发明名称 METHOD AND ASSEMBLY FOR THE PRODUCTION OF A COMPOSITE BLADE
摘要 The invention relates to a compaction assembly comprising a shaping mold (24) delimiting an upwardly open housing, capable of receiving a woven preform cut out beforehand (10a), and a vertically moveable compaction tool (128) and forming, with the shaping mold, (24), a compaction assembly for said preform placed beforehand in the housing. The compaction tool (128) includes at least one foot portion (128A). The compaction tool (128) comprises at least three separate compaction blocks (1281-1287). Application to the manufacturing of composite fan blades for a turbomachine.
申请公布号 EP3052304(A1) 申请公布日期 2016.08.10
申请号 EP20140789324 申请日期 2014.10.03
申请人 SNECMA 发明人 MARCHAL, YANN;ENGEL, JEREMY;GIMAT, MATTHIEU
分类号 B29C70/48;B29B11/16;B29B13/06;B29C43/36;B29K21/00;B29L31/08 主分类号 B29C70/48
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