A system is provided for an aircraft (20). This aircraft system includes an aircraft wing (24) extending spanwise from a wing base (36) to a wing tip (34). The aircraft wing (24) extends chordwise from a leading edge (42) to a trailing edge (44). The aircraft wing (24 extends laterally between a first surface (46) and a second surface (48). The aircraft wing (24) includes a first section (50), a second section (52) and a third section (54). The second section (52) extends spanwise between and connects the third section (54) and the first section (50). The second section (52) is pivotally connected to first section (50) at a first hinge line (56). The third section (54) is pivotally connected to the second section (52) at a second hinge line (58) that is angularly offset from the first hinge line (56) by a first acute angle (62).


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    Titel :

    FOLDING WINGS FOR AN AIRCRAFT


    Weitere Titelangaben:

    FALTFLÜGEL FÜR EIN FLUGZEUG
    AILE PLIABLE POUR UN AÉRONEF


    Beteiligte:
    HABCHI JASON (Autor:in) / LE CAITLIN (Autor:in) / BARRAZA PAUL (Autor:in) / KESTLER STEVEN (Autor:in) / GHANDOUR IMAD D (Autor:in)

    Erscheinungsdatum :

    2024-08-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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