Effect of grain refinements on the microstructure and thermal behaviour of Mg–Li–Al alloy

Journal of Thermal Analysis and Calorimetry, Apr 2018

The light as-cast Mg–9Li–1.5Al alloys were manufactured and modified by 0.2 mass% Zr, commercial 0.2 mass% TiBor and 0.2 mass% AlSr master alloys. The thermal derivative analysis using UMSA platform was utilised to characterise a crystallisation process. Samples were heated up to 700 °C and then freely cooled down (~ 0.6 °C s−1) to ambient temperature in order to simulate the natural cooling of casts. Dilatometry study was used to identify changes in solid state. The relative elongation of unmodified and modified alloys was measured in the temperature range from 20 to 400 °C, with a heating rate 1.0 °C s−1. The effects of Zr, TiBor and AlSr content on the microstructure of analysed magnesium alloys were investigated. Evaluation of microstructure was identified by light microscope, scanning electron microscopy, X-ray diffraction and energy-dispersive X-ray spectroscopy. The results showed that the addition of TiBor reduced the grain size of Mg–9Li–1.5Al cast alloy from 930 to 530 µm, while the addition of AlSr master alloy reduced the grain size to 480 µm. Moreover, an addition of TiBor and AlSr simultaneously reduced the grain size to 430 µm. The addition of Zr causes a reduction in grain size to 630 μm. The addition of grain refinement causes changes in crystallisation process and variations in the coefficient of linear thermal expansion (CTE).

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Effect of grain refinements on the microstructure and thermal behaviour of Mg–Li–Al alloy

Journal of Thermal Analysis and Calorimetry https://doi.org/10.1007/s10973 Effect of grain refinements on the microstructure and thermal behaviour of Mg-Li-Al alloy Mariusz Kro´ l 0 1 0 Institute of Engineering Materials and Biomaterials, Faculty of Mechanical Engineering, Silesian University of Technology , Konarskiego 18a St., 44-100 Gliwice , Poland 1 & Mariusz Kro ́l The light as-cast Mg-9Li-1.5Al alloys were manufactured and modified by 0.2 mass% Zr, commercial 0.2 mass% TiBor and 0.2 mass% AlSr master alloys. The thermal derivative analysis using UMSA platform was utilised to characterise a crystallisation process. Samples were heated up to 700 C and then freely cooled down (* 0.6 C s-1) to ambient temperature in order to simulate the natural cooling of casts. Dilatometry study was used to identify changes in solid state. The relative elongation of unmodified and modified alloys was measured in the temperature range from 20 to 400 C, with a heating rate 1.0 C s-1. The effects of Zr, TiBor and AlSr content on the microstructure of analysed magnesium alloys were investigated. Evaluation of microstructure was identified by light microscope, scanning electron microscopy, X-ray diffraction and energy-dispersive X-ray spectroscopy. The results showed that the addition of TiBor reduced the grain size of Mg-9Li-1.5Al cast alloy from 930 to 530 lm, while the addition of AlSr master alloy reduced the grain size to 480 lm. Moreover, an addition of TiBor and AlSr simultaneously reduced the grain size to 430 lm. The addition of Zr causes a reduction in grain size to 630 lm. The addition of grain refinement causes changes in crystallisation process and variations in the coefficient of linear thermal expansion (CTE). Magnesium-lithium alloys; Thermal expansion; Thermal derivative analysis; Grain refinement Introduction Following the World War II, Mg–Li-based alloys, as an emerging light structural metallic material, have been presumed to be extensively used in aerospace and civilian areas, such as transport, electronics packaging and sports manufacturing for their high specific strength and specific stiffness, excellent damping and electromagnetic shielding properties [ 1, 2 ]. In the beginning, the analysis of Mg–Li-based alloys and composites including applications, microstructures, mechanical properties and processing technologies was regularly presented. Furthermore, the development in the research of intermetallic particles reinforced Mg–Li matrix composites was studied [ 3, 4 ]. Mg–Li-based alloys are the lightest among the magnesium alloys and serve as the important structural materials for aerospace industry. They maintain high cold formability, and the problems of magnesium–lithium binary alloys, such as poor resistance to corrosion and low strength, limit their utilisation [5]. There are few standard ways to enhance the strength