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).


    Access

    Download


    Export, share and cite



    Title :

    LOAD ABSORBING TIE ROD FOR AIRCRAFT STRUCTURE INTEGRATION


    Additional title:

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


    Contributors:

    Publication date :

    2023-10-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    LOAD ABSORBING TIE ROD FOR AIRCRAFT STRUCTURE INTEGRATION

    PALLE JOHN WYCLIFFE | European Patent Office | 2023

    Free access

    LOAD ABSORBING MEMBER AND VEHICLE LOAD ABSORBING STRUCTURE

    MATSUO YASUHIDE / KAGAMI AYAKA / MATSUI HATSUMI et al. | European Patent Office | 2021

    Free access

    Load absorbing member and vehicle load absorbing structure

    MATSUO YASUHIDE / KAGAMI AYAKA / MATSUI HATSUMI et al. | European Patent Office | 2022

    Free access


    LOAD ABSORBING STRUCTURE FOR VEHICLE

    European Patent Office | 2023

    Free access