2022 Volume 63 Issue 6 Pages 835-844
Non-equiatomic high-entropy alloys (HEAs) for which the mixing (Smix), configuration (Sconfig), and equivalent ideal (Sideal) entropies satisfy Smix > Sconfig = Sideal were reported for Co–Cr–V–Fe–(Al, Ru, or Ni) systems. Three Co20Cr20Fe20V10X30 (X = Al, Ru, or Ni) alloys (referred to as Al30, Ru30, and Ni30 alloys) were studied here using conventional arc melting and subsequent annealing. The X-ray diffraction profiles revealed that the Al30, Ru30, and Ni30 alloys annealed at 1600 K for 1 h exhibited B2 ordered, hcp, and fcc structures, respectively. A single structure was verified by scanning electron microscopy observations combined with elemental mapping via energy-dispersive X-ray spectroscopy. Thermodynamic calculations of Smix normalized by the gas constant (Smix/R) revealed that Al30, Ru30, and Ni30 alloys at 1600 K had Smix/R = 0.833, 1.640, and 1.618, respectively, where the latter two alloys exceeded Sconfig/R = 1.557. A compositionally optimized Al-containing HEA for Smix with a single bcc structure was computationally predicted and verified experimentally for the Al6Co27Cr34Fe19V14 alloy (Al6 alloy). The non-equiatomic Al6 alloy with Sconfig/R = 1.480 exhibited Smix/R of 1.703 at 1600 K, surpassing Sconfig/R = ln 5 = 1.609 for the exact equiatomic (EE) quinary alloy. The bcc Al6, hcp Ru30, and fcc Ni30 alloys were regarded as ultra-high mixing entropy alloys (UMHEAs) according to Smix > Sconfig. Structure-dependent Smix and the mixing enthalpy of constituent binary EE alloys are useful for future UHMEAs as a subset of HEAs.
The present study addresses the systematic development of high-entropy alloys (HEAs)1,2) by utilizing precise thermodynamic calculations based on the CALculation of PHase Diagram (CALPHAD) scheme. The specific objective is to develop non-equiatomic HEAs, with the mixing (Smix), configuration (Sconfig), and its equivalent ideal entropies (Sideal) satisfying Smix > Sconfig (= Sideal). The variation of Smix from Sconfig is frequently discussed in some literature.3–6) Followed by these early studies, the present authors adopted a thermodynamic approach and calculated the value of Smix using Thermo-Calc7,8) and a specially designated database for HEAs (TCHEA4). The present study was motivated by the authors’ previous precise thermodynamic calculations,9) indicating that Smix < Sconfig (= Sideal) holds for most of the exact equiatomic (EE) HEAs with a single bcc structure; in particular, for Al-containing bcc EE HEAs. Only one exception was reported,9) for the bcc CrMoNbTaTiVZr HEA10) at 1300 K, with Smix/Sconfig = 1.004. In addition to bcc EE HEAs, six of the nine fcc EE HEAs at 1600 K exhibited Smix < Sconfig, except the fcc CoCrFeMnNi HEA2) with Smix/Sconfig = 1.087, the fcc CoCuFeMnNi HEA11) with Smix/Sconfig = 1.003, and the fcc CuIrNiPdPtRh HEA12) with Smix/Sconfig = 1.032. In addition, it was reported9) that hcp EE HEAs13–15) comprising heavy lanthanides with and without Y behaved as an ideal solution, exhibiting Smix/Sconfig = 1. Among the above exceptions, the authors have come to recognize that those HEAs that satisfy Smix > Sconfig are ultra-high mixing entropy alloys (UHMEAs), for which the solid solution is more stable than for conventional HEAs, owing to Smix > Sconfig. The significance of UHMEAs lies in the fact that Smix > Sconfig differs from N-element EE HEAs that merely exhibit large Sconfig (= Sideal) = ln N owing to high N. The previous study9) was performed for EE HEAs only; thus, it is worth exploring UHMEAs by extending the category of HEAs to non-equiatomic types.
In the present study, single-phase non-equiatomic HEAs with bcc, hcp, and fcc structures and with Smix/Sconfig > 1 were fabricated as UHMEAs.