of metallic materials through decreases in grain size and can be divided into two groups like thermal and chemical methods. The thermal method of grain refinement is superheating, and chemicals are zirconium, carbon, silicon carbide, manganese, titanium, calcium, strontium, antimony, cerium additions and Elfinal process [ 6, 7 ]. The additional methods capable of raising the strength are an addition of alloying elements. The increase in a third element—for example aluminium—to Mg–Li-based alloys serves to change the strength relating to intermetallic particle formation [ 1, 3 ]. The mechanical properties of Mg–Li alloys increase apparently with the addition of Al content, during the elongation of alloys reduces dangerously when the Al TiBor AlSr10 Mg Balance Balance Balance Balance Balance mass% 4.9 0.95 0.17 0.06 0.09 Balance 10.07 0.13 0.08 \ 0.10 Balance content is higher than 6 mass%. Titanium, strontium and zirconium are also a useful alloying element to improve Mg–Li properties [ 2, 6 ]. According to the Mg–Li binary phase diagram, if the Li content is less than around 5.5 mass%, the metal is formed of a single a(Mg) phase with hcp structure. When the Li content is within 5.5 and 11 mass%, the hcp a(Mg) phase coexists with bcc-structured b(Li) phase, while the structure has only a single bcc-structured b(Li) phase when the Li content is higher than 11 mass% [ 8, 9 ]. Nucleation of the primary phase is the initial step in the transition of molten alloys into the solid state. Nucleation control has been the subject of many studies [ 10, 11 ]. In the case of Mg alloys, a finer grain size increases most mechanical properties, including yield strength due to the high Hall–Petch coefficient, corrosion resistance and creep resistance [ 12–15 ]. In this study, the ternary alloys Mg–9Li–1.5Al (mass%) were manufactured and modified by processed by commercial Zr, TiBor and AlSr master alloys. The microstructure evolution, thermal derivative analysis, dilatation, scanning electron microscopy, X-ray diffraction and energy-dispersive X-ray spectroscopy techniques were used to examine the effect of grain refinements. Experimental Within the framework of the present work, alloys of magnesium with lithium and aluminium and with Zr, TiBor and AlSr as grain refinement have been melted, casted and examined. The raw materials used in these experiments were magnesium with technical grade (min. 99.5% Mg), aluminium 3N8 (99.98% Al), lithium (99.9% Li), TiBor, AlSr and Zr as refinements were utilised. Melting and casting of alloys were carried out using laboratory vacuum induction furnace VSG 02 from the company Balzers. Melts held in a crucible of Al2O3 in shape of ø 60 mm 9 80 mm, using the ceramic material sheath thermocouple for measuring the temperature of melting and casting alloys. Melting temperature was approx. 700/720 C and the melting time approx. 5 min., which, taking into account the strong bath stirring electrodynamic eddy currents in enough for the complete homogenisation of the melt. Grain refinement was introduced at the end of the melting process from the vacuum containers. After placed of grain refinement in the alloy, melts kept in the liquid state for 2 min, followed by the casting. The chemical composition of analysed Mg–Li–Al alloys and used grain refinements are given in Tables 1 and 2. The linear thermal expansion coefficient of the investigated magnesium–lithium–aluminium alloys was measured in argon atmosphere using the Bahr 805A/D dilatometer over a temperature range from ambient temperature to 400 C at heating and cooling rates of 1 C s-1. The thermocouple type S was utilised to measure changes in temperatures. Cylindrical samples in shape 10 mm in length and 4 mm in diameter were used in dilatometry test. The thermal derivative analysis (TDA) was done on the prepared cylindrical samples in shape of 18 mm in diameter and 20 mm using UMSA device [ 10, 11, 14 ]. Samples were melted at 700 C in an argon atmosphere. Following isothermal holding for 90 s, all the melts were solidified and cooled to ambient temperature in the crucibles with argon protection in the furnace to minimise the oxidation. The signal from the thermal derivative analysis was acquired using a high-speed National Instruments data acquisition system. The recorded data were analysed in Fityk software. The cooling curves and corresponding derivative curves were plotted to define thermal events, based on the first and second derivative of cooling curve. The test samples were solidified