The present invention relates to an aircraft including a fuselage and a thruster downstream of the fuselage. The thruster includes a power turbine, located inside a main flow jet, and at least one fan, located inside a secondary flow jet and mechanically driven by the power turbine. The main flow jet of the power turbine and the secondary flow jet of the fan are concentric. The power turbine is supplied with gases from two gas turbine gas generators via two supply channels. The gas turbine gas generators have axes parallel to that of the fuselage. The air inlet sleeve is spaced apart from the fuselage, and the supply channels each have a hatch for controlling the flow between a position for guiding the gas flow to the power turbine and a position for ejecting the gases into the atmosphere while bypassing the power turbine.


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    Title :

    AERONEF AVEC UN ENSEMBLE PROPULSIF COMPRENANT UNE SOUFFLANTE A L'ARRIERE DU FUSELAGE


    Additional title:

    AIRCRAFT COMPRISING A PROPULSION ASSEMBLY INCLUDING A FAN ON THE REAR OF THE FUSELAGE
    FLUGZEUG MIT EINER ANTRIEBSANORDNUNG MIT EINEM GEBLÄSE AM HINTEREN TEIL DES RUMPFES


    Contributors:

    Publication date :

    2020-01-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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    TANTOT NICOLAS JEROME JEAN | European Patent Office | 2020

    Free access

    AERONEF AVEC UN ENSEMBLE PROPULSIF COMPRENANT UNE SOUFFLANTE A L'ARRIERE DU FUSELAGE

    TANTOT NICOLAS JÉRÔME JEAN | European Patent Office | 2017

    Free access

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    REIGNER PIERRE-ALAIN JEAN PHILIPPE / BEAUJARD ANTOINE JEAN-PHILIPPE / CURLIER AUGUSTIN MARC MICHEL | European Patent Office | 2017

    Free access