A latch pin actuator (600) comprises a primary lock (702) having a curvature (712) configured to allow a latch pin (602) into a housing (604) when the primary lock (702) is in an unlocked position, and wherein the primary lock (702) is configured to prevent the latch pin (602) from entering a housing (604) in a locked position, by facing the curvature (712) in a different direction in the locked position, a spring (706) and a piston (710). The primary lock (702) is attached to a primary lock cam (608) and has a notch (716) as a fracture evident geometry. The spring (706) is biased to lock the primary lock (702). The piston (710) is configured to unlock the primary lock (702).


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    Titel :

    FOLDING WING SYSTEM


    Weitere Titelangaben:

    KLAPPFLÜGELSYSTEM
    SYSTÈME D'AILE PLIABLE


    Beteiligte:

    Erscheinungsdatum :

    2020-08-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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