at an average cooling rate of approximately 0.6 C s-1 in the range of liquidus and solidus temperature. The cooling rate was determined using the following formula: Tliq CR ¼ tsol Tsol tliq where Tliq and Tsol are the liquidus and solidus temperatures, respectively, and tliq and tsol the times from the cooling curve that correspond to liquidus and solidus temperatures, respectively. The Newtonian method was applied in this research to determine the baseline. This means that the thermal gradient across the specimen is considered to be zero and that heat transfer between the casting and the mould occurs through convection. The Fourier method is another method used to calculate the baseline in which the positions of two thermocouples at the beginning and end of the solidification process are considered. However, it is much more complicated than the Newtonian method. Besides, a thermal contraction of the metal occurs during solidification, the exact positions of the two-thermocouple tips are difficult to estimate [ 16–18 ]. The base line has been predicted by the sixth polynomial fitting (dT/dt)BL = a0?a1T?a2t)BL = a0?a1T?a2T2?a3T3?a4T4?a5T5?a6T6 between the beginning and the end of solidification in the first derivative curve. The sixth-order polynomial yields a correlation coefficient greater than 0.97. Metallographic specimens were horizontally sliced at the position that is 10 mm from the top. The as-cast grains of the etched samples were measured using polarised light in optical microscope Leica equipped Q-WinTM image analyser. The grain size was determined by the linear intercept method at the centre of transverse sections. The X-ray qualitative and quantitative microanalysis and the analysis of a surface concentration of cast elements in the examined magnesium–lithium–aluminium unmodified and modified alloys have been made on the scanning electron microscope ZEISS SUPRA 35 with a system EDAX XM4 TRIDENT consisting of spectrometer EDS, WDS and EBSD (20 kV, 15 mm of work distance and 30 lm of aperture). Phase composition was determined by the X-ray diffraction technique utilising the X’Pert apparatus including a cobalt lamp with 40 kV voltage. The calculation was done by angle range of 2H: 30 –110 . The 35 1 – –6K34 0 1 / ion 33 s n a xp 32 e l a rm31 e h t fto 30 n e i iffc 29 e o C28 250 34.3 32.9 33.0 32.1 32.6 Material The analysis of coefficient of linear thermal expansion of Mg–9Li–1.5Al (Table 3 and Fig. 1) has validated the fact that CTE depends on temperature. Untreated Mg–9Li– 1.5Al alloy has CTE about 29.4 10-6 K-1, and with further increase in temperature to 250 C, CTE increases to 34.3 10-6 K-1. Further increase in temperature to 400 C caused a decrease in CTE to 31.9 10-6 K-1. Analysis of the heating and cooling dilatometric curves of analysed materials modified by TiBor and AlSr is characterised by a linear decrease in linear expansion coefficient as a function of temperature. Moreover, based on changes in elongation during heating and cooling cycle, it was found that shape of Mg–9Li–1.5Al Mg–9Li–1.5Al+0.2Zr Mg–9Li–1.5Al+0.2Tibor Mg–9Li–1.5Al+0.2Sr Mg–9Li–1.5Al+0.2Tibor+0.2Sr 50 100 150 200 250 Temperature/°C 300 350 400 graphs has a linear relationship that means no transitions in solid state occur. The phase composition of the investigated alloys treated by grain refinements and untreated was examined by XRD technique. The XRD profile of unmodified alloy demonstrates that there are two phases—b(Li) phase (matrix phase, a solid solution of magnesium in body-centred cubic (bcc) lithium lattice) and a(Mg) phase (solid solution of lithium in hexagonal close-packed (hcp) magnesium lattice), which is faithful with the observation using a light microscope. No peaks of Al including phase are noticed that suggests most of Al exists in a solid solution state. However, with the addition of Zr, new peaks correspond to the Zr phases. Furthermore, with the addition of TiBor and AlSr, no additional peaks were observed. Optical micrographs of Mg–9Li–1.5Al cast alloy and after modification by Zr, TiBor and AlSr are given in Fig. 2. It can be observed that the structure of the analysed alloys is fundamentally formed of light grey a(Mg) phase and dark grey b-Li phase, which is in consistent with the Mg–Li binary system [ 8, 9 ]. Most of the a(Mg) phase is elongated ribbon-like, where b(Li) phase fills the area between a(Mg) phase grains, separated by boundaries between two phases. In the duplex phase matrix, the ratio of a and b phases is 40/60. There