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发明公开
EP2595877A1 STRUKTURBAUTEIL MIT ZUMINDEST EINER HAUPTLAST-TRAGENDE BEPLANKUNGSSCHALE UND EINER TRÄGERSTRUKTUR ZUR BEFESTIGUNG DER HAUPTLAST-TRAGENDEN BEPLANKUNGSSCHALE SOWIE STRÖMUNGSKÖRPER MIT EINEM SOLCHEN STRUKTURBAUTEIL 有权
与至少一个KEY LAST佩带BEPLANKUNGSSCHALE和结构件的载体结构，用于固定主LAST佩带BEPLANKUNGSSCHALE和流动机身采用这样的结构成分

  • 专利标题： STRUKTURBAUTEIL MIT ZUMINDEST EINER HAUPTLAST-TRAGENDE BEPLANKUNGSSCHALE UND EINER TRÄGERSTRUKTUR ZUR BEFESTIGUNG DER HAUPTLAST-TRAGENDEN BEPLANKUNGSSCHALE SOWIE STRÖMUNGSKÖRPER MIT EINEM SOLCHEN STRUKTURBAUTEIL
  • 专利标题（英）： Structural component comprising at least one main-load-bearing covering shell and a carrier structure for fixing the main-load-bearing covering shell, and flow body comprising such a structural component
  • 专利标题（中）： 与至少一个KEY LAST佩带BEPLANKUNGSSCHALE和结构件的载体结构，用于固定主LAST佩带BEPLANKUNGSSCHALE和流动机身采用这样的结构成分
  • 申请号： EP11741107.4
    申请日： 2011-07-20
  • 公开(公告)号： EP2595877A1
    公开(公告)日： 2013-05-29
  • 发明人: ZUARDY, Ichwan , ZAHLEN, Pierre , HERRMANN, Axel, Siegfried
  • 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： Schatt, Markus F.
  • 优先权： US365863P 20100720; US365873P 20100720; US365882P 20100720; US365857P 20100720; DE102010031690 20100720; DE102010031688 20100720; DE102010027695 20100720; DE102010027696 20100720
  • 国际公布： WO2012010305 20120126
  • 主分类号： B64C1/12
  • IPC分类号： B64C1/12 ;  B64C3/26 ;  B32B3/08 ;  B32B5/18
STRUKTURBAUTEIL MIT ZUMINDEST EINER HAUPTLAST-TRAGENDE BEPLANKUNGSSCHALE UND EINER TRÄGERSTRUKTUR ZUR BEFESTIGUNG DER HAUPTLAST-TRAGENDEN BEPLANKUNGSSCHALE SOWIE STRÖMUNGSKÖRPER MIT EINEM SOLCHEN STRUKTURBAUTEIL
摘要：
The invention relates to a structural component (1), comprising at least one main-load-bearing covering shell (B) and a carrier structure (T) for fixing the covering shell, wherein the covering shell (B) is designed in the form of a sandwich and formed by an inner skin section (11), an outer skin section (12) and a shear-load-absorbing core layer (13) which is disposed between said two sections and connects the inner and the outer skin sections (11, 12) to one another in a planar manner, wherein the carrier structure (T) is formed by at least one panel-shaped connecting part (22) which extends between and transversely to said inner and outer skin sections and is connected along a reference longitudinal direction (L-R) to the covering shell (B). In order to support the covering shell (B) on the carrier structure, the connecting part is located outside the carrier structure (T) and is fastened to the inner skin section (11) resting thereon in a planar manner, wherein at least one profiled support (V0; V1, V2, V3, V4) extending along the reference longitudinal direction (L-R) is provided in the covering shell (B) in order to form a reinforcing section in the connecting region (14) of the panel-shaped connecting part (22). The profiled support is connected to the inner skin section (11) and the outer skin section (12) in order to stabilise the covering shell (B) when the latter sustains damage and thereby provides support from the outside.
摘要（中）：

本发明涉及的结构部件的流体的（1），包括至少一个衬壳（B）那样载有主负载，具有芯层（33），所述内衬壳做吸音减震剪切负荷和确实包括一个多元化 在泡沫层的纵向延伸旁边的海誓山盟布置核心层部分（33A），所述worin核心层部分在两侧由一个核心层加强区域抵靠彼此相互连接（37） 穿过核心层垂直地延伸到核心层（33）的纵向延伸。

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