1. Introduction
Today, amorphous metallic alloys, also known as bulk metallic glasses (BMG), attract much attention as recent works report on new ways of production, high mechanical properties such as tensile strength, proportional limit, hardness, good wear behavior and corrosion resistance of these [
1,
2,
3]. For example, the American company “Liquidmetal” has patented a technology for the manufacture of products from BMGs for medicine and industrial needs [
4]. However, the application of the BMG alloys is not widespread, especially as structural materials. These materials are very sensitive to cooling rates during casting, which is the main method for their production. Therefore, the size and shape of the amorphous metals are limited.
In contrast to casting, selective laser melting (SLM) technology provides high cooling rates combined with the capability of complex-shaped parts building, while the dimensions of parts are only limited to the working zone of a machine. Applying SLM for obtaining BMGs provoked great interest in the past ten years indicating the promising outlook for this research area [
5,
6,
7,
8,
9]. Nevertheless, BMG alloys are difficult materials for laser processing as experimental works exposed partial crystallization of the obtained parts. However, according to Ouyang et al., the content of the crystalline phase could be controlled by processing parameters [
10]. The authors observed the crystalline phase in the heat-affected zone of the iron-based BMG. Similar findings were described for the zirconium-based BMGs. [
11,
12,
13,
14]. Further investigation revealed cracking of the iron-based BMGs during SLM resulting in poor strength, while zirconium-based ones were crack-free [
9,
16]. Due to high vitrification ability and crack resistance during laser processing zirconium alloys are found to be the most suitable for the SLM.
Pauly et al. experimentally proved that the SLM method can produce completely amorphous metal alloys with mechanical strength comparable to similar cast alloys [
17]. Common examination of the printed Zr-based BMGs to prove their key properties include indentation and nanoindentation [
5,
11,
18,
19], compression tests [
4,
5,
20], four-point bending [
18,
19], impact toughness and fatigue strength tests [
19,
20] and pin-on-disk wear behavior tests [
5,
18].
Of the known zirconium-based BMG alloys, the following commercial alloys have become widespread: Vit 1, Vit 106, Vit 106a and AMZ 4. The composition and basic thermal properties of these alloys are summarized in
Table 1. In this table, the composition of the alloys is listed in atomic percentages.
Based on this table, it was decided that the use of Vit 1 alloy in the work is hazardous to health. There are similarities in composition and properties between Vit 106, Vit 106a and AMZ 4 alloys, so it was decided to choose a more accessible material for research. In our case, Vit 106 turned out to be the more accessible material.
Previous works revealed partial crystallization of the BMGs during SLM [
25]. Research to date has not yet determined its influence on the properties of amorphous materials. Thus, this work aimed at studying the microstructure of the Vit-106 alloy after SLM and the influence of the features observed on the properties of the BMG material.
2. Materials and Methods
2.1. Materials
In total, 5 Vit-106 specimens were studied within this work. Specimen №1 was an as-received Vit-106 alloy plate. However, a defect layer is expected on the surface of the plate after casting in molds. Therefore specimen №2 was prepared by grinding an as-received plate on the depth of 30 µm. Specimen №3 is also a Vit-106 plate subjected to heat treatment in order to achieve full crystallization. Previous studies revealed the SLM process parameters that lead to partial crystallization of the Vit-106 alloy [
25]. These parameters were used for the SLM production of two 5-layered specimens No. 4 and No. 5 with different laser scanning speeds V, laser power P, powder layer thickness H and hatch distance S (
Table 2).
To obtain crystalline Vit-106 specimens, amorphous plates were annealed in a Termionik T1 vacuum furnace (JSC Termionik, Podolsk, Russia). Powder for the SLM process was manufactured by milling an amorphous Vit-106 chip in distilled water in a planetary ball mill Retsch pm100 (Retsch, Haan, Germany). An amorphous Vit-106 chip was obtained by machining Vit-106 plates. The average size of powder particles was controlled by optic microscopy every 15 minutes. Because milling time is a key parameter that determines the size of powder particles. Short time results in coarse particles and a broad range of sizes while long milling leads to submicron particles. Therefore, an experimentally optimal time for powder production with an average particle size of 50 µm required for most SLM machines was found (
Table 3). Since it is impossible to obtain a spherical shape by ball milling, irregularly shaped 20-50 µm powder was used in the current work. After milling, the powder was dried and sieved to provide a 20-50 µm particle size interval.
Figure 1 demonstrates the prepared powder.
2.2. SLM
A Laboratory SLM rig was used to build multilayered specimens. The process took place in an argon atmosphere to prevent oxidation. Amorphous Vit-106 plates were used as a substrate. For the obtained samples, the scanning speed is as the only variable parameter, since it influences the cooling rate, and consequently the crystallization, more than the other parameters.
