Foot stool of unmanned aerial vehicle
By using assembly strips, alloy rods, hydraulic columns and feet in the drone tripod, combined with technical means such as elastic capsules, buffer bodies, hydraulic columns and centralized discs, the problems of low inclination and safety factor when the drone is reserved on rugged ground are solved, and higher safety and efficiency of reserved on land are achieved.
CN222646303UActive Publication Date: 2025-03-21SHANDONG AOXIANG AVIATION TECHNOLOGY CO LTD
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Patent Information
- Application Number
- CN202421536281.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-07-02
- Publication Date
- 2025-03-21
- Estimated Expiration
- 2034-07-02
AI Technical Summary
Technical Problem
The existing drone tripods are easily tilted when placed on rugged ground, reducing the safety factor and efficiency of backup landing.
Method used
A drone tripod was designed, using assembly strips, alloy rods, hydraulic columns and feet, and absorbing and dispersing impact forces through technical means such as elastic capsules, buffer bodies, hydraulic columns and centralized discs, thereby improving the stability and safety of drone drop.
Benefits of technology
It effectively reduces the impact force of the drone during backup landing, improves the safety factor and efficiency of backup landing, and extends the service life of the rack and feet.
✦ Generated by Eureka AI based on patent content.
Abstract
The utility model relates to the technical field of unmanned aerial vehicle foot stands, in particular to an unmanned aerial vehicle foot stand which comprises a rack, a plurality of assembly holes used for assembly of an unmanned aerial vehicle are formed in the rack, assembly strips are symmetrically installed on the rack, and the unmanned aerial vehicle foot stand is characterized in that elastic bags used for reducing the impact effect are arranged on the assembly strips. Second alloy rods used for transmitting impact force are symmetrically arranged on the assembly strip, and a plurality of elastic shafts used for absorbing the impact force are arranged on the second alloy rods. Through the arrangement of the elastic bag and the buffer body, the impact force generated during landing of the unmanned aerial vehicle can effectively reduce damage to the rack, the transmission amplitude of the first alloy rod on the second alloy rod can be effectively relieved by the buffer body, part of the impact force can be directly dispersed by the elastic shaft, vertical floating borne by the second alloy rod is effectively reduced, and the service life of the unmanned aerial vehicle is prolonged. Therefore, the safety coefficient of landing preparation of the unmanned aerial vehicle is improved, and the efficiency of landing preparation of the unmanned aerial vehicle is improved.
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