Aerial survey unmanned aerial vehicle for geographic information data acquisition

By designing detachable flight components and aerial cameras, the existing aerial survey drones are solved, and the drone is easily assembled, compact packaging and reduced transportation costs are achieved.

CN222663802UActive Publication Date: 2025-03-25郭大锌
1 Cites 0 Cited by

Patent Information

Application Number
CN202421506331.8
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-06-28
Publication Date
2025-03-25
Estimated Expiration
2034-06-28

AI Technical Summary

Technical Problem

The existing aerial survey drones have complex structures, and the connecting rod and landing gear are fixedly connected to the installation block and cannot be disassembled, resulting in large size and inconvenient portability.

Method used

A aerial survey drone for geographic information data acquisition is designed, which includes a detachable flight assembly and an aerial camera. The body consists of upper and lower mounting plates, flight control modules, clamp modules and removable support tubes. The support tubes are connected to the motor, propeller and signal lines, and all components are pluggable and removable.

Benefits of technology

It realizes the convenient assembly and decomposition of drones, and the disassembled parts are packed more compactly, making them easy to store, transport and carry, reduces transportation costs and space occupation, and facilitates maintenance and upgrades.

✦ Generated by Eureka AI based on patent content.
Patent Text Reader

Abstract

The utility model discloses an aerial survey unmanned aerial vehicle for geographic information data acquisition. The aerial survey unmanned aerial vehicle comprises a vehicle body, four flight assemblies detachably installed on the periphery of the vehicle body and an aerial camera detachably installed at the bottom of the vehicle body. The aircraft body comprises an upper mounting plate and a lower mounting plate which are oppositely arranged up and down, and a flight control module is fixed between the upper mounting plate and the lower mounting plate; clamping block modules are arranged at four corners between the upper mounting plate and the lower mounting plate; the flight assembly comprises a horizontally-arranged supporting pipe and a motor located at one end of the supporting pipe, a propeller is installed on the motor, a signal line is connected to the motor, and the signal line penetrates out of the other end of the supporting pipe and then is connected with the flight control module in a pluggable mode; the other end of the supporting pipe is fixedly clamped in the clamping block module; the supporting pipe is further fixedly connected with a rising and falling supporting assembly, and the rising and falling supporting assembly is detachably connected with the supporting pipe.
Need to check novelty before this filing date? Find Prior Art