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Article

Characterization of Aluminum Alloy–Silicon Carbide Functionally Graded Materials Developed by Centrifugal Casting Process

1
Materials Science Department, Faculty of Materials Science and Engineering, Transilvania University of Brasov, 29 Eroilor Bld., 500036 Brasov, Romania
2
Materials Engineering and Welding Department, Faculty of Materials Science and Engineering, Transilvania University of Brasov, 29 Eroilor Bld., 500036 Brasov, Romania
3
Department of Product Design, Mechatronics and Environment, Faculty of Product Design and Environment, Transilvania University of Brasov, Colina Universitatii Street, no. 1, 500068 Brasov, Romania
*
Author to whom correspondence should be addressed.
Submission received: 19 January 2021 / Revised: 8 February 2021 / Accepted: 8 February 2021 / Published: 11 February 2021

Abstract

:
The continuous development of modern industries rises the necessity for functionally graded materials. This research starts from the consideration that the incorporation of SiC particles in the molten aluminum alloy can be difficult due to the very low wettability of SiC particles. In order to increase their wettability, SiC particles were covered with a layer of metallic copper. The incorporation of SiC particles into the aluminum alloy mass was performed by centrifugal casting. The secondary hypoeutectic Al-Si alloy used in this study was elaborated within the crucible of a resistors heated furnace. The metallic coating of SiC particles, in addition to the effect of increasing their wettability by molten metal, also has a role in preventing the formation of aluminum carbide in case of heating above 700 °C. A great amount of attention was paid to the parameters used during the centrifugal casting process. The results showed that adjusting the proportion of SiC particles within the composite allows us to obtain values of the thermal expansion coefficient within previously established limits. The present work demonstrates that the coating of SiC particles covered with a thin layer of metallic Cu creates the conditions to easily incorporate them into the molten Al mass, thus obtaining FGMs with controlled properties.

1. Introduction

The alert pace in which technology develops nowadays leads us with no doubt to what the researchers named “Industry 4.0”. This stage of industry development is not possible without the astonishing development of materials engineering research. Considering the growing importance that nowadays is given to Industry 4.0, obtaining functionally graded materials (FGMs) becomes vital. It should be kept in mind that functional structures with a gradient of properties are found in nature (for example in animal tissues). These structures have a high wear resistance at the exterior at the same time as a ductile interior.
There are almost no areas of technology where new materials are not needed. The need to develop property gradient materials has arisen with the development of modern industries that are increasingly demanding products that behave differently depending on the demands [1]. Based on these considerations, in 1984, in Japan, the concept of FGM first appeared. A large number of researchers have turned their attention to FGMs. Some of them focused on the analysis of the production process of these materials as well as on the modelling and simulation of the process [2,3,4,5,6] while others turned their attention to the inevitably generated residual stresses of FGMs due to thermal mismatch of each basic material using experimental and analytical methods [7,8] or their characterization [1]. Over time, a number of techniques have been developed in order to obtain FGMs: Powder metallurgy, vapor deposition, solid free form fabrication, centrifugal casting, and additive manufacturing [9,10].
In the large family of new developed materials, composites materials play an important role nowadays. Taking into account that an assembly of two or more materials with completely different properties leads to a composite with superior properties surpassing those of each component basic material, we realize why significant amounts are invested in researching these materials. Precisely for this improvement in terms of properties when compared to those of each component, these materials have special applications, for example in the aerospace industry [11,12,13], in the biomedical industry as well as in other engineering applications that require new materials with superior properties.
Composites of aluminum metallic matrix with various types of reinforcers already show a wide spread in various industries, such as automotive, aviation, military, etc. Al matrix reinforced with SiC composite materials are of great interest especially for the automotive industry [14,15,16,17,18,19,20,21,22]. Compared to aluminum alloys, they have superior properties such as high strength, high fatigue strength, high specific modulus, and high hardness. Due to the high thermal conductivity (180–200 W·m−1K−1) they can be successfully used as thermal radiators in the electronics industry.
A large number of research from prestigious universities and/or research institutes has been conducted in the study of aluminum alloy composites reinforced with SiC particles [17,22,23,24]. However, the actual published data are limited regarding the obtaining process, while most articles deal with specific properties of the composites. Most researchers reported the use of the stirring-casting method to incorporate SiC particles [25]. Therefore, deficiencies were encountered due to the fact that SiC particles cannot be moistened by the aluminum alloy. With copper being one of the elements almost perfectly wetted by aluminum, a number of articles refer to the coating of SiC particles with a thin layer of copper leading to a correct wetting by the aluminum alloy [14,26,27].
Increasing the wettability of SiC particles by coating them with Cu films could be an important factor in increasing the cohesion between the metal matrix and the reinforcing material when producing aluminum-based composites [24,28,29,30,31].
Based on these considerations, the present research aims to describe the process of incorporation of the free SiC particles (coated with Cu) into the basic metallic mass (aluminum alloy). Beside the non-wetting phenomenon, the resistance of the aluminum oxide layer also occurs during the embedment of the SiC particles. In order to overcome this difficulty, the use of centrifugal casting (with vertical rotation axis in this case) is proposed. It should be emphasized that the present research continues the previous ones in this field [24].
The use of centrifugal casting in the processing of metal matrix composites (MMC) with aluminum matrix and ceramic reinforcing elements (Al2O3, SiC, TiB2, etc.) is analyzed by several researchers [32,33,34,35].
Production of FGMs using centrifugal casting involves two types of procedures: Ex-situ FGM and in-situ FGM. Ex-situ processing involves the previous synthesis of the metal matrix composite (MMC) by the stirring casting method [36] followed by the casting of the composite slurry in the centrifugal casting unit. During the in-situ processing, the reinforcement is added to the base metal mass directly in the shell of the centrifugal casting system in which the liquid alloy of the metal matrix is already present. The in-situ method was also used in this paper.
The samples were analyzed by means of metallographic analysis (MA), X-ray diffraction analysis (XRD), scanning electron microscopy (SEM), dilatometric analysis (DIL) and differential thermal analysis (DTA).
Considering the literature background, the present research shows how the coating of SiC particles with a thin layer of metallic Cu essentially influences their incorporation into the molten aluminum alloy metal mass. By now, the most frequently reported method applied by other researchers was stirring casting, while this paper is focused on the use of centrifugal casting in the in-situ configuration and on the emerging advantages in obtaining FGMs. Furthermore, by means of thermal analysis, the authors aimed to demonstrate that the coefficient of thermal expansion of these Al-SiC composites can be controlled by varying the proportion of SiC.

