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Article

Effects of ErF3 Particles on the Structure and Physicomechanical Properties of A359 Alloy

1
Physics and Technology Faculty, National Research Tomsk State University, 634050 Tomsk, Russia
2
State Corporation for Assistance to Development, Production and Export of Advanced Technology Industrial Product «Rostec», 119991 Moscow, Russia
*
Author to whom correspondence should be addressed.
Metals 2023, 13(8), 1463; https://doi.org/10.3390/met13081463
Submission received: 10 May 2023 / Revised: 27 June 2023 / Accepted: 4 August 2023 / Published: 14 August 2023

Abstract

:
In this work, the impact of ErF3 submicroparticles on the microstructure and mechanical properties of the A359 alloy was studied. ErF3 particles provided a homogeneous structure in castings produced via the casting method. The modifying effect of ErF3 particles on the structure of Al–Si alloys is realized through the mechanism of restraining the crystallization front and is achieved through the reduction in the formation of clusters of iron phases and eutectic lamellar silicon. It was found that the addition of 1 wt% ErF3 to the A359 alloy leads to a decrease in the average grain size by 21% and an increase in the yield strength by 14%, in tensile strength by 16%, in the microhardness of Al15(FeMn)3Si2 phase by 34% and in the Al15(FeMnCr)3Si2 phase by 7%. The heat treatment of the A359 alloy with ErF3 particles increased the yield strength by 36% and the tensile strength by 34%. The absence of an effect of ErF3 particles on the hardness values of the A359 alloy, as well as on the fracture process of the A359 alloy, was observed. The negative influence of ErF3 particle agglomerates and clusters on the strength characteristics of the investigated alloys was observed. Approaches for further exploring the potential of ErF3 particles as a strengthening phase in cast aluminum alloys of the Al–Si system were proposed.

1. Introduction

Casting is a versatile method of industrial aluminum production, widely utilizing Al–Si alloys due to their high liquid fluidity and specific strength, coupled with low cost [1]. Despite the advantages of Al–Si alloys, there is a need to enhance the mechanical properties of cast aluminum alloys for weight reduction, increased reliability, and fuel efficiency in the designs of transportation vehicles, including cars and aviation. High mechanical properties in aluminum alloys are achieved through microalloying (up to 0.5 wt%) with scandium, which provides an increase in yield strength of up to 80% and tensile strength of up to 45% [2,3,4], through the modification of the grain structure [5] and through dispersion strengthening [6]. Due to the high cost of Sc in deformable Al–Mg alloys, its concentration is reduced by adding cheaper Zr [7,8,9,10,11,12,13]. However, the combination of Sc and Zr is not effective in Al–Si cast alloys [14], and the modifying effect of Sc is only revealed at high concentrations (up to 1 wt%) as part of it enters the composition of the silicon eutectic and the rest forms the AlSc2Si2 phase, which initiates the growth of needle-like iron-rich Al5FeSi phase [15,16,17]. Therefore, the addition of 0.4–0.8% Sc increases the yield strength by 8–20% and the ultimate tensile strength by 11–35% in both as-cast and heat-treated conditions [18,19,20].
Currently, various approaches are being developed for the alloying of Al–Si alloys and other cast aluminum alloys with rare-earth metals (REMs), such as zirconium [21,22], cerium [23], lanthanum [24], and erbium [25,26,27,28], with similar mechanisms to scandium that affect the strength properties of aluminum alloys. The most interesting one is the use of erbium due to its market price being 32 times lower than scandium and its ability to form an Al3Er phase that has similar parameters of a crystal lattice to aluminum [29]. This phase is expected to effectively refine the alloy structure by creating additional crystallization centers. Due to the differences in melting temperatures between aluminum (660 °C) and erbium (1529 °C), master alloys based on aluminum (typical for all REMs) are utilized for erbium’s introduction to alloys. These master alloys are produced via methods, such as the direct alloying or hydriding of REMs [30], using metallic erbium as a raw material. Erbium is found in natural minerals in the form of an oxide [31], which, through an intermediate compound of fluoride or chloride, is synthesized into metallic erbium.
However, it is possible to introduce ex situ micro- and nanoparticles into the metal melt to improve the mechanical properties of Al–Si alloys. Depending on their type and size, such particles can have a modifying [32], strengthening [33,34], or combined [35] effect on the structure and physicomechanical properties of aluminum–silicon alloys. Previous studies have shown positive effects of scandium fluoride particles on the mechanical properties of the A356 alloy [36], including simultaneous increases in yield strength, tensile strength, and ductility. These mechanical behavior characteristics are related to significant differences in physical characteristics (thermal conductivity, electrical conductivity, the coefficient of the thermal linear expansion (CTLE)) between the matrix and strengthening particles. The higher the degree of mismatch between the CTLE coefficients of the particles and matrix, the higher the density of geometrically forced dislocations formed around the particles during alloy crystallization [36]. The formed dislocations contribute to the increase in the strength properties of the alloy due to the entanglement of linear defects and the hindering of their movement under material loading. The CTLE of erbium fluoride (11 × 10−6 K−1 [37]) is half that of aluminum (23 × 10−6 K−1 [38]), which can positively affect the mechanical properties of Al–Si alloys. The use of erbium fluoride as a strengthening phase will allow the optimization of the technological process of obtaining high-strength alloys based on Al–Si, since erbium fluoride is an intermediate product in the production of metallic erbium (Figure 1). Thus, the aim of this work is to investigate the effect of erbium fluoride particles on the structure and physicomechanical properties of the aluminum alloy A359.

