Protective coating systems for gas turbine engine...

C - Chemistry – Metallurgy – 23 – C

Patent

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Details

C23C 26/00 (2006.01) C23C 14/10 (2006.01) C23C 16/40 (2006.01) C04B 35/16 (2006.01) C04B 35/48 (2006.01)

Patent

CA 2645293

Protective coating systems for gas turbine engine applications and methods for fabricating such protective coating systems are provided. An exemplary method of fabricating a protective coating system on a substrate comprises forming a bond coating on the substrate, forming a silicate layer on the bond coating, forming a thermal barrier coating overlying the silicate layer, and heating the thermal barrier coating.

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