The invention discloses an auxiliary safety mechanism of a rotorcraft, which relates torotorcrafts. The auxiliary safety mechanism of the rotorcraft is simple in structure, convenient to install and reliable in buffering. The rotorcraft comprises an empennage, the bottom of the empennage is a horizontal transverse wing, and the auxiliary safety mechanism is connected to the bottom of the transverse wing. The auxiliary safety mechanism comprises a supporting shaft, a pair of symmetrically-arranged supporting plates and a pair of supporting mechanisms. The supporting shafts are connected to thebottom of the transverse wing, sleeves are arranged at the ends, facing the supporting shafts, of the supporting plates, the supporting plates are connected to the supporting shafts through the sleeves, penetrating holes are formed in the supporting plates, and the supporting mechanisms correspond to the supporting plates in a one-to-one mode. Theauxiliary safety mechanism has the effects of avoiding collision and improving safety on the whole.

    一种旋翼机辅助安全机构。涉及旋翼机。提供了一种结构简单,方便安装,缓冲可靠的旋翼机辅助安全机构。所述旋翼机包括尾翼,所述尾翼的底部为水平设置的横翼,所述辅助安全机构连接在横翼的底部;所述辅助安全机构包括支撑轴、一对对称设置的支撑板和一对支撑机构,所述支撑轴连接在横翼的底部,所述支撑板朝向支撑轴的一端设有套管,所述支撑板通过套管连接在支撑轴上,所述支撑板上设有穿孔,所述支撑机构与支撑板一一对应。本发明从整体上具有避免发生碰撞,提高安全性的作用。


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    Title :

    Auxiliary safety mechanism of rotorcraft


    Additional title:

    一种旋翼机辅助安全机构


    Contributors:
    LIN HAITONG (author)

    Publication date :

    2020-10-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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