DRY SLIDING WEAR BEHAVIOUR OF STIR CAST LM 25/ZrO 2 METAL MATRIX COMPOSITES

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Govindan Karthikeyan GowthamiThankachi Raghuvaran Jinu ISSN 1333-1124 eissn 1849-1391 DRY SLIDING WEAR BEHAVIOUR OF STIR CAST LM 25/O 2 METAL MATRIX COMPOSITES Summary In the present study, an investigation into wear properties has been carried out to identify the influence of O 2 as the reinforcement material on the LM25 MMC composite. Aluminum LM25 is selected as the base material, and it is reinforced with varying proportions of, 3, 6, 9, 12 and 15% of zirconia (O 2 ) manufactured by stir casting. Six tensile test and wear test samples were prepared according to the ASTM B-557-M-94 and ASTM G99 standards. Then, the prepared samples were subjected to the wear test using a pin-on-disc wear tester by varying the parameters such as loads of 1 N, 2 N and 3 N and sliding distances of 1, m, 1,2 m and 1,4 m for various percentages of O 2 reinforcement composites, and corresponding wear losses were measured. The wear test results reveal that an increase in the percentage of O 2 decreases the wear loss. It is also found that an increase in load and sliding distances increases the wear loss and hence the low wear loss is obtained for the sample which contains 15% of O 2 and is subjected to a wear test load of 1 N at a 1 m sliding distances. Finally, the wear test samples are subjected to the surface roughness test. The surface roughness test reveals that an increase in the percentage of O 2 enhances smoothness and decreases surface roughness. Key words: metal matrix composites, aluminium LM25 alloy, zirconia (O 2 ), sliding wear test 1. Introduction Metal Matrix Composites (MMCs) have emerged as an important class of materials used in structural, wear, thermal, transportation and electrical applications because they offer a high strength-to-weight ratio, high stiffness and good wear resistance [1]. The aluminum based metal matrix composites are excellent novel materials for applications in aerospace, automotive and transportation industries [2]. The fabrication methods of the aluminum based composites can be categorized into three processes: solid-state methods, semisolid state methods and liquid state methods [3]. Stir casting is a liquid state method for composite fabrication, in which a dispersed phase is mixed with a molten matrix metal by mechanical stirring [3]. The aluminum LM25 alloy exhibits low density and high thermal conductivity. However, its wear resistance is low [4-5]. In order to avoid this drawback, this LM25 alloy was reinforced with O 2 to form LM25- O 2 composites. This composite is used for marine TRANSACTIONS OF FAMENA XXXIX-4 (215) 89

G. Karthikeyan, G.R. Jinu Dry Sliding Wear Behaviour of casting, the manufacture of motorcars, engine parts, switch boxes, hydraulic systems (piston, cylinder) and in food-processing industries. Ceramic materials, such as SiC, TiC, TiB 2, B 2, AIN, Si 3 N 4, Al 2 O 3 and SiO 2 are generally used to reinforce aluminum alloys[6]. Among all the reinforcements used in aluminum based composites O 2 particulates alone have shown potential superiority in improving mechanical properties and microstructure. Further, O 2 particulates provides noticeable weight saving. The O 2 reinforcement is very attractive as it exhibits a density of 8.18 gm/cm 3, the melting point of 186 C, UTS-425 MPa, VHN-15, and Young s modulus of 98 GPa. It was also found that O 2 shows superior strength and higher hardness and fracture toughness with a slight reduction in ductility [8]. Wear resistance is the most important property of a material, when it is a candidate for engineering applications. Hence, this property of various aluminum alloys has been widely investigated by researchers [3]. The studies on LM25/O 2 reinforced composites are not found in any of the previous investigations. It was also found that only a few papers studied the sliding wear behaviour of composites with the O 2 reinforcement material in situ [7-8]. Wear properties of composites mainly depend on the grain size [6]. Various studies carried out on Al 2 O 3, SiC, TiO 2, TiB 2, O 2, Si 3 N 4 in various contact situations showed mild wear [5, 9-1]. It has also been found that the wear test carried out on Al-SiC MMCs used for commercial break pads confirmed that the break loss increases with the increasing sliding velocity [11]. It has also been found that the transfer layer of MMCs acted as a protective cover, and it helped to reduce both wear rate and friction coefficient. So, this experimental method was chosen for the present study. The literature review showed, that MMCs play a vital role in replacing metals, due to their advanced mechanical and metallurgical properties. A lot of researchers have concentrated on developing new composites such as Al 661, LM25 reinforced with various elements such as TiB 2, SiC, TiC, B 2, AIN, Si 3 N 4, Al 2 O 3 and their wear properties were analyzed in earlier studies [3-5]. No papers have been found to analyze the effect of O 2 on the LM25 base material while subjected to wear. The papers mainly concentrated on developing a new composite material by taking LM25 as the base material and varying the percentage of O 2 to identify the influence of O 2 on the wear behaviour. 2. Materials and Methods 2.1 Materials The aluminium LM25 alloy was taken as the base material and the O 2 powder (particle size 1-1µm) was chosen as the reinforcement material. The corresponding chemical compositions are given in Table 1 and 2. In this study, six cast samples were prepared by keeping LM25 as the base material and varying the weight percentage of O 2 as follows: %, 3%, 6%, 9%, 12% and 15%. Casting was carried out by using a stir casting process as shown in Fig. 1 (a-b). Initially, the aluminum LM25 alloy was melted in a pot by heating in a blower furnace at 85 c for 15 min. The O 2 powder was preheated at 575 C in a separate muffle furnace. The furnace temperature was raised above the liquid temperature of LM25 to about 85 C to melt LM25 completely and then LM25 was added to the preheated O 2 powder slowly. Stirring was carried out with the help of a drilling machine for about 15 minutes, and the stirring rate maintained the speed of about 95 rpm. This mixture was then poured into the mould cavity, and was cooled at the room temperature. This procedure was repeated in the preparation of six specimens with different proportion of O 2 as shown in Fig.1(a-b). 9 TRANSACTIONS OF FAMENA XXXIX-4 (215)

