TURBINE ENGINE FUEL INJECTOR WITH OXYGEN CIRCUIT

A system for an aerial vehicle includes a splash plate (132), a fuel nozzle (128) and a gas circuit (136). The splash plate (132) includes a splash plate surface (156, 160). The fuel nozzle (128) includes a nozzle orifice (150). The fuel nozzle (128) is configured to direct fuel out of the nozzle or...

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Bibliographic Details
Main Authors JACKSON, Sean R, BINEK, Lawrence A
Format Patent
LanguageEnglish
French
German
Published 14.08.2024
Subjects
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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Summary:A system for an aerial vehicle includes a splash plate (132), a fuel nozzle (128) and a gas circuit (136). The splash plate (132) includes a splash plate surface (156, 160). The fuel nozzle (128) includes a nozzle orifice (150). The fuel nozzle (128) is configured to direct fuel out of the nozzle orifice (150) to impinge against the splash plate surface (156, 160). The gas circuit (136) includes a gas passage (166) and a gas outlet (174). At least a portion of the gas passage (166) is formed by and embedded within the splash plate (132). The gas passage (166) extends through the splash plate (132) to the gas outlet (174).
Bibliography:Application Number: EP20240157190