# Evaluation of Sintering Behavior of Premix Al-Zn-Mg-Cu Alloy Powder

Authors: Haris Rudianto; Gwang Joo Jang; Sang Sun Yang; Yong Jin Kim; Ivo Dlouhy
Journal: Advances in Materials Science and Engineering
 (2015)

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## Abstract

Sintering of light aluminium alloys powder has been investigated as a way to substitute steels in automotive and aerospace industries. Premix Al-5.5Zn-2.5Mg-0.5Cu composite powder called Alumix 431D was analyzed in this research. Sintering was carried out under ultra high purity nitrogen gas and before reaching sintering temperature, green samples were delubricated at 400°C for 30 min. The powder possesses high sinterability by reaching 96% relative density at 580°C sintering temperature. Formation of liquid phase seems to support achieving high sintering density. Optimum mechanical properties also were obtained under those conditions. T6 heat treatment was done to improve the mechanical properties by formation of precipitation strengthening, and MgZn2 appears to be dominant strengthening precipitate. X-ray diffraction, optical microscopy, and SEM-EDS were used to characterize powder, and sintered and heat treated samples.


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## Body

## 1. Introduction

Sintering technology of aluminium powder has been considered to be a low cost manufacturing process for automotive parts. With rising price of oil, this can be alternative for industry to produce low cost and light weight parts and other light weight applications [1, 2]. Thanks to their attractive mechanical properties the lower density aluminium alloys and their composites prepared by powder metallurgy route appear to be important candidate materials for applications and sinterability conditions of aluminium composites powder.From all possible parameters compaction pressure has important role in affecting the matrix composite density besides the sintering temperature. Optimum compaction pressure can support powder to reach optimum sintering density. Variable pressure will greatly influence the green density. There are advantages and disadvantages by using low and high compaction pressure. No surface machining after sintering is desirable and expected from high compaction pressure. However at low compaction pressure, the cost of power needed is also low and safe for wearability of mold [3].Sintering of aluminium powder has difficulty to wet with another particle due to its oxide layer, Al2O3. The thickness of this oxide layer can be up to 100 nm. High melting point of Al2O3 hinders diffusivity of aluminium during sintering. Magnesium is considered to be an agent to remove oxide layer due to its reactive behavior at lower temperature to form spinel, MgAl2O4. Sintering atmosphere is as well important factor to gain high densification. Nitrogen gas is considered to be suitable atmosphere for sintering of aluminium powder, because nitrogen gas is able to increase diffusivity during sintering of aluminium by liquid phase formation [4, 5].AA7XXX alloys, which contain Zn, Mg, and Cu, have been proved to have high mechanical properties by utilizing their heat treatable properties. Ratio of Zn and Mg in this alloy is important for formation of strengthening precipitate MgZn2. Ready to press Alumix 431D which has chemical composition of Al-5.5Zn-2.5Mg-0.5Cu was investigated in this research. This powder is a new version of Alumix 431, which has similar chemical compositions. Some researchers did investigation on Alumix 431 with lower compaction pressure, and Martín and Castro did so with compaction pressure of 400 MPa [4]. Although with this pressure, it gave acceptable sintering density, there will be huge shrinkage especially on surface, so finishing work after sintering is necessary. So, the purpose as well as aim of this research is to investigate sinterability of the improved chemical compositions of Alumix 431D with high compaction pressure.


