FUEL INJECTOR MANIFOLD HAVING TRIM DEVICE THEREIN

A fuel injector assembly can include a manifold (101) defining a manifold channel (103) and a nozzle (105) extending from the manifold. The nozzle can be configured to direct flow from the manifold channel into a combustor. The nozzle can define a fuel inlet (107) open to the manifold channel, a fue...

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Bibliographische Detailangaben
Hauptverfasser:	RYON, Jason A, TIBBS, Andy W, WILLIAMS, Brandon P
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS 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 WEAPONS
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Beschreibung
Zusammenfassung:	A fuel injector assembly can include a manifold (101) defining a manifold channel (103) and a nozzle (105) extending from the manifold. The nozzle can be configured to direct flow from the manifold channel into a combustor. The nozzle can define a fuel inlet (107) open to the manifold channel, a fuel outlet (109) configured to be open to a combustor, and a throat (111) fluidly connecting the fuel inlet to the fuel outlet. The assembly can include a trim device (113) inserted into the manifold. The trim device can be configured to adjust flow between the manifold channel and the fuel inlet to adjust flow through the throat and out of the fuel outlet.