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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    Title :

    Alignment and safety device for the cowls of aircraft engine nacelles


    Additional title:

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


    Contributors:

    Publication date :

    2018-03-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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