An aerodynamic aircraft wall has external and internal surfaces and is equipped with at least one vortex generator. The vortex generator has at least one active wall projecting with respect to the external surface of the aerodynamic wall and a connecting system connecting the vortex generator to the aerodynamic wall. The connecting system includes at least one support in part pressed firmly against the internal surface of the aerodynamic wall, at least one first fastener connecting the support and the active wall, and at least one second fastener connecting the support and the aerodynamic wall and having a head flush with the external surface of the aerodynamic wall.


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    Titel :

    AERODYNAMIC AIRCRAFT WALL COMPRISING AT LEAST ONE VORTEX GENERATOR, AND AIRCRAFT COMPRISING THE SAID AERODYNAMIC WALL


    Beteiligte:
    KRIER ERWAN (Autor:in) / DE OLIVEIRA GRÉGORY (Autor:in) / BOURDIEU THOMAS (Autor:in) / BAS ADRIEN (Autor:in)

    Erscheinungsdatum :

    05.12.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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