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US Patent 10815886 High tip speed 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 12085027 Compressor bleed for gas turbine engine
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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 11987352 Fluid systems that include a co-flow jet
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US Patent 11920617 Fluid systems and methods that address flow separation
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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 11655825 Compressor including aerodynamic swirl between inlet guide vanes and impeller blades
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edited on 24 May, 2023
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US Patent 11655768 High fan up speed engine
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=10815886
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US Patent 11485472 Fluid systems that include a co-flow jet
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US Patent 11480063 Gas turbine engine with inlet pre-swirl features
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Website URL
https://pdfpiw.uspto.gov/.piw?Docid=10815886
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edited on 6 Apr, 2022
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US Patent 11293293 Turbomachines that include a casing treatment
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 US Patent 10815886 High tip speed gas turbine engine

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
10815886
Date of patent
October 27, 2020
Patent application number
15625101
Date Filed
June 16, 2017
Patent primary examiner
‌
Lindsay M Low

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