2. Experimental Details

2.1. Materials

For the present research, a secondary hipoeuthectic Al-Si alloy with a high iron content was chosen as a base metal to be pressure casting. The chemical analysis performed with a Spectromax XF-BT spectrometer is presented in Table 1.
The silicon carbide powder used in this research was superfine (600 grit) with an average grain size of 137 μm and a 3.16 g·cm−3 density, provided by Alfa Aesar GmbH, Kandel, Germany.
In order to increase the wettability of the SiC particles in AlSi alloy the particles were covered with a Cu film (treated SiC) using a coating solution with the following composition: Distilled water, copper sulphate (CuSO4), sodium hydroxide (NaOH), sodium and potassium tartrate (KNaC4H4O6·4H2O), and 37% formaldehyde (CH2O). In order to facilitate the coating process of the SiC particles they must be activated firstly. The applied activation consisted of distilled water, hydrochloric acid (HCl), and palladium chloride (PdCl2). All the components of the activation and coating solutions were provided by Chemical Company SA, Iasi, Romania.

2.2. Equipment

All components were weighed with a RADWAG AS 60/220.X2 (Radom, Poland) analytical balance.
The chemical analysis of the base alloy was performed with a Spectromax (Kleve, Germany) XF-BT spectrometer.
The activation of SiC particles was achieved by mixing them in the activating solution in a IKA C-MAG HS 7 (IKA-Werke GmbH & Co. KG, Staufen im Breisgau, Germany) magnetic stirrer with heating and ceramic heating plate, which offers excellent chemical resistance.
The calcination was performed in an electric oven with resistors, UTTIS Romania type (București, Romania), model CE4x2x1 with 3.5 kW power.
The alloy was melted in a laboratory size electric oven with resistors. The centrifugal casting was performed on a vertical axis casting plant, with installation also located in the laboratories of Materials Science Department and presented in Figure 1.
The shell was coated with a thermoreactive binder (20 mm thickness) in order to decrease the intensity of the thermal exchange with the environment, keeping the liquid alloy as long as possible in the liquid state in order to intensify the embedding process of the SiC particles.
Structural analysis was performed using an Omnimet-Buehler analysis system equipped with a Nikon microscope (1000× maximum magnification) and software programs suitable for quantitative structural analysis.
The X-ray diffraction patterns were recorded on a Bruker (Billerica, MA, USA) AXS D8 discover XRD (X-ray Diffraction) using a monochromatic Al X-ray source to identify the phases and constituents.
The samples were also analyzed with a scanning electron microscope (SEM, Quanta FEI, Eindhoven, The Netherlands) equipped with an X-ray energy dispersion spectroscopy system (X-EDS, INCA Oxford Instruments, Abingdon, UK).
The dilatometric analysis was performed on a DIL LINSEIS L75 Platinum Series dilatometer, within 25–550 °C temperature range deploying 10 K·min−1 heating rate in the dynamic step [37]. The experimental runs comply with the ASTM E228: 2011 standard procedures. Specimens’ dimensions were set as 105 × 5 mm.
Differential thermal analysis was performed using a NETZCH STA 449 F3 Jupiter (Selb, Germany). NETZCH Proteus—Thermal Analysis—version 5.2.1 software was used for processing the DTA-TG experiment. The DTA peaks were established on the heating curve along with the transformation enthalpy [28,29,38,39,40].

