Fuselages for aircraft

Details Fuselages for aircraft Fuselages for aircraft

B - Operations, Transporting

64

C

B64C 1/00 (2006.01) B64C 1/14 (2006.01)

Patent

CA 2243422

An aircraft and a fuselage for an aircraft are provided. The fuselage comprises front and rear tapered double curvature skin portions (1, 2) and a central single curvature skin portion (3). Cabin doors (4, 5, 6, 7) are set into double curvature tapered portions (1, 2) of the fuselage in single curvature skin areas (19, 20, 27, 28). The single curvature skin areas are either extensions (19, 20) of the single curvature central portion (3) of the fuselage or comprise "patches" (27, 28) of single curvature skin immediately each surrounding each door in the double curvature tapered portions (1, 2) of the fuselage.

Cette invention se rapporte à un aéronef et à un fuselage conçu pour cet aéronef. Ledit fuselage comporte des parties d'enveloppe avant et arrière (1, 2) coniques à double courbure et une partie d'enveloppe centrale (3) à courbure unique. Les portes des cabines (4, 5, 6, 7) sont façonnées dans les parties coniques (1, 2) à double courbure du fuselage dans des zones de l'enveloppe à courbure unique (19, 20, 27, 28). Ces zones de l'enveloppe à courbure unique peuvent, soit constituer des prolongements (19, 20) de la partie centrale à courbure unique du fuselage, soit être des "pans" (27, 28) d'enveloppe à courbure unique jouxtant chacune des portes dans les parties coniques à double courbure (1, 2) du fuselage.

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