In the field of aeronautics, there is disclosed an aircraft with reduced installation noise and specifically an aircraft wing and jet engine system including an aircraft wing and at least one jet engine with high bypass ratio attached to the wing, suitable for emitting a jet intercepted by a first portion of the trailing edge of the wing. The range formed by the set of angles with orientation α defined by a vector following the direction of the jet and by a vector following the tangent at a point of the first portion of the trailing edge and oriented towards the wing tip of the wing, is included within a range of angles selected from the range delimited by 5° and 65°, and the range delimited by 115° and 175°.


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    Titel :

    SYSTEME DE REDUCTION DU BRUIT D'INSTALLATION D'UNE AILE D'AVION


    Weitere Titelangaben:

    SYSTEM FOR REDUCING THE NOISE OF AN AEROPLANE WING INSTALLATION
    SYSTEM ZUR GERÄUSCHREDUZIERUNG EINER FLUGZEUGFLÜGELANLAGE


    Beteiligte:
    JORDAN PETER (Autor:in) / CAVALIERI ANDRÉ (Autor:in) / WOLF WILLIAM (Autor:in) / PIANTANIDA SELENE (Autor:in) / JAUNET VINCENT (Autor:in) / HUBER JÉRÔME (Autor:in)

    Erscheinungsdatum :

    2019-12-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

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



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