An aircraft including a main landing gear compartment which comprises a rear transverse wall, and a base wall forming a sealed barrier between a first, pressurized area and a second, non-pressurized area. The main landing gear compartment includes a body, produced in a single piece from composite material, separating the first, pressurized area and the second, non-pressurized area. The body includes a first part corresponding to the base wall, as well as a second part corresponding to the rear transverse wall. At least two longitudinal beams made of composite material, are connected to the body. This single body makes it possible to eliminate a large number of parts, to simplify the assembly process, and to reduce the duration thereof.
AÉRONEF COMPRENANT UNE CASE DE TRAIN D'ATTERRISSAGE PRINCIPALE PRÉSENTANT UNE COQUE RÉALISÉE D'UN SEUL TENANT
AIRCRAFT INCLUDING A MAIN LANDING GEAR BOX HAVING A SHELL MADE IN A SINGLE PIECE
LUFTFAHRZEUG MIT EINEM HAUPTFAHRWERKSKASTEN, DER EINE AUS EINEM STÜCK GEFERTIGTE SCHALE AUFWEIST
2024-06-12
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2023
|AÉRONEF COMPRENANT UNE CASE DE TRAIN D'ATTERRISSAGE PRINCIPALE RENFORCÉE
Europäisches Patentamt | 2024
|Aéronef comprenant une case de train d’atterrissage principale renforcée
Europäisches Patentamt | 2022
|Europäisches Patentamt | 2024
|Europäisches Patentamt | 2022
|