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US Patent 11268453 Lubrication system for aircraft engine reduction gearbox

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Date Filed
March 17, 2021
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Date of Patent
March 8, 2022
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Patent Application Number
17203902
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Patent Citations
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US Patent 10364752 System and method for an integral drive engine with a forward main gearbox
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US Patent 10371060 Compound engine assembly with confined fire zone
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US Patent 10371170 Noise reduction using IGV flow ejections
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US Patent 10378438 Reverse flow gas turbine engine with radially outward turbine
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US Patent 10385785 Air inlet for a gas turbine engine
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US Patent 10393027 Gas turbine engine shaft architecture and associated method of disassembly
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US Patent 10422243 Gas turbine engine dual towershaft accessory gearbox and starter generator assembly
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US Patent 10422286 Turbine engine with epicyclic reduction gear train
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US Patent 10458422 Turbine engine provided with a lubrication unit
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US Patent 10465611 Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
•••
Patent Citations Received
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US Patent 12000344 Aircraft turbine engine with an off-axis propeller
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US Patent 11680525 Lubricant filter for a turbine engine
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US Patent 11971085 Gearbox assembly
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Patent Inventor Names
Michel Desjardins
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Vincent Savaria
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11268453
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Patent Primary Examiner
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Derek D Knight
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