An aircraft assembly may comprise an interior aircraft monument, an aircraft structure, and a load absorbing tie rod coupled to the interior aircraft monument and the aircraft structure. The load absorbing tie rod may include an outer cylinder (126) coupled to the aircraft structure, a piston (128)located at least partially within the outer cylinder (126) and coupled to the interior aircraft monument, and a compressed gas located in a volume defined by the piston (128)and the outer cylinder (126).


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    Titel :

    LOAD ABSORBING TIE ROD FOR AIRCRAFT STRUCTURE INTEGRATION


    Weitere Titelangaben:

    LASTAUFNEHMENDE ZUGSTANGE ZUR INTEGRATION EINER FLUGZEUGSTRUKTUR
    TIRANT D'ANCRAGE ABSORBANT LA CHARGE POUR INTÉGRATION DE STRUCTURE D'AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    04.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16F SPRINGS , Federn



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