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Novel hydrogen fuel cell used for driving unmanned aerial vehicle

A technology of fuel cells and drones, which is applied in the direction of power system fuel cells, fuel cells, fuel cell components, etc., can solve the problems of drone flight controllability and low flight efficiency, and improve flight controllability Excellent performance and flight efficiency, high electrical conductivity, and good corrosion resistance

Inactive Publication Date: 2019-09-24
JIANGSU BINGCHENG HYDROGEN ENERGY TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is: in order to overcome the deficiencies of the prior art unmanned aerial vehicle's flight controllability and low flight efficiency, provide a kind of drone that can control the flight height and direction of the unmanned aerial vehicle at any time according to the needs, and at the same time improve the flight controllability And flight efficiency, as a green new energy, will not pollute the environment, can improve the life of drones, and is used to drive new hydrogen fuel cells for drones

Method used

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  • Novel hydrogen fuel cell used for driving unmanned aerial vehicle

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Embodiment Construction

[0036] The present invention is described in further detail now in conjunction with accompanying drawing. These drawings are all simplified schematic diagrams, which only illustrate the basic structure of the present invention in a schematic manner, so they only show the configurations related to the present invention.

[0037] Such as figure 1 As shown, a new type of hydrogen fuel cell for driving a drone, the new type of hydrogen fuel cell is set on the drone; the drone includes a left wing 2, a right wing 3, a torso 1 and an tail wing 4;

[0038] The left wing 2 is provided with a first left-wing support 21 and a second left-wing support 22, and the first left-wing support 21 is arranged at a position farther away from the torso 1 part of the drone than the second left-wing support 22 ; The left-wing first motor 211, the left-wing first motor controller 214, the left-wing first hydrogen fuel cell 213, the left-wing first converter 212, the left-wing second motor 215, and t...

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Abstract

The invention relates to a novel hydrogen fuel cell used for driving an unmanned aerial vehicle. The novel hydrogen fuel cell is characterized in that the novel hydrogen fuel cell is arranged on the unmanned aerial vehicle; the unmanned aerial vehicle comprises a left wing, a right wing, a trunk and an empennage part; the left wing is provided with a left wing first bracket and a left wing second bracket; and the right wing is provided with a right wing first bracket and a right wing second bracket. According to the novel hydrogen fuel cell used for driving the unmanned aerial vehicle, the flight height and direction of the unmanned aerial vehicle can be controlled at any time according to the needs, the flight controllability and the flight efficiency of the unmanned aerial vehicle are improved, controllers are arranged for all motors and propellers, thus manipulation sensitivity is improved, meanwhile, different power sources are adopted during flight, thus fuel can be saved, and the cruising ability of the unmanned aerial vehicle is improved.

Description

technical field [0001] The invention relates to a novel hydrogen fuel cell, in particular to a novel hydrogen fuel cell for driving an unmanned aerial vehicle. Background technique [0002] In the prior art, lithium batteries are generally used as the flight power source of drones. However, lithium batteries should not be made too large, otherwise it will affect the weight of the drone and reduce the flight safety and flight quality of the drone. Therefore, the existing lithium batteries for driving unmanned aerial vehicles generally have the problem of short battery life. [0003] At the same time, because the lithium battery in the prior art should not be too large and the battery life is short, in order to ensure the battery life, the number and sensitivity of the electronic control components installed on the drone are generally not high, and the flight controllability and flight efficiency are low. . [0004] In addition, lithium-ion batteries are mostly used in the p...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64D27/24
CPCB64C39/024B64D27/24H01M8/0206H01M8/0208H01M8/04029H01M8/04955H01M2250/20B64U10/10B64U50/19B64U2201/20Y02T50/60Y02T90/40Y02E60/50
Inventor 朱艾成朱浩
Owner JIANGSU BINGCHENG HYDROGEN ENERGY TECH CO LTD
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