The invention discloses an unmanned aerial vehicle ejection method. An unmanned aerial vehicle power ejection mechanism is included. The unmanned aerial vehicle power ejection mechanism comprises a base, a launching frame, a rotating assembly, a launching pad, a clamping unit and a power assembly. The launching pad is connected with the power assembly through a pulley block and a traction rope. The base comprises an upper base body, a lower base body and a lifting assembly; the rotating assembly comprises an electric telescopic rod, a first lifting oil cylinder and a second lifting oil cylinder. The power assembly comprises a power base and a power tank, and a spraying pipe is arranged on the left side of the power tank. By arranging the power assembly, the launching pad, the clamping unit, the traction rope and the pulley block, ejection-assisted take-off of the fixed-wing unmanned aerial vehicle is achieved, a field runway does not need to be adopted, and the height and angle of the launching frame can be adjusted. The unmanned aerial vehicle ejection method has the advantages that the unmanned aerial vehicle is not limited by runways, the method is relatively wide in application, the unmanned aerail vehicle ejection is not easy to damage during takeoff, so that loss is reduced.

    本发明公开了无人机弹射方法,包括一种无人机动力弹射机构;无人机动力弹射机构包括底座、发射架、转动组件、发射台、卡接单元和、动力组件;发射台通过滑轮组和牵引绳与动力组件相连;底座包括上底座、下底座和升降组件;转动组件包括电动伸缩杆、一号举升油缸和二号举升油缸;动力组件包括动力座和动力罐,动力罐左侧设有喷管。本发明通过设置动力组件、发射台、卡接单元、牵引绳和滑轮组,从而实现对固定翼无人机的弹射起飞,无需采用现场的跑道,还可以调整发射架的高低和角度。本发明具有不会受跑道的限制应用相对更广、起飞不易发生损坏从而减少损失的优点。


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    Title :

    Unmanned aerial vehicle ejection method


    Additional title:

    无人机弹射方法


    Contributors:
    NIE YONGBIN (author) / LIU YAFENG (author) / LIU ZEFENG (author) / TAN MENG (author) / WANG YINING (author)

    Publication date :

    2021-10-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    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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