Plating turbine engine components

C - Chemistry – Metallurgy – 25 – D

Patent

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Details

C25D 5/02 (2006.01) F01D 5/28 (2006.01)

Patent

CA 2217843

A process is provided for plating a coating onto a gas turbine engine component without detrimentally effecting air flow through cooling holes by injecting a maskant into the cooling passage to fill the cooling holes with the maskant, plating the external surface of the component with a coating, then removing the maskant from the component.

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