emission in a gas turbine, air fuel mixer, gas turbine and swirler
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United States of America Patent
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Oct 19, 2021
Grant Date -
Aug 24, 2017
app pub date -
Oct 16, 2015
filing date -
Oct 17, 2014
priority date (Note) -
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Abstract
A method for reducing NOx emissions in a gas turbine in which a flow of primary air and a flow of fuel are fed into a dual annular counter rotating swirler, the primary air flow being fed into the inner and outer annular chambers, wherein the method comprises the step of injecting the flow of fuel into the inner annular chamber; another embodiment is a gas turbine air fuel mixer comprising a dual annular counter rotating swirler comprising a fuel supplying element adapted to supplying fuel inside the inner chamber of the swirler; another embodiment is a gas turbine provided by such air fuel mixer.
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