An aircraft engine, comprising a thermal engine, an axial turbine having a turbine inlet, and an exhaust assembly fluidly connecting the thermal engine to the axial turbine. The exhaust assembly includes a housing and a deflector removably mounted within the housing. The deflector has circumferentially distributed vanes. The deflector is a first deflector, having a first set of geometric characteristics, that is removable from the housing and replaceable by a second deflector having a second set of geometric characteristics different from the first set of geometric characteristics. The first deflector is one of a first class of deflectors and the second deflector is one of a second class of deflectors, the first and second class of deflectors respectively defining first and second exhaust flow profiles that differ from each other.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT ENGINE WITH EXHAUST HAVING REOVABLE DEFLECTOR


    Weitere Titelangaben:

    MOTEUR D'AERONEF COMPRENANT UN ECHAPPEMENT A DEFLECTEUR AMOVIBLE


    Beteiligte:
    LEFEBVRE GUY (Autor:in) / GOVER CHRISTOPHER (Autor:in)

    Erscheinungsdatum :

    2024-06-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02B INTERNAL-COMBUSTION PISTON ENGINES , Brennkraftmaschinen mit innerer Verbrennung mit Verdrängerwirkung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT ENGINE WITH EXHAUST HAVING REMOVABLE DEFLECTOR

    LEFEBVRE GUY / GOVER CHRISTOPHER | Europäisches Patentamt | 2024

    Freier Zugriff


    Vertical take-off and landing (VTOL) aircraft with exhaust deflector

    LAUDER TIMOTHY FRED | Europäisches Patentamt | 2018

    Freier Zugriff

    VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT WITH EXHAUST DEFLECTOR

    LAUDER TIMOTHY FRED | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft anti-icing systems having deflector vanes

    JOHNSON RICK A / PHAM VICTOR D / GALLY DANIEL H et al. | Europäisches Patentamt | 2019

    Freier Zugriff