A retractable landing gear system configured to contour an aircraft fuselage includes a landing wheel having an axle, a wheel rotation strut assembly coupling the landing wheel to the aircraft fuselage and an actuation strut assembly configured to move the wheel rotation strut assembly between various positions including a deployed position and a stowed position. The axle of the landing wheel is pivotably coupled to a distal end of the wheel rotation strut assembly and configured to pivot relative to the wheel rotation strut assembly as the actuation strut assembly moves the wheel rotation strut assembly between the deployed and stowed positions such that the landing wheel generally contours the aircraft fuselage when the wheel rotation strut assembly is in the stowed position.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Contouring retractable landing gear systems


    Beteiligte:

    Erscheinungsdatum :

    27.07.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Contouring Retractable Landing Gear Systems

    ISAAC MARK LORING / KOOIMAN JAMES EVERETT / HOGUE CHARLES DAVID | Europäisches Patentamt | 2021

    Freier Zugriff

    RETRACTABLE LANDING GEAR

    LUCE WILLIAM E | Europäisches Patentamt | 2018

    Freier Zugriff

    Retractable landing gear

    LUCE WILLIAM E | Europäisches Patentamt | 2019

    Freier Zugriff

    RETRACTABLE LANDING GEAR

    LUCE WILLIAM E | Europäisches Patentamt | 2016

    Freier Zugriff

    Retractable landing gear

    LUCE WILLIAM E | Europäisches Patentamt | 2018

    Freier Zugriff