Abstract:
© 2021 Elsevier Ltd Tungsten carbide‑cobalt (WC-Co) thermal spray coatings are widely used for ambient temperature wear applications but are typically generated from feedstocks with 1–5 μm carbide particles rather than more desirable <1 μm carbide particles, due to challenges of carbide dissolution and carbon loss in-flight. This work explores a novel processing route for the WC-Co system that has been conceptually proven for the Cr3C2-NiCr system. The tendency for carbides to dissolve in-flight is maximised in this approach, with subsequent heat treatment used to precipitate submicron carbide particles. Part 1 of this two-part series assessed the theoretical feasibility of applying this concept to the Co-W-C system for WC-17wt%Co composites, and characterised high velocity oxygen fuel (HVOF), plasma Ar-He and plasma Ar-H2 coatings. In this follow-up paper, the powder and coating samples were characterised by Differential Scanning Calorimetry (DSC), followed by heat treatments below and above the identified phase transition temperatures. Compositional and microstructural analysis led to identification of the reactions accounting for each of the DSC peaks. These observations were contrasted with theoretical predictions as a function of the extent of carbide dissolution/decomposition and carbon loss in the as-sprayed coatings.
