发明授权
- 专利标题: Structural arrangement, aircraft or spacecraft and method
- 专利标题(中): 结构安排,飞机或航天器和方法
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申请号: EP12188066.0申请日: 2012-10-11
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公开(公告)号: EP2581204B1公开(公告)日: 2017-12-27
- 发明人: Seack, Oliver , Bruns, Alexander
- 申请人: Airbus Operations GmbH
- 申请人地址: Kreetslag 10 21129 Hamburg DE
- 专利权人: Airbus Operations GmbH
- 当前专利权人: Airbus Operations GmbH
- 当前专利权人地址: Kreetslag 10 21129 Hamburg DE
- 代理机构: Isarpatent
- 优先权: DE102011084472 20111013; US201161546764P 20111013
- 主分类号: B29C70/68
- IPC分类号: B29C70/68 ; B29C70/24 ; B64C9/38 ; B29L31/00 ; B29C70/00 ; B64C9/02 ; D03D1/00 ; D03D25/00 ; B29L31/30
摘要:
The structural assembly (200) has box (202) having fiber sections (212,214) which are connected to each other at a crossing point (216). The fiber portion (212) has sub portions (218,220) which are connected to sub portions (232,233) of exterior wall (204) of box. The fiber section (214) has inner and outer ribs (222,224) which extend to inner and outer space (208) of box. A load (230) applied on attachment point (226) formed in outer rib is transferred by fiber section (214) to support element while another load (235) is transferred between sub portions (232,233) by fiber section (212). An independent claim is included for method for manufacture of structural assembly.
公开/授权文献
- EP2581204A3 Structural arrangement, aircraft or spacecraft and method 公开/授权日:2013-05-29
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