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Method for forming a structural component of an aircraft or spacecraft, and forming device

机译:形成飞机或航天器的结构部件的方法以及形成装置

摘要

In a method for forming a structural component of an aircraft or spacecraft a preform comprising at least one band is formed by means of braiding around a core. A severing cut is introduced at least in portions into the at least one band of the preform to form two band portions of the at least one band. The two formed band portions of the at least one band are then deformed into a predetermined shape by means of a deformation tool which can be guided along the severing cut. A deformation device is used to carry out the method. A structural component is produced by means of the method and/or the deformation device.
机译:在一种用于形成飞机或航天器的结构部件的方法中,包括至少一个带的预成型件是通过绕芯编织而形成的。将切断切口至少部分地引入到预成型件的至少一个带中,以形成至少一个带的两个带部分。然后借助于变形工具将至少一个带的两个形成的带部分变形为预定形状,该变形工具可以沿着切断切口被引导。使用变形装置来执行该方法。通过该方法和/或变形装置来制造结构部件。

著录项

  • 公开/公告号US9375882B2

    专利类型

  • 公开/公告日2016-06-28

    原文格式PDF

  • 申请/专利权人 MAREK BERESINSKI;

    申请/专利号US201213483561

  • 发明设计人 MAREK BERESINSKI;

    申请日2012-05-30

  • 分类号B29C70/22;B29C70/54;B29D99;

  • 国家 US

  • 入库时间 2022-08-21 14:30:03

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