The invention relates to a cabin floor (2) suitable for being installed horizontally in a peripheral fuselage segment of an aircraft, said cabin floor (2) comprising a first planar structural portion (21) and a second planar structural portion (22), each portion (21, 22) comprising a linking end (23) and an attachment end (24), the attachment ends (24) being suitable for being attached to said fuselage segment, the cabin floor (2) being characterised in that the linking ends (23) of said first portion (21) and said second portion (22) are pivotably connected to one another so as to be able to switch between a folded state, in which the two portions (21, 22) are not aligned, and an unfolded state, in which the two portions (21, 22) are aligned.
PLANCHER DE CABINE POUR AERONEF ET PROCEDE DE MONTAGE D'UN TEL PLANCHER
CABIN FLOOR FOR AIRCRAFT AND METHOD FOR INSTALLING SUCH A FLOOR
KABINENBODEN FÜR FLUGZEUGE UND VERFAHREN ZUM EINBAU SOLCH EINES BODENS
2019-01-09
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
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