Aircraft fuselage

Details Aircraft fuselage Aircraft fuselage

B - Operations, Transporting

64

C

B64C 1/00 (2006.01) B64C 1/40 (2006.01) B64D 45/00 (2006.01)

Patent

CA 2618390

The present invention provides an aircraft fuselage which comprises a bulletproof layer in at least partial areas, an aircraft fuselage being understood as both a primary fuselage structure of an aircraft, i.e., sheeting and associated frames and stringers (519), aircraft fuselage insulation (504), and also cabin internal paneling (509), which encloses a pressurized cabin on the outside toward the primary fuselage structure. In this way, it may be possible to ensure bulletproof security (511, 512) of the aircraft fuselage and thus prevent danger to passengers (510) and/or flight-relevant systems of the aircraft.

L~invention concerne un fuselage d~aéronef, dont certaines parties au moins comprennent une couche pare-balles. L~on entend par fuselage d~aéronef une structure principale de fuselage d~un aéronef, autrement dit le tôlage et les ossatures et les lisses associées (519), l~isolation (504) de fuselage d~aéronef, ainsi que les panneaux internes de cabine (509) qui enveloppent une cabine pressurisée vers la structure principale de fuselage. Il est donc possible de réaliser une protection pare-balles (511, 512) du fuselage de l~aéronef et de préserver la sécurité des passagers (510) et/ou le bon fonctionnement des systèmes critiques de l~aéronef.

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