Hello DJr9515
As far as I'm aware, most carbides used in TS coatings come in the form of cermets or carbide/metal matrix composites like WC/Co. I think the primary reason that carbides are not sprayed alone is that they oxidise or decompose or volatilise readily at their rather high melting points. Coatings produced from pure carbides I guess would have very poor properties. Additions of a metal matrix allows carbides to be sprayed at a lower temperature or heat input. The metal matrix gives much needed ductility/toughness to the coating, while benefiting from the very hard wear resistant carbide particles.
Quote:There is typically a 3:1 ratio by weight of carbide to metal matrix.
Typically I would say they range from 7-50% NiCr matrix
Quote:The metal matrix is present to bond the carbide to the substrate
Its needed to bond everything together and provide some ductility and toughness
Quote:and to provide a high degree of corrosion resistance.
Chromium carbide by itself is corrosion and temperature resistant and is not really made any more so by the addition of NiCr apart from dramatically increasing coating density so protection the substrate better.
NiCr general is used as a matrix or binder for chromium carbide because they are metallurgically compatible, have similar high temperature and corrosion resistance. The composite nature of hard particles in softer tougher matrix gives them very useful coating properties.
HVOF is now the preferred method of application, even though many old aerospace specs still call up plasma spray.
Hoping that's of some help
I'll come back if I find any decent links.
Fergus