Ejector (1) for load (2), including a guide means (4), including: a first top rod (BS1), a first bottom rod (BI1), the first top rod (BS1) being hinged with the aircraft (3) at a first top hinge (AS1), and with the first bottom rod (BI1) at a first median hinge (AM1), the first bottom rod (BI1) being hinged with the load (2) at a first bottom hinge (AI1), the axes of the first three hinges (AS1, AM1, AI1) being parallel, a second top rod (BS2), a second bottom rod (BI2), the second top rod (BS2) being hinged with the aircraft (3) at a second top hinge (AS2), and with the second bottom rod (BI2) at the second median hinge (AM2), the second bottom rod (BI2) being hinged with the load (2) at a second bottom hinge (AI2), the axes of the second three hinges (AS2, AM2, AI2) being parallel, and a synchronization means (5) suitable for copying, by applying a gain thereto, the angle of the first top hinge (AS1) to the angle of the first median hinge (AM1), suitable for copying, by applying a gain thereto, the angle of the second top hinge (AS2) to the angle of the second median hinge (AM2) and suitable for copying, by applying a gain thereto, the angle of the first top hinge (AS1) to the angle of the second top hinge (AS2).


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    Titel :

    DISPOSITIF DE GUIDAGE POUR EJECTEUR


    Weitere Titelangaben:

    EJECTOR GUIDE DEVICE
    AUSWERFERFÜHRUNGSVORRICHTUNG


    Beteiligte:
    GUARALDO DENIS (Autor:in)

    Erscheinungsdatum :

    01.04.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

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



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