The invention provides an alignment and safety device (20) for the cowls (11, 41) of the nacelle of an aircraft engine formed by first and second parts (23, 43) to be arranged opposite of each other at the lower edges of the cowls (11, 41) that comprise first and second alignment arms (31, 51) configured with a portion (33, 53) arranged to enter inside the inner space of the nacelle covered by the opposite cowl (41, 11). One of the parts (23, 43) comprises a blocking member (81) configured to be interposed between the cowls (11, 41) after being unlatched to facilitate their opening operation and also when they return to the closed position from an open position if they are misaligned to facilitate its alignment and subsequent latching applying a force F on the blocking member (81).


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    Titel :

    Alignment and safety device for the cowls of aircraft engine nacelles


    Weitere Titelangaben:

    Ausrichtungs- und Sicherheitsvorrichtung für die Hauben von Flugzeugtriebwerksgondeln
    Alignement et dispositif de sécurité pour les capots d'une nacelle de moteur d'aéronef


    Beteiligte:

    Erscheinungsdatum :

    14.03.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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