Method for repairing a component by coating

A method for repairing a component such as a turbine blade is provided. At the end of its operating time, the component has, for example, a depletion of aluminium in a region near the surface. The application of a repair layer is provided including particles with an increased proportion of aluminium...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Jensen, Jens Dahl, Klingemann, Jens, Krüger, Ursus, Körtvelyessy, Daniel, Lüthen, Volkmar, Reiche, Ralph, Stier, Oliver
Format: Patent
Sprache:eng
Online-Zugang:Volltext bestellen
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