中国有色金属学报(英文版)

Trans. Nonferrous Met. Soc. China 28(2018) 1073-1083

Microstructural evolution during unsteady-state horizontal solidification of Al-Si-Mg (356) alloy

J. O. LIMA1, C. R. BARBOSA1, I. A. B. MAGNO1,2, J. M. NASCIMENTO2, A. S. BARROS2, M. C. OLIVEIRA1,2, F. A. SOUZA1,2, O. L. ROCHA1,2

1. Federal Institute of Education, Science and Technology of Pará, IFPA, 66093-220, Belém, PA, Brazil;

2. Federal University of Pará, Institute of Technology, UFPA, 66075-110, Belém, PA, Brazil

Received 30 April 2017; accepted 27 September 2017

Abstract:

The increasing demand for reducing vehicle weight in the automotive and aerospace industries has raised the need to develop improved structural aluminum-based alloys. Thus, horizontal solidification experiment with the Al-7%Si-0.3%Mg (mass fraction) alloy was carried out. A water-cooled horizontal directional solidification device was developed and used. Microstructural characterization was carried out using traditional techniques of metallography, optical microscopy and SEM microscopy. The Thermo-Calc software was used to generate the solidification path of the investigated alloy with addition of 0.17% Fe (mass fraction). The effects of the thermal parameters such as the growth rate (VL), cooling rate (TC) and solidification local time (tSL) on the formation of the macrostructure and on the dendritic microstructure evolution were evaluated. A columnar to equiaxed transition (CET) was found for VL and TC values from 0.82 to 0.98 mm/s and from 1.71 to 2.55 °C/s, respectively. The microstructure was characterized by the measurement of the primary and secondary dendrite arm spacings (λ1 and λ2, respectively). Experimental laws of λ1=f(VL, TC) and λ2 =f(tSL) were proposed. It is observed that the interdendritic region is composed of the following eutectic mixture: a(Al)+Si+p-Al8Mg3FeSi6+q-Mg2Si.

Key words:

Al-Si-Mg alloy; microstructural transition; dendrite arm spacing; transient heat flow;

1 Introduction

Aluminum casting alloys are commonly used in automotive and aerospace industry due to their good casting characteristics, mechanical properties as well as good corrosion resistance and weldability [1-10]. It is known that about 80% of these alloys belong to the Al-Si system. In these alloys, the Si alloying element can reduce shrinkage during solidification, the porosity in castings and the thermal expansion coefficient, improve the weldability, increase the flowability, as  well as the solidification cracking and mechanical strength.

Al-Si alloys of 3xxx series, with addition of Mg and/or Cu, are most commonly used in the transportation industry, especially in the manufacture of motor vehicles and aircraft [1-4]. In unmodified alloys, the Si particles have a lamellar morphology, which act as initiators for crack propagation and have a negative influence on ductility. On the other hand, the ductility can be improved by changing the lamellar morphology to a fibrous or spheroidal morphology, by imposing, for example, high growth rate (VL) and cooling rates (TC) during solidification, or by the addition of a chemical modifier or by heat treatment, or by a combination of these processes. Coarse and brittle intermetallic phases, such as Al2Cu and Mg2Si, can be formed during solidification with low TC values, promoting deleterious effects on the mechanical properties. However, the increase in TC results in more refined microstructures and, therefore, better mechanical properties.

It is emphasized that significant progress in the development of theoretical and experimental studies to design mechanical and surface properties as a function of thermal and microstructural parameters of metal alloys has been elaborated, considering the directional solidification technique, both in steady and unsteady state conditions. Thus, theoretical and experimental investigations on the effects of thermal parameters (VL and TC) on microstructural evolution in binary aluminum-based alloys [1-21] have been developed more than three decades ago and more recently for multicomponent alloys [22-27], all with emphasis on directional solidification.

