3.2 Density and Porosity
Table 3.1
Sl No | Particulars | ρth (g/cm3) | ρact (g/cm3) | Porosity (%) |
| | | AN | EP II | AN | EP II |
1 | 0% Beryl | 2.78 | 2.75 | 2.77 | 1.08 | 0.36 |
2 | 6% Beryl | 2.79 | 2.76 | 2.78 | 1.07 | 0.35 |
The Table 3.1 presents the theoretical and experimental densities calculated and measured, respectively. The Al 2024 and beryl possess densities of 2.78 and 2.65 g/cm3, respectively. The density is an important characteristic to be determined for any material system, since it reflects on the weight as well as the porosity level or any other type of defects like blow holes, shrinkage, porosity, inclusion etc, that would have originated during the casting process. While the density of Al 2024 2% Beryl composite in the annealed condition is 2.75 g/cm3, on the other hand, the density values of the ECAP processed composites are nearly same as that of the theoretical density values. This demonstrates unequivocally that ECAP has made a significant impact in lowering the porosity value that exist in the casting. The density value decreases during the ECAP process, as the material is continuously subjected to high strain rates. Similar findings are reported by Balog et al. [22], wherein Al-AlN composites processed with ECAP have attained greater than 98% of the theoretical value. In this work also, the same trend is noticed for Al-Beryl composites containing different levels of Beryl particles.
3.3 ECAP process influencing Surface hardness (SH) and Surface Roughness (SR)
As regards the ECAP process of Al2024 alloy and its composite, the hardness increased in the ascending order AN, EPI and EPII, wherein AN is exhibiting the lowest hardness and UTS, on the other hand EPII is showing the highest. The value EPI is showing in between AN and EP II.
Now coming to the literature aspects, it is reported by A. Muralidhar et al. [23], increasing the number of passes during ECAP, the hardness level has increased and at the same time, the grain refinement has taken place. The same behavior is seen in the present work also and hence it is in line with the published [23] work. The study by Lokesh and Mallik [24] regarding the effect of ECAP on the mechanical properties and structural features in Al6061-SiCp composites produced by stir cast method showed increase in UTS as well as hardness for the ECAP processed (three passes) samples. It is further reported that the better mechanical properties obtained are attributed to the substantial decrease in the grain size. The work done by the same authors have reported [25] enhancements in strength & hardness as well as grain refinement in Al6061-Grp composites made by stir cast technique. Ramesh Kumar et al. [26] reported the beneficial effect of ECAP in Al5083 alloy at room temperature, wherein the hardness has increased with increase in four number of passes. The microstructural evolution and strengthening mechanism of Mg alloy processed through ECAP (2 passes) have been reported by Gopi et al. [27]. In this particular study, two passes of ECAP have enhanced the hardness, increased the UTS and at the same time grain size decrease is seen. The hall Petch equation [28] also reports the relationship exists between the hardness and grain size. As reported, [28] higher the hardness, finer is the grain size. This is covered in detail in section 3.5 down the text.
As regards the surface roughness (SR) it is observed that the ECAP processed with pass II samples have aided in reducing the surface roughness parameters. Similar findings have been reported [29–30] on the surface roughness of Al-Si alloy with the additions of other elements, wherein the addition of phosphorus to the base alloy has been reported to be beneficial in reducing the surface roughness level and increasing the hardness value. In our work also, the addition of Beryl has dramatically decreased the SR value and enhanced the hardness level. As stated, [31], the obvious reason for the trend obtained in respect of surface roughness after two passes of ECAP may be due to increase in the strain rate resulting in grain boundary sliding, thus yielding smoother surface and superior surface topographical features compared to the annealed samples [32].
3.4 Microscopic Examination
The microscopic examination involved both optical microscopy and scanning electron microscopy, which are covered in detail below.
3.4.1 Light microscopy
The light micrographs pertaining to Al-B-0 AN, Al-B-6 AN, Al-B-0 EP II and Al-B-6 EP II are shown in Figs. 3.4 a & b and 3.5 a & b respectively. From the light micrographs, it is very well seen that the second major element in Al 2024 alloy being Cu alloy shown in these Figs. 3.4 a and b, 3.5 a and b The Al grains, grain boundaries are also marked in the same Figs. 3.4 b and 3.5 b. One can easily make out the differences in the grain sizes by comparing Fig. 3.4 a with Fig. 3.4 b and Fig. 3.5 a with Fig. 3.5 b. There is a gradual reduction in the grain size when the annealed sample undergoes ECAP process with pass I and pass II. In the present work, the number of passes has been restricted to two only in the present work.
The grain size measurements have been carried out using the ASTM standard involving comparison method. Thus, the grain size of Al-B-0 AN, Al-B-6 AN, Al-B-0 EP II and Al-B-6 EP II are 88, 83, 32 and 21 microns, respectively. A similar work done by Mohamed Ibrahim ABD EL AAL and M.M. SADAWY [33] have clearly demonstrated regarding the grain size effect following ECAP in pure Al samples, with increase in number of passes, the grain size reduction has been reported. Thus, the present work gets incredibly good backing from the published work [33]. In another investigation done by Yong Li and T G Langdon [17] ECA pressing of Al 6061 alloy with 10 wt.% Al2O3 particles, wherein reduction in the grain size after effecting 5 number of passes has been reported. This work also gives able support to the present finding of ECAP effect in Al Beryl composites. The literature reports [17, 33] and the present work go hand in hand with each other from the point of undergoing grain size decreases during plastic deformation process and its effect on the properties.