2.3. Working Procedure

The main difficulty encountered in the production of composites with metal matrix based on aluminum and SiC reinforcement is the low wettability of ceramic materials by the metal bath [41,42]. There are a number of studies that have shown that the coating of SiC particles with a metal such as Si, Fe, Mn, or Cu results in a substantial increase of their wettability.
Choh and Oki clearly demonstrate that the addition of metallic Cu to the surface of SiC particles considerably increases their wettability by molten aluminum [42].
In the present research, the authors started from the considerations presented above and did not aim to measure the wettability of SiC particles in aluminum alloy but to demonstrate the applicability and advantages of the method.
The SiC particles were coated with Cu in order to improve their wettability in the molten alloy metal bath. The coating of the SiC particles with a thin layer of copper was performed by a two steps process: Step 1, the activation of the particle surface and step two consisting in the actual coating process. To improve the adhesion of Cu to SiC particle’s surface they were activated in a solution with the following composition: 500 mL H2O, 0.5 mL HCl, and 0.25 g of PdCl2. The activation process followed these steps:
-
100 g of SiC particles were introduced in the activating solution then mixed with the magnetic stirrer for 30 min;
-
SiC particles were filtered and washed;
-
SiC particles were calcinated at 150 °C for 40 min (heated together with the furnace).
After the activation, the particles were submerged for 60 min (with sample collection after 30 min) in a coating solution having the following composition: 2000 mL distilled H2O, 20 g CuSO4, 20 g NaOH, 100 g KNaC4H4O6·4H2O, 20 mL CH2O.
An empirical calculus was used to determinate the copper requirement within the coating solution, based on the following simplifying hypotheses:
-
All SiC particles were considered perfectly spherical;
-
A medium granulation value of 137μm was considered. It should be mentioned that SiC powder was supplementary sorted by particles size criteria in order to increase its uniformity;
-
An even layer of Cu of 1µm was considered on the surface of SiC particles.
Based on these simplifying hypotheses and taking into account that 25 g SiC charges were used, the result was a need of 8 g of CuSO4.
In order to have the safety of a sufficient content of Cu in the coating bath, the presented composition was reached (containing 2.5 times more CuSO4 than the calculated minimum necessary).
The working parameters for both activation and coating stages are presented in Table 2.
For the embedment of the SiC particles into the aluminum alloy metallic base, three different variants of the centrifugal casting process with vertical rotation axis were used:
  • V1—The alloy overheated at 850 °C was poured in the resting (nonrotating) shell. Afterwards, the Cu-coated SiC particles were introduced and preheated to 900 °C. Then the shell was rotated with 1500 rpm speed. It should be mentioned that after the solidification of the composite sample it was found that during the pre-heating stage the agglomeration of SiC particles occurred.
  • V2—followed the same steps as the first version but this time the agglomerations of particles were crushed and only afterwards introduced in the shell.
  • V3—room temperature uncoated SiC particles were introduced into the resting shell, which was afterwards rotated with 1500 rpm until solidification of the alloy. The casting of the aluminum alloy was done while the shell was rotating.
The resulted muff shaped composites (Øext = 110/Øint = 90 × 80 mm) were cut into samples that were further tested in terms of their structural and thermal properties. The XRD patterns were obtained from Cu-coated SiC particles in order to prove the coating existence on the particles.
To facilitate the analysis of the samples they were embedded in epoxydic resin and the surface was metallographically processed to be observed under the microscope. The structural analysis was not the main objective of this characterization, but the embedment characteristics was.
Differential thermal analysis was performed under protective argon atmosphere (argon flow 20 mL/min) with a heating/cooling rate of 10 °C·min−1. Dilatometric analysis was performed in air with 10 °C·min−1 heating rate.

