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Self-stabilization wind resistance unmanned aerial vehicle

A drone and arm technology, applied in the field of drones, can solve problems such as falling and unstable flight of drones, and achieve the effect of good stability and convenient installation and disassembly

Pending Publication Date: 2018-04-06
SICHUAN COLLEGE OF ARCHITECTURAL TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the problem that when the UAV often encounters bad weather during the flight, it is easy to cause the UAV to fly extremely unstable or even have the risk of falling

Method used

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  • Self-stabilization wind resistance unmanned aerial vehicle

Examples

Experimental program
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Effect test

Embodiment 1

[0035] as attached figure 1 , attached figure 2 The self-stabilizing wind-resistant UAV of this embodiment includes a center cabin 1, a battery cabin 2, an arm 3, a vector drive device 4, a flipping part 41, a mounting seat 411, a steering gear 1 412, a gear shaft 1 413, and a transmission rod. 414, rotating part 42, steering gear 2 421, gear shaft 2 422, rotor device 5, landing gear device 6, vertical tube assembly 61, horizontal tube 62, vibration damping device 63, center hatch cover 7, GPS device 8, self-stabilizing Wind-resistant unmanned aerial vehicle, the machine arm 3 is connected with the central cabin 1 to form the body frame, the rotor device 5 is installed on the drive of the vector drive device 4, and the vector drive device 4 is connected with the control system to control the rotor device 5 relative to the machine. The arm 3 moves, and the vector driving device 4 includes a turning part 41 and a rotating part 42. When the UAV encounters bad weather, the turni...

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PUM

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Abstract

The invention relates to the technical field of unmanned aerial vehicles, in particular to a self-stabilization wind resistance unmanned aerial vehicle. The self-stabilization wind resistance unmannedaerial vehicle comprises a center cabin, a battery cabin, vehicle arms, vector drive devices, rotor wing devices, undercarriage devices and a control system. The vector drive devices are installed onthe vehicle arms. The vehicle arms are connected with the center cabin to form a vehicle body frame. The rotor wing devices are installed on the vector drive devices. The vector drive devices are connected with the control system, so that the rotor wing devices are controlled to move relative to the vehicle arms. Each vector drive device comprises a turnover part and a rotation part. The turnoverparts and the vehicle arms are connected in an up-down turnover mode. The rotation parts and the rotor wing devices are connected rotationally. The self-stabilization wind resistance unmanned aerialvehicle solves the problem that an unmanned aerial vehicle flies unstably and even has a crash risk when the unmanned aerial vehicle encounters severe weather in the flight process.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a self-stabilizing and wind-resistant unmanned aerial vehicle. Background technique [0002] With the development of society, drones are used more and more widely, such as express transportation, aerial photography, crop monitoring, news reports, power inspections, and film and television shooting. Rotor drones change the rotor speed by adjusting the motor speed. Realize the change of lift to control the flight, such as quadrotor UAV, when the sum of the lift of the four propellers of the aircraft is equal to the total weight of the aircraft, the lift of the aircraft is balanced with the gravity, and the aircraft can hover in the air, but when there is no When the man-machine is affected by bad weather, the UAV is affected by forces in different directions during the flight, which may easily cause the overall force of the UAV to be extremely unstable, so that the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64C1/30B64C25/32
CPCB64C1/30B64C25/32B64C39/02B64U50/19B64U30/20B64U2101/00
Inventor 刘辉扬
Owner SICHUAN COLLEGE OF ARCHITECTURAL TECH