A landing gear structure for a drone

CN224690475UActive Publication Date: 2026-08-28HEFEI HONGCHANG INFORMATION TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202522135080.8
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-10-10
Publication Date
2026-08-28
Estimated Expiration
2035-10-10

AI Technical Summary

Technical Problem

[0004]为避免无人机下落时磕碰,一般会在无人机下落位置设置有起落架,而现有的起落架大多缓冲效果较差,无人机下落的冲击力得不到缓冲容易造成机体损坏;

Benefits of technology

1.本实用新型通过设置缓冲机构,能够当无人机下落时,底部会与支撑板顶部接触,受到无人机下落冲击力影响,会带动套杆、连接块、推动杆和推动块向下移动,推动块会带动拉簧进行拉伸,通过拉簧产生的拉力起到缓冲的作用,与此同时活塞板将壳体下半部分组成一个密闭的空腔,推动块向下移动时,会带动活塞板向下移动,对空气进行压缩,压缩气体的反作用力还会起到辅助缓冲的作用,通过多级缓冲的方式,有效提高了缓冲的效果,避免机体损坏;

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Abstract

The utility model relates to the technical field of unmanned plane, and disclose a landing gear structure for unmanned plane, including base and support plate, the base is located at the bottom of support plate, the top of base is fixedly connected with four sleeves, the inner wall sliding connection of sleeve has sleeve rod, the utility model discloses through setting buffer mechanism, can when unmanned plane falls, the bottom will contact with support plate top, is influenced by unmanned plane falling impact force, will drive sleeve rod, connecting block, push rod and push block to move down, push block will drive the extension of tension spring, and the tension of tension spring produces the effect of buffering, at the same time, the piston plate will form a closed cavity with the lower half part of shell, when push block moves down, will drive piston plate to move down, and the air is compressed, and the reaction force of compressed gas also plays the role of auxiliary buffering, through multistage buffering mode, effectively improve the effect of buffering, avoid the body damage.
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Citation Information

Patent Citations

  • Undercarriage damping structure for unmanned aerial vehicle

    CN212766724U