Invention Grant
- Patent Title: Additive manufacturing method for making holes bounded by thin walls in turbine components
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Application No.: US16662730Application Date: 2019-10-24
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Publication No.: US11713682B2Publication Date: 2023-08-01
- Inventor: Ronald Scott Bunker
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Dinsmore & Shohl LLP
- Main IPC: B33Y10/00
- IPC: B33Y10/00 ; F01D5/18 ; B22F3/24 ; B22F10/28 ; B22F5/04 ; B22F7/08 ; F01D25/28 ; B23K15/00 ; B23K26/382 ; B23K26/34 ; B23K26/384 ; B22F7/04 ; C23C24/08 ; B23K101/00 ; B23K103/18 ; B22F10/25 ; B22F10/68 ; B22F10/66

Abstract:
A method of forming a passage in a turbine component includes: using an additive manufacturing process to form a first support structure on a first surface of the turbine component; forming a second support structure on a second surface of the turbine component, the second support structure being spaced apart from the first support structure; and forming a passage in the turbine component between the first and second support structures.
Information query