发明名称 Flexible and twistable composite material unit for connection of helicopter rotor blades to hub
摘要 The production of a long flexible, twistable, long composite part (17) comprising rods (1) of longitudinal fibres embedded in a resin and enclosed in a vulcanised elastomer (20) consists of separately making an assembly of elementary layers (5), each layer being obtained by laying side-by-side rods (1) of impregnated fibres and keeping them in a non-rigid state in a fabrication mould (6). The fibre rods (1) have their ends (3) placed between cut-out pieces of resin impregnated fibre layers. The layers are made rigid under pressure and heat followed by a cooling process. Several of the elementary layers (5) are assembled together to form a bundle (18) of rods regularly spaced. An elastomer (20) in a viscous state is injected into the bundle. The elastomer (20) is vulcanised to form a composite unit that is flexible and twistable. The resin used is a thermoplastic. The ends of the rods have a rectangular section and the central part joins the ends through a very short transition section having a constant cross sectional surface area. The cut-out pieces have fibres oriented at more or less 45 deg to the rod fibres.
申请公布号 FR2756211(A1) 申请公布日期 1998.05.29
申请号 FR19960014461 申请日期 1996.11.26
申请人 EUROCOPTER FRANCE 发明人 LEGENDRE PHILIPPE MAURICE RENE;DENANTE MARC PIERRE CHRISTIAN
分类号 B29C45/00;B29C70/08;B29C70/34;B29C70/76;B29D99/00;B64C27/32;(IPC1-7):B29C70/20;B29C70/46;B29C70/02 主分类号 B29C45/00
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