Fuel nozzle and burner section of a gas turbine engine

A fuel nozzle 51 is disclosed which comprises an inlet 55 for receiving fuel and an outlet 71 for discharging fuel. The outlet 71 intersects a longitudinal centerline CL of the nozzle 51 and produces a skewed spray pattern. Also disclosed is a fuel injector 31 having a fuel nozzle outlet 71 such tha...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	GRAVES, CHARLES B
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING BURNERS COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF WEAPONS
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