Dry Sliding Wear Behaviour of Stir Cast LM25/O2 Metal Matrix Composites G. Karthikeyan, G.R. Jinu (a) Schematic view of stir casting setup (b) Photographic view of stir casting setup Fig. 1 (a-b) Casting of MMC by using stir casting method. Table 1 Chemical composition of aluminum LM25 alloy (weight percentage).1% Mg.2-.6% Si Fe 6.5 7.5%.5% Mn.3% Ni.1% Zn.1% Pb.1% Sn.5% Ti.2% Al Bal Table 2 Chemical composition of O2 (weight percentage) SiO2.25% TiO2.16% Fe2O3.7% Y2O3 3 to 5% bal 2.2 SEM-EDS analysis with element distribution Energy dispersive spectrometry (EDS) analysis had been applied to all prepared samples of various percentages of O2 before they were subjected to the wear test. The present section, helps to find out information about the type of the element present in all cast samples. Fig. 2 (b), (d), (f) and (h) shows the EDS of aluminium LM25 with its elements. And Fig. 2 (a), (c), (e) and (g) presents the topographical image produced by a scanning electron microscope (SEM). From the graph obtained from the EDS test the results are used to confirm the chemical composition of the LM 25/O2 composites, such as aluminium, zirconium, iron, copper, magnesium, zinc, silicon and all other elements present in the prepared composites as shown in Fig. 2 (b), (d) (f) and (h). The shrinkage and porosity were not identified in the micrograph. This is evidence of good quality casting. An increase in the percentage of O2, resulted in the oxide formation at the pin surface, and the developed oxides act as a wear protective layer for various loads. This is clearly seen in Fig. 2 (d), (f) and (h). Finally, the EDS analysis confirmed the presence of aluminium and O2 particles, as shown in Fig 2 (b), (d), (f) and (h). TRANSACTIONS OF FAMENA XXXIX-4 (215) 91

G. Karthikeyan, G.R. Jinu Dry Sliding Wear Behaviour of Stir Cast LM25/O2 Metal Matrix Composites cps/ev 25 2 15 Mn Mg Al Si Y Mn 1 5 2 4 6 kev (a) 8 1 12 1 12 (b) cps/ev 7 6 5 4 3 Mn Fe Al Si Y Mn Fe 2 1 2 4 6 kev (c) 8 (d) cps/ev 35 3 25 2 15 C O Fe Zn Mg Al Si Fe Zn 1 5 1 2 3 4 (e) 5 kev 6 7 8 9 1 (f) cps/ev 1 8 6 O Ti Mn Al Y C Fe Mg Si Ti Mn Fe Y 4 2 2 (g) 4 6 8 kev 1 12 14 16 (h) Fig. 2 SEM images and EDS patterns of various composites (a) SEM image of LM25 (b) EDS pattern of LM25 (c) SEM image of LM25-3% O2 composites (d) EDS pattern of LM25-3% O2 composites (e) SEM image of LM25-6% O2 composites (f) EDS pattern of LM25-6% O2 composites (g) SEM image of LM25-9% O2 composites (h) EDS pattern of LM25-9% O2 composites 2.3 Sliding wear test The wear test was conducted by using a computerized wear test pin-on-disc machine (DUCOM, TR-2LE-PHM-4) as per ASTM G99 standard [12]. The EN31 steel was used as the counter disc material. Before testing, acetone was applied to clean the surface of the pin and 92 TRANSACTIONS OF FAMENA XXXIX-4 (215)