## 2. Materials and Experiments

In this research, Alumix 431D was analyzed which has chemical compositions of Al-5.5Zn-2.5Mg-0.5Cu with 1.5 wt% of lubricant. The powder was supplied by Ecka Granules, Germany. This powder has theoretical density of 2.79 g/cm3. Dry method particle size analyzer was used to estimate particle size distribution of this powder. DSC-TGA was carried out to investigate thermal behavior of this powder and carried out under ultra high purity nitrogen gas (99.9999%) up to 800°C. X-ray diffraction (XRD) was used to determine phase compositions in particular to identify precipitates after sintering and T6 heat treatment, and the diffraction pattern was obtained by Rigaku Diffractometer with Cu Kα radiation (λ
=
0.154 nm) in the range of 20–100° by the step and scanning speed of 0.02° and 5°/min. Microstructure was observed by scanning electron microscopy (SEM) along with energy dispersive X-ray spectroscopy (EDS) from Carl Zeiss Ultra Plus and Oxford Instruments X-MAX, respectively.Powder was compacted with dual action press at 700 MPa. Green density was measured by dividing mass by volume. Sintering was under ultra high purity nitrogen gas for 99.9999% and before reaching the sintering temperature, compacted samples were delubricated at 400°C for 30 min. Sintering density was obtained by using Archimedes method.Hardness test and tensile test were carried out to investigate mechanical properties. Rockwell hardness was performed to measure hardness of the sintered and heat treated materials, and the hardness was measured with Rockwell B hardness scale with 100 kgf and 1/16 in diameter of diamond ball indenter. Instron instrument was used to carry out tensile test with crosshead speed of 1 mm/min. Tensile test specimen was made according to ASTM E8 standard with 25 mm gauge length, 6 mm width, and 3 mm thickness. To optimize mechanical properties relating to microstructure of the sample, T6 heat treatment was applied. Sintered samples were heated until reaching solid solution condition at 520°C and followed by water quenching and artificial aging for 24 hours at 173°C. Dispersion strengthening by precipitates was expected after T6 heat treatment.


## 3. Results and Discussion

### 3.1. Powder Characterization

Powder was characterized to identify its morphology as shown by Figure1(a). The figure shows irregular shape of powder which is commonly expected from powder made by gas atomization process. Irregular shape of powder tends to have better compactability due to its shape which is able to fill spaces between each particle during compaction compared to circular shape. And another powder characterization is particle size distribution measurement. Dry method was carried out to measure average particle size for this powder, particle size distribution graph as shown in Figure 1(b), and average size of this powder is 105.3 µm. Particle size distribution is one of powder characteristics which strongly affect the sinterability of this material. Effect of particles size on sintering behaviour of aluminium powder was investigated by Liu et al. From their research outcomes, aluminium alloys powder with ~100 µm particle size has been found to supply optimum sintering density [5].Figure 1
(a) Particle morphology and (b) particle size distribution of Alumix 431D powder.
(a)
(b)Determination of thermal properties of this powder is important to estimate its sintering temperature and delubricating temperature. Figure2 shows DSC-TGA curves of Alumix 431D. As it is obvious from DSC graph (blue line), this powder has two endothermic peaks. The first one at 450°C is supposed to be eutectic reaction of Al-Mg and followed by highest peak at 640°C and supposed to correspond to eutectic reaction of Al-Zn. According to Zn content in this alloy powder for 5.5 wt%, it is expected to have higher melting point based on Al-Zn phase diagram where approximately 640°C is a minimum temperature to have liquid phase of Al-5.5Zn. Eutectic reaction of Al-Cu was expected in the trace at 540°C, but the graph shows this with little appearance, due to small amount of Cu on this powder for 0.5 wt%. From DSC curves, sintering conditions can be estimated, as sintering temperature is expected at 0.6–0.75 from melting point to be able to have strong bond between particles.Figure 2
DSC-TGA graph of Alumix 431D powder.At TGA graph (black line), it seems mass of powder decreased starting from 300 to 350°C and increased little more starting from 450°C to 550°C. The first declining line is supposed to remove lubricant from powder, as this powder content lubricant for 1.5 wt%, and from the line it is completely reduced for 1.5 wt% at 350°C. Adding lubricant into powder is to ease ejection force during compaction and to increase cohesive behavior between particles which supports diffusivity during sintering. But lubricant should be removed thoroughly before reaching sintering temperature. And 400°C seems to be safe temperature to completely reduce lubricant from powder. Gaining mass from 450 to 550°C seems to be resulting from reaction between aluminium oxide and magnesium and corresponding to DSC line at 450°C which is supposed to be eutectic point of Al-Mg. And another reason for gaining mass during these temperatures is reaction between aluminium and nitrogen gas to form aluminium nitride (AlN). But detection of aluminium nitride is still questionable due to lacking of proves by X-ray diffraction from sintered aluminium alloy which used nitrogen gas as atmosphere.


