Systems and methods for folding landing gear of a cargo aircraft. One embodiment is a main landing gear of an aircraft that includes a shock strut coupled to a truck with one or more wheels, and a yoke pivotally coupled with the shock strut via a lower trunnion, and pivotally coupled with an aircraft structure via an upper trunnion. The yoke is configured to pivot about the upper trunnion in a direction back toward a tail of the aircraft and up toward a fuselage of the aircraft, and the shock strut is configured to pivot about the lower trunnion in a direction forward toward a nose of the aircraft and up toward the fuselage of the aircraft to retract the one or more wheels.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Folding main landing gear for cargo aircraft


    Beteiligte:

    Erscheinungsdatum :

    15.03.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    FOLDING MAIN LANDING GEAR FOR CARGO AIRCRAFT

    COTTET JUSTIN DUANE | Europäisches Patentamt | 2020

    Freier Zugriff

    PIVOTING MAIN LANDING GEAR FOR CARGO AIRCRAFT

    COTTET JUSTIN DUANE | Europäisches Patentamt | 2020

    Freier Zugriff

    Pivoting main landing gear for cargo aircraft

    COTTET JUSTIN DUANE | Europäisches Patentamt | 2022

    Freier Zugriff

    LANDING GEAR FOR CARGO AIRCRAFT

    SCHMIDT GREGORY M / COTTET JUSTIN DUANE | Europäisches Patentamt | 2020

    Freier Zugriff

    Landing gear for cargo aircraft

    SCHMIDT GREGORY M / COTTET JUSTIN DUANE | Europäisches Patentamt | 2022

    Freier Zugriff