发明名称 Process and system for making an armature for a part made of composite material
摘要 <p>Method for making reinforcement for a composite material part made from the reinforcement core in a curved matrix. The reinforcement consisting of superimposed layers of parallel strands each at right angles to the next and all sewn together. Before laying down the strands a mathematical model of the reinforcement (A) is created and held in memory and for each layer, from the model, a further model is created and controls a positioning system (3) to move a tool (1) to deposit and or fix the strands (F). Also claimed is the reinforcement formed and the finished composite using it.</p>
申请公布号 EP0754795(A1) 申请公布日期 1997.01.22
申请号 EP19960401437 申请日期 1996.06.28
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 CAHUZAC, GEORGES
分类号 D04H3/05;D04H3/115;D05B23/00;H05K1/03;B29B11/16;B29K101/10;B29K105/08;D04H3/002;D04H3/004;D04H3/04;(IPC1-7):D04H3/04;D04H18/00 主分类号 D04H3/05
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