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US Patent 10711797 Inlet pre-swirl gas turbine engine

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Date Filed
June 16, 2017
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Date of Patent
July 14, 2020
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Patent Application Number
15625212
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Patent Citations Received
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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
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US Patent 11788465 Bleed flow assembly for a gas turbine engine
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US Patent 11970957 Acoustic turbofan airfoil apparatus
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US Patent 12012898 Gas turbine engine with acoustic spacing of the fan blades and outlet guide vanes
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
10711797
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Patent Primary Examiner
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Joseph J Dallo
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