An aircraft has an upper portion and a lower portion provided with a first and second axle. The first axle is provided with a braked wheel and the second axle is provided with a motorized wheel. A landing gear of the aircraft includes a main arm pivoting with respect to the strut on which the first axle is fixed. The second axle is fixed on the strut, and a main actuator moves the first axle between a remote position and a close position with respect to the upper portion. In the close position, the braked and motorized wheels are simultaneously in contact against a running plane, and in the remote position, the braked wheels are in contact against the running plane while the motorized wheel is at a distance from the running plane.
ATTERRISSEUR D'AÉRONEF DOTÉ D'AU MOINS UNE ROUE MOTORISÉE
AIRCRAFT LANDING GEAR WITH AT LEAST ONE MOTORISED WHEEL
FAHRWERK EINES FLUGZEUGS MIT MINDESTENS EINEM ANGETRIEBENEN RAD
12.02.2025
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
Atterrisseur d’aéronef doté d’au moins une roue motorisée
Europäisches Patentamt | 2023
|Atterrisseur d’aéronef doté d’au moins une roue motorisée
Europäisches Patentamt | 2022
|ATTERRISSEUR D'AERONEF DOTE D'AU MOINS UNE ROUE MOTORISEE
Europäisches Patentamt | 2021
|ATTERRISSEUR D'AERONEF DOTE D'AU MOINS UNE ROUE MOTORISEE
Europäisches Patentamt | 2023
|ATTERRISSEUR D'AERONEF DOTE D'AU MOINS UNE ROUE MOTORISEE
Europäisches Patentamt | 2022
|