A retractable landing gear for an aircraft. The landing gear comprises a rocker arm hinged to a structure of the aircraft and carrying at least one wheel that is able to move between a deployed position and a retracted position, a shock-absorber hinged to the structure, a connecting rod connecting the rocker arm and the shock-absorber, a strut provided with two connecting links that are hinged to each other and respectively hinged to shock-absorber and connected to an actuator fastened to the structure. The connecting rod is out of alignment with the shock-absorber when a force applied to the shock-absorber is less than a predetermined force, and the landing gear comprises a locking device provided with an elastic return member and a stop device for locking the strut when the wheel is in the deployed position, and then for securing the wheel in the deployed position.
ATTERRISSEUR À BALANCIER RETRACTABLE MUNI D'UN MOTEUR ÉLECTRIQUE ET AÉRONEF MUNI D'AU MOINS UN TEL ATTERRISSEUR
RETRACTABLE LANDING GEAR PROVIDED WITH A TRAILING LINK AND AN ELECTRIC MOTOR, AND AN AIRCRAFT PROVIDED WITH AT LEAST ONE SUCH LANDING GEAR
EINZIEHFAHRWERK MIT EINER GESCHLEPPTEN LENKERACHSE UND EINEM ELEKTROMOTOR, UND EIN LUFTFAHRZEUG MIT MINDESTENS EINEM SOLCHEN FAHRWERK
25.06.2025
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2024
|atterrisseur pivotable muni d’un système d’immobilisation
Europäisches Patentamt | 2025
|