TY - JOUR
T1 - Influence of annealing and tempering on the wear and corrosion behavior of WC/W2C reinforced composites fabricated by laser powder bed fusion
AU - Zhou, Yiqi
AU - Sang, Ke
AU - Wang, Wenqian
AU - Zhang, Guofeng
AU - Kong, Decheng
AU - Yan, Yu
AU - Li, Xiaogang
AU - Qu, Xuanhui
AU - Dong, Chaofang
AU - Yang, Zhigang
AU - Chen, Hao
AU - Zhang, Chi
N1 - Publisher Copyright:
© 2026 Elsevier Ltd.
PY - 2026/7
Y1 - 2026/7
N2 - WC/W2C particle reinforced stainless steel composites were fabricated via laser powder bed fusion (LPBF) and subsequently heat‑treated under two schemes: direct tempering (200–600 °C) and solution annealing at 1050 °C followed by tempering. The effects of these heat treatments on the microstructure, wear performance, corrosion behaviour, and mechanical properties were systematically investigated. While low‑temperature tempering (≤ 400 °C) promoted carbon redistribution and increased retained austenite from 17.6 % to 61.7 %, tempering at 600 °C—as well as the solution‑annealed and tempered condition—suppressed austenite (≈ 0 %) and triggered extensive precipitation of Cr‑rich carbides. Solution annealing homogenized the matrix, eliminated austenite, and thickened the in-situ reaction layers to ∼5 μm. Intergranular corrosion susceptibility correlated directly with carbide‑induced Cr‑depleted zones, with the highest degree of sensitization (DOS > 220) occurring after the 600 °C and 1050 °C + 600 °C treatments, significantly exceeding that of other conditions (DOS < 150). Wear resistance was governed primarily by matrix hardness; wear volume loss increased markedly from 2 × 104 μm3 to 5 × 105 μm3, attributed to abrasive carbide debris and thermal softening. Compression tests demonstrated high deformability (> 60 %) after heat treatment; however, the as‑built composite exhibited the highest compressive strength (∼4500 MPa) but underwent premature failure, owing to residual stress.
AB - WC/W2C particle reinforced stainless steel composites were fabricated via laser powder bed fusion (LPBF) and subsequently heat‑treated under two schemes: direct tempering (200–600 °C) and solution annealing at 1050 °C followed by tempering. The effects of these heat treatments on the microstructure, wear performance, corrosion behaviour, and mechanical properties were systematically investigated. While low‑temperature tempering (≤ 400 °C) promoted carbon redistribution and increased retained austenite from 17.6 % to 61.7 %, tempering at 600 °C—as well as the solution‑annealed and tempered condition—suppressed austenite (≈ 0 %) and triggered extensive precipitation of Cr‑rich carbides. Solution annealing homogenized the matrix, eliminated austenite, and thickened the in-situ reaction layers to ∼5 μm. Intergranular corrosion susceptibility correlated directly with carbide‑induced Cr‑depleted zones, with the highest degree of sensitization (DOS > 220) occurring after the 600 °C and 1050 °C + 600 °C treatments, significantly exceeding that of other conditions (DOS < 150). Wear resistance was governed primarily by matrix hardness; wear volume loss increased markedly from 2 × 104 μm3 to 5 × 105 μm3, attributed to abrasive carbide debris and thermal softening. Compression tests demonstrated high deformability (> 60 %) after heat treatment; however, the as‑built composite exhibited the highest compressive strength (∼4500 MPa) but underwent premature failure, owing to residual stress.
KW - Corrosion resistance
KW - Laser powder bed fusion
KW - Metal matrix composites
KW - Wear performance
UR - https://www.scopus.com/pages/publications/105029352299
U2 - 10.1016/j.triboint.2026.111811
DO - 10.1016/j.triboint.2026.111811
M3 - 文章
AN - SCOPUS:105029352299
SN - 0301-679X
VL - 219
JO - Tribology International
JF - Tribology International
M1 - 111811
ER -