The reference alloy for UHMEAs was the fcc Co20Cr20Fe20Mn20Ni20 HEA (the Cantor alloy);2) the motivation was to fabricate bcc, hcp, and fcc UHMEAs by optimizing the components and compositions of the reference alloy. The authors’ strategy for the development of UHMEAs was to determine a prototypical alloy consisting of main/common and supplemental inclusions. The main inclusion was to be composed of a set of common components and compositions, whereas the supplemental one was a structure-designated element (forming element, former, or structure determinant) intended to form a single bcc, hcp, or fcc structure. Such alloy design, controlling the structure with forming elements, such as Al, Ru, and Ni for bcc, hcp, and fcc structures, was somewhat different from the conventional ones, focusing on the similarities between elements with respect to their chemical features and/or geometrical factors in terms of their atomic differences. Taking HEAs as example metallic materials, Cu can be substituted by Ni and vice versa, owing to exchangeability.16) The exchangeability works for Ti, Zr, and Hf in the same group in the periodic table. The role of exchangeability in metallic materials can be the same as isomorphous substitution17) between Si4+ and Al3+ in oxides and clay minerals18) in high-entropy ceramics and oxides.
The following section describes two essential aspects of determining a prototypical alloy. The first aspect is based on the authors’ previous analysis9) of Smix, revealing that Cr–Mn and Co–Cr atomic pairs, respectively, in the Co20Cr20Fe20Mn20Ni20 HEA significantly decreased and increased Smix relative to Sconfig. This led to the selection of Cr and omission of Mn as constituent elements. The second aspect, based on a preliminary study, was the use of a private database for interaction parameters Ωij(ci, T) of a sub-regular solution model. Specifically, the values of Ωij(ci, T) were stored in a private database from a previous database for solid solutions (SSOL4) where its latest version is SSOL8.19) As for the extraction procedure, the authors referred to the contents described in the Thermo-Calc user’s manual. The values of Ωij(ci, T) were stored as a function of the content of the i-th element (ci) and absolute temperature (T). The analysis of Ωij(ci, T) suggested that Co–Cr, Cr–Fe, Cr–Ni, Co–V, and Fe–Ni atomic pairs in the bcc structure tended to increase Smix owing to the negative sign9) of the temperature coefficient of Ωij(ci, T). On the other hand, Mn-containing atomic pairs also exhibited a similar tendency, but atomic pairs were limited to Mn–Cu and Mn–Zr. Hence, the constituent elements of Mn with the ability to increase Smix were not included in the constituent elements of the reference Co20Cr20Fe20Mn20Ni20 HEA. These aspects led to the substitution of Mn with V while retaining Cr, leading to the EE Co20Cr20Fe20Ni20V20 alloy as a prototypical alloy.
Subsequently, the composition of the prototypical EE Co20Cr20Fe20Ni20V20 alloy was optimized in terms of the appearance of the fcc structure, resulting in the Ni30 alloy (Co20Cr20Fe20Ni30V10) as the first candidate for UHMEAs. Preliminary thermodynamic calculations revealed that stabilizing the Ni30 alloy as an fcc HEA was achieved by suppressing the precipitation of the sigma (σ) phase. Then, the Al30 alloy was considered as the second candidate for UHMEAs by replacing Ni from the fcc-former with Al from the bcc-former.1) Finally, the Co20Cr20Fe20Ru30V10 alloy was considered as the third candidate for UHMEAs in the same replacing scheme by referring to the literature.20) In deciding Ru as an hcp-former, the authors focused on the ratio of the compositions of cFe:cRu = 2:3. This ratio matches the formation of an hcp structure from the Fe–Ru binary phase diagram21) by referring to the authors’ previous work20) for the hcp Fe12Ir20Re20Rh20Ru28 HEA. Hence, it was expected that Ru would affect the formation of hcp UHMEAs with the help of Fe. The features of the three UHMEA candidates all had in common that the Co20Cr20Fe20V10 as the main/common inclusion was accompanied by structural determinants of Al, Ru, and Ni, from bcc-, hcp-, and fcc-former.
2.2 Thermo-Calc and TC-PythonThermodynamic calculations were performed using Thermo-Calc7,8) ver. 2021a, using the TCHEA4 database. The details of the calculations of Smix and other thermodynamic quantities were the same as those in the authors’ previous studies.9) An important aspect of calculating Smix was to set it to zero for pure constituent elements, which was achieved by selecting the designated structure as the standard element reference (SER).9) A compositionally optimized alloy for Smix/R was modeled using TC-Python22) which is a Python™ language-based software development kit available with Thermo-Calc. TC-Python allows for easy and flexible coupling of Thermo-Calc calculations with other software programs. The optimization eventually resulted in the Al6Co27Cr34Fe19V14 alloy (Al6 alloy).
