A structural assembly for an aircraft having pairs of main gantries distributed in the longitudinal direction, two transverse panels fixed to the front and the rear of the pairs of main gantries to together define a compartment for a landing gear of the aircraft, at least one pair of secondary gantries between the main gantries, at least one crossmember parallel to the transverse panels and that straddles at least one secondary gantry, and, for each secondary gantry and each crossmember straddling the secondary gantry, a connecting rod mounted to be able to freely rotate, via a first end, on a lower part of the crossmember and, via a second end, on an outer lateral part of the secondary gantry. Such an arrangement reduces the vertical bulk of the structural assembly.


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    Titel :

    STRUCTURAL ASSEMBLY FOR AN AIRCRAFT


    Beteiligte:
    ORTEU BENOIT (Autor:in) / MIL LUDOVIC (Autor:in) / LAGANIER LIONEL (Autor:in) / MARTY DOMINIQUE (Autor:in) / ROBERT PHILIPPE (Autor:in)

    Erscheinungsdatum :

    2023-05-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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