Integrated fuel nozzle connection
Number of patents in Portfolio can not be more than 2000
United States of America
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Jan 25, 2022
Grant Date -
Jan 17, 2019
app pub date -
Jul 14, 2017
filing date -
Jul 14, 2017
priority date (Note) -
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Abstract
A gas turbine includes a compressor, a turbine, and a combustor disposed downstream from the compressor and upstream from the turbine. The combustor includes an end cover. The combustor also includes a flange. The flange includes an internal fluid passage defined within the flange and the flange is coupled to an internal face of the end cover. A fuel port is integrally joined with the flange. The fuel port extends through the end cover between the flange and an inlet positioned outside of the end cover. The inlet of the fuel port is in fluid communication with the internal fluid passage of the flange.
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