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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    Title :

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


    Contributors:

    Publication date :

    2019-12-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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