Tribological Performance of High-Entropy Coatings (HECs): A Review

Materials (Basel). 2022 May 21;15(10):3699. doi: 10.3390/ma15103699.

Abstract

Surface coatings that operate effectively at elevated temperatures provide compatibility with critical service conditions as well as improved tribological performance of the components. High-entropy coatings (HECs), including metallic, ceramics, and composites, have gained attention all over the world and developed rapidly over the past 18 years, due to their excellent mechanical and tribological properties. High-entropy alloys (HEAs) are defined as alloys containing five or more principal elements in equal or close to equal atomic percentage. Owing to the high configurational entropy compared to conventional alloys, HEAs are usually composed of a simple solid solution phase, such as the BCC and FCC phases, instead of complex, brittle intermetallic phases. Several researchers have investigated the mechanical, oxidation, corrosion and wear properties of high-entropy oxides, carbides, borides, and silicates using various coating and testing techniques. More recently, the friction and wear characteristics of high-entropy coatings (HECs) have gained interest within various industrial sectors, mainly due to their favourable mechanical and tribological properties at high temperatures. In this review article, the authors identified the research studies and developments in high-entropy coatings (HECs) fabricated on various substrate materials using different synthesis methods. In addition, the current understanding of the HECs characteristics is critically reviewed, including the fabrication routes of targets/feedstock, synthesis methods utilized in various research studies, microstructural and tribological behaviour from room temperature to high temperatures.

Keywords: configurational; feedstock; high-entropy alloys (HEAs); high-entropy coatings (HECs); solid solutions; tribological behaviour.

Publication types

  • Review

Grants and funding

The authors would like to acknowledge the financial support from Natural Sciences and Engineering Research Council (NSERC) Project Number CRDPJ 530409-18 and the Consortium for Research and Innovation in Aerospace in Québec (CRIAQ) Project Number MANU-1719.