3. Results and Dissscussion

3.1. XRD

The X-ray diffraction patterns of the Cu-coated SiC particles, for two different durations of the coating stage, are presented in Figure 2.
At a first look at the XRD patterns depicted in Figure 2 one can observe that the Cu phase appears at multiple angular positions after the 60 min coating time when compared to the 30 min coating time pattern. This can suggest that together with the growth of the coating time, the Cu quantity also increases, as expected. This aspect can be translated into a better wettability of the SiC particles in the aluminum alloy.
Although it is expected that part of the metallic coating will be detached from the ceramic particles, according to the research results shown in Figure 3 it is found that the Cu film remains attached to the SiC particle, its role being to help integrate more of the SiC particle in the aluminum metal mass. SEM analyzes were performed on the presented sample, which also demonstrates the presence of copper on the surface of the SiC particle—Figure 3 and Table 3. The presence of pores and microcracks at the Al alloy-SiC interface is a result of the surface preparation process of the metallographic sample.

3.2. Morphological Analysis

Morphological analysis highlights how the SiC particles were actually embedded in the aluminum alloy metallic base, for each research variant. It is worth mentioning that the first two variants (V1, V2) both individual SiC particles and SiC agglomerations were concentrated in the interior surface of the casted muffs. This phenomenon is rather unexpected. Due to the formation of SiC agglomerations air bubbles appear in their rear. This fact leads to the decrease of the density of the agglomerations below the density of the alloy thus resulting in its displacement inwards. The density ratio for the liquid alloy and SiC particles (2.6/3.1) is in favor of concentrating the silicon carbide on the outer surface of the cylindrical samples. This behavior of the SiC particles was confirmed only in the case of the composite bush molded in the third process (V3).
The corresponding metallographic images for each analyzed variant are presented as follows: V1Figure 4; V2Figure 5; V3Figure 6.
For the V1 method the SiC particles coated with a thin layer of Cu were preheated at 900 °C and introduced as such in the metallic mass. Due to the preheating stage the particles started to conglomerate and formed lumps that were not crushed afterwards. As a result, the SiC particles were not evenly distributed. Instead, some agglomerations appear in certain areas of the samples (Figure 4c). As an effect of the centrifugal casting, certain agglomerations were dispersed, thus well-embedded single particles also appear in the sample (Figure 4a). The use of activated particles (covered with a thin layer of Cu) is clearly highlighted in Figure 4b where the presence of copper is very well observed. The activated SiC particles show a good adhesion to the metal mass, which is proved by the fact that, although the samples were processed with abrasive paper, the particles were not removed from the surface (Figure 4d).
Within the V2 variant of the process, the SiC particles were preheated at 900 °C and similar to V1 method, lumps appeared as a result of the agglomeration process. In order to avoid having particles agglomerations in the final composite material, the preheated SiC lumps were crushed, which resulted in a much more uniform dispersion of them in the sample volume, even in the areas with high density of embedded particles (Figure 5c). The existence of the thin layer of Cu on the surface of the particles favored their incorporation process in the metal matrix even for single particles (Figure 5a). The use of SiC particles covered with a consistent layer of Cu has the effect of an increased embedding in the base metal mass, as it can be observed from Figure 5b. Variant V2 also ensures a good adhesion of the particles to the sample surface even in the situation of a small contact surface (Figure 5d).
For the V3 method, the introduction of SiC particles was performed at room temperature, without preheating. It can be easily observed that most SiC particles are uniformly dispersed in the metal mass of aluminum alloy. This is explained by the fact that without the heating stage, as a source of conglomeration processes, the particles remained dispersed. Although this time the particles were not treated, the absence of the Cu layer on the surface of the particles did not lead to a sharp decrease in their adhesion to the metal matrix. In Figure 6c one can observe that the particle is well embedded in the alloy even if it is inserted on the surface.

