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Foundry core assembly for manufacturing a turbomachine blade, associated method of manufacturing a blade and associated blade
Foundry core assembly for manufacturing a turbomachine blade, associated method of manufacturing a blade and associated blade
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机译:用于制造涡轮机叶片的铸造芯组件,制造叶片的相关方法以及相关叶片
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摘要
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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