Plane with stressed-skin fuselage and floor structure

摘要

The aircraft has two rods (4a, 4b) provided for connecting a fuselage shell (10) and a floor structure (1), where the rods are longitudinally movable. The rods are connected with a cross beam (2) of the floor structure, and run in a transverse direction of the aircraft. The rod (4a) is arranged at a shell frame (11) of the fuselage shell. The rod (4b) runs in a pointed angle to an aircraft transverse direction. A third rod runs below the floor structure in right angle to the floor structure.