In the case of theoretical studies on the evolution of the dendritic microstructure in binary alloys [11-16], it is highlighted that only those proposed by HUNT and LU [14] for primary spacings and BOUCHARD and KIRKALDY (BK) [16] for primary and secondary spacings assume solidification in unsteady-state heat flow conditions. On the other hand, for multicomponent alloys, it is known in the literature that the theoretical Rappaz and Boettinger (RB) model [22] has been proposed. In general, these models have presented mathematical expressions that correlate the primary dendrite arm spacing λ1 and the secondary dendrite arm spacing λ2 with VL, TC and tSL, given by the simplified general formula: (λ1 and λ2) = Constant (VL, TC and tSL)n, where tSL is the time interval between the passage of liquidus and solidus isotherms by a fixed point in the metal, and n is the exponent. It is observed in BK equations [16] that the exponent (n) assumes to be -1/2 for the primary dendrite arm spacing varying with cooling rate and -2/3 for the secondary dendrite arm spacing varying with grooth rate, i.e., λ1 and λ2, respectively. It is known that the HL model, for primary dendritic growth [14], presents a complex mathematical expression, however, its experimental application [2-4,10,17] has shown that the slope of the simulated curve has generated an exponent (n) very close to that proposed by BOUCHARD and KIRKALDY. In the RB model [22], the exponent (n) is equal to 1/3 for variation of the secondary dendritic spacing with the solidification local time, i.e., λ2.

Experimental investigation on microstructural evolution of binary and multicomponent Al-Si-based alloys was developed in literature and Table 1 highlights some of these works, whose results present experimental laws of dendritic growth, represented by power-type mathematical equations, similar to those of the theoretical models [14,16,22].

Table 1 Experimental laws of primary and secondary dendritic growth for Al-Si-based alloys

It is observed in Table 1 that the Al-Si casting alloys are well studied and there is a lot of knowledge on the influence of alloying elements and solidification thermal parameters on the microstructure evolution. These investigations play a relevant role in designing components and equipment with mechanical properties suitable to the transportation industry. Furthermore, CHEN et al [28] has investigated the correlation among microstructure and heat treatment parameters and composition of Mg element with mechanical properties in Al-7Si-XMg cast alloys. The results showed that more refined microstructures allowed to obtain higher tensile properties after thermal treatment. Thus, this study may contribute to the liquid metal processing in automotive and aerospace industry aiming at designing of a required alloy microstructure, considering a better understanding of the thermal parameters and processes occurring in Al-Si-Mg alloys. In this sense, the main purpose of this paper is to investigate the effects of thermal parameters (VL, TC and tSL) on the dendritic microstructure evolution of the Al-7%Si-0.3%Mg (mass fraction) alloy horizontally solidified under transient heat flow as well as to perform a comparative analysis of the experimental λ2 values theoretically calculated with the Rappaz and Boettinger theoretical model [22]. In addition, the solidification path of the investigated alloy will be determined experimentally and compared with the theoretical predictions obtained by Thermo-Calc software. The obtained results have been compared  with others found in literature under different growth conditions.

2 Experimental

Transient horizontal directional solidification (THDS) experiment was carried out with Al-7%Si- 0.3%Mg alloy, prepared from the weighing of its high purity Al, Si elements and from a Mg-based alloy, which was inserted into a refractory crucible and introduced into a muffle-type melting furnace. The chemical compositions of the metals and the final investigated alloy are summarized in Table 2. The addition of the Si and Mg alloying elements occurred only after the initial melting of the aluminum solvent. In order to verify the liquidus temperature (TL), the investigated alloy was thermally characterized by obtaining its experimental solidification path. The horizontal solidification of the alloy was conducted using a water-cooled directional solidification device. Figures 1 and 2 show the schemes of the thermal characterization and complete solidification assembly used in this work, respectively. The horizontal solidification setup was designed to permit heat extraction only through the water-cooled system placed in the lateral mold wall. The stainless steel mold used had a wall thickness of 3 mm, a length of 150 mm, a height of 60 mm, and a width of 60 mm.