also exists some particlelike (Fig. 2e—marked in white circle) phase in the alloy. The granular-dispersive phase of the intermetallic compounds is randomly spread in the a and b matrices. Darker particles have most probably resulted from the aluminium addition in the form of g(LiAl) phase as suggested in [ 8, 9, 19, 20 ]. SEM analysis of marked circles shows high concentration of Al, indicating that it is g(LiAl) phase. Moreover, the addition of grain refinements effects in the conversion of the elongated-striped a(Mg) phase with a blocky structure and rounded corners. Moreover, optical metallography indicated fully dense alloys. Analysis of grain size of analysed alloys after thermal derivative analysis cooled at a rate of 0.6 C s-1 appointed by the method of linear interception length shows that the grain refining appearance is different for each alloy (Figs. 3 and 4). Once Zr is added, there is a significant reduction in grain size. The Mg–9Li–1.5Al alloy was refined from 930 to 640 lm by 0.2 mass% Zr. The results showed that the addition of TiBor master alloy decreased the grain size of Mg–9Li–1.5Al cast alloy to 500 lm, while the addition of AlSr master alloy reduced the grain size to 480 lm. Moreover, an addition of TiBor and AlSr simultaneously reduced the grain size to 430 lm. The relatively small grain size of Mg–9Li–1.5Al?0.2TiBor?0.2Sr is not obviously reflected in its hardness related to Mg–9Li– 1.5Al?0.2TiBor. It can be noted that addition of AlSr refiner slightly increases in hardness. In general, the hardness did not increase with TiBor and Zr addition (Fig. 5). Furthermore, investigated alloys were characterised by SEM equipped with EDS and computer-controlled imaging system. The SEM images of analysed Mg–Li–Al alloys point out dark grey and grey areas relating to the b(Li) phase and a(Mg) phase, respectively, as shown in Fig. 6a. Because lithium is invisible in SEM image, b-phase is darker. Grain refinement of analysed magnesium–lithium– aluminium alloy by 0.2 mass% Zr causes appearance to Fig. 3 Microstructure of the grain size for Mg–9Li–1.5Al base alloy at various addition of grain refinements: a Mg–9Li–1.5Al, b Mg–9Li– 1.5Al?0.2Zr, c Mg–9Li–1.5Al?0.2TiBor, d Mg–9Li–1.5Al?0.2Sr, e Mg–9Li–1.5Al?0.2TiBor?0.2Sr, Nomarski contrast Mg–9lLi–1.5Al+0.2Zr alloys, respectively. Containing Sr, an element with a larger atomic number, bone-like bright intermetallic compounds (indicated as 3) are situated along the phase boundary as well as across a-phase. EDS point analysis, which was done at location 3, demonstrates the high concentration of Mg, Sr and Mg, Al, Sr, respectively. Considering Al dissolved in the matrix, it can be concluded that these compounds can be related to Al4Sr or Mg2Sr as suggested in [ 6 ]. Shape and location of recognised phases in analysed alloys could be directly related to the order of nucleation in the intermetallic compounds. The solidification pathways of as-cast (Fig. 7a) and after modification by 0.2 mass% Zr (Fig. 7b) and 0.2 mass% TiBor (Fig. 7c) and 0.2 mass% AlSr (Fig. 7d) master alloys have been investigated by thermal derivative analysis. Figure 7a shows typical cooling curves and its first derivative curves which were used to determine characteristic points during solidification. For the alloy with 0.2 mass% Zr, only five well-defined points are observed, i.e. at 597.7 C (1-TN-nucleation temperature), 578.9 C (2TG-maximum temperature of growth), 526.1 C (4-TSOLsolidus temperature), 503.3 C (5-TS-a?b solvus temperature) and 473.3 C (6-TER-end of reactions) as shown in Fig. 7b. No more exothermic peaks were found after modification by Zr that can be corresponded to compounds of Al3Zr as suggested in [ 21, 22 ]. It must be noted that the melting temperature of Al3Zr intermetallic compound according to the literature [9] is 1580 C. Results from the thermal derivative analysis (Table 4) present that the addition of 0.2 mass% Zr does not change the nucleation temperature, i.e. 596.5 C and, however, decreases the solidus temperature from 549.1 C of investigated magnesium alloys. For both analysed alloys, no significant changes in temperature in other reactions like TG, TS and TER were observed. The solidification time for the cooling rate 0.6 C s-1, as the difference of the times, at which the liquidus and solidus temperatures occur in Mg–9Li–1.5Al and Mg–9Li–1.5Al?0.2Zr, amounts to Dt = 106 and 134 s, respectively. Addition of TiBor and AlSr causes to appearance new well-defined exothermic peak (marked as point 3 in