An aircraft pressurized cabin door (1) having an outer panel (2) and a door structure (3) including: two circumferential beams (4) fastened to the lateral edges of the door; a plurality of longitudinal beams (5a, 5b) which are arranged substantially perpendicularly between the circumferential beams (4) and are fastened to the outer panel (2), each longitudinal beam (5a, 5b) extending from one circumferential beam (4) to the other. At least one longitudinal beam (5b) is a beam that has a variable cross-section which increases from the ends (B, M) of the beam to the center (H, L) of the beam, with two bent support bars.
PORTE DE CABINE PRESURISEE D'AERONEF A STRUCTURE FORMEE DE POUTRES A SECTION EVOLUTIVE
AIRCRAFT PRESSURIZED CABIN DOOR WITH A STRUCTURE FORMED BY BEAMS HAVING A VARYING CROSS-SECTION
FLUGZEUGDRUCKKABINENTÜR MIT EINER STRUKTUR; DIE AUS TRÄGERN MIT UNTERSCHIEDLICHEM QUERSCHNITT GEBILDET IST
2024-01-10
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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