A landing gear system comprises a bogie beam, a landing gear axle pivotally mounted to the bogie beam, a steering rack, a linear actuator assembly, and a steering control link. The steering rack is secured transversely to the bogie beam and is longitudinally spaced apart from the landing gear axle. The linear actuator assembly is operable to laterally translate the steering rack. The steering control link is longitudinally extendable and has an actuator end secured to the steering rack, and an axle end of the steering control link engaged with the landing gear axle. The steering control link and the landing gear axle are pivotable relative to the bogie beam about a common axis.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    MAIN LANDING GEAR COMPACT AXLE STEERING


    Weitere Titelangaben:

    DIRECTION COMPACTE POUR TRAIN D'ATTERRISSAGE PRINCIPAL


    Beteiligte:
    MARTIN DENNIS W (Autor:in) / ACKS JAMES (Autor:in)

    Erscheinungsdatum :

    2020-09-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Main landing gear compact axle steering

    MARTIN DENNIS W / ACKS JAMES | Europäisches Patentamt | 2020

    Freier Zugriff

    Main landing gear compact axle steering

    MARTIN DENNIS W / ACKS JAMES | Europäisches Patentamt | 2016

    Freier Zugriff

    MAIN LANDING GEAR BIAS AXLE STEERING

    MARTIN DENNIS W / ACKS JAMES | Europäisches Patentamt | 2021

    Freier Zugriff

    Main landing gear bias axle steering

    MARTIN DENNIS W / ACKS JAMES | Europäisches Patentamt | 2023

    Freier Zugriff

    LANDING GEAR WITH STEERABLE AXLE

    BENNETT IAN / MENEZES ROBERT / SHAW PAUL | Europäisches Patentamt | 2018

    Freier Zugriff