A dual axis hinge (350) configured for pivotally securing a cowl (320) to a fixed structure (310) of an aircraft is disclosed. In various embodiments, the dual axis hinge includes a link (360) having a first end (361) and a second end (363); a first pin (362) configured to pivotally secure the first end of the link to the fixed structure and a second pin (364) configured to pivotally secure the second end of the link to the cowl; and a first hinge stop (366) configured for connection to the cowl and a second hinge stop (368) configured for connection to the link.


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    Title :

    DUAL AXIS HINGE RADIAL DISPLACEMENT LIMITER


    Additional title:

    RADIALVERSCHIEBUNGSBEGRENZER FÜR ZWEIACHSIGES GELENK
    LIMITEUR DE DÉPLACEMENT RADIAL DE CHARNIÈRE À DEUX AXES


    Contributors:
    PRETTY SEAN (author)

    Publication date :

    2021-07-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / E05D Scharniere oder andere Aufhängevorrichtungen für Türen, Fenster oder Flügel , HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS, OR WINGS



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