Vertical takeoff power supply system, fixed wing unmanned aerial vehicle and working method

A vertical take-off and power supply system technology, applied to aircraft parts, unmanned aircraft, aircraft, etc., can solve the problems of power consumption, large power consumption, and affecting the cruising mileage and time of drones, so as to reduce power consumption, The effect of meeting the power demand and prolonging the cruising mileage and time

Active Publication Date: 2016-11-23
江苏冰城氢能科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, during the vertical take-off process of traditional UAVs, a large amount of electric energy is consume

Method used

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  • Vertical takeoff power supply system, fixed wing unmanned aerial vehicle and working method
  • Vertical takeoff power supply system, fixed wing unmanned aerial vehicle and working method
  • Vertical takeoff power supply system, fixed wing unmanned aerial vehicle and working method

Examples

Experimental program
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Effect test

Embodiment 1

[0030] like figure 1 As shown, the present embodiment 1 provides a vertical take-off power supply system, including: a power supply device 1 located on the ground; the power supply device 1 is suitable for maintaining power supply to the UAV 2 when the UAV 2 takes off vertically ; and when the UAV 2 reaches a predetermined height, the UAV 2 is separated from the power supply device 1 for power supply.

[0031] As an optional implementation of the vertical take-off power supply system, the vertical take-off power supply system also includes: an adsorption device and a charging terminal; the adsorption device is suitable for inserting the plug 102 of the charging terminal into the charging interface of the drone, and After the drone reaches a predetermined height, the adsorption device drives the charging end to fall off, so that the drone is detached from the power supply device for power supply;

[0032] Specifically, the power supply device includes: a main processor module,...

Embodiment 2

[0042] On the basis of Embodiment 1, this Embodiment 2 also provides a working method of the vertical take-off power supply system, that is, when the UAV takes off vertically, the power supply device is suitable for maintaining power supply to the UAV; and when there is no After the man-machine reaches the predetermined height, the UAV is powered off from the power supply device.

[0043] The vertical take-off power supply system also includes: an adsorption device and a charging terminal; the adsorption device is suitable for inserting the plug of the charging terminal into the charging interface of the drone, and when the drone reaches a predetermined height, the adsorption device drives the charging terminal to fall off; The man-machine is powered from the power supply device; the power supply device is provided with a wire wheel for coiling the transmission wire.

[0044] The power supply device includes: a main processor module, a main power line carrier module connected ...

Embodiment 3

[0046] On the basis of Embodiment 1, Embodiment 2 also provides an unmanned aerial vehicle.

[0047] The unmanned aerial vehicle includes: an onboard processor module, an unmanned aerial vehicle power system controlled by the onboard processor module, and the vertical take-off power supply system; The power supply system inside the man-machine is powered.

[0048] The power supply system in the drone includes: a charging and discharging control module and a lithium battery.

[0049] The power system of the UAV includes: a horizontal power subsystem 3 and a vertical power subsystem 4 controlled by an onboard processor module; wherein the horizontal power subsystem 3 is located at the fuselage and includes: a horizontal propeller mechanism; The vertical power subsystem 4 includes: a vertical propeller 401 mechanism symmetrically arranged at the left and right wings 5 ​​places; The GPS module for man-machine positioning is connected.

[0050] The vertical propeller 401 mechani...

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Abstract

The invention relates to a vertical takeoff power supply system, a fixed wing unmanned aerial vehicle and a working method. The vertical takeoff power supply system comprises a power source power supply device located on the ground. The power source power supply device is suitable for keeping supplying power to the unmanned aerial vehicle when the unmanned aerial vehicle vertically takes off. After the unmanned aerial vehicle reaches the preset height, the unmanned aerial vehicle is separated from power supply of the power source power supply device. The power source power supply device is used for continuously supplying power to the unmanned aerial vehicle when the unmanned aerial vehicle vertically takes off, the requirement for vertical takeoff electric energy is met, electric energy consumption of the unmanned aerial vehicle is greatly reduced, the cruising mileage of the unmanned aerial vehicle is increased, and the cruising time of the unmanned aerial vehicle is prolonged.

Description

technical field [0001] The invention relates to a vertical take-off power supply system, a fixed-wing unmanned aerial vehicle and a working method. Background technique [0002] Due to the characteristics of fast maneuvering, low cost of use, and simple maintenance and use, UAVs have been widely used at home and abroad. [0003] However, during the vertical take-off process of traditional UAVs, a large amount of electric energy is consumed, and a large amount of electric energy is consumed, which will seriously affect the cruising range and time of UAVs. [0004] Therefore, how to reduce or avoid the power consumption of the UAV when it takes off vertically is a technical problem in this field. Contents of the invention [0005] The purpose of the present invention is to provide a vertical take-off power supply system and working method to effectively reduce the self-power consumption of the drone during vertical take-off. [0006] In order to solve the above technical p...

Claims

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Application Information

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IPC IPC(8): B64C39/02B64D41/00H02J7/00
CPCH02J7/0027B64C39/02B64D41/00H02J7/00036B64U10/25
Inventor 李忠朱艾成朱浩
Owner 江苏冰城氢能科技有限公司
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