4.7 Article

Microstructure and tribological behavior of CoCrFeNiMo0.2/SiC high-entropy alloy gradient composite coating prepared by laser cladding

Journal

SURFACE & COATINGS TECHNOLOGY
Volume 467, Issue -, Pages -

Publisher

ELSEVIER SCIENCE SA
DOI: 10.1016/j.surfcoat.2023.129681

Keywords

Laser cladding; Gradient composite coating; Microstructure; Microhardness; Wear resistance

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This paper explores a new method of ceramic reinforced CoCrFeNiMo0.2 high entropy alloy composite gradient coating to strengthen face-centered cubic structured alloys. The study reveals that as the silicon carbide addition increases, the microstructure of the coatings changes, resulting in the generation of body-centered cubic phase. The second, third, and fourth layers exhibit significantly higher hardness, attributed to the presence of body-centered cubic structure, carbide, and grain boundary strengthening effects. The wear mechanism changes from adhesive wear to abrasive wear as the number of layers increases, leading to reduced wear rates.
To strengthen face-centered cubic structured high entropy alloys, this paper explores a new method of ceramic reinforced CoCrFeNiMo0.2 high entropy alloy composite gradient coating. In this study, four sets of gradients were created by first preparing a pristine alloy coating without silicon carbide content on the substrate, followed by preparing composite coatings with varying silicon carbide mass fractions (8 %, 16 %, 24 %) on the pristine coatings. The coatings were then analyzed for their phase composition, microstructure, microstructure evolution process, and friction wear properties. The study reveals that the microstructure of the initial alloy coating consists of a single-phase face-centered cubic solid solution. It is observed that intragranular segregation occurs in the coating, resulting in the boundary enrichment of Mo and Cr elements. As the silicon carbide addition increases, the segregation behavior becomes more pronounced, and the generation of body-centered cubic phase is observed. The second, third, and fourth layers exhibit significantly higher average hardness, measuring at 594 HV, 722 HV, and 788 HV respectively. This can be attributed to the presence of body-centered cubic structure, carbide, and grain boundary strengthening effects. On average, the hardness of these layers is three to four times higher than that of the first layer. With an increase in the number of layers, the wear mechanism changes from adhesive wear to abrasive wear. The wear rates of the second, third, and fourth layers were all reduced by at least 87 % compared to the first layer. However, there were different forms of abrasive wear observed between these layers. The findings of this study have significant engineering implications.

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