An aircraft landing gear well roof including a first reinforced main structure and a second reinforced main structure spaced from each other in a transverse direction of the roof and equipped with respective mounting for articulating a structural element of the first landing gear and mounting for articulating a structural element of the second landing bear. A membrane connecting the first reinforced main structure and the second reinforced main structure is disposed between them in the transverse direction.


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    Titel :

    LANDING GEAR WELL ROOF


    Beteiligte:
    BELLET DANIEL (Autor:in) / GALLANT GUILLAUME (Autor:in) / LOYANT FRANÇOIS (Autor:in) / LEGARDEZ ALEXANDRE (Autor:in) / ROUX SIMON (Autor:in)

    Erscheinungsdatum :

    30.06.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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