2.3 ExperimentsAlloy ingots (weight, 5 g) with nominal compositions of Al30Co20Cr20Fe20V10, Co20Cr20Fe20Ru30V10, and Co20Cr20Fe20Ni30V10 (at%) alloys (Al30, Ru30, and Ni30 alloys) were prepared via arc-melting from raw metals with industrial purity of 99.99%Co, 99.9%V, 99.995%Ni, 99.9%Cr, 99.99%Al, 99.95%Fe, and 99.9%Ru. The raw materials in the form of fragments and Ru powders were weighed at the designed molar ratio and mixed uniformly in a mixer. The 5-g samples were formed into button-shaped ingots (diameter, ∼10 mm; height, ∼5 mm). After arc melting, the samples were annealed at a high temperature to confirm the equilibrium phases. The as-prepared ingots were annealed for 1 h with a magnesium oxide crucible as the contacting material in an electric furnace. The annealing temperature was fixed at 1600 K, which was determined by preliminary thermodynamic calculations using Thermo-Calc. The chamber of the furnace was vacuumed (∼10−2 Pa) in advance and then filled with high-purity Ar gas at ambient pressure. The samples were homogenized by annealing, followed by cooling in a furnace or quenching in water. The cross-sections of these alloys, which were cut into two pieces perpendicular to the base, were examined for their structure using X-ray diffraction (XRD). Co radiation with a wavelength (λ) of 0.1788965 nm (Co-Kα1) was used for the XRD analysis. The samples’ morphologies were studied using scanning electron microscopy (SEM) as secondary electron (SE) images, and the distributions of the elements in the same area as the SE images were analyzed using energy-dispersive X-ray spectroscopy (EDX) equipped with SEM.
2.4 Numerical calculation of thermodynamic and physical quantitiesIn the authors’ previous studies, the following thermodynamic and physical quantities were computed using conventional procedures:23,24) configuration entropy normalized by the gas constant (Sconfig/R), mixing enthalpy (ΔHmix) calculated using Miedema’s empirical model, the delta parameter (δ), the valence electron concentration (VEC),25) and Smix. The present study intentionally distinguished between ΔHmix and Hmix, with the former corresponding to the mixing enthalpy calculated using the Miedema model, while the latter was computed using Thermo-Calc. Based on simple deductions of these quantities and on previous studies, Sconfig was equivalent to the ideal entropy (Sideal), ΔHmix was calculated by referring to literature,26–28) and δ corresponded to the difference between the constituent atomic sizes.29) By contrast, the VECs of transition metals (TMs) and alloys containing TMs were calculated by averaging the intrinsic VEC of the i-th element (VEC)i. Then, (VEC)i corresponded exactly to the number of groups in the periodic table of the constituent i-th element, except for Al, for which (VEC)Al was 3 by referring to the original literature.25) A detailed description of the Smix calculation scheme can be found in the authors’ previous work.9)
Figure 1 shows that the (a) Al30, (b) Al6, (c) Re30, and (d) Ni30 alloys exhibited a single phase for temperatures around 1600 K. As a reference, Fig. 1(e) shows that the common inclusion, Co20Cr20Fe20V10 (the Co28.5714Cr28.5714Fe28.5714V14.2857 alloy), tended to exhibit a mixture of bcc, hcp, and fcc structures in the intermediate range of temperatures (800–1600 K), while it exhibited a single bcc region within 80 K just above 1500 K. This narrow temperature interval was not advantageous for the reference case in Fig. 1(e) (Co20Cr20Fe20V10, the Co28.5714Cr28.5714Fe28.5714V14.2857 alloy) to form a single bcc phase. Figure 1 shows that a chaotic state in a mixture structure of the common inclusion in Fig. 1(e) was eliminated in Figs. 1(a), (c), (d) by adding structure-forming elements. The predicted stable structure at ∼1600 K was a B2-ordered structure for (a) the Al30 alloy, hcp for (c) the Ru30 alloy, and fcc for (d) the Ni30 alloy, as well as bcc for (b) the Al6 alloy as an optimized alloy for Smix. These predicted structures were confirmed by preliminary experiments for as-prepared ingots without being subjected to annealing (XRD data for ingots are not shown in the present paper).
Property diagrams, calculated using Thermo-Calc 2021a and the TCHEA4 database, for (a) Al30, (b) Al6, (c) Re30 and (d) Ni30 alloys, together with (e) Co20Cr20Fe20V10 (Co28.5714Cr28.5714Fe28.5714V14.2857 alloy) as the common inclusion for comparison.
