发明名称 PROCEDE DE REALISATION DE PIECES COMPOSITES AVEC PREFORME A DRAPAGE HYBRIDE
摘要 <p>A method for manufacturing a thin structural component made of composite and intended to withstand, on the one hand, working loads and, on the other hand, accidental loadings. The method involves creating a dry fiber preform of the component that is to be manufactured, and impregnating the aforementioned perform with a matrix-forming resin by resin transfer. The perform is created by assembling at least one structural layer, a first surface reinforcing layer on a first face of the aforementioned structural layer, and a second surface reinforcing layer on a second face of the structural layer. A number of plies in the two surface reinforcing layers is first of all calculated so that the finished component will be able to withstand the accidental loadings, then a number of plies in the structural layer is calculated, with due consideration given to increases in structural strength contributed by the surface reinforcing layers so that the finished component will be able to withstand the working loads.</p>
申请公布号 FR2924049(B1) 申请公布日期 2009.12.11
申请号 FR20070059358 申请日期 2007.11.28
申请人 AIRBUS FRANCE 发明人 SOULA DENIS;GOHIER SEBASTIEN;MARKOWSKI ANAIS
分类号 B29C70/48;B29L31/30 主分类号 B29C70/48
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