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US Patent 11867082 Rotor blade with detachable tip

Patent 11867082 was granted and assigned to General Electric on January, 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

Nicholas Joseph Kray0

Nitesh Jain0

Abhijeet Jayshingrao Yadav0

Date of Patent

January 9, 2024

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Patent Application Number

172362360

Date Filed

April 21, 2021

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Patent Citations

US Patent 8790087 Interlocking blade sheath

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US Patent 7114912 Fan blade with embrittled tip

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US Patent 8033790 Multiple piece turbine engine airfoil with a structural spar

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US Patent 8251658 Tip cap for turbine rotor blade

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US Patent 8974884 Part comprising a structure and a shape memory alloy element

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US Patent 9145787 Rotatable component, coating and method of coating the rotatable component of an engine

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Patent Primary Examiner

Eric J Zamora Alvarez

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CPC Code

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Patent abstract

A rotor blade for a gas turbine engine is provided. The rotor blade includes a blade body formed of a first material; and a tip component removably connected to the blade body, the tip component formed of a second material that is different than the first material.

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