### 3.2. Sintering Behavior

Sintering is a process to bond compacted particles by using thermal force below melting point to be able to produce high dense materials. Sintering of this powder was carried out at 560°C–585°C for 1 hour. And atmosphere for sintering was ultra high purity nitrogen gas, because it has been proved that nitrogen gas supports densification process during sintering by reducing the pressure inside the pores which leads to pore filling mechanism [1]. Sintering density was measured to observe the densification behaviour as shown by Figure 3(a). It is expected that sintering density increased with increasing sintering temperature and it seems that optimum density was obtained at 580°C sintering temperature by reaching 96% relative density. At 585°C, sintering density decreased because of abundance of liquid phase and grain growth which leads to particle agglomeration and formed porosity. This phenomenon is called Oswald ripening [6].Figure 3
(a) Sintering density and (b) HRB hardness as a function of sintering temperature for Alumix 431D powder, and it seems that 580°C is an optimum sintering temperature.
(a)
(b)Compaction pressure has some effects on sintering properties of metal powder, because it supports having better interparticle bonding during sintering. To be able to produce high dense materials, using high compaction is suggested prior to sintering. That is the main reason that this research used high compaction pressure for 700 MPa. And the advantage of using high compaction pressure is the fact that surface of the sintered materials appears to be fully densified, so finishing process after sintering is not necessary. According to Figure4(a) pores still remain at body center of samples, and this is related to liquid phase and uncompleted pore filling process during sintering. For highly compacted powder, interparticle bonding reaction could be done at lower temperature due to strong surface energy which leads to easy reaction between each particle, as shown by the graph, and Alumix 431D has high sintering density at 580°C. Lower compaction pressure will need higher sintering temperature with lower sintering density as proved by Martín and Castro. They showed Alumix 431 powder has optimum sintering temperature at 610°C reaching only 94.9% relative sintering density using 400 MPa as compaction pressure [4]. The disadvantage of using high compaction pressure is reducing wearability of mold and needing more power during compaction process even if it will give clean-porosity surface.Figure 4
(a) SEM image of sintered Alumix 431D and (b) selected area and location for mapping and point elemental analysis of sintered Alumix 431D by EDS numbered from 1 to 4.
(a)
