TY - JOUR
T1 - Wide-Temperature-Range Tribological Properties of In Situ Ceramic-Reinforced TaMoTiCr Refractory High-Entropy Alloy Composites
AU - Gao, Chenguang
AU - Pei, Xuhui
AU - Chen, Zhuo
AU - Wang, Hanming
AU - Hu, Mingchuan
AU - Du, Yin
AU - Wang, Haifeng
N1 - Publisher Copyright:
Copyright © 2026, Northwest Institute for Nonferrous Metal Research.
PY - 2026/9
Y1 - 2026/9
N2 - In-situ ceramic phase-reinforced TaMoTiCr refractory high-entropy alloy (RHEA) composites were prepared by spark plasma sintering with the addition of 2.5wt% and 5.0wt% h-BN, separately. Results show that the h-BN promotes the uniform formation of (Ti, Ta)N, TaB2, and MoB ceramic phases within the body-centered cubic matrix, significantly increasing microhardness to 1136.95 HV. Tribological test results show that the composite with the addition of 2.5wt% h-BN presents great performance at room temperature with an ultra-low wear rate of 1.64×10-7 mm3·N-1·m-1, while the composite with the addition of 5.0wt% h-BN shows optimal performance at 300 °C. Above 800 °C (elevated temperature condition), lubricious oxide tribolayers, rich in Cr2O3, TiO2, and B2O3, form on the material surface, effectively reducing friction and wear. At 1000 °C, the composite with the addition of 2.5wt% h-BN achieves a wear rate of 5.22×10-7 mm3·N-1·m-1. This in situ ceramic reinforcement approach effectively enhances wear resistance of RHEAs across a wide temperature range, offering great potential for advanced aerospace applications.
AB - In-situ ceramic phase-reinforced TaMoTiCr refractory high-entropy alloy (RHEA) composites were prepared by spark plasma sintering with the addition of 2.5wt% and 5.0wt% h-BN, separately. Results show that the h-BN promotes the uniform formation of (Ti, Ta)N, TaB2, and MoB ceramic phases within the body-centered cubic matrix, significantly increasing microhardness to 1136.95 HV. Tribological test results show that the composite with the addition of 2.5wt% h-BN presents great performance at room temperature with an ultra-low wear rate of 1.64×10-7 mm3·N-1·m-1, while the composite with the addition of 5.0wt% h-BN shows optimal performance at 300 °C. Above 800 °C (elevated temperature condition), lubricious oxide tribolayers, rich in Cr2O3, TiO2, and B2O3, form on the material surface, effectively reducing friction and wear. At 1000 °C, the composite with the addition of 2.5wt% h-BN achieves a wear rate of 5.22×10-7 mm3·N-1·m-1. This in situ ceramic reinforcement approach effectively enhances wear resistance of RHEAs across a wide temperature range, offering great potential for advanced aerospace applications.
KW - in-situ ceramic phase
KW - refractory high-entropy alloy ceramic composite
KW - spark plasma sintering
KW - tribological performance
UR - https://www.scopus.com/pages/publications/105045249251
U2 - 10.12442/j.issn.1002-185X.20250490
DO - 10.12442/j.issn.1002-185X.20250490
M3 - 文章
AN - SCOPUS:105045249251
SN - 1002-185X
VL - 55
SP - 2165
EP - 2178
JO - Xiyou Jinshu Cailiao Yu Gongcheng/Rare Metal Materials and Engineering
JF - Xiyou Jinshu Cailiao Yu Gongcheng/Rare Metal Materials and Engineering
IS - 9
ER -