Dry Sliding Wear Behaviour of G. Karthikeyan, G.R. Jinu the disc. The initial roughness of all cast samples was tested, the data of which is given in Table 4. Then, all six samples were subjected to the wear test for a load range of 1 N, 2 N and 3 N at a constant speed of 2 rpm, sliding velocity of 2.5 m/s and continuous sliding distance of 1 m, 12 m and 14 m, respectively. While testing, the circular disc was rotated, and the pin specimen was kept stationary and perpendicular to the disc. Initially, the samples were weighed by using a simple pan electronics weighing machine with the precision of. 1 g.. The contour face disc was cleaned with an organic solvent to remove the traces obtained during each test. Similarly, the pin was also weighed before and after the testing to identify the amount of wear loss in each test. The obtained weight loss resulted from each test was converted into the wear loss based on the corresponding density of prepared composites by using equation (2). First, the densities of all cast samples are calculated by using equation (1). Density = Wear loss = ( ) / (r-disc radius, n-sliding velocity, t-time) (1) 2) The coefficient of friction is obtained from the experiments using a data acquisition system for the steady-state period of the last considered 1s. From the calculated wear volume, the specific wear rate and the coefficient of friction (COF) were calculated by using the following equation from literature [12]. Coefficient of Friction = 2.4 Surface Roughness Test A cylindrical rod of 8 mm in radius and 4 mm in length was prepared for the wear test. Then, the wear tested samples were subjected to the surface roughness test by using a Mitutoyo, SJ21 tester. The reason for using the surface roughness test is to find the influence of O 2 on the surface roughness performance of the component. Irregular surface may form nucleation sites for cracks or corrosion. It is also noted that rough surfaces usually wear more quickly and have a higher coefficient of friction than smooth surfaces. On the other hand, roughness may promote adhesion [1]. 3. Results and discussion 3.1 Effect of wear on various composites The wear results were observed for various loads of 1, 2 and 3 N for six cast samples of LM25 with, 3, 6, 9, 12 and 15 % of O 2 reinforced composites as given in Fig. 3 (a-c). For obtaining each point in the curve five tests were performed and an average of all the five values is applied to obtain the points in the curve. The wear loss of pure LM25 is compared with various percentages of O 2 reinforced composites for all the above three load levels. From Fig. 3 (a), 3 (b) and 3 (c), it is clear that lower wear was obtained in the composites which were reinforced with a higher weight percentage of O 2, and this holds true for all the three load levels. Hence, it is clearly observed that the percentage of an increase in O 2 reduces the wear loss. Similarly, while comparing Fig. 3 (a) with 3(b) and 3 (c), it is found that when the load increases, the wear loss also increases in all six samples. It is also noted that the wear loss decreases gradually with an increase in the percentage of the O 2 reinforcement, when compared to pure LM25. In the wear samples, an increase in O 2 decreases the wear in a non-linear manner [13-14]. (3) TRANSACTIONS OF FAMENA XXXIX-4 (215) 93

G. Karthikeyan, G.R. Jinu Dry Sliding Wear Behaviour of Wear loss (micrometer) 25 2 15 1 5 5 1 15 2 25 3 35 4 Time (S) Load 1 N Al LM25 Al LM25-3%O2 Al LM25-6%O2 Al LM25-9%O2 Al LM25-12%O2 Al Lm25-15%O2 3 (a) Wear loss(micrometer) 3 25 2 15 1 5 5 1 15 2 25 3 35 4 Time(S) Load 2 N Al LM25 Al LM25-3%O2 Al LM25-6%O2 Al LM25-9%O2 Al LM25-12%O2 Al LM25-15%O2 3 (b) Wear loss(micrometer) 3 25 2 15 1 5 5 1 15 2 25 3 35 4 Load 3 N Al LM25 Al LM25-3%O2 Al LM25-6%O2 Al LM25-9%O2 Al LM25-12%O2 Al LM25-15%O2 Time(s) 3 (c) Fig. 3 (a-c) Wear loss of various composites under different load (a) 1 N, (b) 2 N and (c) 3 N 3.2 Effect of weight loss on load The effects of weight loss when the load is varied for 25 sec are shown in a graph (Fig. 4). it is obvious from the graph, that the wear loss increases with an increase in load from 1 to 2, and 3 N, respectively. Similarly, while comparing the weight loss from 1 to 3 N, the percentage of weight loss for 3 N is higher. When comparing pure LM25 with the 15% O 2 reinforcement, a significant difference in the wear loss is observed. In the same way, while comparing the percentage of the weight loss in LM25 and various percentages of the O 2 reinforcement it is observed that the weight loss decreases with an increase in the percentage of the O 2 reinforcement [12]. 94 TRANSACTIONS OF FAMENA XXXIX-4 (215)

