US Patent 12000308 Rotor blade assemblies for turbine engines
Patent 12000308 was granted and assigned to General Electric on June, 2024 by the United States Patent and Trademark Office.
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US Patent 12000308 Rotor blade assemblies for turbine engines
Article
Patent abstract
A rotor blade assembly for a turbine engine, including an airfoil blade including an inner diameter end and an outer diameter end, a lower blade carrier coupled to the inner diameter end of the airfoil blade and rigidly coupled to a disk via a pin, an upper blade carrier coupled to the outer diameter end of the airfoil blade, and an outer drum coupled to the upper blade carrier via a radial joint. The radial joint supports radial motion of the upper blade carrier relative to an axis extending through a center of the rotor blade assembly.
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Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
Patent Inventor Names
Bhaskar Nanda Mondal0
Thomas O. Moniz0
Vinod Shashikant Chaudhari0
Date of Patent
June 4, 2024
0Patent Application Number
178937470
Date Filed
August 23, 2022
0Patent Citations
Patent Primary Examiner
CPC Code
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