Figure 2 shows the XRD patterns for the (a) Al30, (b) Al6, (c) Ru30, and (d) Ni30 alloys annealed at 1600 K for 1 h. Annealing of the Al30, Ru30, and Ni30 alloy samples was followed by furnace cooling, whereas annealing of the Al6 alloy sample was followed by quenching in water. A preliminary experiment revealed that water quenching, instead of furnace cooling, was necessary for the annealed Al6 alloy sample, to suppress a mixture of complicated compounds. The XRD profiles shown in Fig. 2 demonstrate that the alloys exhibited distinct peaks corresponding to the presence of crystalline grains. From the XRD patterns, the structures of the alloys were identified as chemically ordered B2 for the Al30 alloy, bcc for the Al6 alloy, hcp for the Re30 alloy, and fcc for the Ni30 alloy. As shown in Fig. 2(a), the Al30 alloy sample exhibited a (100) chemically ordered reflection peak at 2θ ∼ 36°, accompanied by faint-ordered reflections from (111) and (210) at 2θ ∼ 65° and ∼ 88°, respectively. In addition, Fig. 2(a) reveals weak shoulder peaks at each right side (high 2θ side) of the reflection peak, except for the (111) and (210) reflection peaks. These shoulder peaks were attributed to the Co-Kα2 radiation with λ = 0.179285 nm, owing to the high crystallinity (fine crystalline grains) of the Al30 alloy. The appearance of the shoulder peaks was preliminary confirmed experimentally for standard pure Si powders.
XRD patterns measured using the Co-Kα radiation, for Al30, Al6, Re30, and Ni30 alloys annealed at 1600 K for 1 h.
Specifically, λ = 0.179285 nm of the Co-Kα2 radiation was approximately 0.217% longer than that of the Co-Kα1 radiation with λ = 0.1788965 nm, explaining the presence of the shoulder peaks at the high 2θ side owing to the Co-Kα2 radiation. The differences between the ordered B2 and disordered bcc structures of the Al30 and Al6 alloys, respectively, were supported by the thermodynamic calculation results, as shown in Fig. 1.
Further investigations were performed using the SEM and EDX methods. Figure 3 shows an SE image and EDX element mapping images, for the Al30 alloy annealed at 1600 K for 1 h. The SE image reveals different-brightness grains, with sizes ranging from a few to several hundred micrometers. The EDX mapping images at the same location as the SE image revealed a homogeneous distribution of constituent elements both inside the grains and over other grains, including the grain boundary under the current observation conditions of a few hundred micrometer scale or more. The experimental results in Figs. 1–3 indicate that the Al30 alloy annealed at 1600 K for 1 h had a single B2 structure. Similar SE and EDX images were observed for the Al6, Ru30, and Ni30 alloy samples (The data are not shown in the present paper).
SE image obtained using SEM, and element-mapping images obtained using EDX, for the Al30 alloy annealed at 1600 K for 1 h.
The estimated lattice constants of the Al30, Al6, and Ni30 alloys with the B2, bcc, and fcc structures were aB2 = 0.2884 nm, abcc = 0.2890 nm, and afcc = 0.3590 nm, respectively. The aB2 and abcc values were close to aCr,bcc = 0.28846 nm, whereas the afcc value was near aCo,fcc = 0.3544 nm. On the other hand, the lattice constants for the Ru30 alloy were ahcp = 0.2617 nm and chcp = 0.4201 nm, and the resultant ratio was c/a = 1.605. These data were not close to aRu,hcp = 0.2706 nm, cRu,hcp = 0.4458 nm, and (c/a)Ru,hcp = 1.5824, although the Ru30 alloy contained as much as 30 at%Ru as the major component.
The above results were analyzed based on the thermodynamic and physical properties of the alloys, as listed in Table 1. The Al30, Al6, Ru30, and Ni30 alloys exhibited VECs of 6.0, 6.87, 7.5, and 8.1, respectively, while the value of Sconfig/R was the same (1.557) for the Al30, Ru30, and Ni30 alloys, and was 1.480 for the Al6 alloy. The values of ΔHmix/kJ mol−1, computed using the Miedema model and based on the original literature,26,30) ranged from approximately −7.1 to −14, somewhat larger and more negative than the values for conventional HEAs,29) for which ΔHmix/kJ mol−1 ranges from 0 to −5. The value of δ was in the 2.5–3.7 for the Ni30, Ru30, and Al6 alloys with the bcc, hcp, and fcc structures, respectively; these values were within the δ values range (0.4–4.6) for disordered HEAs.29) On the other hand, the value δ = 5.5 for the Al30 alloy with the B2 structure was also in the range for ordered HEAs (4.6 < δ < 6.4).29)
Table 1 contains further precise calculation results for Smix/R, obtained using Thermo-Calc. The Smix/R values for the Al30, Al6, Ru30, and Ni30 alloys were 0.833, 1.703, 1.640, and 1.618, respectively. These results indicate that the Ru30 and Ni30 HEAs, respectively, have larger values of Smix/R = (1.640, 1.618) than Sconfig/R = 1.557, and that the Al6 HEA also has a higher value of Smix/R = 1.703 than Sconfig/R = 1.480. Hence, Al6, Ru30, and Ni30 alloys were regarded as a new class of UHMEAs, because they satisfy Smix > Sconfig, together with the CoCrFeMnNi HEA reported based on the authors’ previous precise thermodynamic calculations.9) The ratio of Smix (at 1600 K)/Sconfig was as high as 1.15 for the Al6 alloy, the highest reported value.