Table 2 Chemical compositions of metals and alloys (mass fraction, %)

Fig. 1 Scheme of thermal characterization apparatus to obtain solidification path

Fig. 2 Experimental complete horizontal directional solidification setup [27]

In order to determine the thermal parameters (VL, TC and tSL), a thermal mapping was carried out in the  liquid metal along with the THDS by insertion of thermocouples located at strategic positions from the cooled interface. The thermocouples readings, shown in Fig. 2 were used to generate a plot of positions from metal/mold interface (P) as a function of time (t) corresponding to the liquidus front passing by each thermocouple. A best fitting curve on these experimental points has generated a power function of position as a function of time, i.e., P=f(t). The derivative of this function with respect to time has yielded values for VL. The TC profile was calculated by considering the thermal data recorded immediately after the passing of the liquidus front by each thermocouple. The method used for measuring TC was detailed by ROCHA et al [17]. The tSL was determined by difference between the time of passage of the solidus isotherm and the time of passage of the liquidus isotherm for a given point in the casting [2].

After the horizontal directional solidification, the resulting ingot was subjected to metallography techniques to characterize and reveal the structure on a macrostructural and microstructural scales. Transverse and longitudinal sections at 2, 4, 6, 10, 15, 20, 30, 40, 50, 60, and 70 mm, whose positions are in the columnar growth region, and 2, 4, 6, 10, 15, 20, 30, 40, 50, 60, 70, 80, 90, 100 and 110 mm, respectively, of the directionally solidified ingot from the metal-mold interface were electropolished and etched with a solution of Keller’s reagent (10 mL HF, 15 mL HCl, 25 mL HNO3, 50 mL H2O) during 15 s for micrograph examination and measurement of primary and secondary dendrite arm spacings. The method used for measuring λ1 on the transverse section was the triangle method [8,17]. On the other hand, λ2 was measured by averaging the distance between adjacent side-branches on the longitudinal section of a primary dendrite [8,17]. Figure 3 schematically shows the techniques used to measure the λ1 and λ2 values, respectively.

3 Results and discussion

Figures 4(a) and (b) show the theoretical and experimental solidification paths obtained by the thermal characterization (Fig. 1) and Thermo-Calc software (non-equilibrium conditions), respectively. In order to better represent the inflection points for precipitation of the intermetallic phases, the first derivative of the experimental curve representing the solidification path of the investigated alloy has been determined, as shown in Fig. 4(b). It is observed that the microstructure of investigated 356 alloy in the as-cast state consists of dendritic primary phase of α(Al-rich) solid solution with interdendritic regions of Al-Si eutectic, in which various intermetallic phases such as β-Al5FeSi, π-Al8Mg3FeSi6 and Mg2Si are present.

The experimental cooling curves referring to the thermal mapping performed on the metal during horizontal solidification are shown in Fig. 5. It has been used to determine the VL, TC and tSL values, which are shown in Fig. 6. It is observed that the water-cooled device imposes high growth and cooling rates for positions near the metal/mold interface (cooled interface).

Fig. 3 λ1 and λ2 measurement techniques used in this work (n: number of side branches)

Fig. 4 Theoretical and experimental solidification paths obtained by Thermo-Calc software (a) and experimental methodology (b) of Fig. 1

Fig. 5 Experimental cooling curves obtained for six thermo- couples inserted in metal (TSH, TL and TE are temperatures of superheat, liquidus and eutectic, respectively)

