公开(公告)号：EP2252504A1

公开(公告)日：2010-11-24

申请号：EP09717217.5

申请日：2009-02-16

申请人： Airbus Operations GmbH

发明人： DITTMAR, Volker ,  ROHDE, Jens ,  BRUNKEN, Renke ,  LANGE, Matthias

IPC分类号： B64C1/14

CPC分类号： B64C1/1492 ,  B64C1/061

摘要： The invention relates to the fuselage structure of an airplane comprising an outer skin (1) that is stiffened through a plurality of vertical transverse ribs (7) and a plurality of horizontal longitudinal ribs (8), wherein the outer skin (1) comprises a plurality of windows (5), each of which comprises a window frame (6). To be able to freely and flexibly select both the size and the arrangement of viewing or penetration openings in the fuselage hull, it is provided according to the invention that at least one transverse rib (7) runs through the window frame (6) of a window (5) so that the transverse rib ends in an upper section (9) of the window frame (6) and in a lower section (10) of the window frame (6).

公开(公告)号：EP2252504B1

公开(公告)日：2012-12-19

申请号：EP09717217.5

申请日：2009-02-16

申请人： Airbus Operations GmbH

发明人： DITTMAR, Volker ,  ROHDE, Jens ,  BRUNKEN, Renke ,  LANGE, Matthias

IPC分类号： B64C1/14

CPC分类号： B64C1/1492 ,  B64C1/061