FUEL CONDITIONER, COMBUSTOR AND GAS TURBINE IMPROVEMENTS
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United States of America Patent
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app pub date -
Dec 20, 2013
filing date -
Mar 15, 2013
priority date (Note) -
Abandoned
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Abstract
Advanced gas turbines and associated components, systems and methods are disclosed herein. A gas turbine configured in accordance with a particular embodiment includes a rotor operably coupled to a shaft and a stator positioned adjacent to the rotor. A coolant line extends at least partially through the stator to transfer heat out of an air flow within a compressor section of the gas turbine.
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