A latch (12) is for connecting a panel to a structure, comprising: a bracket (30); a sliding body (32), translationally movable within the bracket; and a hooking arm (34) comprising a hook (74) and connected to the sliding body. The hooking arm is movable relative to the sliding body between an inclined and a parallel conformation. The sliding body can be moved between an unlocking position and a locking position. In the unlocking position, the hooking arm (34) is in an inclined conformation and in a first axial position relative to the bracket. In the locking position, the hooking arm is in the parallel conformation and in a second axial position. In an intermediate position, the hooking arm is in the parallel conformation and in the first axial position.


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    Title :

    HOOK LATCH FOR AIRCRAFT PANEL


    Contributors:

    Publication date :

    2024-04-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    E05C Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster , BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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