Vertical take-off and landing (VTOL) aircraft of the fixed-wing type, comprising a centre section defining a centreline of the aircraft, and a pair of wings, arranged on either side of the centre section, wherein the wings extend longitudinally from the centre section away from and mutually symmetrical with respect to a plane of symmetry extending through the centreline, wherein each wing comprises a main wing section extending longitudinally from the centre section, wherein the main wing section is configured for generating lift in an upward direction, a wingtip section extending longitudinally from the main wing section in a downwards sloping manner with respect to the main wing section, and a control surface provided in the wingtip section.


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    Titel :

    FIXED-WING AIRCRAFT


    Weitere Titelangaben:

    STARRFLÜGELFLUGZEUG
    AÉRONEF À VOILURE FIXE


    Beteiligte:

    Erscheinungsdatum :

    30.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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