ENGINE COMPONENT FOR A GAS TURBINE
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United States of America Patent
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Issued Date -
Oct 21, 2010
app pub date -
Aug 29, 2008
filing date -
Sep 5, 2007
priority date (Note) -
Abandoned
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Abstract
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.
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