(b)Hardness of sintered Alumix 431D was investigated to measure how sintering density corresponded to mechanical properties. Figure3(b) shows highest hardness was obtained at same optimum sintering temperature of 40 HRB. This shows that porosity plays important role in mechanical properties of sintered aluminium as porosity tends to reduce resistance of sintered aluminium to deformation.Microstructure of sintered sample is shown in Figure4(a), and it shows there are sintering precipitates inside the grains and at grain boundaries shown by white color. SEM picture shows quite high densification level with lower rate of pore. Elemental analysis was performed by EDS to determine chemical compositions on selected locations as shown in Figure 4(b). Figure 5 shows the element distributions from some locations as obtained by EDS analysis. The point analysis clearly shows differences in chemical compositions in locations numbered from 1 to 4 as shown in Table 1. This indicates reaction and diffusion during sintering in liquid state. Locations number 1 and number 2 seem to be α aluminium and locations number 3 and number 4 are intermetallic phases. Location number 3 contains high amount of zinc, and it is related to some intermetallic phase such as MgZn2. And number 4 shows tin as an impurity and high amount of magnesium, which is related to formation of spinel MgAl2O4 as a result from reaction between magnesium and oxide layer on aluminium particles as follows:(1)
3
Mg
+
4
Al
2
O
3
⟶
3
MgAl
2
O
4
+
2
AlThis reaction results in decomposition of magnesium on grain boundary or close to pore, so it is expected to see some magnesium in grain boundary. Magnesium behavior during sintering was investigated by several researchers. Pieczonka et al. showed that magnesium moves to surface of aluminium particles at temperature of 450°C by dilatometry measurement [7]. And Lumley et al. investigated the effect of magnesium content on oxide layer removal from aluminium particles, and they showed that 0.5 wt% of magnesium is enough to remove oxide layer during sintering [8]. This reaction between magnesium and oxide layer is usually below sintering temperature. Point number 15 shows that there is tin, and it seems to be an impurity coming from this alloy powder.Table 1
Elemental analysis from selected location in Figure4(b) of sintered Alumix 431D.
Number
Al (wt%)
Zn (wt%)
Mg (wt%)
Cu (wt%)
Sn (wt%)
O (wt%)
Si (wt%)
1
62.76
4.81
1.5
0.89
—
0.32
—
2
61.8
5.33
1.47
1.13
—
0.31
—
3
48.97
12.56
5.52
5.39
—
2.09
—
4
48.54
4.71
4.39
1.27
6.72
6.96
0.73Figure 5
Elemental distribution analysis by EDS of sintered Alumix 431D starting with Al, Zn, and Cu which homogenously dispersed throughout the surface and Mg, O, and Sn seem to be concentrated at certain places on the surface.To investigate intermetallic phases during sintering, X-ray diffraction was carried out as shown in Figure6. Aluminium is dominant peak in the XRD spectrum followed by intermetallic MgZn2 and CuAl2 phases. MgZn2 is a precipitate which is expected to be formed during sintering due to possibility of formation of GP zones, η
′ and η, even though this phase is coherent with α aluminium. CuAl2 is precipitate which is commonly found in Al-Cu alloy and easily formed at room temperature at certain amount of Cu. And there is unknown phase on XRD peak pattern, and it seems to be the responsibility of tin which was found on EDS point analysis.Figure 6
X-ray diffraction pattern of sintered Alumix 431D powder.


