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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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