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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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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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