2. Materials and Methods

The production of AlErF3 master alloy. To produce erbium fluoride, an aqueous solution of erbium oxynitride was poured into a solution of hydrofluoric acid (HF) in combination with vigorous stirring.
Er(NO3)3 + 3HF → ErF3↓ + 3HNO3.
The resulting solution was washed with distilled water until the pH reached 6–7. The presence of nitrate ions was determined using a qualitative reaction with diphenylamine. Filtration was performed using a vacuum Buchner funnel and a “blue ribbon” filter. The gel-like erbium fluoride was dried in an oven at 70 °C for 12 h, followed by annealing in a furnace at 800 °C for 1 h. The resulting erbium fluoride was loaded into a planetary ball mill with WC balls (3 mm in diameter) at a balls to ErF3 mass ratio of 3:1. Erbium fluoride was crushed at a frequency of 14 Hz in air for 2 h. An aluminum powder with a purity of 99.7% and an average particle size of 105 μm was added to the ball mill at an Al to ErF3 ratio of 9:1, along with ceramic balls at the same ratio to obtain a homogeneous mixture of Al–ErF3. Mixing was performed at a frequency of 10 Hz for 4 h, followed by sieving through a 150 μm mesh. The resulting mixture was pressed into a mold with a diameter of 13 mm at a pressure of 390 MPa.
The Production of Al–Si–ErF3 Alloys. The studied alloys were produced by casting into a steel mold followed by heat treatment, according to the regime (T6): hardening with incomplete artificial aging. The industrial aluminum alloy A359 (Al 85.1–91.6%; Si 8–11%, Mn 0.2–0.5%; etc.) was used as the starting material for the study. In the experiment, 1.71 kg of the alloy was placed in a graphite–chamotte crucible and melted in a vertical muffle furnace at a temperature of 780 °C with a hold time of 2 h. The crucible with the melt was moved to an open-type furnace to maintain the temperature. After the mechanical removal of slag from the melt surface, Al–ErF3 master alloy preheated to 200 °C was introduced into the melt, weighing 190 g (amount of 1 wt%). One minute after the introduction of the master alloy, the melt was stirred with an original mixing device [39] for 2 min. The melt at a temperature of 705–720 °C was fed into the gate of the original steel coquille [40] heated to a temperature of 170–190 °C (Figure 2). Two castings of a rectangular cross-section of 100 × 150 × 10 mm were cast from one crucible (the gate and feeder areas were not used in the experiments). The method for obtaining the initial alloy without erbium was similar. For the heat treatment of the obtained alloys, the castings were placed in a muffle furnace heated to 450 °C. After holding for 1 h, the castings were sharply cooled via immersion in water heated to 80 °C. The cooled castings were placed in a furnace heated to 270 °C, incubated for 4 h and cooled together with the furnace.
Research methods. The surface morphology of ErF3 particles was investigated using a scanning electron microscopy (SEM) Quanta 200 3D (the equipment of Tomsk Regional Core Shared (EqTRCS)). The phase composition and structural parameters of powder were studied using X-ray diffraction with a Shimadzu XRD-6000 diffractometer (EqTRCS) in Cu Kα radiation. The quantitative content of phases in the powder was assessed through a full profile Rietveld analysis using the POWDER CELL 2.4 software and the PDF4+ crystal structure database. The chemical composition of the alloys was determined using an iCAP 7400 Duo optical emission spectrometer. Samples sized 100 × 10 × 10 mm were cut from the top and bottom parts of each casting and were then mounted to the chuck of a lathe. The samples were processed via a diamond turning tool at a low feed rate to obtain fine chips sized 3 mm. Chips of 1 g were calcined at 800 °C for 2 h, followed by dissolution in a mixture of hydrochloric, hydrofluoric, and nitric acids using a microwave decomposition system at 180 °C. The quantitative content of resulting solutions was analyzed for the major elements: Al, Si, Fe, Mn, Mg, and Er. Electron microscopic studies of the surface microstructure and the cross-section of the coated sample, as well as elemental analysis and fractographic studies of sample fractures after tensile tests were conducted using a Tescan MIRA 3 LMU scanning electron microscope equipped with an Oxford Instruments Ultim Max 40 energy-dispersive X-ray spectrometer. The alloy microstructure was studied through optical microscopy with the application of Metam LV 34 microscope (EqTRCS). The grain structure of the alloys was investigated through metallographic samples after electrolytic etching on an Olympus GX 71 (EqTRCS) optical microscope with an Olympus U-TP530 polarization filter. The investigation of the structure via transmission electron microscopy (TEM) methods was carried out using a microscope JEOL JEM-2100 microscope at an accelerating voltage of 300 kV on foils made via ion thinning using an Ion Sliser EM 09100IS system in a vacuum environment at a voltage of 6–8 kV and a tilt angle of 2–4°. Brinell hardness and Vickers hardness measurements of alloys were performed in this study. For the Brinell hardness experiment, a Metolab 703 hardness tester (EqTRCS) was used. A spherical indenter with a radius of 2.5 mm was used with a force of 62.5 kg and an exposure time of 10 s. For the Vickers hardness experiment, a Metolab 502 hardness tester (EqTRCS) was used. A spherical diamond indenter was used with a force of 50 g and an exposure time of 30 s. Tensile experiments were performed using an Instron 3369 (EqTRCS) universal electromechanical testing machine at a loading rate of 0.1 mm/min. For each group of alloys, 6 samples were made. Samples were cut from castings using electroerosion cutting and flat blades with a length and width of the working part of 25 and 6 mm, respectively; a thickness of 2 mm; and a rounding radius of 14 mm.

