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US Patent 10711797 Inlet pre-swirl gas turbine engine

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Patent attributes

Patent Jurisdiction

United States Patent and Trademark Office

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Patent Number

Date of Patent

July 14, 2020

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Patent Application Number

156252120

Date Filed

June 16, 2017

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Patent Citations Received

US Patent 12116929 Bleed flow assembly for a gas turbine engine

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US Patent 12085019 Object direction mechanism for turbofan engine

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US Patent 12104501 Cantilevered airfoils and methods of forming the same

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US Patent 11480063 Gas turbine engine with inlet pre-swirl features

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US Patent 11655768 High fan up speed engine

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US Patent 11767790 Object direction mechanism for turbofan engine

US Patent 11788465 Bleed flow assembly for a gas turbine engine

US Patent 11970957 Acoustic turbofan airfoil apparatus

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