The invention discloses an aerial remote sensing surveying and mapping unmanned aerial vehicle damping device, and relates to the technical field of remote sensing surveying and mapping auxiliary equipment. The aerial remote sensing surveying and mapping unmanned aerial vehicle damping device comprises an unmanned aerial vehicle body and spiral blades. A buffer seat is arranged below the unmannedaerial vehicle body, buffer springs are symmetrically arranged on the left and right sides in the buffer seat, and the bottom tail ends of the buffer springs are fixedly connected with buffer plates.Buffering supporting columns are fixedly connected below the buffering plates, a first supporting plate and a second supporting plate are fixedly installed below the buffering supporting columns, damping rods are arranged between the first supporting plate and the second supporting plate, a damping spring converts external acting force into elastic force to achieve the primary damping effect, andthe buffering supporting columns extrude the buffering springs to be stretched and contracted through the buffering plates. The buffer springs convert external acting force into elastic force, dampingrotating rollers push plungers to move upwards in first plunger pipes through the second supporting rod and push rods, the plungers inflate anti-collision air bags through second plunger pipes, the anti-collision effect of the anti-collision air bags is improved, the unmanned aerial vehicle body is fully protected, and the service life of the unmanned aerial vehicle body is prolonged.

    本发明公开了一种航空遥感测绘无人机减震装置,涉及遥感测绘辅助设备技术领域,包括无人机机体以及螺旋叶片,无人机机体下方设置缓冲座,缓冲座内左右两侧对称设置缓冲弹簧,缓冲弹簧底部末端与缓冲板固定连接,缓冲板下方固定连接缓冲支柱,缓冲支柱下方固定安装支板一以及支板二,支板一与支板二间设置减震杆,减震弹簧一将外部作用力转化为弹性力,实现初步减震作用,缓冲支柱通过缓冲板挤压缓冲弹簧拉伸和收缩,缓冲弹簧将外部作用力转化为弹性力,减震转辊通过支杆二以及推杆推动柱塞在第一柱塞管内向上移动,柱塞通过第二柱塞管对防撞气囊进行充气,提高防撞气囊的防撞效果,对无人机机体进行充分的保护,延长其使用寿命。


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    Titel :

    Aerial remote sensing surveying and mapping unmanned aerial vehicle damping device


    Weitere Titelangaben:

    一种航空遥感测绘无人机减震装置


    Beteiligte:
    SUN YAFEI (Autor:in) / ZHANG JUANJUAN (Autor:in) / ZHANG ZHIMIN (Autor:in) / DING LEIXIANG (Autor:in) / HOU SHAOYANG (Autor:in)

    Erscheinungsdatum :

    2021-02-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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