An assembly is provided for an aircraft. This assembly includes a keeper, a latch, a lock and an electric sensor. The latch includes a handle and a hook structure operatively coupled to the handle. The hook structure is engaged with the keeper when the handle is in a closed position. The hook structure is disengaged from the keeper when the handle is in an open position. The lock includes a lock element configured to move between a locked position and an unlocked position. The lock is configured to lock the handle in the closed position when the lock element is in the locked position. The lock is configured to unlock the handle from the closed position when the lock element is in the unlocked position. The electronic sensor is configured to provide a signal when the lock element is in one of the locked position or the unlocked position.


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    Title :

    Aircraft latch Assembly with Lock Sensor(s)



    Publication date :

    2025-01-16


    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 / E05B LOCKS , Schlösser



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