3. Results and Discussion

Figure 3 shows photographs of ErF3 powder particles. The obtained powder consists of agglomerates of a submicron particle. The sizes of the fine particles are 10–100 μm, and the sizes of the large particles are 0.3–1.7 mm. The surfaces of the large particles are covered with particles with a size of 46 ± 31 μm and submicron particles, as seen in Figure 3b.
The mechanical processing of the ErF3 powder in a planetary mill for 20 min leads to the crushing of the main mass of large particles. The powder is completely sieved through a sieve with a cell size of 500 μm; the average particle size of erbium fluoride is 90 ± 63 μm, excluding submicron particles (Figure 4a). Figure 4b shows that mechanical activation for 2 h allows us to obtain a homogeneous powder composed of erbium fluoride from individual particles of 0.8 ± 0.3 μm and their agglomerates up to 100 μm.
The diffraction pattern of the erbium fluoride powder after 120 min of crushing in a planetary mill is presented in Figure 5. The result of the decoding of the obtained diffractogram is presented in Table 1. The obtained powder exhibits an ErF3 phase with a coherent scattering region size of 18 nm and a microstrain value of 2.2 × 10−3.
Table 2 illustrates chemical composition in terms of Al, Si, Fe, Mn, Mg, and Er of the investigated alloys. The composition of the alloys is sufficiently homogeneous throughout the casting volume. Results show that the alloys correspond to the standard, and the erbium content in A359 + ErF3 alloy is close to the calculated value (~0.75 wt%).
SEM images of the A359 alloy are shown in Figure 6. The alloy consists of α-Al crystals (dark areas), silicon (gray areas), and intermetallic phases (light areas): Al5FeSi, Al15(FeMn)3Si2, Al2Cu, and Al15(FeMnCr)3Si2.
Figure 6a shows that the microstructure of the A359 alloy before heat treatment consists of an iron–manganese skeleton Al15(FeMn)3Si2 phase, a needle-like Al5FeSi phase, an Al2Cu (θ) phase, and primary crystals of Al15(FeMnCr)3Si2 phase in the obtained alloys. The Al2Cu θ phase is represented by small spherical formations, which do not have a negative effect on the mechanical properties of the alloy [41]. In the Al–Si system alloys, a triple eutectic Al–Si–Al5FeSi is formed in areas of high iron concentration [42]. The Al5FeSi phase initiating cracks is represented as needles in the polished surface and as elongated plates in the volume [42]. The addition of manganese to Al–Si alloys allows for the binding of the needle-like phase Al5FeSi into less negative skeletal formations (Chinese hieroglyphs) Al15(FeMn)3Si2 [41]. When the concentration of manganese exceeds 1% and iron exceeds 0.8%, primary crystals of Al15(FeMn)3Si2 may form [41]. Chromium or nickel are introduced as compensators for such compounds. Figure 6f shows that it does not prevent the formation of primary crystals of Al15(FeMnCr)3Si2 [43]. The resulting alloy showed a greater homogeneity of the distribution of iron-containing phases on the surface of grinds compared to the initial alloy, and practically no presence of the primary crystals of Al15(FeMn)3Si2 was detected.
The optical micrographs of the alloys (Figure 7) show the α-Al grains (light areas) and β-phase (dark) silicon. The Al15(FeMn)3Si2 skeletal phase and primary crystals of Al15(FeMnCr)3Si2 are also detected in the plane of metallographic grinds. In view of the absence of a pronounced dendritic structure of the obtained alloys, it is difficult to assess the effect of ErF3 particles on the sizes of α-Al.
In the plane of thin sections of alloys before heat treatment, the eutectic silicon phase occupies 20–30% of the section area. The alloy without the addition of erbium trifluoride shown in Figure 7a. In the alloy there are areas of accumulation of mostly needle-shaped β-phase silicon with linear size up to 100 μm. The introduction of erbium trifluoride particles shown in Figure 7b leads to the reduction in size of the β-phase with linear dimensions up to 30 μm and some rounding of the ends. The β-phase acquires a globular shape, and its sizes are reduced to 8 ± 5 μm for alloys of both groups as a result of heat treatment (T6).
