首页> 外国专利> Core structure manufacturing method for airplane, involves positioning core layers with defined distance, and inserting reinforcement unit in hollow space between layers, where reinforcement unit and layers form integral core structure

Core structure manufacturing method for airplane, involves positioning core layers with defined distance, and inserting reinforcement unit in hollow space between layers, where reinforcement unit and layers form integral core structure

机译:飞机芯结构的制造方法,包括定位一定距离的芯层,并将增强单元插入层之间的中空空间,其中增强单元和层形成整体芯结构

摘要

The method involves fastening core structure layers (1, 2) by clamping devices, and positioning the core structure layers with a defined distance (a). A reinforcement unit (3) is inserted in a hollow space (4) between the core structure layers, where the reinforcement unit and the core structure layers form an integral core structure (10). Warm areas of the core structure layers are locally heated, and the reinforcement unit is inserted into the warm areas. The core structure layers are separated using a spacer unit and are sealed by sealing units e.g. lacquers and resins. An independent claim is also included for a device for manufacturing a core structure, comprising clamping devices.
机译:该方法包括通过夹紧装置紧固芯结构层(1、2),并以限定的距离(a)定位芯结构层。在芯结构层之间的中空空间(4)中插入加强单元(3),其中,加强单元和芯结构层形成一体的芯结构(10)。芯结构层的温暖区域被局部加热,并且加固单元被插入温暖区域。芯结构层使用间隔单元分开,并通过例如密封单元密封。漆和树脂。还包括一种用于制造芯结构的装置的独立权利要求,该装置包括夹紧装置。

著录项

  • 公开/公告号DE102006056568A1

    专利类型

  • 公开/公告日2008-06-05

    原文格式PDF

  • 申请/专利权人 AIRBUS DEUTSCHLAND GMBH;

    申请/专利号DE20061056568

  • 申请日2006-11-30

  • 分类号B32B3/22;B32B1/06;B64C1;

  • 国家 DE

  • 入库时间 2022-08-21 19:49:33

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