A landing gear of an aircraft, including a strut including two arms forming a rotational axis for retracting the gear, a rotating tube mounted in a mobile manner such that it rotates inside the strut about a pivoting axis, a sliding rod that is mobile in a translatory manner in the rotating tube along the pivoting axis, and carries wheels of the gear at one of its ends, and at least one bearing point that is located on one of the elements of the gear at a distance from the retraction axis and can bear necessary efforts for the retraction, the bearing point being located on the rotating tube.
TRAIN AVANT D'AERONEF A DISPOSITIF DE COMMANDE UNIQUE POUR LE RELEVAGE ET LA DIRECTION
NOSE LANDING GEAR WITH ACTUATING DEVICE FOR GEAR RETRACTION AS WELL AS FOR THE STEERING
BUGFAHRWEK MIT STELLVORRICHTUNG, WELCHE SOWOHL DAS EINFAHREN DES FAHRWEKS ALS AUCH DESSEN LENKUNG BEWERKSTELLIGT
2016-04-20
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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