1 Potential of palm kernel activated carbon epoxy (PKAC-E) composite as solid 2 lubricant: Effect of load on friction and wear properties 3 K.W. Chuaa, M.F.B. Abdollaha,b,*, N.A. Mat Tahira, H. Amiruddina,b 4 5 a 6 Faculty of Mechanical Engineering, Universiti Teknikal Malaysia Melaka, 7 Hang Tuah Jaya, 76100 Durian Tunggal, Melaka, Malaysia b 8 Centre for Advanced Research on Energy, Universiti Teknikal Malaysia Melaka, 9 Hang Tuah Jaya, 76100 Durian Tunggal, Melaka, Malaysia 10 * 11 Corresponding author: mohdfadzli@utem.edu.my 12 13 HIGHLIGHT 14 Wear rate and friction coefficient of PKAC-E composite decreases with applied load. 15 However, at higher load, friction coefficient increases slightly and remains almost invariant 16 17 18 with applied load. Palm kernel activated carbon epoxy composite (PKAC-E) has a potential to act as a selflubricating material at low load under unlubricated conditions. 19 20 21 22 23 24 25 1 26 ABSTRACTS 27 The aim of this study is to investigate the effect of load on the friction and wear properties of palm 28 kernel activated carbon epoxy (PKAC-E) composite. The PKAC-E composite specimen was 29 fabricated by hot compression molding method. Dry sliding test was performed by using a pin-on- 30 disc tribometer at various load conditions with constant sliding speed and distance. The experimental 31 results show that wear rate and friction coefficient of PKAC-E composite decreases with applied 32 load. However, at higher load, friction coefficient increases slightly and remains almost invariant 33 with applied load. In addition, some adhesive and abrasive wear types were identified on the worn 34 surfaces. The main conclusion of this work is that PKAC-E composite show unique properties as 35 solid lubricant at low load under unlubricated conditions. 36 37 Keywords: Palm kernel activated carbon, wear, coefficient of friction 38 39 40 41 42 43 44 45 46 47 48 49 50 2 51 1.0 INTRODUCTION 52 For a decade, many researchers have investigated different types of solid lubricants as 53 reinforcement or coating materials for tribological applications (Erdemir et al., 2000; Heimberg et al., 54 2001; Tokoroyama et al., 2006; Liu et al., 2009; Baradeswaran, 2011; Abdollah et al., 2012; 55 Masripan et al., 2013). 56 Recently, the potential of local waste materials as substitute reinforcement in fabrication of 57 lightweight materials, such as metal matrix composites and polymer matrix composites has attracted 58 lots of attentions due to its self-lubricating properties and adopt zero waste strategy at affordable cost 59 (Zamri et al., 2010; Zamri et al., 2011; Aigbodion et al., 2011; Bakry et al., 2013;). 60 A few researcher found out that porous carbon also known as activated carbon, such as palm 61 shell activated carbon (PSAC), exhibited its potential to act as a self-lubricating material when 62 reinforced in aluminium alloy, which significantly improved wear resistance by increasing PSAC 63 content up to 10 wt.% (Zamri et al., 2010; Zamri et al., 2011). Gomes et. al., 2001 stated in his study 64 of carbon-carbon composites, the friction coefficient is almost independent in sliding speed but 65 highly affected by test temperature. 66 In general, as observed from prior studies, there are a limited number of studies to investigate 67 the potential of activated carbon materials as solid lubricants in polymer matrix composites. Hence, 68 the goal of this paper is to study the effect of applied load on the friction and wear properties of palm 69 kernel activated carbon epoxy (PKAC-E) composite. 70 71 72 73 74 75 3 76 2.0 METHODOLOGY 77 2.1 Specimen Preparation 78 In this study, the materials used are palm kernel activated carbon (PKAC), West System 105 79 Epoxy Resin (105-B) and West System 206 Slow Hardener (206-B). All specimens were fabricated 80 by hot compression molding method. The PKAC particulate was ground into smaller particle and 81 mixed with epoxy resin (E) and hardener at a composition ratio of 70 wt.% PKAC and 30 wt.% E. 82 The compression process was conducted using hot press machine at 80oC and 2.5 MPa of 83 compression pressure. The green specimen was then cured under room temperature for 2 - 3 days. 84 85 The length and diameter of the specimen was 30 mm and 10 mm, respectively, as shown in Figure 1. 86 87 88 Figure 1 PKAC-E specimen 89 90 91 2.2 Dry sliding test 92 The dry sliding testing was performed to determine the friction coefficient and wear rate 93 between the contact surfaces using a pin-on-disc tribometer. The testing procedure followed the 94 ASTM standard G99-95a (Standard Test Method for Wear Testing with a Pin-on-Disk Apparatus). 