Figure 7 shows the macrograph for the investigated alloy horizontally solidified. It can be seen by the solidification macrostructure that a columnar to equiaxed transition (CET) appears and that CET has occurred in a zone, represented by a dash line inside  Fig. 7, instead of a sharp plane parallel to the metal/mold interface. It is evidenced that the effects of the thermosolutal convection, promoted by the growth direction of the horizontal solidification, have influenced the CET to occur in ranges of VL (0.82 to 0.98 mm/s) and TC (1.71 to 2.55 oC/s), as shown by Figs. 6(a) and (b), respectively. The same CET characteristic found in this work has been observed in our recent articles for multicomponent Al-Si based alloys with addition of Cu alloying element [25,27]. Typical longitudinal and transverse microstructures of the Al-7%Si-0.3%Mg alloy along the length of the THDS casting are also shown in Fig. 7. It is observed that the microstructure is characterized by a dendritic morphology along the horizontally solidified ingot, and coarser microstructure has been noted for lower VL and TC values, i.e., the primary and secondary dendrite arm spacings increase with the distance from the heat-extracting surface. This has been depicted by Figs. 6(a) and (b).

Fig. 6 Thermal parameters resulting from horizontal solidification of Al-7%Si-0.3%Mg alloy (CET is columnar to equiaxed transition)

Fig. 7 Macrograph and optical micrographs of transverse and longitudinal sections of Al-7%Si-0.3%Mg alloy ingot (P is position from metal/mold interface)

The influence of the thermal parameters has been evaluated in the evolution of the dendritic microstructure. For this end, the VL, TC and tSL experimental variations as a function of the liquidus isotherm position (P), presented in Fig. 6, were correlated with the λ1 and λ2 values measured in the ingot of horizontally solidified alloy in this work and the results found are consolidated in Figs. 8 and 9.

It is observed from Figs. 8(a) and (b) that the exponents -1.1 and -0.55 have characterized the variation of the primary dendrite arm spacings with the growth rate and the cooling rate, which are absolutely equal to the indices found by PERES et al [2] and CARVALHO et al [4], for the vertical upward and horizontal solidified binary Al-7%Si alloy, respectively. It can be understood that both the addition of the Mg element in the formation of multicomponent Al-7%Si- 0.3%Mg alloy and the solidification growth direction (upward and horizontal) do not affect the experimental laws of primary dendritic growth. It is also noted that the λ2 values of these authors are very close to the values of this work. This should be emphasized that the value of -0.55 is very close to the value of -0.50 proposed by the BK mathematical model [16].

Fig. 8 Experimental laws of dendritic growth for horizontally solidified Al-7%Si-0.3%Mg alloy

Fig. 9 Comparison between results obtained from this work with those from literature for secondary dendritic spacing

Figures 8(c) and (d) show the dependence of secondary dendrite arm spacing as function of growth rate and cooling rate. It is observed that the exponents -2/3 and -1/3 characterize the experimental growth laws of λ2 as a function of VL and TC for R2≥0.7 (R2 is the coefficient of determination). On the other hand, a better agreement of the growth laws for λ2 values measured in the columnar grains region, i.e., for high VL and TC values evidenced. In this sense, it can be seen that the CET affects the secondary dendritic growth law for the investigated alloy. It is observed in Fig. 8(c) that the index value of mathematical expression that correlates λ2 as a function of VL is equal to -2/3 for both binary Al-7%Si and multicomponent Al-7%Si-0.3%Mg alloys, upward and horizontally solidified, referring to the work of PERES et al [2] and to this work, respectively. It is evidenced that the solidification direction does not affect the growth law for secondary dendritic spacing and that the exponent proposed in the BK equation (λ2) seems to be valid for ternary Al-based alloys. Figure 8(d) presents a comparative analysis between the experimental results for multicomponent Al-7%Si- 0.3%Mg alloy, obtained under the conditions assumed in this work and those of the work in Ref. [24]. It is observed that the exponent of -1/3 characterizes the λ2 growth law as a function of TC, for both investigations. However, it is noted that the experimental law proposed by CHEN et al [24] presents a better approximation in the isotropic growth region, i.e., composed of equiaxed grains.