Fig. 7c–e) probably becomes from nucleation of metastable intermetallic phase g(LiAl) with B2 structure [ 8, 9, 20 ] 3-Tg(LiAl) observed at 552.6 C (Mg–9Li– 1.5Al?TiBor), 559.1 C (Mg–9Li–1.5Al?AlSr) and 546.8 C (Mg–9Li–1.5Al?0.2TiBor?0.2Sr), however, more studies must be done. Modification of Mg–9Li–1.5Al alloy by AlSr master alloy causes slight decreases in nucleation temperature to 582.7 C, but strongly reduces a solidus temperature to 535.3 C in accordance with the unmodified alloy. The addition of TiBor and AlSr10 master alloys causes l+0.2Zr white granular particles of the intermetallic compounds randomly spread in the a and b matrix (Fig. 6b). EDS point analysis carried out on particles (indicated as 3) to determine the chemical composition shows that the mixture consists of high concentration of Zr, Al and Mg elements, which the most probably resulted in the form of Al3Zr phases as suggested in [ 21, 22 ]. With the addition of TiBor master alloy as grain refinement to the Mg–9Li–1.5Al alloy, no other phases are observed in microstructure (Fig. 6c). Figure 6d, e shows the SEM images and EDS analysis of the Mg–9Li–1.5Al?Sr and Mg–9Li–1.5Al?TiBor?Sr Fig. 6 SEM micrographs with EDS analysis in labelled points of Mg–Li–Al alloys: a Mg–9Li–1.5Al, b Mg–9Li–1.5Al?0.2Zr, c Mg–9Li– 1.5Al?0.2TiBor, d Mg–9Li–1.5Al?0.2Sr, e Mg–9Li–1.5Al?0.2TiBor?0.2Sr decreases in nucleation temperature and solidus temperature to 579.32 and 520 C, respectively. The addition of TiBor and AlSr master alloys increases a crystallisation time to 132 s for Mg–9Li–1.5Al?TiBor, 146 s for Mg–9Li–1.5Al?TiBor and 143 s for Mg–9Li– 1.5Al?0.2TiBor?0.2Sr. Moreover, an addition of Sr causes a reduction in a period between the solidus temperature and solvus temperature. Based on thermal derivative analysis, it was found that only addition of TiBor and AlSr simultaneously causes a decrease in temperature of maximum growth of primary b(Li) phase from 581.3 to 575.6 C. In general, no exothermic peaks, corresponding to precipitation of Mg2Sr, with melting temperature 680 C [ 8, 9 ], were observed during analysis of crystallisation process of Mg–Li–Al alloys containing Sr as grain refinement. This may be the causes that the amount of Mg2Sr intermetallic compound is very low, below the level of detection of the method. The crystallisation pathway of investigated unmodified and modified magnesium alloys, based on thermal derivative analysis, microstructure investigation, SEM observation and study of binary and ternary systems [ 8, 9 ], may be proposed as: 1 2 1 –s C ° / t d / T d 1 –s C ° / t d / T d 4 5 6 3 (solvus line in Mg–Li binary system) causing forming of a(Mg) and b(Li) according to reaction b(Li)? a(Mg)?b(Li). Thermal derivative analysis can be implemented to registration melting and cooling processes of Mg–Li– Al alloys. Conclusions The effects of addition of 0.2 mass% Zr, 0.2 mass% TiBor and 0.2 mass% AlSr grain refiners on the crystallisation process during solidification of the Mg–9Li–1.5Al alloy such as TN, TG, TSOL, TS and TER, linear coefficient of thermal expansion, microstructure and hardness were studied. The results are summarised as follows: At a 0.6 C s-1 cooling rate, the solidification time of Mg–9Li–1.5Al alloy is increased by adding grain retirements. In analysed material, an addition of Zr does not change TN, TG, TS and TER; however, decreases TSOL. The addition of TiBor and AlSr causes a reduction in nucleation and solidus temperature. Analysis of the heating and cooling dilatometric curves of analysed materials modified by TiBor and AlSr is characterised by a linear reduction in coefficient of linear thermal expansion as a function of temperature. No transitions in the solid state occur during heating and cooling cycles. The as-cast Mg–9Li–1.5Al alloy comprises a(Mg) and b(Li) phases. AlSr addition results in the formation of new intermetallic compound distributed along the phase boundary as well as across a-phase. EDX analysis shows that the precipitated compounds are Al4Sr or Mg2Sr. The addition of Zr, TiBor and AlSr in level 0.2 mass% reduces the grain size of analysed magnesium alloy. The strongest effect in reduction in grain size (grain size decreased almost twice) was achieved when TiBor and AlSr simultaneously were used. 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Mariusz Król. Effect of grain refinements on the microstructure and thermal behaviour of Mg–Li–Al alloy, Journal of Thermal Analysis and Calorimetry, 2018, 1-10, DOI: 10.1007/s10973-018-7223-x