The invention relates to the technical field of helicopter devices, in particular to a helicopter automatic inclinator structure which comprises a lower tray and an upper tray rotationally installed on the lower tray, the bottom end of the lower tray is fixedly connected with an assembling base through a corrugated bottom pipe, and the bottom end of the upper tray is fixedly connected with an assembling top seat through a corrugated top pipe. Anti-torsion arms are arranged between the lower tray and the assembling base and between the upper tray and the assembling top base, each anti-torsion arm comprises a bottom arm rod and a top arm rod arranged at one end of the bottom arm rod, U-shaped bases are fixedly connected to the side walls of the upper tray and the assembling base, bottom sliding grooves are formed in the surfaces of the two sides of each bottom arm rod, and the bottom sliding grooves are communicated with the bottom arm rods. According to the anti-torsion arm assembly and disassembly device for the helicopter automatic inclinator, the anti-torsion arm can be disassembled and assembled on the helicopter automatic inclinator conveniently and simply, the disassembly and assembly convenience of the anti-torsion arm can be improved, and the deformed or rusted anti-torsion arm can be more conveniently and rapidly replaced.

    本发明涉及直升机器件技术领域,具体为一种直升机自动倾斜器结构,包括下托盘和转动安装于所述下托盘上的上托盘,所述下托盘的底端通过波纹底管固定连接有装接底座,所述上托盘的底端通过波纹顶管固定连接有装接顶座,所述下托盘与装接底座之间以及所述上托盘与装接顶座之间均设置有防扭臂,所述防扭臂包括底臂杆和设置于所述底臂杆一端的顶臂杆,所述上托盘和装接底座的侧壁均固定连接有U形底座,所述底臂杆的两侧表面均开设有底滑槽,所述底滑槽上滑动连接有装配底轴,本发明使得防扭臂在直升机自动倾斜器上拆装操作便捷简单,有利于提高防扭臂的拆装便捷性,更加便于对发生变形或生锈的防扭臂进行快速更换处理。


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    Titel :

    Automatic inclinator structure of helicopter


    Weitere Titelangaben:

    一种直升机自动倾斜器结构


    Beteiligte:
    SUN ZHIWU (Autor:in)

    Erscheinungsdatum :

    2022-11-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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