US Patent 12116934 Turbine engine fuel injector with oxygen circuit
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US Patent 12116934 Turbine engine fuel injector with oxygen circuit
Article
Patent abstract
A system is provided for an aerial vehicle. This system includes a splash plate, a fuel nozzle and a gas circuit. The splash plate includes a splash plate surface. The fuel nozzle includes a nozzle orifice. The fuel nozzle is configured to direct fuel out of the nozzle orifice to impinge against the splash plate surface. The gas circuit includes a gas passage and a gas outlet. At least a portion of the gas passage is formed by and embedded within the splash plate. The gas passage extends through the splash plate to the gas outlet.
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Patent Applicant
Patent Jurisdiction
Patent Number
Patent Inventor Names
Lawrence A. Binek0
Sean R. Jackson0
Date of Patent
October 15, 2024
0Patent Application Number
181084040
Date Filed
February 10, 2023
0Patent Citations
Patent Primary Examiner
CPC Code
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