Turbine blade of a gas turbine and method for coating a turbine blade of a gas turbine

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United States of America Patent

PATENT NO 10006298
SERIAL NO

12877007

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Abstract

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A method for coating a turbine blade of a gas turbine is disclosed. The method includes applying a lacquer coat to a region of the turbine blade, where the lacquer coat includes chromium particles and/or chromium alloy particles, halides, and a binding agent. The method further includes drying the applied lacquer coat at a temperature between 50° C. and 600° C. with disintegration of the binding agent and subsequent reactive connection at a temperature between 900° C. and 1160° C.

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Patent Owner(s)

Patent OwnerAddress
MTU AERO ENGINES GMBHMUNICH GERMANY MUNICH BAVARIA

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Lange, Richard Markt Indersdorf, DE 3 8
Manier, Karlheinz Scheyern, DE 3 16
Morant, Max Aschau, DE 5 9
Pillhoefer, Horst Roehrmoos, DE 27 180
Strasser, Michael Erdweg, DE 65 847
Walter, Heinrich Friedberg, DE 24 114

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