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US Patent 11927110 Component for a turbine engine with a cooling hole

Patent 11927110 was granted and assigned to General Electric on March, 2024 by the United States Patent and Trademark Office.

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Patent attributes

Patent Applicant

General Electric

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Current Assignee

General Electric

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Patent Jurisdiction

United States Patent and Trademark Office

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Patent Number

Patent Inventor Names

Zachary Daniel Webster0

Gregory Terrence Garay0

Kirk D. Gallier0

Aaron Ezekiel Smith0

Date of Patent

March 12, 2024

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Patent Application Number

175823050

Date Filed

January 24, 2022

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Patent Citations

US Patent 9447794 Inducer and diffuser configuration for a gas turbine system

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US Patent 6897401 Non-separating diffuser for holes produced by a two step process

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US Patent 7992272 Method and apparatus for milling thermal barrier coated metals

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US Patent 9279330 Gas turbine engine component with converging/diverging cooling passage

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US Patent 10773344 Systems and methods for manufacturing film cooling hole diffuser portion

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Patent Primary Examiner

Phutthiwat Wongwian

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CPC Code

0

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Patent abstract

An apparatus and method relating to a cooling hole of a component of a turbine engine. The cooling hole can extend from an inlet to an outlet to define a connecting passage. The cooling hole can contain a diffusing section. The diffusing section can be defined by an interior surface having variable geometries.

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