### 3.3. T6 Heat Treatment

The T6 heat treatment is usually done to aluminium alloys to optimize their mechanical properties. The investigated powder has similar alloy system to 7XXX (Al-Zn-Mg-Cu) alloy. These materials are heat treatable and they possess a potential to form strengthening precipitates such as MgZn2 and CuAl2. These strengthening precipitates will form after reaching optimum aging conditions and have been solutionized and water quenched before. Figure 7(a) shows hardness of the sintered samples after T6 heat treatment as a function of sintering temperature. As expected, hardness of 68 HRB was achieved as the highest hardness and obtained after being sintered at 580°C sintering temperature followed by T6 heat treatment. And previously, this sintering condition also gave highest sintering density and hardness. Tensile strength load curves are showed in Figure 7(b), and there is an improvement in sample after T6 heat treatment by reaching the tensile strength 513 MPa with 5% elongation. The improvement of tensile strength after T6 heat treatment is related to strengthening precipitates which impede dislocation movement during tensile deformation and, as a result, tensile strength increased. Strengthening precipitates which were formed during T6 heat treatment were investigated by XRD as shown by Figure 8. MgZn2 was found to be dominant strengthening precipitates in this powder followed by CuAl2. The process of these precipitates formation is as follows:(2)
Supersaturated
solid
solution
⟶
Guinier-Preston
Zones
(
GPZ
)
⟶
η
′
⟶
η
MgZn
2Hexagonal close-packed (HCP) crystal structure of MgZn2  η phase formed after increasing time of η
′ phase to arrange into the incoherent equilibrium phase. This η phase is the obstacle dislocation movement, and as a result increasing mechanical properties are observed [9–11].Figure 7
(a) Hardness and (b) stress-strain curve at tensile test of Alumix 431D before and after T6 heat treatment (for 580°C sintering temperature).
(a)
(b)Figure 8
X-ray diffraction pattern of Alumix 431D after T6 heat treatment.SEM supplemented by EDS microanalyses was performed to observe microstructures after T6 heat treatment as shown in Figures9(a) and 9(b). Compared to sintered samples (as shown in Figure 3(a)), Figure 9(a) shows that some intermetallic phases represented by white colour seem to dissolve in aluminium during T6 heat treatment. Elemental analysis (shown in Figures 9(b) and 10) showed that aluminium, zinc, and copper are homogenously dispersed throughout the sample as well as shown by sintered samples without T6 treatment. And in addition, high concentration of magnesium is still located at grain boundaries as well as sample after sintering (Figure 3(b)), and this might be related to the strengthening precipitate MgZn2 and the oxide layer as oxygen content is still near the grain boundary. There are unknown phases on XRD peak pattern in Figure 8, and, based on EDS elemental analysis, there are two different elements which are iron and tin. These elements are not subjects of chemical constitution in this aluminium alloy, so they are impurities. And they are responsible for unknown phase on XRD graph. Table 2 shows different chemical composition on selected point analysis by EDS, and it seems that chemical compositions of T6 heat treated sample have been homogenized as shown by their similar data representing elements distribution and chemical compositions in selected locations.Table 2
Elemental analysis of Alumix 431D after T6 heat treatment from Figure9(b).
Number
Al (wt%)
Zn (wt%)
Mg (wt%)
Cu (wt%)
O (wt%)
1
79.65
5.54
1.82
1.57
0.35
2
78.96
5.88
1.91
1.74
0.34
3
76.66
5.81
2.42
1.83
0.85
4
78.1
5.68
1.88
1.69
0.32
5
78.25
5.76
