发明名称 COMPACTING ASSEMBLY AND METHOD OF FABRICATING A COMPOSITE BLADE FOR A TURBINE ENGINE
摘要 Compacting assembly comprising a shaper mold (24) defining an upwardly open housing suitable for receiving a woven preform (10a) that has previously been cut out, and a vertically movable compacting tool (128) that, together with the shaper mold (24), forms a compacting assembly for compacting said preform previously placed in the housing. The compacting tool (128) comprises at least a root portion (128A). The invention is applicable to fabricating turbine engine composite blades.
申请公布号 US2016243777(A1) 申请公布日期 2016.08.25
申请号 US201415026282 申请日期 2014.10.03
申请人 SNECMA 发明人 MARCHAL Yann;GIMAT Matthieu
分类号 B29D99/00;F01D5/28;B29C70/48;B29C43/00;B29C45/00 主分类号 B29D99/00
代理机构 代理人
主权项 1. A compacting assembly for compacting a woven preform obtained by three-dimensionally weaving yarns in order to form a composite blade for a turbine engine, said preform having portions for predefining the airfoil, the root of the blade, and between the airfoil and the root, the tang of the blade, the compacting assembly comprising a shaper mold defining an upwardly open housing suitable for receiving a woven preform, and a vertically movable compacting tool for co-operating with the shaper mold to form a compacting assembly enabling said preform to be compacted when it is placed in the housing, wherein the compacting tool comprises at least a root portion, further comprising a deformable skin covering at least part of the compacting tool facing the sharper mold.
地址 Paris FR