Figure 8 shows the grain structure of the studied alloys as a result of electrolytic etching of metallographic specimen. It is known that during casting in coquille the crystallization of the melt starts on the walls of the mold. The average grain size of α-Al was 315 ± 131 μm in the areas of the A359 alloy castings bordering the coquille. It was found that in similar areas of A359 + ErF3 alloy castings the average grain size of α-Al was 304 ± 136 μm. Thus, the introduction of ErF3 particles into the A359 alloy did not lead to a change in the average grain size in the casting sections bordering the coquille. The maximum grain size of the studied areas of the A359 alloy castings was achieved in the central part, where the average grain size of α-Al was 518 ± 215 µm. In similar areas of A359 + ErF3 alloy castings, the average grain size of α-Al was 412 ± 164 μm. Thus, the introduction of ErF3 particles into the A359 alloy led to a reduction in the average grain size of α-Al in the central part of the casting.
Inoculant particles should have a high affinity for lattice parameters with the crystallizing metal [44] to act as a nucleation site for the effective refinement of the grain structure of the matrix alloy. Aluminum and silicon have a face-centered cubic lattice, while erbium fluoride has an orthorhombic lattice. Additionally, another mechanism of particle influence on the alloy structure is known when particles in contact with each other are located along the boundaries of the growing grain [45].
Generally, during the crystallization of α-Al grains, the dominant direction of the propagation of the crystallization front is formed, which can displace intermetallic phases suspended in the melt from the crystallization region. This effect leads to the formation of clusters of intermetallic phases, which form areas of reduced strength in the resulting castings. In turn, submicro- and nanoparticles in the melt can encircle the growing grains, forming a barrier between the growing aluminum grain and the feeding melt. This inhibits the crystallization front and promotes the formation of grain nuclei outside the main crystallization front. Summarizing the results of the study of the microstructure of the obtained alloys: based on the difference in the crystal lattices of Al and ErF3, ErF3 particles cannot be effective centers of crystallization, while a high uniformity of the structure of alloys containing ErF3 particles is noted. It can be concluded that the contribution of ErF3 particles to the structure of Al–Si alloys is to reduce the formation of clusters of iron phases and eutectic lamellar silicon. Schematically, the implementation of this mechanism is shown in Figure 9.
As can be seen from Figure 10, ErF3 particles in the alloy are on the grain boundaries of α-Al. This fact may be an indirect confirmation of the implementation of the mechanism of holding back the crystallization front by ErF3 particles. The results of the EDX analysis of the area shown in Figure 10a are presented in Table 3.
The density of the A359 alloy is 2.73 ± 0.01 g/cm3. The alloy with erbium fluoride is less homogeneous in density, measuring 2.72 ± 0.03 g/cm3. Figure 6d shows that the reason for this density is the presence of more pores in the alloy volume. The hardness and microhardness values of the studied alloys are presented in Table 4. It can be seen that the hardness value of the A359 alloy increases from 86.3 to 118.6 HB as a result of heat treatment (T6) and does not depend on the addition of ErF3 particles. In the A359 alloy, the microhardness value of the Al15(FeMn)3Si2 phase is 107.6 HV. The addition of ErF3 particles to the A359 alloy provides an increase in the Al15(FeMn)3Si2 phase microhardness from 107.6 to 143.9 HV. At the same time, the heat treatment of the alloy increases the microhardness values of the Al15(FeMn)3Si2 phase and reduces the particles contribution to its increase. This dependence correlates with the noted positive effect of ErF3 particles on the morphology of eutectic silicon before the alloy heat treatment.