3.3. Dilatometric Analysis

The results of the dilatometric analysis presented in Figure 7 show a relatively lower dilatation of the composite (alloy with embedded SiC particles) than of the alloy itself. The variation curves of the coefficient of expansion according to the temperature, obtained by the derivation of the expansion curves, depict a normal allure in the case of the alloy, in the sense that it also highlights the silica exit from the solid supersaturated alpha solution, with the maximum at 300 °C. It is worth mentioning that the alloy used in the experiments was cast in cast iron ingots, which ensures high cooling rates. In the case of the composite (alloy + SiC particles), the variation curve of the thermal expansion coefficient according to the temperature has two particularities, namely the value of the expansion coefficient is lower than in the case of the alloy without SiC particles and the appearance of the peak oriented downward, at temperature of 200 °C. Both features can be explained by the presence of SiC particles in the alloy. As it is known, the value of the thermal expansion coefficient for silicon carbide is 4 × 10−6 °C−1, which explains the decrease of the expansion coefficient value for the composite. The presence of the downward oriented peak may correspond to a dissolution of the silicon, which separated during the solidification on the surface of the inclusions of SiC (heterogeneous germination), in the alloy.

3.4. Thermal Analysis

The results of the thermal analysis are presented in Figure 8.
By comparing the DTA curves recorded for the alloy and for the composite, it turns out that in the case of the composite, the value of the melting heat (energy) is lower (314.8 J·g−1) than in the case of the alloy (372.9 J·g−1). This difference corresponds to the volume of alloy replaced by the embedded SiC particles. As it is known, silicon carbide melts at much higher temperatures.
The metallic coating of SiC particles, in addition to the effect of increasing their wettability by molten metal, also has a role in preventing the formation of aluminum carbide in case of heating above 700 °C.
Hashim et al. [43] reported that a concentration of Si between 7 to 15% in the alloy prevents the formation of the Al4C3 phase as a result of the chemical reaction of Al with SiC according to chemical relation (1).
4Al + 3SiC → Al4C3 + 3Si
If this reaction takes place extensively, the formation of the Al4C3 compound leads to a degradation of the composite properties (for example its strength decreases due to the formation of weak phases at the interface).
To confirm this fact, the thermal analysis was performed up to 800 °C (Figure 9). It can be easily noticed on the DTA curve that during heating no transformations occur after the aluminum melts, which means that the metal coating protects the reinforcement particles during the heating process.

4. Conclusions

The present research focused on the incorporation conditions of SiC particles by the liquid alloy by covering them with Cu (element which is moistened by the liquid alloy) under the conditions of centrifugation process.
The authors show that by combining centrifugal casting with coating of SiC particles with a thin layer of Cu, one can successfully obtain Al-SiC composite alloys with a uniform distribution of the reinforcer in the metal matrix.
When producing these composites, greater attention should be paid to avoiding the agglomeration of SiC particles. A drawback needs to be solved, namely the impossibility to achieve a homogeneous/uniform distribution of SiC particles in the base metal mass.
It was found that the results obtained by the DTA analysis are consistent with those obtained by the DIL method and thus the presence of SiC particles in the volume of the alloy is confirmed. At the same time, the structural observations under the optical microscope observed at the surface of the samples, are also confirmed by the DTA and DIL analyzes carried out in the volume of the samples.
Another novelty highlighted by the present research shows that by adjusting the proportion of SiC in the composite, it is possible to classify the value of the coefficient of thermal expansion within desired limits.

Author Contributions

Conceptualization, B.V., I.M., and T.B.; methodology, B.V., T.B., and I.M.; investigation, B.V., I.M., T.B., D.M., M.A.P., M.C., C.G., and D.C.; writing—original draft preparation, T.B., B.V., C.G., and I.M.; writing—review and editing, C.G., D.M., M.C., D.C., and M.A.P.; supervision, B.V., I.M., and T.B.; project administration, I.M., B.V., and T.B. All authors have read and agreed to the published version of the manuscript.

Funding

This research received no external funding.

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Acknowledgments

We hereby acknowledge the structural funds project PRO-DD (POS-CCE, O.2.2.1., ID 123, SMIS 2637, contract no. 11/2009) for providing the infrastructure used in this paper.

