Floor structure in an aircraft with continuous panels

Details Floor structure in an aircraft with continuous panels Floor structure in an aircraft with continuous panels

B - Operations, Transporting

60

N

B60N 2/015 (2006.01) B64C 1/18 (2006.01) B64D 11/06 (2006.01)

Patent

CA 2636550

The present invention relates to a floor structure (1) in an aircraft, as well as to an aircraft that comprises such a floor structure (1). The floor structure (1) comprises a multitude of seat rails (2) that extend parallel in relation to each other, and at least one floor panel (3). The floor panel extends over the multitude of seat rails (2) and rests on the individual seat rails (2). In order to be able to fasten interior equipment components (6) to the seat rails (2) situated underneath the floor panels (3), the at least one floor panel (3) comprises a plurality of through-holes (5) through which the interior equipment components (6) of the aircraft can be locked into place on the seat rails (2).

La présente invention concerne une structure de plancher (1) dans un aéronef, ainsi qu'un aéronef qui comprend une telle structure de plancher (1). La structure de plancher (1) comprend une multitude de rails de siège (2) qui s'étendent parallèlement les uns par rapport aux autres, et au moins un panneau de plancher (3). Le panneau de plancher s'étend sur la multitude de rails de siège (2) et repose sur les rails de siège individuels (2). Afin de pouvoir fixer des composants d'équipement intérieur (6) aux rails de siège (2) situés en dessous des panneaux de plancher (3), le ou les panneaux de plancher (3) comprennent une pluralité de trous débouchants (5) à travers lesquels les composants d'équipement intérieur (6) de l'aéronef peuvent être verrouillés en place sur les rails de siège (2).

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