Dual orifice pilot fuel injector

A gas turbine engine fuel nozzle assembly (12) has concentric primary and secondary pilot fuel nozzles (58, 59) with circular primary and annular secondary exits (98, 100) respectively and a main fuel nozzle (61) spaced radially outwardly of the pilot fuel nozzles (58, 59). The primary and secondary...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	HSIAO, GEORGE CHIAUN, MANCINI, ALFRED ALBERT, BENJAMIN, MICHAEL ANTHONY, CHAUVETTE, CLAUDE HENRY
Format:	Patent
Sprache:	eng ; fre ; ger
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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!