发明授权
- 专利标题: Structural component with rib and cross member element
- 专利标题(中): 结构件与肋和横梁元件
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申请号: US12638423申请日: 2009-12-15
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公开(公告)号: US08439307B2公开(公告)日: 2013-05-14
- 发明人: Philipp Westphal , Wolf-Dietrich Dolzinski , Thorsten Roming , Thorsten Schroeer , Dieter Kohlgrueber , Marius Luetzenburger
- 申请人: Philipp Westphal , Wolf-Dietrich Dolzinski , Thorsten Roming , Thorsten Schroeer , Dieter Kohlgrueber , Marius Luetzenburger
- 申请人地址: DE Hamburg DE Cologne
- 专利权人: Airbus Operations GmbH,DLR-Deutsches Zentrum fuer Luft- und Raumfahrt e.V.
- 当前专利权人: Airbus Operations GmbH,DLR-Deutsches Zentrum fuer Luft- und Raumfahrt e.V.
- 当前专利权人地址: DE Hamburg DE Cologne
- 代理机构: Jenkins, Wilson, Taylor & Hunt, P.A.
- 优先权: DE102007030026 20070629
- 主分类号: B64C1/18
- IPC分类号: B64C1/18
摘要:
The present invention provides a fuselage structure for an aircraft or spacecraft with an outer skin. The fuselage structure comprises a rib element for stiffening the outer skin and ad cross member element. Here the rib element is bent in the shape of an arc to correspond to an inner contour of the outer skin. The cross member element connects two arc sections of the rib element transversely to each other. The cross member element has a higher strength than the rib element. From another point of view the invention provides an aircraft with such a fuselage structure.
公开/授权文献
- US20130009008A1 STRUCTURAL COMPONENT WITH RIB AND CROSS MEMBER ELEMENT 公开/授权日:2013-01-10
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