Method of repairing a stationary shroud of a gas turbine...

Electric heating – Metal heating – By arc

Reexamination Certificate

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Details

C219S121590, C219S121470, C219S076160, C219S121460, C029S889100

Reexamination Certificate

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06914210

ABSTRACT:
A stationary shroud of a gas turbine engine made of a base metal is repaired by removing any damaged material from a flow-path region of the stationary shroud to leave an initially exposed base-metal flow-path surface; and applying a base-metal restoration overlying the initially exposed flow-path surface. The base-metal restoration is applied by furnishing a source of a structural material that is compatible with the base metal, and depositing the source of the structural material overlying the initially exposed base-metal flow-path surface of the stationary shroud by plasma transferred arc welding to form a repaired base-metal flow-path surface. An environmentally resistant rub coating may be applied overlying the base-metal restoration.

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