In the HEA literature, Smix is often presented as Sconfig or its equivalent Sideal. This misrepresentation can be avoided by recognizing that Smix is the sum of Sconfig and the excess entropy Sexcess, as expressed by eq. (1)
\begin{equation} S_{\text{mix}}=S_{\text{ideal(config)}}+S_{\text{excess}} \end{equation} | (1) |
The following considers only Sexcess in the reversible process based on the authors’ previous achievements.9) In the case of EE alloys as the simplest example, Smix(T) of the multi-component alloy of interest can be obtained by averaging the quantity of the constituent binary alloys over the contents of the alloy. Other alloys with non-equiatomicity can be dealt with using eq. (2) for Sexcess, similar to eq. (3) for Hmix, which is the formulation of a sub-regular solution model. $\varOmega_{\text{ij}(\text{A}_{50}\text{B}_{50})}$ on the right-hand side of eq. (3) is a constant at the binary equiatomic A–B compositions of A50B50, and is a simple case of Ωij(ci, T). Replacing $\varOmega_{\text{ij}(\text{A}_{50}\text{B}_{50})}$ in eq. (3) with $S_{\text{excess}(\text{A}_{50}\text{B}_{50})}$ yields eq. (2).
\begin{equation} S_{\text{excess}} = 4\sum_{j = 1}^{N}\sum_{i > j}^{N}S_{\text{excess(A${_{50}}$B${_{50}}$)}}c_{i}c_{j} \end{equation} | (2) |
\begin{equation} H_{\text{mix}} = 4\sum_{j = 1}^{N}\sum_{i > j}^{N}\Omega_{\text{${ij}$(A${_{50}}$B${_{50}}$)}}c_{i}c_{j} \end{equation} | (3) |
\begin{align} &S_{\text{mix(alloy),approx}}/R \\ &\quad = (S_{\text{ideal(=config)}} + S_{\text{excess}})R = -\sum_{i = 1}^{N}c_{i}\ln c_{i} \\ &\qquad + 4\sum_{j = 1}^{N}\sum_{i > j}^{N}\{S_{\text{mix,i-j}}/(R\ln 2) - 1\}c_{i}c_{j} \end{align} | (4) |
An example of the structure dependence of Smix is presented in Table 2. A feature of the Co20Cr20Fe20V10 main inclusion lies in the high value of $S_{\text{mix}(\text{A}_{50}\text{B}_{50})}/(R\ln 2)$ ∼ unity or more for most of the constituent atomic pairs consisting of Co, Cr, Fe, and V for the yellow-hatched columns. Only a set of exceptions was observed in the Co–V atomic pair for the hcp and fcc structures. Table 2 indicates that the efficient selection of atomic pairs with $S_{\text{mix}(\text{A}_{50}\text{B}_{50})}/(R\ln 2) > 1$ leads to UHMEAs. In addition, large and negative values of $S_{\text{mix}(\text{A}_{50}\text{B}_{50})}/(R\ln 2)$ are shown in red letters in Table 2 for atomic pairs with Al mainly, indicating a decrease in Smix for the alloys with Al as a constituent element.
The Smix values of EE-HEAs can be calculated even for a multi-component alloy with N elements, just by averaging the values of $S_{\text{excess,i-j}} \equiv S_{\text{excess}(\text{A}_{50}\text{B}_{50})}$ over the constituent atomic pairs. Equation (4) explains the actual approximation procedure for estimating Smix of an alloy, Smix(alloy),approx, using the values of $S_{\text{mix}(\text{A}_{50}\text{B}_{50})}/(R\ln 2)$ listed in Table 2. The term, Smix,i-j/(R ln 2) − 1, in eq. (4) corresponds to Sexcess, and is zero for ideal solutions. The first term on the right-hand side of eq. (4), $ - \sum_{i = 1}^{N}c_{i}\ln c_{i}$, corresponds to Sconfig, where the coefficient four on the right side of eq. (4) is required to compensate for the cicj term at the equiatomic composition (ci = cj = 0.5). The estimation using eq. (4) and the data from Table 2 yielded Smix/R = 1.506 for the Al6 UHMEA, 0.737 for the Al30 HEA, 1.647 for the Ru30 UHMEA, and 1.658 for the Ni30 UHMEA. Comparisons of Smix/R in Table 2 indicate that the evaluations based on eq. (4) and Table 2 were valid at the rates of 88.5%, 96.7%, 99.6%, and 102.5% for the Al6 UHMEA, Al30 HEA, Ru30 UHMEA, and Ni30 UHMEA, respectively. The relative error between the value of Smix using eq. (4) combined with the data from Table 2 and the thermodynamical Smix computed using Thermo-Calc was at most 10%. The parabolic approximation as a function of ci for the second term on the right-hand side of eq. (4) mainly caused errors. Specifically, the inclusion of 10 at%V and 30 at%X (X = Al, Ru, or Ni) degraded the estimation accuracy for the Al30 HEA, Ru30 UHMEA, and Ni30 UHMEA, whereas as small as 6 at% inclusion of Al as well as non-equiatomicity of Al6 UHMEA yielded the worst accuracy. However, the estimation of Smix using eq. (4) provided acceptable reliability when considering the simple formulae in eq. (4), based on the empirical method for estimating Smix. In contrast, the values of $S_{\text{mix}(\text{A}_{50}\text{B}_{50})}/(R\ln 2)$ listed in Table 2 provide a useful guide for judging whether the alloys of interest are suitable for forming UHMEAs by their magnitude of $S_{\text{mix}(\text{A}_{50}\text{B}_{50})}/(R\ln 2) > 1$.
