COMBINED HEATING FOR SOLDERING AN ARMOR CLADDING ONTO A TIP BY MEANS OF INDUCTION AND LASER

The present invention relates to a method for coating a component (1) of a gas turbine or an aircraft engine, in particular for producing a blade-tip armor cladding on a blade of a gas turbine or aircraft engine, in which a coating material is applied to the component with a solder and the component...

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Bibliographic Details
Main Author HANRIEDER HERBERT
Format Patent
LanguageEnglish
Published 15.11.2012
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Summary:The present invention relates to a method for coating a component (1) of a gas turbine or an aircraft engine, in particular for producing a blade-tip armor cladding on a blade of a gas turbine or aircraft engine, in which a coating material is applied to the component with a solder and the component is heated inductively, with at least the solder of the coating material being heated by means of a laser (4) in such a way that solder connection between the component and the coating material is achieved, as well as a corresponding device for carrying out the method.
Bibliography:Application Number: US201213468429