Turbine fuel delivery apparatus and system

A fuel nozzle for a turbine is disclosed. The fuel nozzle includes a housing, a plurality of fuel passages disposed within the housing, and a plurality of air passages disposed within the housing. A total flow area of the plurality of fuel passages is substantially equal to a total flow area of the...

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Bibliographische Detailangaben
Hauptverfasser: Oskin, Sergey Adolfovich, Hadley, Mark Allan, Hall, Joel Meador, Yerokhin, Sergey Konstantinovich, Meshkov, Sergey Anatolievich
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A fuel nozzle for a turbine is disclosed. The fuel nozzle includes a housing, a plurality of fuel passages disposed within the housing, and a plurality of air passages disposed within the housing. A total flow area of the plurality of fuel passages is substantially equal to a total flow area of the plurality of air passages.