| 摘要 |
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.
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