Removal of thermal barrier coatings

Cleaning and liquid contact with solids – Processes – For metallic – siliceous – or calcareous basework – including...

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134 2217, 427331, 427404, 4274192, B08B 900, B05D 140, B05D 136, C03C 2300

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active

061325201

ABSTRACT:
A gas turbine engine component having a thermal barrier coating is immersed in an inorganic hydroxide bath having a high concentration of alkali or alkaline earth hydroxide with the bath at ambient (atmospheric) pressure and elevated temperature for a time sufficient to effect rapid detachment of the thermal barrier coating for removal from the substrate. The component then optionally can be immersed in a water bath to remove any remaining thermal barrier coating. The thermal barrier coating is removed without detectable damage to the substrate or any bondcoat present thereon.

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