Aircraft pressurized cabin door (1) including an outer panel (2) and a door structure (3). The door structure (3) includes two circumferential beams (4) fastened to the lateral edges of the door (1); a plurality of longitudinal beams (5) arranged substantially perpendicularly between the circumferential beams (4) and fastened to the outer panel (2), each longitudinal beam (5) extending from one circumferential beam (4) to the other. Each longitudinal beam (5) is an open profile of which the opening (18) is directed toward the outer panel (2), this opening (18) being closed by the internal face of the outer panel (2) to which the longitudinal beam (5) is fastened. Each beam includes a structural redundancy element.
PORTE DE CABINE PRESSURISÉE D'AÉRONEF À STRUCTURE FORMÉE DE POUTRES
AIRCRAFT PRESSURIZED CABIN DOOR WITH A STRUCTURE FORMED BY BEAMS
DRUCKKABINENTÜR EINES FLUGZEUGS MIT EINER DURCH TRÄGER GEBILDETEN STRUKTUR
2023-02-15
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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