US Patent 11499433 Turbine engine component and method of cooling
Patent 11499433 was granted and assigned to General Electric Company on November, 2022 by the United States Patent and Trademark Office.
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Daniel Endecott Osgood0
Zachary Daniel Webster0
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US Patent 11499433 Turbine engine component and method of cooling
Article
A turbine engine airfoil and method of cooling includes an outer wall defining an exterior surface bounding an interior and defining a pressure side and a suction side extending between a leading edge and a trailing edge to define a chord-wise direction and extending between a root and a tip to define a span-wise direction. The airfoil can also include at least one cooling conduit and an impingement zone located within the at least one cooling conduit.
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Patent Applicant
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Patent Jurisdiction
Patent Number
114994330
Date of Patent
November 15, 2022
0Patent Application Number
162232790
Date Filed
December 18, 2018
0Patent Citations
Patent Primary Examiner
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