An aircraft with folding mechanism, the aircraft including a fuselage, optionally a payload and/or landing gear attached to the fuselage, at least two longitudinal beams attached to the fuselage that preferably extend parallel to each other and parallel to a first aircraft axis, with lifting units attached to each of the longitudinal beams. At least one crossbeam is attached to the fuselage, and preferably extending parallel to a second aircraft axis and at right angles with respect to the longitudinal beams, with lifting units attached to the crossbeam. The longitudinal beams are rotatably attached to the fuselage by at least one respective first pivot joint configured for pivoting the longitudinal beams around a respective first pivot axis to a pivoted position. The crossbeam is rotatably attached to the fuselage, preferably by at least one second pivot joint, for pivoting the crossbeam around a second pivot axis to a pivoted position.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft with folding mechanism


    Contributors:

    Publication date :

    2024-06-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    AIRCRAFT WITH FOLDING MECHANISM

    INFANTE AGUIRRE FRANCISCO JAVIER / HARMS MICHAEL | European Patent Office | 2022

    Free access

    AIRCRAFT WITH FOLDING MECHANISM

    HARMS MICHAEL / INFANTE AGUIRRE FRANCISCO JAVIER | European Patent Office | 2022

    Free access

    Aircraft with folding mechanism

    INFANTE AGUIRRE FRANCISCO JAVIER / HARMS MICHAEL | European Patent Office | 2022

    Free access

    Folding propeller mechanism of aircraft and aircraft

    LUO JUNCHANG / XU ZHAOHUA / SHA YONGXIANG et al. | European Patent Office | 2025

    Free access

    Folding wing mechanism for aircraft and aircraft

    SUN YINRUI / WANG LI / LIN FAPENG et al. | European Patent Office | 2024

    Free access