发明名称 TURBINE ENGINE BLADE PREFORM
摘要 The invention relates to a blade preform (46) including a strut connecting a plat-form (16) to a blade root portion (14) extending longitudinally in an upstream-downstream direction, an upstream web (26) and a downstream (28) web, which each extend in a direction substantially perpendicular to the longitudinal direction of the blade root and are formed at the upstream and downstream ends of the strut. The upstream (26) and downstream (28) webs connect the upstream and downstream ends of the plat-form (16) to the upstream and downstream ends of the blade root (14). According to the invention, the blade root (14) extends in a direction perpendicular to the longitudinal direction of the blade root over a distance smaller than that of the upstream and downstream webs (26, 28) and the side edges (40) of each web (26, 28) are extended by walls that converge (44) at the flanks of the blade root.
申请公布号 EP3003600(A1) 申请公布日期 2016.04.13
申请号 EP20140733252 申请日期 2014.06.04
申请人 SNECMA 发明人 CONGRATEL, SÉBASTIEN;DUPEYRE, RAPHAËL;KLEIN, GUILLAUME;MATHIEU, DAVID;TANG, BA-PHUC
分类号 B22C9/06;B22C9/22;F01D5/12 主分类号 B22C9/06
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