TY - JOUR
T1 - Influence of sintering temperature on Ti6Al4V-Si3N4-ZrO2 ternary composites prepared by spark plasma sintering
AU - Ogunmefun, Anthony Olakunle
AU - Ayodele, Olusoji
AU - Bayode, Lawrence
AU - Anamu, Ufoma
AU - Olorundaisi, Emmanuel
AU - Mkhatshwa, Sindile
AU - Babalola, Joseph
AU - Ngeleshi, Michael
AU - Odetola, Peter
AU - Olubambi, Peter Apata
N1 - Publisher Copyright:
© 2024 EDP Sciences. All rights reserved.
PY - 2024
Y1 - 2024
N2 - In this study, Ti6Al4V-ZrO2-Si3N4 ternary composites were fabricated using a novel spark plasma sintering technique at different temperatures between 950-1200 C, the pressure of 50 MPa, sintering rate of 100 C/min, and a holding time of 10 min to determine the effect of sintering temperature on the consolidated composites. The microstructures of the fabricated composites were examined by the scanning electron microscope (SEM-EDX). The distinct phases and the nano-mechanical properties of the composite were determined by the X-ray diffractometer and nanoindenter. The results show a non-linear response. At elevated temperatures from the composite sample, CT1-950 C to the composite sample, CT2-1100 C, the densification, and nanomechanical properties experienced an increase, and when the temperature is elevated to 1200 C, composite CT3 declines in values. However, the relative density of all fabricated composites was above 95%, which suggests an overall good densification via the spark plasma sintering technique. The ternary composite fabricated at 1100 C, (CT2) attained maximum values of Vickers hardness, elastic modulus, and nano hardness at 7380 MPa, 177.91 GPa, and 60.06 GPa, respectively, while composite CT3 declines at 1200 C.
AB - In this study, Ti6Al4V-ZrO2-Si3N4 ternary composites were fabricated using a novel spark plasma sintering technique at different temperatures between 950-1200 C, the pressure of 50 MPa, sintering rate of 100 C/min, and a holding time of 10 min to determine the effect of sintering temperature on the consolidated composites. The microstructures of the fabricated composites were examined by the scanning electron microscope (SEM-EDX). The distinct phases and the nano-mechanical properties of the composite were determined by the X-ray diffractometer and nanoindenter. The results show a non-linear response. At elevated temperatures from the composite sample, CT1-950 C to the composite sample, CT2-1100 C, the densification, and nanomechanical properties experienced an increase, and when the temperature is elevated to 1200 C, composite CT3 declines in values. However, the relative density of all fabricated composites was above 95%, which suggests an overall good densification via the spark plasma sintering technique. The ternary composite fabricated at 1100 C, (CT2) attained maximum values of Vickers hardness, elastic modulus, and nano hardness at 7380 MPa, 177.91 GPa, and 60.06 GPa, respectively, while composite CT3 declines at 1200 C.
KW - Nanomechanical properties
KW - Pulsed electric current sintering
KW - Si3N4
KW - Ti6Al4V
KW - Zirconia
UR - http://www.scopus.com/inward/record.url?scp=85188268263&partnerID=8YFLogxK
U2 - 10.1051/mfreview/2024004
DO - 10.1051/mfreview/2024004
M3 - Article
AN - SCOPUS:85188268263
SN - 2265-4224
VL - 11
JO - Manufacturing Review
JF - Manufacturing Review
M1 - 5
ER -