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US Patent 12116934 Turbine engine fuel injector with oxygen circuit

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Date Filed
February 10, 2023
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Date of Patent
October 15, 2024
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Patent Applicant
Raytheon Technologies
Raytheon Technologies
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Patent Application Number
18108404
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Patent Citations
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US Patent 7640726 Injector assembly having multiple manifolds for propellant delivery
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US Patent 7870736 Premixing injector for gas turbine engines
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US Patent 7891191 Combustor, gas turbine combustor, and air supply method for same
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US Patent 7954328 Flame holder for minimizing combustor screech
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US Patent 8783009 Method and system for enhancing start of a turbine engine, and ignition module
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US Patent 9062609 Symmetric fuel injection for turbine combustor
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US Patent 9383145 System and method of boiling heat transfer using self-induced coolant transport and impingements
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US Patent 9803498 One-piece fuel nozzle for a thrust engine
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US Patent 10139108 D5/D5A DF-42 integrated exit cone and splash plate
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US Patent 10570865 Fuel injector with variable flow direction
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•••
Patent Inventor Names
Sean R. Jackson
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Lawrence A. Binek
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
12116934
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Patent Primary Examiner
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Lorne E Meade
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CPC Code
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F02C 3/28
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F02C 7/22
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