An aircraft assembly (20) includes a keeper (44), a latch (46) and a lock (50). The latch (46) includes a handle (51) and a hook structure (62) operatively coupled to the handle (51). The hook structure (62) is engaged with the keeper (44) when the handle (51) is in a closed position. The hook structure (62) is disengaged from the keeper (44) when the handle (51) is in an open position. The lock (50) includes a catch (78), a lever (84) and a spring (86). The lever (84) is configured to rotate about an axis (92) between a locked position and an unlocked position. The lever (84) is aligned with the catch (78) locking the handle (51) in the closed position when the lever (84) is in the locked position. The lever (84) is misaligned from the catch (78) unlocking the handle (51) from the closed position when the lever (84) is in the unlocked position. The spring (86) biases the lever (84) axially along the axis (92) in a direction towards the handle (51).


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    Title :

    AIRCRAFT LATCH ASSEMBLY WITH LOCK


    Additional title:

    FLUGZEUGVERRIEGELUNGSANORDNUNG MIT SCHLOSS
    ENSEMBLE VERROU D'AÉRONEF AVEC VERROU



    Publication date :

    2024-05-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / E05B LOCKS , Schlösser / E05C Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster , BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS



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