首页> 外国专利> Component manufacturing method for e.g. aircraft, involves impregnating added reinforcement fibers with polymer matrix for forming component from elements, where reinforcement fibers are disrupted along parting plane

Component manufacturing method for e.g. aircraft, involves impregnating added reinforcement fibers with polymer matrix for forming component from elements, where reinforcement fibers are disrupted along parting plane

机译:零件制造方法,例如飞机涉及用聚合物基体浸渍添加的增强纤维,以从元件中形成部件,其中增强纤维沿分型面破裂

摘要

The method involves impregnating reinforcement fibers (10) of an element e.g. stringer, partially with a polymer matrix, where the reinforcement fibers include continuous fibers that are provided as multi-ply fabric and braided fabric or knitted fabric. The added reinforcement fibers are impregnated with another polymer matrix for forming a component from the element and another element, where the former component is made of a composite material. The reinforcement fibers are disrupted along a parting plane or cutting parting planes. An independent claim is also included for an element comprising an adding region.
机译:该方法包括浸渍例如纤维的元件的增强纤维(10)。局部地具有聚合物基质的桁条,其中增强纤维包括连续纤维,其被提供为多层织物和编织织物或针织织物。所添加的增强纤维浸渍有另一种聚合物基体,用于由该元件和另一元件形成部件,其中前一部件由复合材料制成。增强纤维沿着分割平面或切割分割平面被破坏。对于包括加法区域的元素也包括独立权利要求。

著录项

  • 公开/公告号DE102010003356A1

    专利类型

  • 公开/公告日2011-09-29

    原文格式PDF

  • 申请/专利权人 DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V.;

    申请/专利号DE20101003356

  • 发明设计人 TOSO YVES;

    申请日2010-03-26

  • 分类号B29C70/34;B29C65/40;B29B15/12;B64C1/06;F03D1/06;F03D11;

  • 国家 DE

  • 入库时间 2022-08-21 17:47:25

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号