The damping device structurally comprises an assembling column, an operator and an assembling ball, the assembling ball is arranged on the operator, the assembling ball is in clearance fit with the operator, the assembling column is installed on the operator, the operator is movably connected with the assembling column, the operator is provided with a processor, an operating panel and a fixing block, the operating panel is arranged on the processor, and the fixing block is arranged on the operating panel. According to the shock absorption device, the mounting plate and the processing plate are spliced and assembled to form the integral shock absorption device, the splicing structure can be selectively disassembled, and the shock absorption device is convenient to assemble and disassemble. Therefore, whether the damping structure clamped in the middle of the mounting structure is replaced or the damping structure connected with the aircraft body is replaced, the assembling structure can be independently taken out to be replaced by disassembling the splicing structure.

    本发明公开了一种无人飞行器的减震装置,其结构包括组装柱、操作器、组装球,操作器上设有组装球,组装球与操作器间隙配合,组装柱安装在操作器上,操作器与组装柱活动连接,操作器设有处理器、操作板、固定块,处理器上设有操作板,操作板与处理器相连接,固定块安装在处理器上,处理器与固定块活动连接,本发明的减震装置通过安装板和处理板之间的拼接组装,构成一个整体的减震装置,拼接结构可选择性进行拆卸,为此无论是在替换被夹合在安装结构中间的减震结构,还是替换与飞行器机体连接的减震结构,均可利用拼接结构的拆卸,将组装结构单独取出进行替换。


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    Title :

    Damping device of unmanned aerial vehicle


    Additional title:

    一种无人飞行器的减震装置


    Contributors:

    Publication date :

    2022-11-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F16F SPRINGS , Federn / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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