Active purge mechanism with backflow preventer for gas turbine fuel injectors

A fuel injector (100) for a gas turbine engine includes an injector body having a feed arm (130) with a nozzle body (135) mounted thereto. A fuel conduit (310) fluidly connects a fuel inlet portion of the feed arm to a fuel circuit (120) in the nozzle body to form a fuel path through the injector bo...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Hall, Troy, Caples, Mark A
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
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