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GAS TURBINE DEVICE USING SUPERCRITICAL FLUID AS COOLING FLUID

  • US 20150167554A1
  • Filed: 04/28/2014
  • Published: 06/18/2015
  • Est. Priority Date: 12/12/2013
  • Status: Active Grant
First Claim
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1. A gas turbine device using a supercritical fluid as a cooling fluid, the gas turbine device comprising:

  • a compressor (100) for compressing air;

    a combustor (200) for burning the air emitted from the compressor (100) and fuel;

    a turbine (300) driven by the burned gas emitted from the combustor (200);

    endcooling passages (400) formed in the combustor (200) and the turbine (300), along which the supercritical fluid as a cooling fluid flows to allow the combustor (200) and the turbine (300) to be cooled.

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