TAPERED FUEL GALLERY FOR A FUEL NOZZLE

A fuel injector (64) is provided for a turbine engine (20). This fuel injector (64) includes a fuel nozzle (80), and the fuel nozzle (80) includes a gallery (98), one or more feed passages (100) and a plurality of exit passages (102). The gallery (98) extends within the fuel nozzle (80) circumferent...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SWABY, Nadia, SREEKANTH, Sri, FRANCIS, Roger N.A
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING BURNERS COMBUSTION APPARATUS COMBUSTION PROCESSES HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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