Aircraft fuselage

Details Aircraft fuselage Aircraft fuselage

B - Operations, Transporting

64

C

B64C 1/00 (2006.01) B64C 30/00 (2006.01) B64D 27/00 (2006.01)

Patent

CA 2673443

The invention relates to an aircraft fuselage comprising a front part (2) with a cockpit, a central part (4) and a rear part (6). The central part of the fuselage includes a first zone (10) which is located at the front part and which increases in width to a maximum width towards the rear of the aircraft, a second zone (12) that decreases in width, and a third zone (14) which has an essentially constant width and which is located behind the second zone (12), width being measured along the pitch axis.

Ce fuselage d'aéronef comporte une partie avant (2) avec un cockpit, une partie centrale (4) et une partie arrière (6). La partie centrale du fuselage présente du côté de la partie avant (2) une première zone (10) dont la largeur, mesurée le long de l'axe de tangage, est croissante jusqu'à une largeur maximale de l'avant vers l'arrière de l'aéronef, une seconde zone (12) dont la largeur est décroissante et une troisième zone (14) en arrière de la seconde zone (12) dont la largeur est sensiblement constante.

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