UAV maximum inclination angle protection device

A technology of maximum inclination and protection device, applied in three-dimensional position/channel control, vehicle position/route/altitude control, non-electric variable control and other directions, it can solve problems such as crash, UAV flip, loss, etc., and achieve accurate flight. Effect

Inactive Publication Date: 2017-02-22
XUZHOU FLY DREAM ELECTRONICS & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Most of the existing drones are controlled by the remote control. During the flight of the drone, due to improper operation or unfamiliar terrain, the drone will turn over or crash, causing certain losses.

Method used

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  • UAV maximum inclination angle protection device
  • UAV maximum inclination angle protection device
  • UAV maximum inclination angle protection device

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Embodiment Construction

[0017] The present invention will be further described below in conjunction with the accompanying drawings.

[0018] Such as image 3 , taking the quadrotor unmanned aerial vehicle as an example, the present invention will be further described.

[0019] A protection device for the maximum inclination angle of an unmanned aerial vehicle is characterized in that it includes a power supply device and a control device.

[0020] Further, the UAV is a multi-rotor UAV.

[0021] Further, the power supply device is a battery.

[0022] Further, the control device includes an electronic speed controller, a receiver and a driving motor.

[0023] Further, the electronic governor is a brushless electronic governor.

[0024] Further, the electronic governor and the driving motor are installed on each rotor of the drone, and the electronic governor is installed under the driving motor.

[0025] The control device includes an electronic governor, an autopilot and a drive motor.

[0026] ...

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PUM

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Abstract

The invention discloses a UAV maximum inclination angle protection device, which comprises a power module and a control module. The power module is a battery. The control module comprises electrical speed regulators, a receiver and drive motors. One electrical speed regulator and one drive motor are installed on each rotor wing of UAV. The protection mechanism is that when the inclination angle of the UAV during flight exceeds the setting value m, the control signals are transmitted through the receiver to the speed regulators, which controls servo motors to decelerate the rotation speed of servo motors. When the flight condition of the UAV reinstates to the horizontal condition, the electrical speed regulator controls the servo motor to accelerate to allow the UAV continue to fly. The device solves the problem of overturning, detour from the normal route and even crash of the UAV during the UAV flight process, thus achieving the precise flight.

Description

technical field [0001] The invention relates to a protection device for the maximum inclination angle of an unmanned aerial vehicle. Background technique [0002] With the rapid rise of the aircraft model industry, especially multi-rotor UAVs have been more and more widely used. For example, it plays an important role in agricultural plant protection, urban aerial photography, meteorological analysis, power inspection and other fields. Most of the existing drones are controlled by remote control. During the flight of the drone, due to improper operation or unfamiliar terrain, the drone will flip or crash, causing certain losses. Contents of the invention [0003] Aiming at the shortcomings of the above-mentioned technologies, the present invention provides a protection device for the maximum inclination angle of the UAV, which solves the problem that the UAV overturns and crashes or is damaged due to the excessive braking speed of the UAV during flight. [0004] A protec...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0808G05D1/101
Inventor 阚森
Owner XUZHOU FLY DREAM ELECTRONICS & TECH
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