Invention Grant
- Patent Title: Foundry core assembly for manufacturing a turbomachine blade, associated method of manufacturing a blade and associated blade
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Application No.: US14380459Application Date: 2013-02-12
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Publication No.: US09890644B2Publication Date: 2018-02-13
- Inventor: Huu-Thanh Tran , Michael Hansom , Christian Bariaud , Patrice Eneau
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1251620 20120222
- International Application: PCT/EP2013/052785 WO 20130212
- International Announcement: WO2013/124189 WO 20130829
- Main IPC: F01D5/14
- IPC: F01D5/14 ; B22C7/02 ; B22C21/14 ; F01D5/18 ; B22C9/04 ; B22C9/10

Abstract:
A foundry core for manufacturing a blade of a turbomachine including a tip section offset, including a core element for forming various internal cavities, the core element including a leading-edge cavity internal core, central cavity internal cores, and a trailing-edge cavity internal core. The internal core for the central cavity adjacent to the internal core for the trailing-edge cavity includes a bulge extending toward the core for the leading-edge cavity.
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