Method for injecting water into a multistage axial compressor of a gas turbine
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United States of America Patent
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Nov 19, 2019
Grant Date -
Jan 31, 2013
app pub date -
Jul 25, 2012
filing date -
Jul 25, 2011
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Abstract
A method is disclosed for injecting water into a multistage axial compressor of a gas turbine. With low equipment cost, a significant power enhancement can be achieved, even under changing boundary conditions, by water being injected at a plurality of points along the axial compressor, and by the injected water mass flow being controlled at the individual injection points in accordance with ambient conditions and operating parameters of the gas turbine in such a way that an evened-out loading in the individual stages of the axial compressor can be created.
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