A structure for an aircraft is disclosed including a fixed part, a panel member which is an outer member of the structure, and a plurality of connection units. Each of the plurality of connection units connects the panel member to the fixed part in an articulated manner. The plurality of connection units collectively forms an iso-static connection between the panel member and the fixed part, so that the structure has an invariant geometry. A suspension system, an engine assembly, and an aircraft including the structure are also disclosed.


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    Titel :

    STRUCTURE, SUSPENSION SYSTEM, ENGINE ASSEMBLY AND AIRCRAFT


    Beteiligte:
    GUO LI (Autor:in) / HUANG YUKUN (Autor:in)

    Erscheinungsdatum :

    26.03.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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