ENGINE COMPONENT FOR A GAS TURBINE

The object of the invention is an engine component for arrangement in the gas flow of a gas turbine. According to the invention, at least one part of the surface of said component subjected to the gas flow in operation comprises a modified amorphous carbon layer containing hydrogen that is applied u...

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Bibliographic Details
Main Authors REINMOELLER, ULF, SIRY, CHRISTIAN
Format Patent
LanguageEnglish
French
German
Published 14.07.2010
Subjects
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Summary:The object of the invention is an engine component for arrangement in the gas flow of a gas turbine. According to the invention, at least one part of the surface of said component subjected to the gas flow in operation comprises a modified amorphous carbon layer containing hydrogen that is applied using a vacuum coating technique.
Bibliography:Application Number: EP20080785760