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US Patent 10711797 Inlet pre-swirl gas turbine engine

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US Patent 12116929 Bleed flow assembly for a gas turbine engine
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US Patent 12104501 Cantilevered airfoils and methods of forming the same
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US Patent 12085019 Object direction mechanism for turbofan engine
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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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US Patent 11970957 Acoustic turbofan airfoil apparatus
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US Patent 11788465 Bleed flow assembly for a gas turbine engine
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US Patent 11767790 Object direction mechanism for turbofan engine
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US Patent 11655768 High fan up speed engine
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=107117970
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US Patent 11480063 Gas turbine engine with inlet pre-swirl features
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Infobox
Is a
Patent
Patent
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
107117970
Date of Patent
July 14, 2020
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Patent Application Number
156252120
Date Filed
June 16, 2017
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=107117970
Patent Primary Examiner
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Joseph J Dallo
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Website URL
https://pdfpiw.uspto.gov/.piw?Docid=10711797
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 US Patent 10711797 Inlet pre-swirl gas turbine engine

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
10711797
Date of patent
July 14, 2020
Patent application number
15625212
Date Filed
June 16, 2017
Patent primary examiner
‌
Joseph J Dallo

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