A wing comprising a fixed main part and a leading edge slat with upper and lower surface rear edges. The wing main part has an upper surface wall, which extends downstream and in alignment with the upper surface rear edge, and a lower surface wall, which extends downstream and in alignment with the lower surface rear edge. The wing has an upper surface gap between the end of the upper surface rear edge and the end of the upper surface wall and a lower surface gap between the end of the lower surface rear edge and the end of the lower surface wall. The wing has an upper surface channel downstream of the upper surface gap and a lower surface channel downstream of the lower surface gap. The wing comprises a suction system connected to each channel and arranged to suck the air contained in the channel.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AILE COMPORTANT UN BEC DE BORD D'ATTAQUE ET PRESENTANT DES MOYENS POUR PREVENIR LE PASSAGE A UNE COUCHE LIMITE TURBULENTE


    Weitere Titelangaben:

    WING WITH A LEADING EDGE SPOUT AND MEANS FOR PREVENTING THE PASSAGE TO A TURBULENT BOUNDARY LAYER
    FLÜGEL MIT EINEM VORDERKANTENAUSLAUF UND MITTELN ZUM VERHINDERN DES ÜBERGANGS ZU EINER TURBULENTEN GRENZSCHICHT


    Beteiligte:

    Erscheinungsdatum :

    04.03.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge