发明名称 PIECE STRUCTURALE EN MATERIAU COMPOSITE RENFORCEE LOCALEMENT ET PROCEDE DE REALISATION D'UNE TELLE PIECE
摘要 The structural part has a reinforcement ply (2) provided between two one-way oriented fiber plies layers (3), where the ply is composed of a fiber (10) describing a spiral trajectory that is concentric with respect to a center of a hole (4). The ply is arranged in a regular way on thickness of the structural part between two layers. External diameter of a reinforcement is defined so that the ply and the adjacent plies are in stack to form a covering zone (ZR) and to realize a connection zone between a one-way ply zone and a reinforcement ply zone. An independent claim is also included for a method for realizing a composite material structural part.
申请公布号 FR2951400(B1) 申请公布日期 2016.12.30
申请号 FR20090057366 申请日期 2009.10.20
申请人 AIRBUS OPERATIONS 发明人 TEULOU OLIVIER
分类号 B29C70/10;B29C70/30 主分类号 B29C70/10
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