95 All tests were performed at room temperature with a constant sliding speed and distance at 200 rpm 96 and 3770 m, respectively. Prior to the sliding test, pin was ground by sliding against 600grit silicon 97 carbide (SiC) paper at one end. Then, both pin and disc were cleaned using acetone in an ultrasonic 4 98 bath. As illustrated in Figure 2, The pin was then mounted vertically on the tester arm at one end and 99 the other pin surface was hold against the rotating EN-31 carbon alloy steel disc (hardened to HRC 100 101 102 62; ground to Ra = 0.8µm) with a diameter and thickness of 16.5 mm and 8 mm, respectively. A coefficient of friction and frictional force encounter by the ball in sliding were measured by a PC based data logging system. The coefficient of friction is then being determined as follows: F W 103 104 (1) Where F is the frictional force in N and W is the applied load in N. 105 The wear at the pin was recorded by measuring the mass of the pin before and after the wear 106 test. The mass loss in mass unit is converted to the volume loss by dividing with bulk density of 107 material. The specific wear rate is then being determined as follows: 108 Vloss mloss (2) 109 k Vloss WL (3) 110 Where Vloss is the volume loss in mm3, mloss is the mass loss in g, is the bulk density of material in 111 g/mm3, k is the specific wear rate of material in mm3/Nmm, W is the applied load in N and L is the 112 sliding distance in mm. 113 The worn surfaces morphology was observed using a digital microscope and profilometer. 114 115 116 117 118 119 120 121 5 Load Rotating EN-31 steel disc Stationary PKAC-E composite PSAC-Al composite Wear track (a) 122 (b) Figure 2 (a) Illustration and (b) schematic diagram of the sliding test using a pin-on-disc tribometer 123 124 125 3.0 RESULTS AND DISCUSSION 126 Figure 3 indicates the friction coefficient decreases with the increase of applied load within 127 the observed range though from 60 N, it increases slightly and remains almost invariant with applied 128 load (Figure 4). The frictional heating, which will induce tribofilm formation, is believed to be 129 responsible for the decrease of friction with the increase of applied load. There was a strong 130 dependence of tribofilm formation on temperature (Komvopoulos et al., 2002). The tribofilm 131 generated from the preferential wear of the soft carbon material results in a carbon based tribofilm 132 adhering on the worn surface which breaks the adhesive joints between the asperities and thereafter 133 leads to low friction (Luo, 2013). However, as stated by Bakry et al. 2013, at higher load, the 134 tribofilm was broken and carbon shows a drastic reduction in lubricity; consequently increases 135 friction coefficient. 136 137 138 6 Average coefficient of friction 0.10 Low load Medium load 0.08 0.06 0.04 0.02 0.00 0 20 40 60 80 Normal load [N] 100 120 139 140 Figure 3 Relationship between applied loads and average friction coefficient of PKAC-E composite 141 142 Coefficient of friction 0.10 0.08 5N 0.06 60N 0.04 100N 80N 0.02 20N 40N 0.00 0 1000 2000 Time [secs] 3000 4000 143 144 Figure 4 Comparison of friction coefficient as a function of time at different load 145 7 146 As regard to the wear, Table 1 shows the distribution of calculated wear rate with applied 147 load. As shown in Figure 5, the wear rate of PKAC-E composite decreased significantly with applied 148 load. From Figure 6, worn surfaces of the material were characterized by some adhesion wear and 149 abrasive wear. However, at higher load, adhesion wear was slightly reduced with smoother surfaces 150 and show signs of fine scratches. A reduction in adhesion is directly responsible for the reduction in 151 friction and wears (Zhao et al., 2014). These results agree with the calculated wear rate values as in 152 Figure 5. Among the experiments conducted there was no seizure condition noticed. 153 154 Table 1 Weight of specimen before and after tribo testing with calculated wear rate Sample Load [N] m1 [g] m2 [g] mloss [g] k [mm3/Nmm] A 5 3.3483 3.3443 0.0040 0.7800 B 20 3.1647 3.1643 0.0004 0.0780 C 40 3.0090 3.0073 0.0017 0.3315 D 60 3.4947 3.4943 0.0004 0.0780 E 80 3.5783 3.5767 0.0016 0.3120 F 100 3.3530 3.3513 0.0017 0.3315 155 156 157 158 159 160 161 162 163 164 165 8 Specific wear rate, k [mm3/Nmm] x 10-7 1.8 1.6 1.4 1.2 1.0 0.8 0.6 0.4 0.2 0.0 0 20 40 60 80 Normal load [N] 100 120 166 167 Figure 5 Relationship between applied loads and wear rate of PKAC-E composite 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 9 183 184 Figure 6 Digital microscope image of worn surfaces of PKAC-E composite testing at (a) 5N, 185 (b) 20N, (c) 40N, (d) 60N, (e) 80N and (f) 100N 186 187 188 4.0 CONCLUSIONS 189 As a conclusion, it was found that the wear rate and friction coefficient of PKAC-E 190 composite was decreasing with the increasing in applied load. However, at higher load, friction 191 coefficient increases slightly and remains almost invariant with applied load. In addition, some 192 adhesive and abrasive wear types were identified on the worn surfaces. From the overall findings, 193 PKAC-E composite show unique properties as solid lubricant at low load under unlubricated 194 conditions. 195 10 196 ACKNWLEDGEMENTS 197 The authors gratefully acknowledge contributions from the members of the Green Tribology 198 and Engine Performance (G-TriboE) research group. This research was supported by the grant from 199 the Ministry of Education Malaysia (Grant No.: ERGS/2013/FKM/TK01/UTEM/02/04/E00016). 200 201 202 REFERENCES 203 Abdollah, M.F.B., Yamaguchi, Y., Akao, T., Inayoshi, N., Miyamoto, N., Tokoroyama, T. and 204 Umehara, N., 2012. Deformation–wear transition map of DLC coating under cyclic impact 205 loading. 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