4.2.2 Structure-dependent HmixIn Table 2, large and negative values of $S_{\text{mix}(\text{A}_{50}\text{B}_{50})}/(R\ln 2)$ are listed in red letters for atomic pairs with Al mainly, decreasing Smix of the alloy when Smix/R is estimated by eq. (4). A similar large and negative value of $H_{\text{mix}(\text{A}_{50}\text{B}_{50})}$ for atomic pairs with Al is listed in Table 3. This similarity between $S_{\text{mix}(\text{A}_{50}\text{B}_{50})}$ and $H_{\text{mix}(\text{A}_{50}\text{B}_{50})}$ indicates that the inclusion of Al in an alloy efficiently leads to the formation of a single bcc (or B2) HEAs, owing to large and negative Hmix, but the resultant alloy does not exhibit a high Smix value for HEAs. This decrease in Smix should be compensated by the decrease in Hmix in the framework of the formula Gmix = Hmix − TSmix, for maintaining the Gmix stabilization by decreasing Gmix. Hence, it is understood that Al-containing HEAs can be of the Hmix-HEA type, rather than of the Smix-HEA type. This proves that the bcc and B2 structures were formed in the present study for the A6 and A30 alloys, respectively, suggesting that a large amount of Al inclusions enhanced the chemical ordering owing to the large and negative Hmix value. The above suggestion was supported by the ΔHmix value calculated using the Miedema model (Table 1) where ΔHmix/kJ mol−1 = −8.3 for the Al6 alloy and −14.3 for the Al30 alloy.
The above values of ΔHmix were not sufficiently valid because of the following two aspects. First, the ΔHmix value used for the evaluation was originally derived for the EE-binary liquid phase,26,30) to use ΔHmix for evaluating the forming ability of amorphous and glassy alloys. Second, the atomic pairs of TM and non-TM (NTM) (where NTM includes Al) were not precisely treated, owing to the limitation on ΔHmix for the liquid phase. Specifically, as has been reported,32) ΔHmix of a solid solution including Al from NTM should be modified by considering the R term (≠ gas constant R) in addition to the P and Q terms.27) The alternatively calculated Hmix values using Thermo-Calc and the TCHEA4 database (and assuming the temperature of 1600 K) instead of ΔHmix calculations using the Miedema model for the TM-NTM in the state of solids for the Al6 and Al30 alloys were Hmix/kJ mol−1 = −3.043 and −25.980, respectively. These values of Hmix, computed using Thermo-Calc and the TCHEA4 database, and assuming the temperature to be 1600 K, also supported the tendency of the Al30 alloy to exhibit considerably larger and more negative Hmix than the Al6 alloy, indicating the Hmix-HEA type of the Al30 alloy.
The values of Hmix can be approximated using eq. (5), using $H_{\text{mix}(\text{A}_{50}\text{B}_{50})}$, and the results are shown in Table 3.
