu and Si phases of T44A-DS8A.
Figure 2. Microstructural observation of the Al6Si2Cu alloy: (a) BSE(backscatter electron) micrograph showing various as-cast phases; (b) BSE micrograph showing the Al2Cu and Si phases of as-cast; (c) BSE micrograph showing various T44A-DS8A phases; and (d) BSE micrograph showing the Al2Cu and Si phases of T44A-DS8A.
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Figure 3. BSE micrographs of the Al6Si2Cu alloy showing dissolution of Al2Cu phase: (a) coarse Al2Cu phase in as-cast sample, (b) T44A, (c) T44A-DS8A, (d) T44A-DS8B, (e) T44B, (f) T44B-DS8A, and (g) T44B-DS8B.
Figure 3. BSE micrographs of the Al6Si2Cu alloy showing dissolution of Al2Cu phase: (a) coarse Al2Cu phase in as-cast sample, (b) T44A, (c) T44A-DS8A, (d) T44A-DS8B, (e) T44B, (f) T44B-DS8A, and (g) T44B-DS8B.
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Figure 4. EPMA analysis of the as-cast Al6Si2Cu alloy (wt.%): (a) as-cast, (b) Al, (c) Cu, (d) Fe, (e) Mn, (f) Si.
Figure 4. EPMA analysis of the as-cast Al6Si2Cu alloy (wt.%): (a) as-cast, (b) Al, (c) Cu, (d) Fe, (e) Mn, (f) Si.
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Figure 5. Mass–fraction of the equilibrium phase diagram of the Al6Si2Cu alloy computed through thermo-calc calculation showing the α and β Fe-rich phase, Cu-rich phase, and Si phase.
Figure 5. Mass–fraction of the equilibrium phase diagram of the Al6Si2Cu alloy computed through thermo-calc calculation showing the α and β Fe-rich phase, Cu-rich phase, and Si phase.
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Figure 6. Microstructure of the Al6Si2Cu alloys after different solution treatments: (a) as-cast; (b) T44A; (c) T44A-DS8A; (d) T44A-DS8B; (e) T44B; (f) T44B-DS8A; and (g) T44B-DS8B.
Figure 6. Microstructure of the Al6Si2Cu alloys after different solution treatments: (a) as-cast; (b) T44A; (c) T44A-DS8A; (d) T44A-DS8B; (e) T44B; (f) T44B-DS8A; and (g) T44B-DS8B.
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Figure 7. XRD (X-ray diffraction) profiles of the Al6Si2Cu alloy showing the diffraction peaks of the typical solution treatment.
Figure 7. XRD (X-ray diffraction) profiles of the Al6Si2Cu alloy showing the diffraction peaks of the typical solution treatment.
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Figure 8. Micro-Vickers hardness of the alloys after various solution treatment schedules: (a) hardness for 2 kg load and (b) hardness of the Al matrix for 25 g load.
Figure 8. Micro-Vickers hardness of the alloys after various solution treatment schedules: (a) hardness for 2 kg load and (b) hardness of the Al matrix for 25 g load.
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Figure 9. Tensile properties of the alloys after various solution treatments: (a) mechanical data at each heat treatment condition; UTS (ultimate tensile strength) elongation, YS (yeild strength) and (b) flow curves of typical sample condition.
Figure 9. Tensile properties of the alloys after various solution treatments: (a) mechanical data at each heat treatment condition; UTS (ultimate tensile strength) elongation, YS (yeild strength) and (b) flow curves of typical sample condition.
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Table 1. Schedule of the double-solution heat treatment.
Table 1. Schedule of the double-solution heat treatment.
SpecimenSolution
First StepSecond StepQuenching
°Ch°Ch
As-cast-----
T44A4854--Water
T44A-DS8A48545158Water
T44A-DS8B48545258Water
T44B4954--Water
T44B-DS8A49545158Water
T44B-DS8B49545258Water
Table 2. Chemical compositions of the main intermetallic phases in the as-cast Al6Si2Cu alloy (wt.%).
Table 2. Chemical compositions of the main intermetallic phases in the as-cast Al6Si2Cu alloy (wt.%).
PhaseSiCuFeMnAlPoint
α10.7-22.08.656.6Al15(Fe, Mn)3Si2
β17.5-23.12.656.6Al5FeSi
Si93.6---6.3Si
θ-51.3--48.6Al2Cu
Table 3. Silicon particle characteristic of the alloy after the solution treatment.
Table 3. Silicon particle characteristic of the alloy after the solution treatment.
SpecimenAs-CastT44AT44A-DS8AT44A-DS8BT44BT44B-DS8AT44B-DS8B
Mean Area (um2)47.131.429.626.131.725.820.6
Aspect Ratio0.160.370.590.770.370.620.83
-130%↑268%↑381%↑130%↑287%↑418%↑
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An, S.; Kim, M.; Huh, C.; Kim, C. Microstructure and Mechanical Property of Al6Si2Cu Alloy Subjected to Double-Solution Heat Treatment. Metals 2022, 12, 18. https://doi.org/10.3390/met12010018

AMA Style

An S, Kim M, Huh C, Kim C. Microstructure and Mechanical Property of Al6Si2Cu Alloy Subjected to Double-Solution Heat Treatment. Metals. 2022; 12(1):18. https://doi.org/10.3390/met12010018

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An, Seongbin, Minsuk Kim, Chaeeul Huh, and Chungseok Kim. 2022. "Microstructure and Mechanical Property of Al6Si2Cu Alloy Subjected to Double-Solution Heat Treatment" Metals 12, no. 1: 18. https://doi.org/10.3390/met12010018

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