FOUNDRY CORE ASSEMBLY FOR MANUFACTURING A TURBOMACHINE BLADE, ASSOCIATED METHOD OF MANUFACTURING A BLADE AND ASSOCIATED BLADE
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 inte...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | 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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