Abstract: The invention relates to an cockpit floor (4) for an aircraft comprising a plurality of spars (14) extending along a longitudinal direction (X) of the aircraft and a plurality of cross-beams (16) assembled to said spars (14) and running along a transverse direction (Y) of the aircraft, the spars (14) and the cross-beams (16) forming a primary structure (12) of the floor (14), the floor also comprising attachment means (64) used to assemble it to the aircraft fuselage. According to the invention, the attachment means comprise a plurality of rods (68) resisting forces applied along the longitudinal (X), each of the rods (68) having an aft end connected to the main structure and a forward end that will be connected to said fuselage, such that each rod is oriented such that its distance from the centre of the floor increases towards the forward end.

Abstract: This invention relates to a floor (4) for an aircraft, and 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) for assembly onto a sealed bottom (68) of the aircraft. According to the invention, the attachment means comprise a plurality of fasteners (66) each comprising at least one junction element with two opposite ends, each of the two opposite ends being articulated about an axis parallel to the (Y) direction.

Abstract: 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.

Abstract: 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.

Abstract: The invention relates to an cockpit floor (4) for an aircraft comprising a plurality of spars (14) extending along a longitudinal direction (X) of the aircraft and a plurality of cross-beams (16) assembled to said spars (14) and running along a transverse direction (Y) of the aircraft, the spars (14) and the cross-beams (16) forming a primary structure (12) of the floor (14), the floor also comprising attachment means (64) used to assemble it to the aircraft fuselage. According to the invention, the attachment means comprise a plurality of rods (68) resisting forces applied along the longitudinal (X), each of the rods (68) having an aft end connected to the main structure and a forward end that will be connected to said fuselage, such that each rod is oriented such that its distance from the centre of the floor increases towards the forward end.

Abstract: This invention relates to a floor (4) for an aircraft, and 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) for assembly onto a sealed bottom (68) of the aircraft. According to the invention, the attachment means comprise a plurality of fasteners (66) each comprising at least one junction element with two opposite ends, each of the two opposite ends being articulated about an axis parallel to the (Y) direction.