1.9
1.74
0.32Figure 9
(a) SEM image of Alumix 431D after T6 heat treatment and (b) selected area and locations for mapping and point elemental analysis by EDS numbered 1–5.
(a)
(b)Figure 10
Elemental distribution analysis by EDS of Alumix 431D after T6 heat treatment starting with Al, Zn, and Cu which homogenously dispersed throughout the surface and Mg, O, Fe, and Sn seem to be concentrated at certain places on the surface.


## 3.1. Powder Characterization

Powder was characterized to identify its morphology as shown by Figure1(a). The figure shows irregular shape of powder which is commonly expected from powder made by gas atomization process. Irregular shape of powder tends to have better compactability due to its shape which is able to fill spaces between each particle during compaction compared to circular shape. And another powder characterization is particle size distribution measurement. Dry method was carried out to measure average particle size for this powder, particle size distribution graph as shown in Figure 1(b), and average size of this powder is 105.3 µm. Particle size distribution is one of powder characteristics which strongly affect the sinterability of this material. Effect of particles size on sintering behaviour of aluminium powder was investigated by Liu et al. From their research outcomes, aluminium alloys powder with ~100 µm particle size has been found to supply optimum sintering density [5].Figure 1
(a) Particle morphology and (b) particle size distribution of Alumix 431D powder.
(a)
(b)Determination of thermal properties of this powder is important to estimate its sintering temperature and delubricating temperature. Figure2 shows DSC-TGA curves of Alumix 431D. As it is obvious from DSC graph (blue line), this powder has two endothermic peaks. The first one at 450°C is supposed to be eutectic reaction of Al-Mg and followed by highest peak at 640°C and supposed to correspond to eutectic reaction of Al-Zn. According to Zn content in this alloy powder for 5.5 wt%, it is expected to have higher melting point based on Al-Zn phase diagram where approximately 640°C is a minimum temperature to have liquid phase of Al-5.5Zn. Eutectic reaction of Al-Cu was expected in the trace at 540°C, but the graph shows this with little appearance, due to small amount of Cu on this powder for 0.5 wt%. From DSC curves, sintering conditions can be estimated, as sintering temperature is expected at 0.6–0.75 from melting point to be able to have strong bond between particles.Figure 2
DSC-TGA graph of Alumix 431D powder.At TGA graph (black line), it seems mass of powder decreased starting from 300 to 350°C and increased little more starting from 450°C to 550°C. The first declining line is supposed to remove lubricant from powder, as this powder content lubricant for 1.5 wt%, and from the line it is completely reduced for 1.5 wt% at 350°C. Adding lubricant into powder is to ease ejection force during compaction and to increase cohesive behavior between particles which supports diffusivity during sintering. But lubricant should be removed thoroughly before reaching sintering temperature. And 400°C seems to be safe temperature to completely reduce lubricant from powder. Gaining mass from 450 to 550°C seems to be resulting from reaction between aluminium oxide and magnesium and corresponding to DSC line at 450°C which is supposed to be eutectic point of Al-Mg. And another reason for gaining mass during these temperatures is reaction between aluminium and nitrogen gas to form aluminium nitride (AlN). But detection of aluminium nitride is still questionable due to lacking of proves by X-ray diffraction from sintered aluminium alloy which used nitrogen gas as atmosphere.


