FUEL CONDITIONER, COMBUSTOR AND GAS TURBINE IMPROVEMENTS

摘要

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.