An aircraft has an upper portion and a lower portion provided with a first and second axle. The first axle is provided with a braked wheel and the second axle is provided with a motorized wheel. A landing gear of the aircraft includes a main arm pivoting with respect to the strut on which the first axle is fixed. The second axle is fixed on the strut, and a main actuator moves the first axle between a remote position and a close position with respect to the upper portion. In the close position, the braked and motorized wheels are simultaneously in contact against a running plane, and in the remote position, the braked wheels are in contact against the running plane while the motorized wheel is at a distance from the running plane.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft landing gear with a motorized wheel selectively positionable relative to a landing gear strut


    Beteiligte:

    Erscheinungsdatum :

    05.08.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aircraft landing gear shock absorber strut

    IAN ROBERT BENNETT | Europäisches Patentamt | 2025

    Freier Zugriff

    AIRCRAFT LANDING GEAR SHOCK ABSORBER STRUT

    BENNETT IAN ROBERT | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft landing gear shock absorbing strut

    URBINATI SIMONE / HILLIARD MATT / SMITH JON | Europäisches Patentamt | 2020

    Freier Zugriff

    AIRCRAFT LANDING GEAR SHOCK ABSORBER STRUT

    BENNETT IAN ROBERT | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT LANDING GEAR SHOCK ABSORBER STRUT

    BENNETT IAN ROBERT | Europäisches Patentamt | 2022

    Freier Zugriff