Floor for aircraft

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Reexamination Certificate

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Reexamination Certificate

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11142320

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.

REFERENCES:
patent: 3155348 (1964-11-01), Ricard
patent: 3405893 (1968-10-01), Rajau et al.
patent: 4674712 (1987-06-01), Whitener et al.
patent: 5086996 (1992-02-01), Roeder et al.
patent: 5222694 (1993-06-01), Smoot
patent: 5586391 (1996-12-01), Micale
patent: 531357 (1941-01-01), None

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