It is known that RAPPAZ and BOETTINGER  (RB) [22] proposed the only predictive model found in the literature for secondary dendritic growth of multicomponent alloys. The general expression is given by

λ2 =5.5(MtSL)1/3                                               (1)

                (2)

where Γ is the Gibbs-Thomson coefficient, c0 is the alloy composition, m is the liquidus slope, cf is the eutectic composition, D is the diffusion coefficient in the liquid, and k is the redistribution coefficient. The subscript “j” represents each alloying element and the sum encompasses all the solute elements of the multi- component alloy.

A theoretical-experimental analysis between the results of this work and those calculated from the RB model was performed and the results are shown in Fig. 9. Table 3 shows the thermophysical properties of the investigated alloy, calculated with the Thermo-Calc software. A comparison with the experimental growth law, obtained by CHEN et al [24], has also been developed. It is observed that the λ2 values calculated by the RB equation overestimate those of this work as well as those of CHEN et al [24]. It should be emphasized that the RB model does not consider a transient heat extraction regime and yet, during its mathematical formulation, the authors have neglected the convective effects that are always present in the horizontal solidification. In spite of these interesting physical characteristics, the literature is scarce on studies dealing with these important effects of solute-induced  convection, particularly for multicomponent alloys.

Table 3 Thermo-physical properties of Al-7%Si-0.3%Mg alloy used in Eq. (2)

The SEM–EDS mapping results for the multicomponent Al-7%Si-0.3%Mg-0.15%Fe alloy are depicted in Fig. 10 for three positions from the metal/mold interface (cooled interface). These images show, for all positions, the presence of the eutectic  a(Al)+Si+p-Al8Mg3FeSi6+q-Mg2Si mixture inside the interdendritic region. It is observed for higher VL and TC values that the Fe and Mg solutes are more segregated in the Al-Si eutectic mixture as intermetallic particles (p-Al8Mg3FeSi6 and q-Mg2Si), dispersed as isolated elements at positions far from the cooled mold. The influence of the VL and TC values on the Si particle morphology can also be evidenced, i.e., it is noted that the Si presents the fibrous and lamellar forms at positions closest to and far from the cooled interface where VL and TC values are higher and lower, respectively. In order to confirm the phases that form during the solidification, SEM-EDS microanalysis has been performed on the micrograph samples shown in Fig. 10, and one of the results of the EDS compositions is shown in Fig. 11 at P=30 mm.

4 Conclusions

1) The dendritic microstructure has been observed along with the THDS of the Al-7%S-0.3%Mg alloy and the mathematical expressions given by λ1=, λ1=, λ2=, λ2=and λ2=  characterize the growth experimental laws of the primary and secondary dendrite arm spacings as a function of growth rate, cooling rate and solidification local time, respectively.

Fig. 10 SEM-EDS images obtained for investigated alloy at three positions in ingot from cooled interface

Fig. 11 EDS spectrum and compositions of Al-7%Si-0.3%Mg-0.15%Fe alloy investigated in this work at P=30 mm

2) The λ2 theoretical values calculated by the RB mathematical expression have overestimated the experimentally determined values of the Al-7%Si- 0.3%Mg alloy horizontally solidified in this work.

3) It was observed that the microstructure of the directionally solidified Al-Si-Mg-Fe alloy (356) in this work is composed of an Al-rich matrix (α) surrounded  by eutectic mixture with the presence of intermetallic phases of Mg and Fe, forming a mixture of phases in  the interdentric regions composed of α(Al)+Si+ p-Al8Mg3FeSi6+q-Mg2Si.

4) The Si particles in the eutectic mixture of the investigated alloy have been characterized to be fibrous and lamellar for high and low VL and TC values, respectively and that the intermetallic phases are more concentrated in the interdendritic regions for higher VL and TC values.