3.4.2 Effect of ECAP process on the Tensile properties and Grain size
Figures 3.6, 3.7 and 3.8 present the UTS, %elongation and grain size in respect of Al-B-0 and Al-B-6 samples in the form of bar diagrams.
The plot of tensile strength for the Al 2024 composites containing 0 and 6 wt.% are displayed in Fig. 5, including the ECAP processed samples. From Fig. 3.6, one can make out the fact that with increase in Beryl content from 0 to 6 wt.%, there is an increase in tensile strength to the tune of 56% and 93% in respect of Al-B-0 EP II and Al-B-6 EP II, respectively compared to their corresponding annealed counterparts.
Also, the Al 2024 composites samples undergoing ECAP have clearly indicated much higher level of improvements in the tensile strength both in single and two passes. Also, the tensile strength has become the maximum for ECAP with pass II. When one compares Al-B-0 AN and Al-B-0 EP II with Al-B-6 AN and Al-B-6 EP II, the difference in the grain size is more in Al-B-6 samples, which shows a difference of 54. Whereas the difference is 60 in Al-B-0 samples. This is because in the first instance, ECAP with EP II has reduced the grain size. In the second instance, a further reduction has taken place due to Vander wall/ intermolecular forces acting between the reinforced particles as well as particles to matrix interaction as reported in the literature, its instance in polymer scienc. This type of trends has been explained based on the work done by other researchers [34–35].
As reported [36], Al-Si-Mg composites containing Beryl particles in the range 2 to 10 wt.% have shown hardness increase with increase in Beryl concentration from 0 to 6 wt. % Further, it is reported [36] that the tensile strength has also increased for the Beryl addition up to 6 wt.%, Likewise, many researches have conducted and reported [37] mechanical property evaluations especially hardness and UTS on Al6061 alloy with Beryl as reinforcement particles and obtained increase in hardness and tensile strength with increase in beryl concentration. Thus, all these research contributions [36–37] have given valuable support to the present findings for getting enhanced hardness as well as UTS in Al/Mg alloys/composites containing other types of reinforcements at varied levels.
As regards % elongation effect, it is quite evident from Fig. 3.7 that ECAP has made good influence on the % elongation on the samples. The annealed samples are showing the highest value whereas EP II is exhibiting the least. The other sample namely EP I is showing % elongation value in between them. Further, it is noticed that as the hardness increases, the % elongation decreases. This type of trend is seen in AN, EP I, EP II samples. This is quite logical with the fact that when the hardness increases, the material will tend to become more and more brittle as evidenced from % elongation data as well as from the supporting literature points [38].
Now referring to Fig. 3.8, the AN sample has shown the highest grain size of 89 microns, whereas EP I display the least. This is quite understandable in view of the fact that the samples undergoing plastic deformation involving ECAP with passes I and II, Pass II has revealed substantial reduction in the grain size compared to AN. The sample with EP I is in between these two samples. Thus, the ECAP has played a dominant role in bringing down the grain size to about 21 microns.
3.4.3 SEM for Tensile damage assessment
The fractographic features of tensile damage have been conducted using scanning electron microscopic (SEM) examination.
The SEM images pertaining to Al-B-0 AN, Al-B-6 AN, Al-B-0 EP II and Al-B-6 EP II are enumerated in Figs. 3.9 a and b vs 3.10 a and b respectively. Now comparing Fig. 3.9 b with Fig. 3.9 a, higher degree of plastic deformation with increased matrix distortion and appearance of deep ridges (marked) are seen in Fig. 3.9 a. Further, the debonding and dislocations effects are more pronounced in (Al-B-0 AN) with larger grain boundaries as seen in Fig. 3.9 a compared to Fig. 3.9 b (Al-B-6 AN). Similarly, the samples Al-B-6 AN and Al-B-6 EP II are compared, the samples Al-B-6 EP II (Fig. 3.10 b) reveal less deformation features, finer grain boundaries and less appearance of ridges compared to Al-B-0 EP II (3.10 a) as well as Al-B-6 AN (3.9 b). Also, the matrix distortion and deformation patterns are less noticed in Al-B-6 EP II (Fig. 3.10 b) compared to all the other three samples (Al-B-0 AN, Al-B-6 AN, Al-B-0 EP II). Thus, the SEM examination gives exceptionally good accountability to the damage features, and they are in line with the tensile data gathered in this work. The work may be summarized that the increasing the Beryl addition from 0 to 6 wt.% to the Al 2024 and subjecting it to ECAP, there is a considerable decrease in the grain size and increase in tensile strength. The reason for these trends may be attributed to the plastic deformation involved. The % elongation tries decreases due to the addition of Beryl content of 6 wt.% in Al 2024 alloy. The same explanation holds good for the Al2024 alloy without Beryl addition as well.