Method for forming thermal barrier coating on hot-gas-path components of gas turbine during operation
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United States of America Patent
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May 28, 2013
Grant Date -
Dec 30, 2010
app pub date -
Nov 10, 2009
filing date -
Jun 29, 2009
priority date (Note) -
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Abstract
Disclosed is a method for formation of a thermal bather coating on a gas turbine during operation thereof, which includes addition of an organic compound containing silicon to a fuel under a first condition in order to form a base layer on the surface of a part coming into contact with a combustion gas of the fuel in the gas turbine during operation thereof, as well as addition of the organic compound containing silicon to the fuel under a second condition in order to form a porous layer having more pores than the base layer above the base layer.
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