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.
ATTERRISSEUR D'AERONEF A PARTIE INFERIEURE ORIENTABLE ET DISPOSITIF D'ORIENTATION SIMPLIFIE
AIRCRAFT LANDING GEAR WITH ADJUSTABLE LOWER PORTION AND SIMPLIFIED DIRECTING DEVICE
FAHRWERK EINES LUFTFAHRZEUGS MIT AUSRICHTBAREM UNTEREN TEIL, UND VEREINFACHTE AUSRICHTVORRICHTUNG
02.06.2021
Patent
Elektronische Ressource
Französisch
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