Gas turbine device using supercritical fluid as cooling fluid
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United States of America Patent
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May 2, 2017
Grant Date -
Jun 18, 2015
app pub date -
Apr 28, 2014
filing date -
Dec 12, 2013
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Abstract
The present invention relates to a gas turbine device using a supercritical fluid as a cooling fluid, the gas turbine device having a compressor for compressing air, a combustor for burning the air emitted from the compressor and fuel, and a turbine driven by the burned gas emitted from the combustor, wherein the gas turbine device includes cooling passages formed in the combustor and the turbine, along which the supercritical fluid as a cooling fluid flows to allow the combustor and the turbine to be cooled.
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