发明名称 Method for manufacturing a fibre reinforced composite workpiece comprising a central body and fins
摘要 <p>The peripheral mandrels 1 are joined together and a filament winding produced around them and then cut, and the peripheral mandrels 1 are turned over and pressed around a central mandrel 16 on which another filament winding has been produced. Polymerization pressing gives the desired component. Application to the manufacture of missile bodies. <IMAGE> <IMAGE></p>
申请公布号 EP0631858(B1) 申请公布日期 1997.02.26
申请号 EP19940401466 申请日期 1994.06.28
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 FAGES, JACQUES
分类号 F42B15/00;B29C53/58;B29C69/00;B29C70/06;B29C70/30;B29C70/54;B29D99/00;F42B10/06;(IPC1-7):B29C70/54 主分类号 F42B15/00
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