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.


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    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 :

    01.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AIRCRAFT ENGINE WITH EXHAUST HAVING REMOVABLE DEFLECTOR

    LEFEBVRE GUY / GOVER CHRISTOPHER | Europäisches Patentamt | 2024

    Freier Zugriff

    Exhaust Flow Deflector

    J. C. Wilson / C. S. Shaw | NTIS | 1974



    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