TURBINE BLADE TIP REPAIR

A method for repairing a blade (20)wherein the blade comprises a metallic substrate (22) shaped to define an airfoil having a tip. A coating (34) is on the tip. The method comprises: machining to at least partially remove the coating (34); plating a nickel-based base layer (32'); and plating an...

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Bibliographische Detailangaben
Hauptverfasser: MINOR, Michael J, PIETRONIRO, Anthony J, SCHUBERT, Mary E, BROWN, Kayleigh J, HISKES, David J, BISCHOF, Christopher J, STRATTON, Eric W, McCALL, Thomas
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:A method for repairing a blade (20)wherein the blade comprises a metallic substrate (22) shaped to define an airfoil having a tip. A coating (34) is on the tip. The method comprises: machining to at least partially remove the coating (34); plating a nickel-based base layer (32'); and plating an abrasive layer (34') comprising a nickel-based matrix (36) and an abrasive (38).