The invention relates to a propulsion assembly comprising a motorized device (32), a pylon (34), an engine attachment system (46, 46.1, 46.2) connecting a front part (40.1) of the motorized device (32) and the pylon (34), and a suspension system (48) connecting the pylon (34) and a rear part (40.2) of the motorized device (32), the suspension system (48) being offset relative to the engine attachment system (46) towards a rear end (E2) of the motorized device (32). In the event of a failure, if the rear part (40.2) is separated from the front part (40.1), the rear part (40.2) remains connected to the hanger (34) without falling off.

    本发明涉及一种推进组件,其包括机动装置(32)、吊架(34)、连接机动装置(32)的前部部件(40.1)和吊架(34)的发动机附接件系统(46、46.1、46.2)以及连接吊架(34)和机动装置(32)的后部部件(40.2)的悬挂系统(48),悬挂系统(48)相对于发动机附接件系统(46)朝机动装置(32)的后端(E2)偏移。在发生故障的情况下,如果后部部件(40.2)与前部部件(40.1)分离,该后部部件(40.2)保持连接至吊架(34)而不会掉落。


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    Titel :

    Propulsion device and aircraft comprising at least one such propulsion device


    Weitere Titelangaben:

    推进装置及包括至少一个这种推进装置的飞行器


    Beteiligte:
    BERJOT MICHAEL (Autor:in) / LANCIAUX R ¨ (Autor:in) / MI (Autor:in) / VENES JEAN-BAPTISTE (Autor:in)

    Erscheinungsdatum :

    07.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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