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    • 1. 发明申请
    • METHOD AND DEVICE FOR INSERTING PREPREG LAYERS INTO SHAPING TOOLS
    • 在工具工具中引入纤维层的方法和布置
    • WO0218121A9
    • 2002-09-19
    • PCT/EP0109949
    • 2001-08-29
    • DEUTSCH ZENTR LUFT & RAUMFAHRTINVENT INNOVATIVE VERBUNDWERKSSAERTEX WAGENER GMBH & CO KGROTH EKKEHARDSCHOEPPINGER CARSTENHERMANN AXELKLEINEBERG MARKUSPABSCH ARNO
    • ROTH EKKEHARDSCHOEPPINGER CARSTENHERMANN AXELKLEINEBERG MARKUSPABSCH ARNO
    • B29C70/30B29C70/54
    • B29C70/30B29C70/541B29C70/543
    • The invention relates to a method for inserting prepreg layers (21, 22, 23) into shaping tools (10) while producing component parts from fiber reinforced composite materials. The inventive method involves the use of a rigid supporting structure (30) having a gas-permeable top side (32) whose outer contour corresponds to the inner contour of the shaping tool (10) for the component part. The wall thickness of the component part is thinner than the inner contour of the shaping tool (10). The interior (31) of the supporting structure (30) is subjected to a pressure that is low relative to the outside pressure. One or more prepreg layers (21, 22, 23) are placed in succession on the gas-permeable top side (32) of the supporting structure (30). The supporting structure (30) with the prepreg layers (21, 22, 23) placed thereon is inserted into the shaping tool (10) in the existence of a low pressure that continues to prevail inside the interior (31) of the supporting structure (30). While doing this, it is ensured that the prepreg layers (21, 22, 23) are arranged between the inner contour of the shaping tool (10) and the outer contour of the top side (32) of the supporting structure (30). Next, the low pressure inside the interior (31) of the supporting structure (30) is discontinued. Lastly, the supporting structure (30) is removed from the shaping tool (10).
    • 在用于模制插入预浸料层(21,22,23)的方法,管芯(10)在制造部件的由具有气体透过性的上侧(32)的纤维复合材料,刚性支撑结构(30)被使用时,(成形工具的内轮廓的外轮廓 10)对应于设备。 尺寸小于模制工具(10)的内部轮廓的尺寸小于部件的壁厚。 支撑结构(30)的内​​部(31)被置于相对于外部压力的负压下。 一层或多层纤维层(21,22,23)连续沉积在支撑结构(30)的透气上侧(32)上。 所述支撑结构(30)置于与纤维层(21,22,23)被引入与在所述支撑结构(30)在所述模具(10)通行的负压的内部(31)继续进行。 确保模具(10)的内轮廓和支撑结构(30)的上侧(32)的外轮廓之间的纤维层层(21,22,23)被布置。 然后,关闭支撑结构(30)的内​​部(31)中的负压。 最后将支撑结构(30)从模具(10)中移除。