Aircraft door with oversizing

Details Aircraft door with oversizing Aircraft door with oversizing

B - Operations, Transporting

64

C

B64C 1/14 (2006.01)

Patent

CA 2643453

The present invention relates to an aircraft fuselage section (1) in whose outer skin construction (4) at least one door opening (5) is provided, which has a width (6), such that it is divided by at least one rib (3) of the fuselage skeleton of the aircraft fuselage section (7) into multiple opening areas (7).

Tronçon (1) de fuselage d'aéronef comportant une structure de revêtement extérieur (4) dans laquelle est ménagée une ouverture (5) de porte présentant une largeur (6) qui, grâce à au moins une nervure (3) du squelette du tronçon (7) de fuselage d'aéronef, permet de la diviser en une pluralité de régions d'ouverture.

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