TURBINE ENGINE FUEL SUPPLY DEVICE AND SYSTEM

PROBLEM TO BE SOLVED: To provide a turbine engine fuel supply device capable of reducing HHV gas consumption, and a system. SOLUTION: A fuel nozzle (70) includes a housing (110), a plurality of fuel passages (115) disposed in the housing (110), and a plurality of air passages (120) disposed in the h...

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Bibliographische Detailangaben
Hauptverfasser:	YEROKHIN SERGEY KONSTANTINOVICH, MESHKOV SERGEY ANATOLIEVICH, HALL JOEL MEADOR, HADLEY MARK ALLAN, OSKIN SERGEY ADOLFOVICH
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a turbine engine fuel supply device capable of reducing HHV gas consumption, and a system. SOLUTION: A fuel nozzle (70) includes a housing (110), a plurality of fuel passages (115) disposed in the housing (110), and a plurality of air passages (120) disposed in the housing (110). A total flow area of the plurality of fuel passages (115) is substantially equal to a total flow area of the plurality of air passages (120). COPYRIGHT: (C)2009,JPO&INPIT