Patent ID: 7709057

Claim:
A method for providing a clean edge at the interface of a portion of a turbine engine substrate coated with a thermal barrier coating system and an adjacent portion of the substrate which is uncoated, wherein the portion of the substrate which is uncoated comprises a zone of non-adherence, wherein the turbine engine substrate comprises a superalloy material, and the coating system comprises a metallic bond coat and a zirconia-based overcoat, said method comprising the step of forming the zone of non-adherence on the substrate between the portion of the substrate to be coated and the rest of the portion of the substrate which is to be uncoated, while roughening the substrate portion which is to be coated, prior to application of the coating system, wherein the zone of non-adherence is adjacent the interface, so that the coating system will not adhere to the zone of non-adherence, but will adhere to the roughened portion of the substrate which is to be coated with the coating system, applying the bond coating, and then applying the zirconia-based overcoat, where the zirconia-based overcoat is applied such that the zirconia-based overcoat directly contacts the substrate in the zone of non-adherence but will not substantially adhere to the zone of non-adherence.