\begin{equation} H_{\text{mix(alloy),approx}} = 4\sum_{j = 1}^{N}\sum_{i > j}^{N}H_{\text{mix,i-j}}c_{i}c_{j} \end{equation} | (5) |
In the present study, experiments were performed by fixing the annealing temperature at 1600 K; this specific temperature was selected by referring to a single structure temperature range based on thermodynamic calculations, as shown in Fig. 1. The structure-dependent Smix and Hmix of binary EE alloys are listed in Tables 2 and 3, respectively, for solids at 1600 K for a single phase, allowing to calculate those of a multicomponent alloy at 1600 K. In reality, however, Smix and Hmix are not constant with respect to T, and rather should be considered as functions of T. The calculation results for Smix and Hmix performed using Thermo-Calc and the TCHEA4 database are shown in Fig. 4. Figure 4(a) shows the Smix/R ratio, computed using Thermo-Calc 2021a and the TCHEA4 database; the results are shown for the Al6, Al30, Ru30, and Ni30 alloys. The solid curves show the Smix/R ratios for the designated single structures as thermodynamically stable phases, whereas the dotted curves indicate the designated single structures of the alloys in metastable states. The solid curves for the Al6, Ru30, and Ni30 alloys with single bcc, hcp, and fcc structures, respectively, exhibit a slight increase in Smix/R with decreasing T, which characterizes UHMEAs. The increase in the Smix/R ratio for the Ru30 and Ni30 alloys at T < 1396 K (Curie temperature, Tc, of pure Co) was attributed to the change in the standard element reference (SER)9) of pure Co for ferro- and para-magnetism, which affected the Al6 alloy at T < 1450 K. This tendency of Co, Tc(fcc) ≤ Tc(hcp) < Tc(bcc), was qualitatively supported by the first-principles prediction of high Tc for ferromagnetic bcc-Co, calculated as reported in the literature33) using the Korringa–Kohn–Rostoker (KKR) Green function and full-potential linearized augmented plane-wave (FLAPW). The reported values33) were $T_{\text{c}}^{\text{KKR}}(\text{fcc-Co}) = 1280$ K, $T_{\text{c}}^{\text{KKR}}(\text{hcp-Co}) = 1300$ K, and $T_{\text{c}}^{\text{KKR}}\text{(bcc-Co)} = 1370$ or 1420 K, as $T_{\text{c}}^{\text{FLAPW}}(\text{fcc-Co}) = 1200$ K, $T_{\text{c}}^{\text{FLAPW}}(\text{hcp-Co}) = 1350$ K, and $T_{\text{c}}^{\text{FLAPW}}(\text{bcc-Co}) = 1670$ K.
(a) Normalized Smix/R calculated using Thermo-Calc 2021a and the TCHEA4 database, for the Al6, Al30, Ru30, and Ni30 alloys. Solid curves denote Smix/R of the designated single structure, whereas dotted curves indicate the designated single structure of the alloys being in a mixture or metastable states. B2 ordering takes place for T < 1810.9 K for the Al30 alloy, whereas a bcc disordered structure is a stable single structure for T > 1343.3 K for the Al6 alloy. Increase in the Smix/R ratio for the Ru30 and Ni30 alloys at T < 1396 K (= Curie temperature, Tc of pure Co) was owing to the change in the standard element reference (SER)9) of pure Co for ferro- and para-magnetism, which presumably affected the Al6 alloy at T < 1450 K. Specific heat at constant pressure (Cp) of Co in the (b) bcc, and (c) hcp and fcc structures.
The Tc values of 1396 K and 1450 K, obtained in the present study, were verified using the calculation results of the specific heat at constant pressure (Cp) of Co for the bcc, hcp, and fcc structures, and the results are shown in Fig. 4(b). Significantly, the ferromagnetic elements (Co, Fe, Ni) increased Smix/R owing to the magnetic specific heat at constant pressure ($C_{p}^{\textit{magnetic}}$) at T < Tc when an alloy of interest and the pure ferromagnetic element possessed the same structure. Specifically, the magnetic second-order transition from ferromagnetism to paramagnetism, which was accompanied by $C_{p}^{\textit{magnetic}}$, contributed to Smix/R as magnetic entropy (Smag) by a factor of $S = \int (C_{p}^{\textit{magnetic}}/T) dT$ around Tc. In Fig. 4(b), Smag tends to correspond to the hatched area surrounded by the λ-shaped Cp curve and the baseline for each structure. This specific increase in Smix/R was supported by the following two results.9) First, as described in Section 1 in the present study, the fcc CoCrFeMnNi HEA2) and the fcc CoCuFeMnNi HEA,11) both containing Co, exhibited Smix > Sconfig at 1600 K. Second, Smix > Sconfig was not observed in the authors’ previous work9) for bcc HEAs without Co. By contrast, the Al30 alloy with a single B2 structure exhibited a considerable decrease in Smix/R with decreasing T. The Al6 and Al30 alloys exhibited critical temperatures for chemical order/disorder (B2/bcc) at TB2/bcc = 1343.3 and 1810.9 K, respectively, where the former for the Al6 alloy was the transition between dual phases (B2 + bcc) and a single bcc structure. Figure 4 suggests that the Al30 alloy formed in a single B2 structure exhibited a small Smix/R < 1, but the Al30 alloy formed in a metastable bcc structure in the range of T > 1810.9 K possessed a rather high Smix/R > 1.41, which was 90% of Sconfig/R = 1.557. The decrease in Smix/R began at T = 1810.9 K with decreasing T, indicating that chemical ordering decreased Smix/R.
