The invention discloses a mooring unmanned aerial vehicle connection balance system which comprises a rotary lantern ring. Adapter holes in bilateral symmetry are formed in the inner wall of the rotary lantern ring; a hinge seat is hinged to the interior of the rotary lantern ring through a transfer jack; a sliding cylinder is integrally formed on the lower side of the hinge seat; the upper end ofthe inner wall of the sliding cylinder is screwed with an electronic dynamometer; a connecting rod is welded at the lower end of the electronic dynamometer; the lower end of the connecting rod penetrates through the sliding cylinder and extends outside; and a mooring rope fixing hole is formed in the lower end of the connecting rod. The previous feedback information of a gyroscope is synthesizeddirectly according to the direction and the magnitude of the tension; therefore, the purpose of sharing the workload of the gyroscope processor is achieved. The structure directly detects the direction and magnitude of the force instead of detecting the deflection degree of the stressed aircraft body, and the feedback step is reduced in the processing link, so that compared with a mooring unmannedaerial vehicle balance system which completely depends on a gyroscope to adjust the balance, the mooring unmanned aerial vehicle balance system of the invention has higher data feedback and processing efficiency.

    本实发明公开了系留无人机连接平衡系统,包括转动套环,转动套环的内壁开设有左右对称的转接孔,且转动套环的内部通过转接孔铰接有铰接座,铰接座的下侧一体成型有滑筒,滑筒内壁的上端螺接有电子测力计,电子测力计的下端焊接有连接杆,连接杆的下端贯穿滑筒延伸至外部,且连接杆的下端开设有系留绳固定孔,而是直接通过拉力的方向和拉力大小综合陀螺仪先前的反馈信息,从而起到分摊陀螺仪处理器工作量的目的,该结构直接检测力的方向和大小,而非检测受力后机体的偏斜呈度,处理环节中减少了反馈步骤,因此有相较于完全依靠陀螺仪调整平衡的系留无人机平衡系统,该系留无人机平衡系统具有更高的数据反馈和处理效率。


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    Title :

    Mooring unmanned aerial vehicle connection balance system


    Additional title:

    系留无人机连接平衡系统


    Contributors:
    HU BIN (author) / ZOU CONGCONG (author)

    Publication date :

    2020-07-03


    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 / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen



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