| 摘要 |
The invention relates to an aircraft floor ( 4 ), preferably a cockpit floor, this floor comprising a plurality of spars ( 14 ) running along a longitudinal direction (X) of the aircraft and a plurality of cross-beams ( 16 ) assembled to the spars and running along a transverse direction (Y) of the aircraft, the floor also comprising attachment means ( 64 ) used to assemble it to fuselage frames. According to the invention, the attachment means comprise a plurality of articulations ( 66 ) each connected to one end of one of the cross-beams ( 16 ), and enabling rotation about the (X) direction.
|
