B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/00 (2006.01) B64C 1/12 (2006.01)
Patent
CA 2644964
A fuselage section (2) comprises an interior that forms a passenger cabin. In horizontal projection the fuselage section according to the invention is geometrically defined by a first exterior skin region (6) and a second exterior skin region (7), wherein the second exterior skin region faces the first exterior skin region. Both the first exterior skin region and the second exterior skin region in longitudinal direction of the passenger cabin comprise in horizontal projection a circular-arc-shaped contour of uniform radius of curvature.
La présente invention concerne une section fuselage (2) qui comprend un intérieur formant une cabine de passagers. Selon l'invention, la section fuselage est définie géométriquement, en projection horizontale, par une première zone d'enveloppe extérieure (6) et une seconde zone d'enveloppe extérieure (7) faisant face à la première zone d'enveloppe extérieure. La première et la seconde zone d'enveloppe extérieure dans la direction longitudinale de la cabine de passagers possèdent en projection horizontale un contour en forme d'arc de cercle présentant un rayon de courbe uniforme.
Dehn Martin
Ipek Ugur
Muhlich Christoph
Wuggetzer Ingo
Airbus Deutschland Gmbh
Airbus Operations Gmbh
Borden Ladner Gervais Llp
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