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°.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

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


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

    Erscheinungsdatum :

    07.12.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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

    JORDAN PETER / CAVALIERI ANDRÉ / WOLF WILLIAM et al. | Europäisches Patentamt | 2016

    Freier Zugriff

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

    JORDAN PETER / CAVALIERI ANDRÉ / WOLF WILLIAM et al. | Europäisches Patentamt | 2019

    Freier Zugriff


    VOILE DE PROPULSION A PROFIL EN AILE D'AVION

    DEBLED ANTOINE | Europäisches Patentamt | 2018

    Freier Zugriff

    VOILE DE PROPULSION A PROFIL EN AILE D'AVION

    DEBLED ANTOINE | Europäisches Patentamt | 2015

    Freier Zugriff