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US Patent 11959393 Turbine engine with reduced cross flow airfoils

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Date Filed
November 10, 2021
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Date of Patent
April 16, 2024
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Patent Application Number
17523505
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Patent Citations
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US Patent 8257032 Gas turbine with a guide vane
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US Patent 8303258 Fan platform fin
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US Patent 8366399 Blade or vane with a laterally enlarged base
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US Patent 8721291 Flow directing member for gas turbine engine
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US Patent 8920127 Turbine rotor non-metallic blade attachment
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US Patent 9359900 Exhaust diffuser
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US Patent 9598967 Airfoil member and composite platform having contoured endwall
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US Patent 9739154 Axial turbomachine stator with ailerons at the blade roots
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US Patent 9745850 Blade cascade and continuous-flow machine
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US Patent 9874221 Axial compressor rotor incorporating splitter blades
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•••
Patent Inventor Names
Simone Rosa Taddei
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Jeffrey D. Clements
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Saurya Ranjan Ray
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Francesco Bertini
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Jaikumar Loganathan
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Lyle Douglas Dailey
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11959393
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Patent Primary Examiner
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Michael L Sehn
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CPC Code
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F01D 5/141
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