Invention Application
- Patent Title: COMPONENT FOR A TURBINE ENGINE WITH A COOLING HOLE
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Application No.: US17582305Application Date: 2022-01-24
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Publication No.: US20220145764A1Publication Date: 2022-05-12
- Inventor: Zachary Daniel Webster , Aaron Ezekiel Smith , Gregory Terrence Garay , Kirk D. Gallier
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D9/06 ; F01D9/02
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.
Public/Granted literature
- US11927110B2 Component for a turbine engine with a cooling hole Public/Granted day:2024-03-12
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