Nacelle air management systems for a high bypass ratio engine are provided. The nacelles air management systems may include an outer cowl and an inner cowl that are configured to provide dual bypass flow channels around an engine core. These systems may be employed to accommodate larger engine fans. The nacelle air management system may also include one or more blocker doors are configured to at least partial obstruct and/or direct air from the dual bypass flow channels to create reverse thrust.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Nacelle for a high bypass ratio engine with multiple flow paths


    Beteiligte:
    JAMES NORMAN J (Autor:in) / RITCHIE KEITH (Autor:in) / SCOTT THOMAS W (Autor:in)

    Erscheinungsdatum :

    18.04.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AIRCRAFT BYPASS TURBOJET ENGINE NACELLE

    GONIDEC PATRICK / BELLANGER ALEXANDRE | Europäisches Patentamt | 2016

    Freier Zugriff


    Nacelle for a bypass turbofan engine

    GONIDEC PATRICK / BELLANGER ALEXANDRE | Europäisches Patentamt | 2016

    Freier Zugriff

    Nacelle for an aircraft bypass turbojet engine

    HURLIN HERVE / KERBLER OLIVIER / GILO OLIVIER | Europäisches Patentamt | 2016

    Freier Zugriff

    CFD Design for Bypass Ratio 15 Nacelle Integration

    Milholen, William E., II | NTRS | 2001