Thermal barrier coating with improved underlayer and pieces...

B - Operations – Transporting – 32 – B

Patent

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Details

B32B 15/04 (2006.01) C23C 4/02 (2006.01) C23C 28/00 (2006.01) F01D 5/18 (2006.01) F16L 59/02 (2006.01)

Patent

CA 2196744

Le revêtement de barrière thermique pour substrat en superalliage utilisé notamment dans les turbomachines comportant un revêtement céramique et une sous-couche interposée entre le substrat et la céramique, est caractérisé en ce que la sous-couche est composée d'un aluminiure de nickel et/ou de cobalt contenant au moins un métal de la mine du platine et au moins un métal promoteur de la formation d'une couche d'oxyde constitué de la variété allotropique a de l'alumine.

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