A deployment or hinge mechanism and, more particularly, a compact unmanned aerial vehicle (UAV) wing deployment mechanism is provided. The deployment mechanism includes a hinged mechanism that stows in a stacked configuration and deploys in a level configuration.

    L'invention concerne un mécanisme de déploiement ou articulé, plus particulièrement, un mécanisme de déploiement d'aile d'aéronef sans pilote (UAV) compact. Le mécanisme de déploiement comprend un mécanisme articulé qui se replie dans une configuration empilée et se déploie dans une configuration à niveau.


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    Title :

    DEPLOYMENT MECHANISM


    Additional title:

    MÉCANISME DE DÉPLOIEMENT


    Contributors:

    Publication date :

    2016-12-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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    Free access