B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/14 (2006.01)
Patent
CA 2714587
The invention relates to the fuselage structure of an aircraft with an outer skin (1) which is reinforced by several vertically aligned transverse ribs (7) and several horizontally aligned longitudinal ribs (8) wherein the outer skin (1) has several windows (5) which each comprise a window frame (6). In order to be able to have a free and flexible choice regarding both the size and arrangement of view or access openings in the fuselage shell it is proposed 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).
L'invention concerne la structure de fuselage d'un avion comportant une enveloppe extérieure (1) renforcée par plusieurs membrures transversales verticales (7) et plusieurs membrures longitudinales horizontales (8), l'enveloppe extérieure (1) présentant plusieurs hublots (5) comportant respectivement un cadre (6). Pour pouvoir choisir de façon libre et flexible la taille ainsi que l'emplacement d'ouvertures de vue ou de passage dans l'enveloppe du fuselage, au moins une membrure transversale (7) s'étend au travers du cadre (6) d'un hublot (5) de telle manière que la membrure transversale se termine dans une partie supérieure (9) et dans une partie inférieure (10) du cadre (6).
Brunken Renke
Dittmar Volker
Lange Matthias
Rohde Jens
Airbus Operations Gmbh
Kirby Eades Gale Baker
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