High capacity aircraft fuselage

Abstract

Abstract Aircraft fuselage comprising two lobes arranged side by side, assembled along two lines of longitudinal junctions. <??>According to the invention, the fuselage comprises an upper beam for reinforcement (28) of the upper junction line; a floor (23) separating an upper volume usable as a cabin (24) and a lower volume (25) usable as a hold; means (32) for supporting the cabin floor these means linking the said floor to the lower part of the fuselage, rows of seats extending from one side to the other of the two-lobe body; a lower reinforcing beam (29) along the lower intersection line; and spaced posts (31), distributed in the rows of seats, linking the upper beam (28) to structural elements located in the lower region of the fuselage (32, 29). <??>Application to a high capacity aircraft in order to permit easy circulation of the passengers from one lobe into the other in accordance with aeronautical safety regulations. <IMAGE>

Inventors

• 👤 Jean Roeder
• 👤 Leslie James Geering

Bibliographic Details