2.3. Characterization
The microstructure of the specimens was studied by optic microscopy Olympus BX 51 (Olympus Corp., Tokyo, Japan) and scanning electron microscopy Phenom ProX (Phenom-World BV, Eindhoven, The Netherlands). The chemical composition of the alloy Zr59Cu14.3Ni11.9Al9.3Nb5.5 was confirmed by energy-dispersive analysis (EDX) in [
25]. In addition, the content of oxygen was measured by the method of reductive melting of material in a helium flow using a Leco TC-600 analyzer (LECO Corporation, St. Joseph, MI, USA). The cross sections of the specimens were polished prior to studying. To increase the contrast for the optic microscopy, some cross sections were etched with a mixture of hydrofluoric and nitric acids. X-ray diffraction (XRD) analysis was used to determine the phase composition of the samples. XRD patterns were obtained by PANalytical Empyrean X-ray diffractometer with CuK
a radiation. Phase composition analysis was performed by PANalytical High Score Plus software, software [
26] and ICCD PDF-2 and COD databases [
27].
Microhardness was measured by the indentation method with loads of 50 g and 500 g for 10 seconds using a Tykon 2500 microhardness tester (TUKON, Norwood, MA, USA). Each specimen was measured 9 times on the preliminary polished surface and cross section. The indentation was located 70 µm away from the edge.
Tribological pin-on-disk tests were performed on the Ducom tribometer (DUCOM, Bangalore, India) at the load of 10 N and sliding velocity 200 min-1 for 900 seconds. A ceramic 6 mm Al2O3 ball was used as a counterbody. The depth of the wear tracks was measured on the Hommel Tester 8000 prophilograph (Jenoptik, Jena, Germany). The roughness of each specimen was measured in two perpendicular directions.
3. Results
3.1. Microstructure and phase composition
Figure 2 shows the cross sections of the specimens № 4 and № 5 at different magnifications. Common SLM microstructure features such as melt pool fragments are observed. Material flows are clearly seen in SEM images (
Figure 3) which are attributed to high viscosity. Similar phenomena were found in silicon glasses subjected to SLM processing [
28]. In contrast to specimen № 5, specimen № 4 had crystalline phases at the layer-substrate interface (
Figure 3). It is possible that lower scanning speed V provoked the crystallization of the sublayers. In specimen № 4, coarser inclusions were detected at the boundary of the vortex (
Figure 3 b, d, Zone I) than inside (
Figure 3 b, d, Zone I). Meanwhile, specimens № 4 had areas free from such inclusions. In addition, Zone III with clear white inclusions around black ones was distinguished in
Figure 3 b. Being bright, the inclusions presumably are lighter phases with deterioration of aluminum. Specimen № 5 demonstrated no such precipitations as dark inclusions were surrounded by homogenous grey areas. Dark areas observed in the microstructure are presumably either the intermetallic Al inclusions or oxide crystals as raw material contains 0.058 % wt. of oxygen.
Figure 4 shows the XRD patterns of the raw alloy, powder and specimens № 3-5. Powder and raw plate share a very similar profile indicating that both materials are in an amorphous state. After annealing the material became crystalline as the “amorphous halo” was no longer observed. Multilayered specimens were found to be partially crystallized as the “amorphous halo” appeared as a smooth part of the curve with its highest intensity at 2θ=39°. Along with that peaks identified as Zr
3O and Al, Zr and Cu intermetallic compounds were revealed. Therefore, the obtained specimens were partially crystalline.
3.2. Mechanical and tribological properties
Figure 5 shows the results of the microhardness tests on the surface of the specimens at 50 g and 500 g. Since no significant difference between the results of the specimens № 1 and № 3 was observed the 50 g tests for specimen № 2 were not performed. Microhardness of the cross sections was measured only for the multilayered specimens made from powder (figure 6). The highest value of 883 HV was demonstrated by the annealed crystalline plate, while the lowest (530 HV) value was measured for the raw amorphous alloy. The microhardness of the SLM specimens was closer to the amorphous ones. Being obtained at the fastest scanning speed, specimen № 5 had the closest to amorphous state hardness value. This may be attributed to the size of crystalline inclusions that grow at low scanning speeds and, hence, low cooling rates [
29]. The hardness results of the fully crystalline specimen № 3 showed a large mean square deviation which was possible due to the size of the crystalline phase which can be comparable to the indentation size (figure 7). The deviation range reduces with the growth of load which increases the size of the dint and averages the contribution of the main material and crystalline inclusions.
The results of tribological tests and roughness measurements are given in
Table 4. Average roughness is neglectable comparing to a wear track depth and it did not affect the results. The maximum profile depth was measured as shown in
Figure 8.
4. Discussion
The obtained multilayered SLM specimens №4 and №5 consisted of an amorphous matrix with crystalline inclusions that spread inhomogeneously and formed a vortex structure. Lower scanning speed V=350 mm/s resulted in coarser inclusions in the substrate-alloy interface and vortexless structure (
Figure 2b). The vortices in the remelted zone were measured to be around 100 μm (
Figure 2 b, d), which corresponds to melt pool size under these conditions [
21]. It can be suggested that either crystalline inclusions or their nuclei are transported by convective melt flows. The surface of the melt material could serve as the source for the nucleates given that a small content of oxides is expected due to residual oxygen in the shield gas. Oxidation was earlier reported to provoke crystallization in Zr-based BMGs [30]. Zr
3O and other oxides were found in the specimens studied within this work (
Figure 5).
