TY - JOUR
T1 - Wear characteristics of aluminium matrix composites reinforced with Si-based refractory compounds derived from rice husks
AU - Adediran, Adeolu Adesoji
AU - Alaneme, Kenneth Kanayo
AU - Oladele, Isiaka Oluwole
AU - Akinlabi, Esther Titilayo
N1 - Funding Information:
The authors received no direct funding for this research. The authors wish to appreciate Dr Philip Oladejo from Botswana International University of Science and Technology for his assistance and Landmark University Centre for Research, Innovation and Development (LUCRID) for their support.
Publisher Copyright:
© 2020 The Author(s). This open access article is distributed under a Creative Commons Attribution (CC-BY) 4.0 license.
PY - 2020/1/1
Y1 - 2020/1/1
N2 - This study investigates the wear behaviour of aluminium metal matrix composites reinforced with 10 wt.% Si-based refractory compounds (SBRC) derived from rice husk (RHs). The wear test was conducted using a pin-on-disk tribometer under varying loads with a fixed sliding distance. Scanning electron microscope was used to characterize the worn-out surface and the wear debris. From the results obtained, as the applied load increases, the coefficient of friction (CoF) value reduces to a significant extent. This reduction might be associated with the presence of graphite phase in all the composites developed. The results showed that for samples subjected to 5 N load, T1650 had the optimum value of wear volume amounting to 25–93% increase in wear volume against other samples. Additionally, for 8 N load, K1650 showed a higher response in wear volume having 26–74% improvement in wear volume. The specific wear rate of the composites developed at 5 N load application can be ranked in the following order: T1600 > K1250 > T1650 > K1650 > T1250. A severe agglomeration, possibly caused by fragmentation of the clustered debris, dominated the morphology of the worn-out surface. From the EDS spectra, the iron content appears to be low while the oxygen content very high, this is an indication that the tribolayer island was oxidized. An optical photograph showing the wear profile was also taken. It is inferred that the initial wear mechanism of the composites is adhesive, this later converted to abrasive.
AB - This study investigates the wear behaviour of aluminium metal matrix composites reinforced with 10 wt.% Si-based refractory compounds (SBRC) derived from rice husk (RHs). The wear test was conducted using a pin-on-disk tribometer under varying loads with a fixed sliding distance. Scanning electron microscope was used to characterize the worn-out surface and the wear debris. From the results obtained, as the applied load increases, the coefficient of friction (CoF) value reduces to a significant extent. This reduction might be associated with the presence of graphite phase in all the composites developed. The results showed that for samples subjected to 5 N load, T1650 had the optimum value of wear volume amounting to 25–93% increase in wear volume against other samples. Additionally, for 8 N load, K1650 showed a higher response in wear volume having 26–74% improvement in wear volume. The specific wear rate of the composites developed at 5 N load application can be ranked in the following order: T1600 > K1250 > T1650 > K1650 > T1250. A severe agglomeration, possibly caused by fragmentation of the clustered debris, dominated the morphology of the worn-out surface. From the EDS spectra, the iron content appears to be low while the oxygen content very high, this is an indication that the tribolayer island was oxidized. An optical photograph showing the wear profile was also taken. It is inferred that the initial wear mechanism of the composites is adhesive, this later converted to abrasive.
KW - agglomeration
KW - composites
KW - EDS
KW - metal matrix
KW - morphology
KW - refractory compounds
KW - wear
UR - http://www.scopus.com/inward/record.url?scp=85092252413&partnerID=8YFLogxK
U2 - 10.1080/23311916.2020.1826634
DO - 10.1080/23311916.2020.1826634
M3 - Article
AN - SCOPUS:85092252413
SN - 2331-1916
VL - 7
JO - Cogent Engineering
JF - Cogent Engineering
IS - 1
M1 - 1826634
ER -