An aircraft undercarriage includes a steerable bottom portion carrying one or more wheels and fitted with a steering device configured to turn the steerable bottom portion in response to a steering order. The steering device has a single electromechanical steering actuator having a steering electric motor driving, by a reduction gearing, an outlet pinion on an axis of the steering electric motor. The outlet pinion cooperates with a spur gear secured to the steerable bottom portion. A connection between the steering electric motor and the steerable bottom portion is reversible. The electromechanical steering actuator is fitted with a monitor configured to monitor at least one operating parameter of the steering device and to detect an actuator performance deterioration condition.


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    Title :

    ATTERRISSEUR D'AERONEF A PARTIE INFERIEURE ORIENTABLE ET DISPOSITIF D'ORIENTATION SIMPLIFIE


    Additional title:

    AIRCRAFT LANDING GEAR WITH ADJUSTABLE LOWER PORTION AND SIMPLIFIED DIRECTING DEVICE
    FAHRWERK EINES LUFTFAHRZEUGS MIT AUSRICHTBAREM UNTEREN TEIL, UND VEREINFACHTE AUSRICHTVORRICHTUNG


    Contributors:

    Publication date :

    2021-06-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / F16H Getriebe , GEARING



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