Aircraft fuselage made from longitudinal panels and method...

Details Aircraft fuselage made from longitudinal panels and method... Aircraft fuselage made from longitudinal panels and method...

B - Operations, Transporting

64

C

B64C 1/00 (2006.01)

Patent

CA 2663415

The invention relates to an aircraft fuselage comprising a nose cone (2), a tail section (2) and a central section (3), the central section comprising longitudinal panels (31 - 39) assembled directly with one another, at least one of these longitudinal panels having a length corresponding to the distance between the nose cone and the tail section in order to connect said nose cone with said tail section.

L'invention concerne un fuselage d'aéronef comportant une pointe avant (2), un tronçon arrière (2) et un tronçon central (3), le tronçon central comportant des panneaux longitudinaux (31 - 39) assemblés directement les uns avec les autres, au moins un de ces panneaux longitudinaux ayant une longueur correspondant à la distance entre la pointe avant et le tronçon arrière pour relier ladite pointe avant avec ledit tronçon arrière.

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