## 3.2. Sintering Behavior

Sintering is a process to bond compacted particles by using thermal force below melting point to be able to produce high dense materials. Sintering of this powder was carried out at 560°C–585°C for 1 hour. And atmosphere for sintering was ultra high purity nitrogen gas, because it has been proved that nitrogen gas supports densification process during sintering by reducing the pressure inside the pores which leads to pore filling mechanism [1]. Sintering density was measured to observe the densification behaviour as shown by Figure 3(a). It is expected that sintering density increased with increasing sintering temperature and it seems that optimum density was obtained at 580°C sintering temperature by reaching 96% relative density. At 585°C, sintering density decreased because of abundance of liquid phase and grain growth which leads to particle agglomeration and formed porosity. This phenomenon is called Oswald ripening [6].Figure 3
(a) Sintering density and (b) HRB hardness as a function of sintering temperature for Alumix 431D powder, and it seems that 580°C is an optimum sintering temperature.
(a)
(b)Compaction pressure has some effects on sintering properties of metal powder, because it supports having better interparticle bonding during sintering. To be able to produce high dense materials, using high compaction is suggested prior to sintering. That is the main reason that this research used high compaction pressure for 700 MPa. And the advantage of using high compaction pressure is the fact that surface of the sintered materials appears to be fully densified, so finishing process after sintering is not necessary. According to Figure4(a) pores still remain at body center of samples, and this is related to liquid phase and uncompleted pore filling process during sintering. For highly compacted powder, interparticle bonding reaction could be done at lower temperature due to strong surface energy which leads to easy reaction between each particle, as shown by the graph, and Alumix 431D has high sintering density at 580°C. Lower compaction pressure will need higher sintering temperature with lower sintering density as proved by Martín and Castro. They showed Alumix 431 powder has optimum sintering temperature at 610°C reaching only 94.9% relative sintering density using 400 MPa as compaction pressure [4]. The disadvantage of using high compaction pressure is reducing wearability of mold and needing more power during compaction process even if it will give clean-porosity surface.Figure 4
(a) SEM image of sintered Alumix 431D and (b) selected area and location for mapping and point elemental analysis of sintered Alumix 431D by EDS numbered from 1 to 4.
(a)
(b)Hardness of sintered Alumix 431D was investigated to measure how sintering density corresponded to mechanical properties. Figure3(b) shows highest hardness was obtained at same optimum sintering temperature of 40 HRB. This shows that porosity plays important role in mechanical properties of sintered aluminium as porosity tends to reduce resistance of sintered aluminium to deformation.Microstructure of sintered sample is shown in Figure4(a), and it shows there are sintering precipitates inside the grains and at grain boundaries shown by white color. SEM picture shows quite high densification level with lower rate of pore. Elemental analysis was performed by EDS to determine chemical compositions on selected locations as shown in Figure 4(b). Figure 5 shows the element distributions from some locations as obtained by EDS analysis. The point analysis clearly shows differences in chemical compositions in locations numbered from 1 to 4 as shown in Table 1. This indicates reaction and diffusion during sintering in liquid state. Locations number 1 and number 2 seem to be α aluminium and locations number 3 and number 4 are intermetallic phases. Location number 3 contains high amount of zinc, and it is related to some intermetallic phase such as MgZn2. And number 4 shows tin as an impurity and high amount of magnesium, which is related to formation of spinel MgAl2O4 as a result from reaction between magnesium and oxide layer on aluminium particles as follows:(1)
3
Mg
+
4
Al
2
O
3
⟶
3
MgAl
2
O
4
+
2
AlThis reaction results in decomposition of magnesium on grain boundary or close to pore, so it is expected to see some magnesium in grain boundary. Magnesium behavior during sintering was investigated by several researchers. Pieczonka et al. showed that magnesium moves to surface of aluminium particles at temperature of 450°C by dilatometry measurement [7]. And Lumley et al. investigated the effect of magnesium content on oxide layer removal from aluminium particles, and they showed that 0.5 wt% of magnesium is enough to remove oxide layer during sintering [8]. This reaction between magnesium and oxide layer is usually below sintering temperature. Point number 15 shows that there is tin, and it seems to be an impurity coming from this alloy powder.Table 1
Elemental analysis from selected location in Figure4(b) of sintered Alumix 431D.
Number
Al (wt%)
Zn (wt%)
Mg (wt%)
Cu (wt%)
Sn (wt%)
O (wt%)
Si (wt%)
1
62.76
4.81
1.5
0.89
—
0.32
—
2
61.8
5.33
1.47
1.13
—
0.31
—
3
48.97
12.56
5.52
5.39
—
2.09
—
4
48.54
4.71
4.39
1.27
6.72
6.96
0.73Figure 5
Elemental distribution analysis by EDS of sintered Alumix 431D starting with Al, Zn, and Cu which homogenously dispersed throughout the surface and Mg, O, and Sn seem to be concentrated at certain places on the surface.To investigate intermetallic phases during sintering, X-ray diffraction was carried out as shown in Figure6. Aluminium is dominant peak in the XRD spectrum followed by intermetallic MgZn2 and CuAl2 phases. MgZn2 is a precipitate which is expected to be formed during sintering due to possibility of formation of GP zones, η
′ and η, even though this phase is coherent with α aluminium. CuAl2 is precipitate which is commonly found in Al-Cu alloy and easily formed at room temperature at certain amount of Cu. And there is unknown phase on XRD peak pattern, and it seems to be the responsibility of tin which was found on EDS point analysis.Figure 6
X-ray diffraction pattern of sintered Alumix 431D powder.


