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US Patent 11236622 Turbine nozzle airfoil and/or trailing edge profile

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
Date Filed
March 9, 2020
Date of Patent
February 1, 2022
Patent Application Number
16812506
Patent Citations
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US Patent 10060443 Airfoil shape for twelfth stage compressor stator vane
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US Patent 10066641 Airfoil shape for fourth stage compressor stator vane
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US Patent 10087952 Airfoil shape for first stage compressor stator vane
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US Patent 10125623 Turbine nozzle profile
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US Patent 10132330 Airfoil shape for eleventh stage compressor stator vane
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US Patent 10156149 Turbine nozzle having fillet, pinbank, throat region and profile
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US Patent 10161255 Turbine nozzle having non-axisymmetric endwall contour (EWC)
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US Patent 10233759 Airfoil shape for seventh stage compressor stator vane
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US Patent 10287886 Airfoil shape for first stage compressor rotor blade
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US Patent 10288086 Airfoil shape for third stage compressor stator vane
•••
Patent Citations Received
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US Patent 11377961 Internal core profile for a turbine nozzle airfoil
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
11236622
Patent Primary Examiner
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Courtney D Heinle

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