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US Patent 11852035 Multi-cover gas turbine engine component

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
0
Date Filed
January 28, 2022
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Date of Patent
December 26, 2023
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Patent Applicant
Raytheon Technologies
Raytheon Technologies
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Patent Application Number
17587027
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Patent Citations
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US Patent 7296977 Damping material, damping arrangement and method for designing a damping arrangement
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US Patent 7322223 Creep forming a metallic component
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US Patent 7753654 Aerofoils for gas turbine engines
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US Patent 7993105 Hollow fan blade for gas turbine engine
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US Patent 8205476 Shape correcting components
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US Patent 8256118 Method of manufacturing a turbine fan blade
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US Patent 9010166 Forming apparatus
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US Patent 9121287 Hollow fan blade with honeycomb filler
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US Patent 9169731 Airfoil cover system
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US Patent 9359901 Aerofoil assembly
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•••
Patent Inventor Names
Daniel A. Bales
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Michael DuPont
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Eric W. Malmborg
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11852035
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Patent Primary Examiner
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Elton K Wong
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CPC Code
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F01D 5/187
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F05D 2220/36
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F05D 2240/30
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F01D 5/18
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F01D 5/14
0
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F01D 5/12
0
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F01D 5/147
0
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F01D 5/184
0

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