To reduce the overall mass of an engine assembly for aircraft, this assembly comprises a part of the fuselage of an aircraft, a turbomachine comprising an unfaired propeller, together with an annular row of unfaired after-guide vanes located aft of the propeller and rotationally fixed in relation to a longitudinal axis of the turbomachine, and a mounting pylon. At least part of the leading edge of the pylon is incorporated within the annular row between two after-guide vanes.


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    Title :

    ENSEMBLE MOTEUR POUR AERONEF COMPRENANT UN BORD D'ATTAQUE DE MAT INTEGRE A UNE RANGEE ANNULAIRE D'AUBES DIRECTRICES DE SORTIE NON CARENEES


    Contributors:

    Publication date :

    2018-04-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



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