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Method of producing a composite shell element, composite shell element, means of transport and use

机译:复合壳元件的制造方法,复合壳元件,运输工具和使用

摘要

Systems and methods for fabrication of composite shell elements and to the assembly of large scale structures comprising such composite shell elements are provided. The composite shell elements comprise two regions in which the resin is cured to different levels. As a consequence, the flexibility of the first region is greater than the flexibility of the second region. Since the first region defines a bending line, the composite shell element can be deformed along the bending line during assembly of the large scale structure. Thus, tolerances in fabrication of the composite shell elements may be compensated for in a time-efficient manner without the need for applying a shimming process.
机译:提供了用于制造复合壳体元件以及用于组装包括这种复合壳体元件的大规模结构的系统和方法。复合壳元件包括两个区域,其中树脂被固化到不同的水平。结果,第一区域的柔性大于第二区域的柔性。由于第一区域限定弯曲线,因此复合壳体元件可在大规模结构的组装期间沿着弯曲线变形。因此,可以以省时的方式补偿复合壳体元件的制造公差,而无需施加匀场过程。

著录项

  • 公开/公告号US9452561B2

    专利类型

  • 公开/公告日2016-09-27

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号US201314063283

  • 申请日2013-10-25

  • 分类号B29C53;B29C53/04;B29C70/54;B29C35/02;B32B3/06;

  • 国家 US

  • 入库时间 2022-08-21 14:30:59

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