Invention Grant
- Patent Title: Method of forming cooling passage for turbine component with cap element
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Application No.: US15862927Application Date: 2018-01-05
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Publication No.: US10933481B2Publication Date: 2021-03-02
- Inventor: Thomas Earl Dyson , Jason Ray Gregg , Nicholas William Rathay
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agent Charlotte C. Wilson; James W. Pemrick
- Main IPC: B23H9/10
- IPC: B23H9/10 ; F01D5/18 ; F01D5/14 ; F01D9/04 ; F01D25/12 ; F01D5/28

Abstract:
Methods of forming a cooling passage on a turbine component having a component wall with an internal surface and an external surface, are disclosed. An opening is formed passing through the component wall and fluidly connecting the internal and external surfaces. The opening includes a metering section extending from the internal surface to a metering end, and a diffuser area extending from the metering end to the external surface. A preformed cap element is added to close a portion of the diffuser area to form the cooling passage with a diffusion section extending from the metering end to the external surface. The preformed metal cap element includes a projection extending internally of the external surface and into the diffusion area to define an internally facing section of the diffusion section. The cooling passage extends through the component wall and fluidly connects the internal surface and the external surface.
Public/Granted literature
- US20190210132A1 METHOD OF FORMING COOLING PASSAGE FOR TURBINE COMPONENT WITH CAP ELEMENT Public/Granted day:2019-07-11
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