US Patent 11939880 Airfoil assembly with flow surface
Patent 11939880 was granted and assigned to General Electric on March, 2024 by the United States Patent and Trademark Office.
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US Patent 11939880 Airfoil assembly with flow surface
Article
Patent abstract
A turbine engine stage includes a plurality of airfoils extending between an inner band and an outer band. Each airfoil in the plurality of airfoils can have an outer wall defining a pressure side and a suction side, with the outer wall extending between a leading edge and a trailing edge. An intervening flow passage is defined between two adjacent airfoils in the plurality of airfoils.
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Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
Patent Inventor Names
Brian David Keith0
Matthew Brian Surprenant0
Paul Hadley Vitt0
Prem Venugopal0
Thomas William Vandeputte0
Date of Patent
March 26, 2024
0Patent Application Number
179801340
Date Filed
November 3, 2022
0Patent Citations
Patent Primary Examiner
CPC Code
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