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US Patent 11982205 Airfoil having a spar assembly for a turbine engine

Patent 11982205 was granted and assigned to General Electric on May, 2024 by the United States Patent and Trademark Office.

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Patent attributes

Patent Applicant

General Electric

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Current Assignee

General Electric

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Patent Jurisdiction

United States Patent and Trademark Office

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Patent Number

Patent Inventor Names

Abhijeet Jayshingrao Yadav0

Balaraju Suresh0

Nicholas Joseph Kray0

Nitesh Jain0

Date of Patent

May 14, 2024

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Patent Application Number

181714900

Date Filed

February 20, 2023

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Patent Citations

US Patent 10648340 High modulus hybrid material rotor blade spar

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US Patent 9429024 Propeller blade with lightweight insert

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US Patent 10227127 Fiber metal laminate reinforced wing spar for retractable underwing mounted landing gear assemblies

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US Patent 10549842 Propeller blades

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US Patent 10563522 Composite airfoil for a gas turbine engine

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US Patent 11401834 Method of securing a ceramic matrix composite (CMC) component to a metallic substructure using CMC straps

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Patent Primary Examiner

Brian Christopher Delrue

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CPC Code

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Patent abstract

An airfoil for a turbine engine having a spar assembly. The spar assembly including a composite spar, a metallic hub, and a composite body. The metallic hub can receive a portion of the composite spar at an interior surface to define an overlapping region. The composite body is located at the overlapping region.

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