The invention relates to a landing gear (10) comprising a supporting structure (11, 12, 13), and a damping cylinder (15) connected to a lever (17) which is hinged to the supporting structure about a hinge axis (A3) between an end position, in which the wheel is moved towards the hinge axis, and an end position, in which the wheel is moved away from the hinge axis, the end positions being on either side of an intermediate position, in which the lever and the cylinder are aligned, and the end away position being defined by a stop (21) which is secured to the supporting structure and against which the lever in the away position is applied to take up the landing forces. The invention also relates to an aircraft comprising at least one such landing gear.
ATTERRISSEUR A LONGUEUR VARIABLE ET AÉRONEF ÉQUIPÉ D'UN TEL ATTERRISSEUR
VARIABLE-LENGTH LANDING GEAR AND AIRCRAFT EQUIPPED WITH SUCH A LANDING GEAR
LÄNGENVERÄNDERLICHES FAHRWERK UND MIT EINEM SOLCHEN FAHRWERK AUSGESTATTETES FLUGZEUG
2024-12-25
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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