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US Patent 11767766 Turbomachine airfoil having impingement cooling passages

Patent 11767766 was granted and assigned to General Electric on September, 2023 by the United States Patent and Trademark Office.

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Contents

Is a
Patent
Patent

Patent attributes

Patent Applicant
General Electric
General Electric
Current Assignee
General Electric
General Electric
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
11767766
Patent Inventor Names
John M. Matthews
Christopher Donald Porter
Matthew Troy Hafner
Date of Patent
September 26, 2023
Patent Application Number
17877085
Date Filed
July 29, 2022
Patent Citations
‌
US Patent 7437876 Augmenter swirler pilot
‌
US Patent 7493767 Method and apparatus for cooling combustor liner and transition piece of a gas turbine
‌
US Patent RE40658 Methods and apparatus for cooling gas turbine nozzles
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US Patent 7665309 Secondary fuel delivery system
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US Patent 7690203 Removable diffusion stage for gas turbine engine fuel nozzle assemblages
‌
US Patent 7707833 Combustor nozzle
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US Patent 7789125 Extended impingement cooling device and method
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US Patent 7836703 Reciprocal cooled turbine nozzle
...
Patent Citations Received
‌
US Patent 12092061 Axial fuel stage immersed injectors with internal cooling
0
Patent Primary Examiner
‌
Eldon T Brockman
CPC Code
‌
F05D 2260/20
‌
F01D 9/065
‌
F01D 5/188
‌
F01D 5/187
Patent abstract

An airfoil includes a leading edge, a trailing edge, a base, and a tip. The airfoil further includes a pressure side wall and a suction side wall that extend between the leading edge, the trailing edge, the base, and the tip. The airfoil further includes a plurality of passages that are defined within the airfoil and extend from an inlet at one of the base or the tip. Each passage of the plurality of passages is defined at least partially by a primary impingement wall and a solid side wall. The primary impingement wall is spaced apart from one of the pressure side wall or the suction side wall such that a primary impingement gap is defined therebetween. The primary impingement wall defines a plurality of impingement apertures that direct air in discrete jets across the impingement gap to impinge upon an interior surface of the airfoil.

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