Dark inclusions in BSE SEM figures are presumably enriched with light elements which may be attributed to the oxides (
Figure 3), Meanwhile, there is a bright halo around the inclusions which suggests the deterioration of the matrix with light elements (
Figure 3 b, d). Thus, it can be concluded that during solidification the inclusions grow due to the diffusion of light elements from the matrix to them. The list of such elements includes oxygen dissolved in the matrix and lighter elements of the alloy Al, Ni, Cu, that form CuZr
2 intermetallic compound in raw material and Al
2Zr
3 и NiZr
2 compounds after annealing (
Figure 4). However, the corresponding intermetallic lines of the specimens are not clear in the XRD patterns (
Figure 4). Therefore, the observed inclusions mainly consist of ZrO
3.
The inclusions in the remelted zone are submicron, and the higher the laser scanning speed the smaller the inclusions (
Figure 3 b, d). The number of inclusions per unit area also decreases. It follows the model for homogeneous nucleation and nuclei growth. Indeed, the cooling rate increases with accelerating the laser scanning speed during solidification which reduces the time of homogeneous nucleation and inclusions grow. Therefore, the concentration and the size of the inclusions are anticipated to be smaller.
An amorphous plate with CuZr
2 intermetallides was taken for the multilayered specimens 4 and 5 [
21]. These inclusions are observed in the nontreated area in
Figure 3 a, c. Part of the substrate material close to the remelted layers is exposed to repeated thermal effects of a laser beam which may cause the growth of these inclusions. This is evidenced by the increased volume of the CuZr
2 particles (
Figure 3b). The size of the typical inclusion reaches 20 μm (
Figure 7). Higher laser scanning speed increases the cooling rate reducing the time of thermal exposure in the range where intensive crystal growth is possible. Therefore, faster scanning speed results in less intense growing of the inclusions.
The coefficient of friction (CoF) of the multilayered specimens remained almost the same as the raw material. At the same time, the wear track depth was significantly less indicating the positive influence of the submicron crystalline inclusions on wear resistance. Interestingly, that wear resistance slightly improves with increasing laser scanning speed from 350 mm/s to 700 mm/s. Obviously, smaller inclusions are beneficial for better wear resistance.
The microhardness of the SLM specimens was found to be higher than for raw material (
Figure 6). This is also explained by the strengthening effect of submicron crystalline inclusions. At the same time, with increasing scanning speed, the microhardness decreases slightly. This trend is opposite to the effect of scanning speed on wear resistance and may be due to a decrease in the volume fraction of the crystalline phase with increasing scanning speed.
The results obtained show that submicron crystalline inclusions formed in an amorphous matrix during SLM can favorably affect mechanical properties such as microhardness and wear resistance. Correlations were revealed between these properties and such structural parameters as size, concentration and volume fraction of inclusions. The influence of such an important process parameter as scanning speed on the forming amorphous-crystalline structure is also shown. All these results can find practical application in the manufacture of structural elements from Zr-based BMG using SLM. At the same time, further systematic study of the influence of oxygen content in the starting material and possible partial oxidation from the gas phase on the forming microstructure, as well as the influence of microstructure on properties, is required.
5. Conclusions
Within this study, multilayered SLM specimens from Vit-106 were obtained, their microstructure was investigated, microhardness and tribological behavior were tested.
The SLM specimens consisted of an amorphous matrix with two types of crystalline inclusions. Submicron CuZr2 particles were found in the remelted vortex structure, while coarser up to 20 µm CuZr2 were observed in the heat-affected zone of the substrate. The nature of the distribution of submicron inclusions shows that they can grow from oxide nuclei transported by convection in the melt pool.
Large crystals in the thermally affected zone are most likely formed during the growth of intermetallic inclusions initially contained in the substrate material.
Submicron crystalline inclusions increase wear resistance and can increase microhardness. The role of oxygen in the formation of the amorphous-crystalline structure, as well as the influence of structural parameters on mechanical properties requires further research.
Author Contributions
Conceptualization, A.V.G. and R.S.Kh.; methodology, R.S.Kh.; software, M.G.; validation, A.V.G., T.V.T and P.P.; formal analysis, P.P.; investigation, R.S.Kh., A.K., M.G.; resources, M.G.; data curation, P.P.; writing—original draft preparation, R.S.Kh., A.V.G.; writing—review and editing, P.P.; visualization, A.K.; supervision, R.S.Kh.; project administration, A.V.G.; funding acquisition, A.V.G. All authors have read and agreed to the published version of the manuscript.
Funding
This work was supported by the Russian Science Foundation (Grant Agreement No. 21–19-00295, https://rscf.ru/project/21-19-00295/).
Data Availability Statement
Data supporting the reported results can be found from the authors.
Acknowledgments
The study was carried out on the equipment of the Center of Collective Use “State Engineering Center” of the MSUT “STANKIN” (project 075-15-2021-695, unique id RF----2296.61321X0013).
Conflicts of Interest
The authors declare no conflict of interest.
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