The invention concerns an aircraft propulsion system (100) comprising a turbojet (102) having a fan casing (103) with a rear face (103a), a pylon (104) with a front part (106a) and a lower spar (106b) with a rear fitting (108) fixed to it, and a front engine attachment (150) fixed between an upper part of the fan casing (103) and the front part (106a), a front arch (152) having two arms (152b-c), each having a first end fixed to the lower spar (106b) and a second end fastened in an articulated manner to the rear face (103a), and two lateral rods (154), each having a first end fastened in an articulated manner to the rear fitting (108) and a second end fastened in an articulated manner to the rear face (103a).With such an arrangement, the forces are transmitted to the rear of the pylon.


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    Titel :

    PROPULSION SYSTEM FOR AN AIRCRAFT COMPRISING A TURBOJET, A PYLON AND ENGINE ATTACHMENT


    Weitere Titelangaben:

    ANTRIEBSSYSTEM FÜR EIN FLUGZEUG MIT EINEM STRAHLTRIEBWERK, EINEM PYLON UND EINER MOTORBEFESTIGUNG
    SYSTÈME DE PROPULSION POUR AÉRONEF COMPRENANT UN TURBORÉACTEUR, UN MÂT ET UNE ATTACHE MOTEUR


    Beteiligte:

    Erscheinungsdatum :

    08.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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