The decrease in Smix/R for the Al30 alloy can be explained by considering the site fraction (f) of the sublattice elements. The change in the value of f is shown in Fig. 5. Considering the fractional composition of the Al30 alloy (Al30Co20Cr20Fe20V10 = Al0.3Co0.2Cr0.2Fe0.2V0.1), the above f values indicate that the B2 structure was an approximately Al–(Fe, Co) ordered structure in which the constituent elements were mainly occupied in sublattices 1–2, respectively. Meanwhile, V and Cr exhibited weak affinity to Al and (Fe, Co). These elemental distributions indicate that the B2 structure of the Al30 alloy as a single-phase exhibits compositional homogeneity on a macroscopic scale but includes an atomistic inhomogeneity owing to the B2 ordering, because of the development of a short-range order. As shown in Fig. 5, the f values for both sublattices of the B2 structure exactly correspond to the alloy content of the Al30 alloy for T ≥ 1810.9 K, although the stable phase was a liquid structure in this temperature range. Figures 4 and 5 and Tables 1 and 2 indicate that the Al30 alloy was classified as neither an UHMEA nor a conventional HEA. More generally, the present results for the Al30 alloy suggest the need to exclude B2 ordered single-phase alloys from the class of HEAs.
Site fraction of sublattice elements for the Al30 alloy, for single stable and metastable B2 ordered structures, and for a stable liquid structure.
There is a shortcoming in Table 2 in that the Smix/(R ln 2) value is listed only for 1600 K, and its temperature dependence is not considered. The disadvantage of Table 2 can be compensated by deriving the molar Gibbs mixing energy (Gmix) of the alloys as a function of T. Below, we show that Gmix can be fitted with eq. (6).9,34)
\begin{equation} G_{\text{mix}} = a + bT + cT\ln T \end{equation} | (6) |
\begin{equation} S_{\text{mix}} = -b - c(\ln T + 1) \end{equation} | (7) |
\begin{equation} H_{\text{mix}} = a - cT \end{equation} | (8) |
At present, there are two ways to predict Smix/R for multicomponent alloys. The first approach utilizes $S_{\text{mix}(\text{A}_{50}\text{B}_{50})}/(R\ln 2)$, as shown in Table 2. This method is convenient for judging the tendency of $S_{\text{mix}(\text{A}_{50}\text{B}_{50})}/(R\ln 2)$ to decrease or increase from $S_{\text{mix}(\text{A}_{50}\text{B}_{50})}/(R\ln 2)$. The evaluation of Smix/R for a multicomponent alloy is valid for UHMEAs because of the slight increase in Smix/R with decreasing T, as shown in Fig. 4. The second method uses the coefficients a, b, and c of eq. (6), to derive Smix/R for a multicomponent alloy. The second method estimates Smix/R more accurately than the first method, but the coefficients a, b, and c should be derived in advance. The combination of the first and second methods will contribute to the development of HEAs in the near future.
Experiments revealed that the Al6Co27Cr34Fe19V14, Al30Co20Cr20Fe20V10, Co20Cr20Fe20Ru30V10, and Co20Cr20Fe20Ni30V10 alloys (Al6, Al30, Ru30, and Ni30 alloys) annealed at 1600 K for 1 h were formed into single bcc, B2 ordered, hcp, and fcc structures. The bcc Al6 alloy with Sconfig/R = 1.480 exhibited Smix/R = 1.703 at 1600 K as an UHMEA, as well as Re30 and Ni30 UHMEAs. The hcp Ru30 UMHEA contained as many 3d transition metals as 70 at%, at the highest amount among the hcp HEAs fabricated via conventional solidification from a melt to date. The inclusion of Co as a ferromagnetic element contributed to increasing Smix/R. The chemical ordering of B2 from the disordered bcc structure decreased Smix/R in the B2 Al30 alloy down to Smix/Sconfig ∼ 0.5, at 1600 K. Evaluations of Smix and Hmix, both with structure dependency, were first performed based on $S_{\text{mix}(\text{A}_{50}\text{B}_{50})}/(R\ln 2)$ and $H_{\text{mix}(\text{A}_{50}\text{B}_{50})}$, respectively, of the binary exact equiatomic constituents. Structure-dependent Smix and Hmix contribute greatly to the further development of UHMEAs and HEAs through a strategy of structure-dependent Smix and Hmix.
This study was supported by JSPS KAKENHI (grant number JP17H03375).