Figure 11 shows typical stress–strain curves of A359 and A359 + ErF3 alloys before and after heat treatment. The alloys exhibit typical Al–Si system alloys deformation behavior: elastic deformation zone prevails over the plastic flow zone, no deformation localization zone is present, and crack propagation work is minimal. Heat treatment according to the (T6) regime provides an increase in the maximum stresses of the elastic zone of the alloys while reducing their plasticity properties. It was found that the effect of erbium fluoride particles on the deformation behavior of the A359 alloy varied depending on the structural state of the alloy. The particles in the cast alloy provided a positive effect on the stress–strain state in the elastic deformation zone and provide an increase in plasticity properties. The particles in the alloy after heat treatment provided a significant increase in elastic stresses with a small contribution to the plastic flow work of the material.
Table 5 shows the mechanical properties of the alloys. According to the results obtained, there is a positive trend in the increase in strength properties of the alloy before and after heat treatment as a result of the addition of particles. In the A359 alloy, in its cast state, the addition of 1 wt% ErF3 leads to an increase in the ultimate strength from 168 to 195 MPa and the relative elongation from 0.7 to 2.3%. In a heat-treated state, the addition of 1 wt% ErF3 to alloy A359 provides an increase in the yield strength from 197 to 267 MPa and in the tensile strength from 213 to 286 MPa and increases the maximum strain for failure from 2.5 to 4.3%. The increase in the yield strength values of the A359 alloy can be associated with the refinement of the average grain size (Figure 8), according to the Hall–Petch law [5]. In turn, the increase in the ductility of A359 + ErF3 alloy can be realized by reducing the clustering of the iron phase (Figure 7) embrittlement of Al–Si alloys.
Figure 12 shows the fracture surface of the A359 alloys before and after heat treatment. It was found that a decrease in maximum deformation does not affect the nature of the fracture. The fracture surface is oriented perpendicularly to the axis of tension, and the surface morphology is characterized by homogeneous cleavage.
Figure 13b shows that the surface of fracture of the A359 alloy is dotted with cracked intermetallics Al15(FeMn)3Si and Al15(FeMnCr)3Si (Table 3). The introduction of erbium fluoride does not affect the fracture behavior of the A359 alloy. The fracture occurs through the mechanism of the shear facet with the formation of a stream-like microrelief. This is probably due to the iron-containing intermetallics acting as stress concentrators, and upon reaching the allowable load, they crack, followed by the fracture of aluminum grains through the transcrystalline mechanism, which is demonstrated in Figure 13c.
Admittedly, to create metal-matrix composites with enhanced strength properties, it is necessary to have a uniform distribution of reinforcing particles [30]. Figure 14a shows that there are areas of accumulation of erbium fluoride on the surfaces of fracture of A359 + ErF3 alloy samples with reduced strength properties. Thus, the introduction of erbium fluoride with preliminary deagglomeration in aluminum micropowder and mechanical mixing using a special mixer does not provide the uniform distribution of particles in the alloy matrix. There are approaches to using ultrasound treatment of the melt and vibrational impact during casting to deagglomerate ex situ-introduced particles and increase their wettability. The influence of ErF3 particles under the complex action of external fields on the structure and the physico-mechanical properties of the A359 alloy will be further studied in the future.