## 3.3. T6 Heat Treatment

The T6 heat treatment is usually done to aluminium alloys to optimize their mechanical properties. The investigated powder has similar alloy system to 7XXX (Al-Zn-Mg-Cu) alloy. These materials are heat treatable and they possess a potential to form strengthening precipitates such as MgZn2 and CuAl2. These strengthening precipitates will form after reaching optimum aging conditions and have been solutionized and water quenched before. Figure 7(a) shows hardness of the sintered samples after T6 heat treatment as a function of sintering temperature. As expected, hardness of 68 HRB was achieved as the highest hardness and obtained after being sintered at 580°C sintering temperature followed by T6 heat treatment. And previously, this sintering condition also gave highest sintering density and hardness. Tensile strength load curves are showed in Figure 7(b), and there is an improvement in sample after T6 heat treatment by reaching the tensile strength 513 MPa with 5% elongation. The improvement of tensile strength after T6 heat treatment is related to strengthening precipitates which impede dislocation movement during tensile deformation and, as a result, tensile strength increased. Strengthening precipitates which were formed during T6 heat treatment were investigated by XRD as shown by Figure 8. MgZn2 was found to be dominant strengthening precipitates in this powder followed by CuAl2. The process of these precipitates formation is as follows:(2)
Supersaturated
solid
solution
⟶
Guinier-Preston
Zones
(
GPZ
)
⟶
η
′
⟶
η
MgZn
2Hexagonal close-packed (HCP) crystal structure of MgZn2  η phase formed after increasing time of η
′ phase to arrange into the incoherent equilibrium phase. This η phase is the obstacle dislocation movement, and as a result increasing mechanical properties are observed [9–11].Figure 7
(a) Hardness and (b) stress-strain curve at tensile test of Alumix 431D before and after T6 heat treatment (for 580°C sintering temperature).
(a)
(b)Figure 8
X-ray diffraction pattern of Alumix 431D after T6 heat treatment.SEM supplemented by EDS microanalyses was performed to observe microstructures after T6 heat treatment as shown in Figures9(a) and 9(b). Compared to sintered samples (as shown in Figure 3(a)), Figure 9(a) shows that some intermetallic phases represented by white colour seem to dissolve in aluminium during T6 heat treatment. Elemental analysis (shown in Figures 9(b) and 10) showed that aluminium, zinc, and copper are homogenously dispersed throughout the sample as well as shown by sintered samples without T6 treatment. And in addition, high concentration of magnesium is still located at grain boundaries as well as sample after sintering (Figure 3(b)), and this might be related to the strengthening precipitate MgZn2 and the oxide layer as oxygen content is still near the grain boundary. There are unknown phases on XRD peak pattern in Figure 8, and, based on EDS elemental analysis, there are two different elements which are iron and tin. These elements are not subjects of chemical constitution in this aluminium alloy, so they are impurities. And they are responsible for unknown phase on XRD graph. Table 2 shows different chemical composition on selected point analysis by EDS, and it seems that chemical compositions of T6 heat treated sample have been homogenized as shown by their similar data representing elements distribution and chemical compositions in selected locations.Table 2
Elemental analysis of Alumix 431D after T6 heat treatment from Figure9(b).
Number
Al (wt%)
Zn (wt%)
Mg (wt%)
Cu (wt%)
O (wt%)
1
79.65
5.54
1.82
1.57
0.35
2
78.96
5.88
1.91
1.74
0.34
3
76.66
5.81
2.42
1.83
0.85
4
78.1
5.68
1.88
1.69
0.32
5
78.25
5.76
1.9
1.74
0.32Figure 9
(a) SEM image of Alumix 431D after T6 heat treatment and (b) selected area and locations for mapping and point elemental analysis by EDS numbered 1–5.
(a)
(b)Figure 10
Elemental distribution analysis by EDS of Alumix 431D after T6 heat treatment starting with Al, Zn, and Cu which homogenously dispersed throughout the surface and Mg, O, Fe, and Sn seem to be concentrated at certain places on the surface.


## 4. Conclusions

High compactability and sinterability by reaching high green density and sintering density were proved for Alumix 431D powder. With high compaction pressure of 700 MPa, sintering density of Alumix 431D reached optimum sintering density at 96% relation to theoretical one. Microstructures showed high densification especially on surface which is expected to reduce finishing work after sintering process, but pores still remain inside the sintered materials due to incomplete pore filling mechanism during sintering.Obtained mechanical properties confirmed microstructural and phase analyses. At optimum sintering conditions, that is, at 580°C, the Alumix 431D showed the highest hardness and tensile strength reaching up to 40 HRB and 329 Mpa for sintered materials and 68 HRB for sintered materials after T6 heat treatment. This means strengthening precipitates from this powder were successfully formed during T6 heat treatment process by increasing their mechanical properties as it has been confirmed by X-ray diffraction showing MgZn2 and CuAl2 as strengthening precipitates.



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*Source: 987687-2015-03-26.xml*