Erosion suppression system and method in an exhaust gas recirculation gas turbine system
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United States of America Patent
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Feb 6, 2018
Grant Date -
Dec 31, 2015
app pub date -
May 29, 2015
filing date -
Jun 30, 2014
priority date (Note) -
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Abstract
In an embodiment, a method includes flowing an exhaust gas from a turbine of a gas turbine system to an exhaust gas compressor of the gas turbine system via an exhaust recirculation path; evaluating moist flow parameters of the exhaust gas within an inlet section of the exhaust gas compressor using a controller comprising non-transitory media programmed with instructions and one or more processors configured to execute the instructions; and modulating cooling of the exhaust gas within the exhaust recirculation path, heating of the exhaust gas within the inlet section of the exhaust gas compressor, or both, based on the evaluation.
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