Acknowledgments

The authors acknowledge the financial support provided by IFPA—Federal Institute of Education, Science and Technology of Pará, UFPA—Federal University of Pará, and CNPq—The Brazilian Research Council (Grants 472745/2013-1, 308784/2014-6 and 302846/2017-4), FAPESPA—Amazon Foundation of Support to Study and Research (Grants ICAAF 064/2016) and CAPES—Coordination of Superior Level Staff Improvement, Brazil.

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Al-Si-Mg (356)合金不稳态水平凝固过程中的显微组织演化

J. O. LIMA1, C. R. BARBOSA1, I. A. B. MAGNO1,2, J. M. NASCIMENTO2, A. S. BARROS2, M. C. OLIVEIRA1,2, F. A. SOUZA1,2, O. L. ROCHA1,2

1. Federal Institute of Education, Science and Technology of Pará, IFPA, 66093-220, Belém, PA, Brazil;

2. Federal University of Pará, Institute of Technology, UFPA, 66075-110, Belém, PA, Brazil

摘  要:汽车和航空航天工业对减少运载工具重量的需求不断增加,这就需要发展改良的结构铝基合金。因此,本文作者研究设计Al-7%Si-0.3%Mg 合金的水平凝固实验。研制并使用水冷式水平定向凝固装置。运用金相、光学显微镜、扫描电镜等传统技术表征材料的显微组织。用Thermo-Calc软件模拟含0.17% Fe(质量分数)合金的凝固路径。研究生长速度(VL)、冷却速度(TC)和凝固局部时间(tSL)等热力学参数对显微组织形成和枝晶显微组织演化的影响。当VL 和TC 值分别为0.82~0.98 mm/s 和1.71~2.55 °C/s时,柱状晶向等轴晶转变(CET)。通过测量一次和二次枝晶间距(分别为λ1和λ2)对显微组织进行表征。提出实验性定律:λ1,2=f(VL, TC),λ2=f(tSL);并观察到枝晶区包含以下共晶混合物:α(Al)+Si+π-Al8Mg3FeSi6+θ-Mg2Si。

关键词:Al-Si-Mg合金;显微组织演化;枝晶间距; 瞬时热流

(Edited by Wei-ping CHEN)

Corresponding author: O. L. ROCHA; E-mail: otavio.rocha@ifpa.edu.br; otvrocha@gmail.com

DOI: 10.1016/S1003-6326(18)64751-X

Abstract: The increasing demand for reducing vehicle weight in the automotive and aerospace industries has raised the need to develop improved structural aluminum-based alloys. Thus, horizontal solidification experiment with the Al-7%Si-0.3%Mg (mass fraction) alloy was carried out. A water-cooled horizontal directional solidification device was developed and used. Microstructural characterization was carried out using traditional techniques of metallography, optical microscopy and SEM microscopy. The Thermo-Calc software was used to generate the solidification path of the investigated alloy with addition of 0.17% Fe (mass fraction). The effects of the thermal parameters such as the growth rate (VL), cooling rate (TC) and solidification local time (tSL) on the formation of the macrostructure and on the dendritic microstructure evolution were evaluated. A columnar to equiaxed transition (CET) was found for VL and TC values from 0.82 to 0.98 mm/s and from 1.71 to 2.55 °C/s, respectively. The microstructure was characterized by the measurement of the primary and secondary dendrite arm spacings (λ1 and λ2, respectively). Experimental laws of λ1=f(VL, TC) and λ2 =f(tSL) were proposed. It is observed that the interdendritic region is composed of the following eutectic mixture: a(Al)+Si+p-Al8Mg3FeSi6+q-Mg2Si.

[1] BAMBERGER M, WEISS B Z, STUPEL M M. Heat flow and dendritic arm spacing in chill-cast Al-Si alloys [J]. Materials Science and Technology, 1987, 3: 49-56.

[2] PERES M D, SIQUEIRA C A, GARCIA A. Macrostructural and microstructural development in Al-Si alloys directionally solidified under unsteady-state conditions [J]. Journal of Alloys and Compounds, 2004, 381: 168-181.

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