FUEL NOZZLE FOR A GAS TURBINE ENGINE

13DV-7453 FUEL NOZZLE FOR A GAS TURBINE ENGINE In one form, a fuel nozzle includes a primary flowpath and a secondary flowpath, each of which includes a pair of axially opposing input and output ends disposed along a common central longitudinal axis. The secondary path is circumferentially disposed...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SETO, STANFORD P, RICHEY, JOHN M, STENGER, RICHARD E, KUTZKO, GUSTAVE G
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING BURNERS COMBUSTION APPARATUS COMBUSTION PROCESSES HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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