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
2021-06-02
Patent
Electronic Resource
French
ATTERRISSEUR D'AERONEF A PARTIE INFERIEURE ORIENTABLE ET DISPOSITIF D'ORIENTATION SIMPLIFIE
European Patent Office | 2021
|ATTERRISSEUR D'AERONEF A PARTIE INFERIEURE ORIENTABLE ET DISPOSITIF D'ORIENTATION SIMPLIFIE
European Patent Office | 2020
|ATTERRISSEUR D'AERONEF MUNI D'UNE PARTIE INFERIEURE ORIENTABLE
European Patent Office | 2015
|ATTERRISSEUR D'AERONEF MUNI D'UNE PARTIE INFERIEURE ORIENTABLE
European Patent Office | 2015
|Procédé de gestion d'une commande d'orientation d'une partie orientable d'un atterrisseur d'aéronef
European Patent Office | 2019
|