4. Conclusions

The introduction of ErF3 particles results in less accumulation of intermetallic phases and reduces the linear sizes of eutectic Si particles by ~70% with the formation of a larger rounding radius on the boundaries. As a result of the heat treatment of the studied alloys, according to the (T6) mode, the eutectic Si particles acquire a globular shape, and their sizes are reduced to 8 ± 5 μm for the alloys of both groups. It was found that the modifying effect of ErF3 particles on the structure of aluminum–silicon alloys is realized through the mechanism of crystallization front inhibition; it weakly affects the indices of the average size of dendritic cells and is manifested to reduce the formation of clusters of iron phases and eutectic lamellar silicon.
It was found that the introduction of 1 wt%ErF3 does not affect the hardness values of the alloy and the microhardness of the Al, Si, and Al5FeSi phases and leads to an increase in the microhardness of the Al15(FeMn)3Si2 phase by 34% and the Al15(FeMnCr)3Si2 phase by 7%. It was found that the addition of 1 wt% ErF3 to the A359 alloy leads to an increase in the values of yield strength from 142 to 162 MPa and ultimate tensile strength from 168 to 195 MPa. Heat treatment, according to the (T6) mode, leads to a decrease in ductility by 57% and 65% for the A359 and A359 + ErF3 alloys, respectively. However, the values of yield strength and ultimate tensile strength increase by 39% and 27%, respectively, in the A359 alloy and by 65% and 47%, respectively, in the A359 + ErF3 alloy. The introduction of erbium fluoride does not affect the character of the destruction of the A359 alloy. The destruction occurs via the shear facet mechanism with the formation of a streaky microrelief. Iron intermetallics act as stress concentrators, the appearance of which initiates the sample cracking via the transgranular mechanism. It was noted that the improvement in the strength properties of the A359 alloy by adding 1 wt% of ErF3 is combined with the negative effect of its agglomerates and clusters, which cannot be eliminated through preliminary deagglomeration in aluminum micropowder and melt processing using a mechanical mixing device. Thus, by ensuring the uniform distribution of ErF3 particles throughout the material volume, a significant increase in the strength properties of the original alloy can be expected.

Author Contributions

Investigation and visualization, N.K. and V.V.; writing—original draft preparation, N.K., V.V. and M.S.; formal analysis, M.S.; writing—review, data curation, and editing, A.K.; methodology, validation, conceptualization, project administration, and funding acquisition I.Z., A.V. and S.V. All authors have read and agreed to the published version of the manuscript.

Funding

This work was carried out with financial support from the Ministry of Education and Science of the Russian Federation (state assignment no. FSWM-2020-0028).

Data Availability Statement

Not applicable.

Acknowledgments

The research was carried out with the equipment of Tomsk Regional Core Shared Research Facilities Center of National Research Tomsk State University. The Center is supported by the Ministry of Science and Higher Education of the Russian Federation, grant no. 075-15-2021-693 (no. 13.RFC.21.0012)).

