A lock is provided for a secondary aircraft cockpit barrier. The lock has a locking tongue, a cavity for receiving the locking tongue, a locking retainer for retaining the locking tongue in the cavity, and a damped locking tongue releasing mechanism for releasing the locking retainer thereby unlocking the locking tongue from the cavity. The damped locking tongue releasing mechanism is damped such that releasing the locking retainer requires at least about 5 seconds.


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    Title :

    LOCK


    Contributors:

    Publication date :

    2021-03-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    E05B LOCKS , Schlösser / B64C AEROPLANES , Flugzeuge



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