Chemical removal of a metal oxide coating from a superalloy...

Cleaning and liquid contact with solids – Processes – Using sequentially applied treating agents

Reexamination Certificate

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Details

C134S002000, C134S006000, C134S019000, C134S027000, C134S029000, C134S030000, C134S036000, C134S037000, C134S042000

Reexamination Certificate

active

06878215

ABSTRACT:
A method of removing a virgin metal oxide coating from the surface of a superalloy gas turbine engine component. The component bearing the applied metal oxide coating is contacted with an aqueous coating-removal solution, typically containing by weight about 10-25% alkali hydroxide, about 1-8% alkanolamine, and about 0.5-5% gluconate salt at a temperature of from about 170° F. (67° C.) to about 210° F. (99° C.), for a time sufficient to remove the metal oxide coating from the superalloy blade by gentle mechanical means. The metal oxide coating can comprise one or more metal oxide layers, such as a chromium oxide layer and an aluminum oxide layer.

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