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. Centrifugal casting installation, with vertical rotation axis. (a) Experimental device, (b) casting process, (c) casting shell design.
Figure 1. Centrifugal casting installation, with vertical rotation axis. (a) Experimental device, (b) casting process, (c) casting shell design.
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Figure 2. Composite’s structural arrangement. (a) 30 min coating time, (b) 60 min coating time.
Figure 2. Composite’s structural arrangement. (a) 30 min coating time, (b) 60 min coating time.
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Figure 3. Presence of copper on the surface of the SiC particle observed. (a) By optical microscope, (b) by SEM analysis, (c) by EDS.
Figure 3. Presence of copper on the surface of the SiC particle observed. (a) By optical microscope, (b) by SEM analysis, (c) by EDS.
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Figure 4. SiC particles distribution within the metallic base alloy — V1. (a) Central embedded SiC particle (×200), (b) Cu on a SiC particle (×500), (c) SiC particles agglomeration (×200), (d) SiC particles agglomeration (×200).
Figure 4. SiC particles distribution within the metallic base alloy — V1. (a) Central embedded SiC particle (×200), (b) Cu on a SiC particle (×500), (c) SiC particles agglomeration (×200), (d) SiC particles agglomeration (×200).
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Figure 5. SiC distribution in the metallic base — V2. (a) Central embedded SiC particle (×200), (b) Cu on a SiC particle (×500), (c) SiC particles agglomeration (×200), (d) SiC particle embedded at sample surface (×200).
Figure 5. SiC distribution in the metallic base — V2. (a) Central embedded SiC particle (×200), (b) Cu on a SiC particle (×500), (c) SiC particles agglomeration (×200), (d) SiC particle embedded at sample surface (×200).
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Figure 6. SiC distribution in the metallic base — V3. (a) Central embedded SiC particle (×200), (b) SiC particles agglomeration (×200), (c) SiC particle embedded at sample surface (×200).
Figure 6. SiC distribution in the metallic base — V3. (a) Central embedded SiC particle (×200), (b) SiC particles agglomeration (×200), (c) SiC particle embedded at sample surface (×200).
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Figure 7. Comparative dilatometric analysis of the alloy and the composite.
Figure 7. Comparative dilatometric analysis of the alloy and the composite.
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Figure 8. Differential thermal analysis (DTA) curves during heating for aluminum alloy and for the composite aluminum alloy—SiC particles.
Figure 8. Differential thermal analysis (DTA) curves during heating for aluminum alloy and for the composite aluminum alloy—SiC particles.
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Figure 9. Differential thermal analysis (DTA) heating curve up to 800 °C for the composite aluminum alloy—SiC particles.
Figure 9. Differential thermal analysis (DTA) heating curve up to 800 °C for the composite aluminum alloy—SiC particles.
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Table 1. Chemical composition of the Al-Si alloy.
Table 1. Chemical composition of the Al-Si alloy.
ElementSiFeCuMnMgZnTiPbAl
[%]8,231,500,1170,1110,0620,1660,0220,01489,70
The sum of the elements is not 100% since the composition includes elements with very low concentrations.
Table 2. Working parameters.
Table 2. Working parameters.
Solution/SiCSiC, gCu Quantity in Solution, gMixing Time, minSamples CodesObservations
Activating solution5.0075100 30 Mixing
Filtration, washing
Calcination at 50 °C, 40 min
Coating solution21.625830VIa30
21.625860VIa60
86.412.5830VIb30
86.412.5860VIb60
172.812.5830VIc30
172.812.5860VIc60
Table 3. Results of EDS analysis on the studied material.
Table 3. Results of EDS analysis on the studied material.
Element LineNet CountsWeight, %Atom, %
C K29210.0118.82
O K101712.6917.90
Al K920350.5642.31
Si K333725.5620.55
Cu L951.180.42
Total 100.00100.00
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Milosan, I.; Bedő, T.; Gabor, C.; Munteanu, D.; Pop, M.A.; Catana, D.; Cosnita, M.; Varga, B. Characterization of Aluminum Alloy–Silicon Carbide Functionally Graded Materials Developed by Centrifugal Casting Process. Appl. Sci. 2021, 11, 1625. https://0-doi-org.brum.beds.ac.uk/10.3390/app11041625

AMA Style

Milosan I, Bedő T, Gabor C, Munteanu D, Pop MA, Catana D, Cosnita M, Varga B. Characterization of Aluminum Alloy–Silicon Carbide Functionally Graded Materials Developed by Centrifugal Casting Process. Applied Sciences. 2021; 11(4):1625. https://0-doi-org.brum.beds.ac.uk/10.3390/app11041625

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Milosan, Ioan, Tibor Bedő, Camelia Gabor, Daniel Munteanu, Mihai Alin Pop, Dorin Catana, Mihaela Cosnita, and Béla Varga. 2021. "Characterization of Aluminum Alloy–Silicon Carbide Functionally Graded Materials Developed by Centrifugal Casting Process" Applied Sciences 11, no. 4: 1625. https://0-doi-org.brum.beds.ac.uk/10.3390/app11041625

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