An aircraft latch mechanism has a latch body having a front end and a rear end and a longitudinal slot extending along a portion of the length of the body. A pair of first cam members flanks the latch body. A handle is pivotally attached to the first cam members. The first cam members are also attached to a pair of over-center links. A mounting bushing extends through the longitudinal slot at the pivot where the first cam members and over-center links attach. Movement of the handle causes a corresponding movement of the first cam members, over-center links, and the connecting structure extending through the slot.


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    Titel :

    Latch mechanism


    Beteiligte:
    BAIC ZELJKO (Autor:in) / MEDINA UBALDO (Autor:in)

    Erscheinungsdatum :

    2017-04-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    E05C Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster , BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS / B64C AEROPLANES , Flugzeuge



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