Protective coating systems for gas turbine engine...

Coating processes – Coating by vapor – gas – or smoke – Base includes an inorganic compound containing silicon or...

Reexamination Certificate

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C427S255700, C427S376200, C427S376400

Reexamination Certificate

active

07993704

ABSTRACT:
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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