FUSELAGE SEGMENT FOR A FUSELAGE OF AN AIRCRAFT, AIRCRAFT FUSELAGE AND AIRCRAFT

摘要

A fuselage segment (12) for an aircraft fuselage comprises a wall (13) with a closed cross section, a first cabin floor (14), a second cabin floor (16), and a cargo hold floor (18). The first cabin floor (14), the second cabin floor (16), and the cargo hold floor (18) are vertically spaced apart from each other and connected to the wall (13). A first passenger region (22) is arranged above the first cabin floor (14), a second passenger region (24) is arranged above the second cabin floor (16), and a cargo region (20) is arranged above the cargo hold floor (18). The cargo region (20) is dimensioned in such a manner that for at least four passenger seats a maximum of 1m3 of cargo hold volume is provided. In this manner an existing aircraft fuselage can be designed in a demand-oriented manner so that it can accommodate two or more passenger regions.