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. Two methods of obtaining erbium alloys: alloying using the hydrogenation technology RZM (1–9) or dispersion strengthening with ErF3 particles (1, 2→5–7→9).
Figure 1. Two methods of obtaining erbium alloys: alloying using the hydrogenation technology RZM (1–9) or dispersion strengthening with ErF3 particles (1, 2→5–7→9).
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Figure 2. Schematic drawing of the process of the production of the alloys under study by pouring the melt into the steel die casting.
Figure 2. Schematic drawing of the process of the production of the alloys under study by pouring the melt into the steel die casting.
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Figure 3. SEM micrographs of ErF3 powder: ~1 mm particles (a) and submicron particles on the surface (b).
Figure 3. SEM micrographs of ErF3 powder: ~1 mm particles (a) and submicron particles on the surface (b).
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Figure 4. SEM micrographs of ErF3 powder after 20 (a) and 120 (b) minutes of grinding in the planetary mill.
Figure 4. SEM micrographs of ErF3 powder after 20 (a) and 120 (b) minutes of grinding in the planetary mill.
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Figure 5. XRD pattern of ErF3 powder after grinding in the planetary mill for 120 min.
Figure 5. XRD pattern of ErF3 powder after grinding in the planetary mill for 120 min.
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Figure 6. SEM micrographs of alloys before and after heat treatment: A359 (a); A359 + (T6) (b); A359 + ErF3 (c); A359 + ErF3 + (T6) (d). Results of element mapping of A359 alloy (e,f); mapping by individual elements (g).
Figure 6. SEM micrographs of alloys before and after heat treatment: A359 (a); A359 + (T6) (b); A359 + ErF3 (c); A359 + ErF3 + (T6) (d). Results of element mapping of A359 alloy (e,f); mapping by individual elements (g).
Metals 13 01463 g006aMetals 13 01463 g006b
Figure 7. Optical micrographs of A359 and A359 + ErF3 alloys before and after heat treatment: A359 (a); A359 + ErF3 (b); A359 + (T6) (c); A359 + ErF3 + (T6) (d).
Figure 7. Optical micrographs of A359 and A359 + ErF3 alloys before and after heat treatment: A359 (a); A359 + ErF3 (b); A359 + (T6) (c); A359 + ErF3 + (T6) (d).
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Figure 8. Optical micrographs of A359 (a,c) and A359 + ErF3 (b,d) alloys: photo of the area in the center of the casting (c,d) and the area on the border with the coquille (a,b).
Figure 8. Optical micrographs of A359 (a,c) and A359 + ErF3 (b,d) alloys: photo of the area in the center of the casting (c,d) and the area on the border with the coquille (a,b).
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Figure 9. Scheme of the effect of ErF3 particles on the structure of Al–Si alloys: alloy without particles at timepoints t1, t2, and t3 (a) and Al–Si + ErF3 alloy at timepoints t1′, t2′, and t3′ (b).
Figure 9. Scheme of the effect of ErF3 particles on the structure of Al–Si alloys: alloy without particles at timepoints t1, t2, and t3 (a) and Al–Si + ErF3 alloy at timepoints t1′, t2′, and t3′ (b).
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Figure 10. ErF3 particles on the grain boundaries of alloy A359: an SEM image of the fracture surface (a) and a TEM image of the alloy (b).
Figure 10. ErF3 particles on the grain boundaries of alloy A359: an SEM image of the fracture surface (a) and a TEM image of the alloy (b).
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Figure 11. Load diagrams of the alloys before and after heat treatment.
Figure 11. Load diagrams of the alloys before and after heat treatment.
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Figure 12. SEM micrographs of the A359 alloy fracture surface before (a) and after (b) heat treatment for detecting secondary (left images) and backscattered electrons (right images).
