DUAL FUEL NOZZLE SYSTEM AND APPARATUS
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United States of America Patent
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Issued Date -
Jul 14, 2016
app pub date -
Aug 19, 2014
filing date -
Aug 20, 2013
priority date (Note) -
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Abstract
In various embodiments, a dual fuel nozzle (200) for use in a gas 200 turbine engine is provided. The nozzle may be configured to supply and gas and a liquid. The dual fuel nozzle (200) may include an interior wall (217). The interior wall (217) may include a shoulder (219). The shoulder (219) may include one or more gas ports (216). Gas may be discharged through the gas ports (216) and penetrate a mixing zone.
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