Dry Sliding Wear Behaviour of G. Karthikeyan, G.R. Jinu 25 wear loss (micrometer) 2 15 1 5 1 2 3 LM 25 LM25-3% O2 LM25-6% O2 LM25-9% O2 LM25-12%O2 LM25-15%O2 Load (N) Fig. 4 Wear Loss for Various Composite Materials A graph was plotted between the various weight percentages of O 2 in LM25/O 2 composites versus the calculated coefficient of friction for the load ranges of 1, 2 and 3 N at a constant speeds of 2 rpm with a sliding velocity 2.5 m/s, and a sliding distance of 14 m, as shown in Fig. 5. So, Fig. 5 shows, that the coefficient of friction is high at the beginning and decreases gradually due to the reinforcement of aluminium alloy with O 2. Similarly, it is also observed that, when the load increases from 1 to 3 N, the coefficient of friction also increases. While comparing the coefficient of friction of pure LM25 with various levels of O 2 reinforcement, it is observed that the coefficient of friction decreases with an increase in the percentage of the O 2 reinforcement. Because the increase in the percentage of O 2 leads to the lowering of the coefficient of friction in the composites, it reduces the pin-to-disc contact. This effect is due to the good bonding and the nature of the reinforcement of O 2. These results are well in agreement with earlier studies [1, 6 & 12]. Coefficient of friction,35,3,25,2,15,1,5 3 6 9 12 15 Wt % of O 2 with LM25 alloy Load 1 N 2 N 3 N Fig. 5 Co-efficient of friction of Al LM 25 Weight % of O 2 A graph was plotted between the various weight percentages of O 2 in LM25/O 2 composites versus wear loss for the sliding distance of 1, 12 and 14 m as shown in Fig. 6. It is observed that, the wear loss in samples of different compositions increases with an increase in the sliding distance. An increase in the percentage of O 2 will decrease the wear loss at all sliding distances. TRANSACTIONS OF FAMENA XXXIX-4 (215) 95

G. Karthikeyan, G.R. Jinu Dry Sliding Wear Behaviour of Wear loss(micrometer) 4 35 3 25 2 15 1 5 Sliding distance 1 m 12 m 14 m 3 6 9 12 15 wt % of O2 with LM25 alloy 3.3 Surface roughness of pin Fig. 6 Wear loss of LM25 - wt % O 2 for various sliding distances The measured worn surface roughness of various composites for the 3 N load is given in Table 3. From the Table 3, it is obvious that the surface roughness value is higher for the pure LM25 alloy, and the roughness value decreases with an increase in the percentage of the O 2 reinforcement material. A graph was plotted between the various weight percentages of O 2 in LM25/ O 2 composites versus surface roughness as shown in Fig. 7. It is obvious that the curve varies linearly up to 6% O 2. Then, the curve decreases slowly with a further increase in the percentage of O 2. Table 3 Worn surface roughness of various composites (3 N load). % of composition Initial surface roughness (Ra) Surface roughness (Ra) (before being subjected to load) (after being subjected to load) Al LM25 3.623 4.31 Al LM25-3% O 2 1.923 2.877 Al LM25-6% O 2 1.23 1.954 Al LM25-9% O 2.998 1.654 Al LM25-12% O 2.888 1.54 Al LM25-15% O 2.8 1.367 Surface roughness(micrometer) 5 4 3 2 1 % 3% 6% 9% 12% 15% Wt % O 2 WITH LM25 ALLOY Fig. 7 Worn surface roughness for various composites 96 TRANSACTIONS OF FAMENA XXXIX-4 (215)

