The landing gear for a Piper Cub® light aircraft, comprises at least two wheels, is attached to a part of the fuselage in front of the center of gravity, and has a fixed tubular reinforcement that is generally triangular in shape, of which the apex is turned downwards, the ends of the base of the reinforcement and the apex of same being coupled, with articulation capability, to a suspension system linked to the wheels. Each end of the base of the reinforcement is angularly coupled to a wheel, by means of a damping member, while the apex of said reinforcement is coupled symmetrically to each of the wheels, by means of a connecting rod.
TRAIN D'ATTERRISSAGE POUR AVION LEGER, COMPRENANT AU MOINS DEUX ROUES
LANDING GEAR FOR LIGHT AIRCRAFT, COMPRISING AT LEAST TWO WHEELS
FAHRWERK FÜR LEICHTFLUZEUG MIT MINDESTENS ZWEI RÄDERN
2020-08-05
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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