The invention provides a helicopter hanging load swing control balancing device. The helicopter hanging load swing control balancing device comprises a damping buffering device, a universal connecting device and an electric rolling wheel device which are installed at the bottom of a helicopter. A groove is formed in the bottom of the helicopter, and the sliding plate is arranged in the groove through a damping buffer device; the universal connecting device is a unilateral universal connecting shaft, the flexible end of the shaft is provided with a cross bearing fixed on a cross U-shaped bracket and is fixed at the bottom of the sliding plate through a flange plate, and the rigid end of the shaft is connected with the electric roller device; and the electric roller device comprises a motor, a roller and a rope wound on the roller.

    本发明提供了一种直升机吊挂载荷摆幅控制平衡装置,包括安装在直升机底部的阻尼缓冲装置,万向连接装置,电动滚轮装置;所述直升机底部设置有凹槽,滑板通过阻尼缓冲装置设置在凹槽内;所述的万向连接装置为单边万向连接轴,轴的柔性一端装有固定在交叉U形支架上的十字轴承,并通过法兰盘固定在滑板底部,轴的刚性一端连接电动滚轮装置;所述电动滚轮装置包括电机、滚轮和缠绕在滚轮上的绳索。


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    Title :

    Helicopter hanging load swing control balancing device


    Additional title:

    直升机吊挂载荷摆幅控制平衡装置


    Contributors:
    LI CHANG (author) / LI XIAOGUANG (author) / HUAN PING (author)

    Publication date :

    2023-03-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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