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US Patent 10815886 High tip speed gas turbine engine

Overview Structured Data Issues Contributors Activity

Is a

Patent attributes

Patent Jurisdiction

United States Patent and Trademark Office

Patent Number

Date of Patent

October 27, 2020

Patent Application Number

15625101

Date Filed

June 16, 2017

Patent Citations Received

US Patent 12116929 Bleed flow assembly for a gas turbine engine

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US Patent 11485472 Fluid systems that include a co-flow jet

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 11293293 Turbomachines that include a casing treatment

US Patent 11655768 High fan up speed engine

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US Patent 11655825 Compressor including aerodynamic swirl between inlet guide vanes and impeller blades

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