A self-adjusting unmanned aerial vehicle thrust line measurement and adjustment method is characterized in that a ball joint is arranged between a thrust nozzle and a mounting plate, the ball joint drives the thrust nozzle to turn automatically as the ball joint can flexibly turn in a certain range, the position where the central axis of the thrust nozzle is coaxial to the central line of a lifting rope is record, meanwhile a fastening device on the ball joint needs to be screwed, and then the problem of coaxiality of the central axis of a rocket and the central axis of the thrust nozzle is solved. The self-adjusting unmanned aerial vehicle thrust line measurement and adjustment method effectively improves the work efficiency, reduces labor intensity of workers and improves the measurement and adjustment accuracy.


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    Titel :

    Self-adjusting unmanned aerial vehicle thrust line measurement and adjustment method


    Beteiligte:
    JIA YIHAI (Autor:in) / YU YUHUA (Autor:in) / FU FEI (Autor:in) / WANG XIN (Autor:in) / WANG YERAN (Autor:in) / GU ZHIGANG (Autor:in) / WU JIANJING (Autor:in)

    Erscheinungsdatum :

    01.04.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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