Dry Sliding Wear Behaviour of G. Karthikeyan, G.R. Jinu 4. Conclusions Wear characteristics of the stir cast LM25/O 2 metal matrix composites were investigated experimentally. From the experimental results, the following conclusions are made: 1. EDS studies were carried out to confirm the presence of aluminium, zirconium, iron, copper, magnesium, zinc, silicon, etc in the developed LM25/ O 2 metal matrix composites. The oxide formation, which acts as a protective layer for the surface at various loads, is also identified based on the EDS results. 2. The percentage of the oxide formation increases with an increase in the percentage of the O 2 reinforcement, which causes a decrease in wear rate. The same result was confirmed in the wear test results. 3. The wear test results showed that the wear loss decreases with an increase in the percentage of O 2. 4. The wear loss increases with an increase in load from 1 to 3 N for all samples. 5. The coefficient of friction of the LM25/O 2 metal matrix composites decreases with an increase in O 2, hence the maximum coefficient of friction is obtained under the 3 N load when compared to the load of 1 and 2 N. 6. The wear test results show that, when the load and the sliding distance increase, wear loss will also increase. Therefore, the maximum wear loss is obtained for the 3 N load and the 14 m sliding distance, which was also confirmed by the wear test results. 7. The surface roughness value decreases with an increase in the percentage of the O 2 reinforcement. REFERENCES [1] S.Tahamtan,A.Havaee,M.Emamy,M.S.Zabihi. Fabrication of Al/A 2 6 -Al 2 O 3 nano/micro composite by combining ball milling and stir casting technology. Materials and Design, 49,347-359 (213). [2] Vencl et al., Tribological behaviour of Al-based MMCs and their application in automotive industry, Tribology in Industry, 26, 3-4, 31-38 (24). [3] S.Goplakrishnan,N.Murugan, Production and wear characterization of AA 661 matrix titanium carbide particulate reinforced composite by enhanced stir casting method.composites:part B, 43, 32-38 (212). [4] Kadir Kocatepe. Effect of low frequency vibration on porosity of LM25 and LM6 alloys Materials and Design, 28, 1767-1775 (27). [5] G.Elango,B.K.Raghunath.Tribological behavior of hybrid (LM25Al+SiC+TiO 2 ) metal matrix composites.procedia engg, 64, 671-68 (213). [6] Mallikarjuna C, Shashidhara SM, Mallik US, Parashivamurthy KI. Grain refinement and wear properties evaluation of aluminium alloy 214 matrix TiB 2 in-situ composites. Mater Des, 32, 3554 9 (211). [7] Joel Hemanth. Development and property evaluation of aluminum alloy reinforced with nano- O 2 metal matrix Composites.Material Science and Engineering A, 57, 11-113 (29). [8] Joel Hemanth. Fracture behavior of cryogenically solidified aluminum-alloy reinforced with nano- O 2 metal matrix composites.journal of Chemical Engineering and Materials Science, 2(8), 11-121 (211). [9] Mandal A, Chakraborty M, Murty BS. Effect of TiB 2 particles on sliding wear behavior of Al 4 alloy. Wear, 262,16 166 (27). [1] Caracostas CA, Chiou WA, Fine ME, Cheng HS. Tribological properties of aluminium alloy matrix TiB 2 composite prepared by in situ processing. Metall Mater Trans A, 28,491 52 (1997). [11] Shorowordi KM, Haseeb, Celis JP. Velocity effects on the wear, friction and tribochemistry of aluminium MMC sliding against phenolic brake pad. Wear, 256,1176 1181(24). [12] Vettivel SC, Selvakumar N, Leema N. Experimental and prediction of sintered W composite by using artificial neural networks. Mater Des, 45,323 335 (213). TRANSACTIONS OF FAMENA XXXIX-4 (215) 97

G. Karthikeyan, G.R. Jinu Dry Sliding Wear Behaviour of [13] Tjong SC, Lau KC. Abrasive wear behavior of TiB 2 particle-reinforced copper matrix composites. Mater Sci Eng A, 282,183 186 (2) [14] Mandal A, Chakraborty M, Murty BS. Effect of TiB2 particles on sliding wear behavior of Al 4 alloy. Wear, 262,16 166 (27) Submitted: 2.1.214 Accepted: 14.1.215 Govindan Karthikeyan, Assistant Professor p_gkarthikeyan@yahoo.co.in Department of Mechanical Engineering, Regional Office, Anna University: Tirunelveli Region-6277, Tirunelveli, Tamilnadu, India GowthamiThankachi Raghuvaran Jinu, Assistant Professor gr_jinu198@yahoo.com Department of Mechanical Engineering, University College of Engineering Nagercoil-6294, Tamilnadu, India 98 TRANSACTIONS OF FAMENA XXXIX-4 (215)