Gas turbine engine premix injectors
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United States of America Patent
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Nov 11, 2014
Grant Date -
Jul 5, 2007
app pub date -
Dec 14, 2006
filing date -
Dec 14, 2005
priority date (Note) -
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Abstract
One embodiment is a gas turbine engine premix injector including a mixing duct, a plurality of air inlet slots leading to the duct, a plurality of gaseous fuel inlet apertures leading to the duct, a plurality of vanes positioned in the duct downstream from said air inlets, a plurality of liquid fuel inlet apertures leading to the duct, and a plurality of discharge windows positioned between the vanes.
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