发明名称 UNIT FOR MOULDING A TURBOMACHINE BLADE, COMPRISING A RAISED PORTION WITH A LARGE CROSS-SECTION
摘要 The invention relates to a moulding unit (210) for producing a turbomachine blade blank. The moulding unit (210) has an upstream portion (270) and a downstream portion (280). According to the invention, the moulding unit (210) comprises a raised portion (231) designed to form a downstream opening which, at the level of the trailing edge, passes through at least one of the side edges of the basin-like portion at the blade tip. The raised portion (231) rigidly secures the upstream portion (270) to the downstream portion (280) and comprises a strengthening protuberance extending in the transverse direction.
申请公布号 WO2017001752(A9) 申请公布日期 2017.02.23
申请号 WO2016FR51581 申请日期 2016.06.27
申请人 SAFRAN AIRCRAFT ENGINES 发明人 VOLLEBREGT, Matthieu, Jean Luc;DUJOL, Charlotte, Marie;ENEAU, Patrice;GUERARD, Coralie;HUCHIN, Patrick, Emilien, Paul, Emile
分类号 B22C9/10;F01D5/18 主分类号 B22C9/10
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