Figure 12. SEM micrographs of the A359 alloy fracture surface before (a) and after (b) heat treatment for detecting secondary (left images) and backscattered electrons (right images).
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Figure 13. SEM micrographs of the alloys fracture surface: surface with ferrous intermetallics (a); mapping of the area with the cracked Al15(FeMnCr)3Si phase (b); transcrystalline cracking of aluminum grains (c).
Figure 13. SEM micrographs of the alloys fracture surface: surface with ferrous intermetallics (a); mapping of the area with the cracked Al15(FeMnCr)3Si phase (b); transcrystalline cracking of aluminum grains (c).
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Figure 14. The agglomeration of ErF3 particles on the A359 + ErF3 alloy fracture surface after tensile test (a) and EDX spectrum from point 2 (b).
Figure 14. The agglomeration of ErF3 particles on the A359 + ErF3 alloy fracture surface after tensile test (a) and EDX spectrum from point 2 (b).
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Table 1. ErF3 powder diffraction pattern interpretation results.
Table 1. ErF3 powder diffraction pattern interpretation results.
PhaseVolume Fraction, Mas. %Lattice
Parameters, Å
CSR Dimensions,
nm
Microdistortions,
∆d/d
ErF3_62 a = 6.3437182.2 × 10−3
100b = 6.8863
c = 4.3935
Note: CSR—coherent scattering regions.
Table 2. Concentration range of Al, Si, Fe, Mn, Mg, and Er (wt%) of the experimental alloys.
Table 2. Concentration range of Al, Si, Fe, Mn, Mg, and Er (wt%) of the experimental alloys.
AlSiFeMnMgEr
A35986.21–91.498.65–10.670.08–0.130.19–0.320.18–0.32
A359 + ErF386.66–90.159.55–10.810.08–1.090.21–0.400.18–0.220.61–0.81
Table 3. Energy dispersive X-ray analysis of the Figures 10a, 13b, and 14a.
Table 3. Energy dispersive X-ray analysis of the Figures 10a, 13b, and 14a.
LabelAlFeMnCrSiErFMgCOCu
163.721.4004.912.78.882.21.134.170.9
265.5713.763.941.6012.3100.240.140.850.421.17
313.040.5002.1871.766.560.131.294.540
49.770.56001.2164.3913.694.951.284.150
Table 4. Hardness and microhardness values of the phases of the investigated alloys.
Table 4. Hardness and microhardness values of the phases of the investigated alloys.
AlloyHBHV(Al)HV(Si)HV(β(Al5))HV(αm(Al15))HV(αm(Al15) + Cr)
A35986.3 ± 2.681.8 ± 692.7 ± 1298.6 ± 6107.6 ± 23230 ± 98
A359 + ErF384.9 ± 4.283.5 ± 695.3 ± 895.4 ± 6143.9 ± 29245 ± 68
A359 (T6)118.6 ± 3.5117.8 ± 6134.7 ± 18128 ± 8153.2 ± 14181 ± 68
A359 + ErF3 (T6)118.1 ± 4.5117.3 ± 7135 ± 13123 ± 8163 ± 14190 ± 55
Note: HB—Brinell hardness; HV—Vickers microhardness of phases; β(Al5)—Al5FeSi; αm(Al15)—Al15(FeMn)3Si2; αm(Al15) + Cr—Al15(FeMnCr)3Si2.
Table 5. Mechanical properties of alloys.
Table 5. Mechanical properties of alloys.
AlloyStateσ0.2, MΠaσB, MΠaεmax, %δ, %
A359As-cast142 ± 7168 ± 113.5 ± 0.80.7 ± 0.2
A359 + ErF3162 ± 8195 ± 134.9 ± 12.3 ± 0.3
A359(T6)197 ± 6213 ± 132.5 ± 0.40.3 ± 0.1
A359 + ErF3267 ± 7286 ± 134.3 ± 0.40.8 ± 0.2
Note: σ0.2—yield strength; σB—ultimate tensile strength; εmax—maximum deformations before failure; δ—elongation.
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MDPI and ACS Style

Kakhidze, N.; Valikhov, V.; Selikhovkin, M.; Khrustalyov, A.; Zhukov, I.; Vasiliev, S.; Vorozhtsov, A. Effects of ErF3 Particles on the Structure and Physicomechanical Properties of A359 Alloy. Metals 2023, 13, 1463. https://doi.org/10.3390/met13081463

AMA Style

Kakhidze N, Valikhov V, Selikhovkin M, Khrustalyov A, Zhukov I, Vasiliev S, Vorozhtsov A. Effects of ErF3 Particles on the Structure and Physicomechanical Properties of A359 Alloy. Metals. 2023; 13(8):1463. https://doi.org/10.3390/met13081463

Chicago/Turabian Style

Kakhidze, Nikolai, Vladimir Valikhov, Mikhail Selikhovkin, Anton Khrustalyov, Ilya Zhukov, Sergey Vasiliev, and Alexander Vorozhtsov. 2023. "Effects of ErF3 Particles on the Structure and Physicomechanical Properties of A359 Alloy" Metals 13, no. 8: 1463. https://doi.org/10.3390/met13081463

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