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US Patent 10815886 High tip speed gas turbine engine

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Date Filed
June 16, 2017
Date of Patent
October 27, 2020
Patent Application Number
15625101
Patent Citations Received
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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
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US Patent 12085019 Object direction mechanism for turbofan engine
0
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US Patent 12104501 Cantilevered airfoils and methods of forming the same
0
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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
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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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US Patent 11767790 Object direction mechanism for turbofan engine
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US Patent 11788465 Bleed flow assembly for a gas turbine engine
•••
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
10815886
Patent Primary Examiner
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Lindsay M Low

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