CN206098554U - Hydrogen cell power in unmanned aerial vehicle field - Google Patents

Hydrogen cell power in unmanned aerial vehicle field Download PDF

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Publication number
CN206098554U
CN206098554U CN201621079848.9U CN201621079848U CN206098554U CN 206098554 U CN206098554 U CN 206098554U CN 201621079848 U CN201621079848 U CN 201621079848U CN 206098554 U CN206098554 U CN 206098554U
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CN
China
Prior art keywords
hydrogen
fuel cell
cell pile
hydrogen fuel
pile
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201621079848.9U
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Chinese (zh)
Inventor
卢致辉
陈金颖
唐霜华
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenzhen Micromulticopter Aero Technology Co Ltd
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Shenzhen Micromulticopter Aero Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shenzhen Micromulticopter Aero Technology Co Ltd filed Critical Shenzhen Micromulticopter Aero Technology Co Ltd
Priority to CN201621079848.9U priority Critical patent/CN206098554U/en
Application granted granted Critical
Publication of CN206098554U publication Critical patent/CN206098554U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/30Hydrogen technology
    • Y02E60/50Fuel cells

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  • Fuel Cell (AREA)

Abstract

The utility model discloses a hydrogen cell power in unmanned aerial vehicle field, including installing the fuel cell on unmanned aerial vehicle, this fuel cell is hydrogen fuel cell pile, and the bottom of hydrogen fuel cell pile has a radiator fan, and radiator fan's play windpiston is just to hydrogen fuel cell pile, one side of hydrogen cell pile is provided with DCDC converter and controller, and the hydrogen cell pile is connected to DCDC converter and controller input end, and unmanned aerial vehicle driving system is connected to its output, the hydrogen cell pile is connected one and is stored up the hydrogen bottle, stores up the hydrogen bottle and provides hydrogen for the hydrogen cell pile, and chu qing is bottled to have hydrogen, and the delivery outlet is continuous with the hydrogen cell pile. The utility model discloses a hydrogen cell power to realize that many rotor unmanned aerial vehicle time of endurance are long, rational in infrastructure, convenient operation's advantage.

Description

A kind of hydrogen fuel cell power supply in unmanned plane field
Technical field
The utility model is related to a kind of unmanned machine battery, and in particular to a kind of hydrogen fuel cell power supply in unmanned plane field.
Background technology
In prior art, the general flying power for adopting lithium battery as unmanned plane, it is excessive that lithium battery is unfit to do, otherwise The overall weight of unmanned plane, heavy burden can be affected greatly to increase, therefore existing lithium battery generally existing cruising time is short Bottleneck problem.
The content of the invention
Technical problem to be solved in the utility model is to provide a kind of hydrogen fuel cell electricity in unmanned plane field
Source, to realize multi-rotor unmanned aerial vehicle cruising time length, the unmanned plane field of rational in infrastructure, easy to operate advantage Hydrogen fuel cell power supply.
The utility model is achieved through the following technical solutions:A kind of hydrogen fuel cell power supply in unmanned plane field, Including the fuel cell being installed on unmanned plane, the fuel cell be hydrogen fuel cell pile, the bottom of hydrogen fuel cell pile With a radiator fan, the outlet air surface of radiator fan is just to hydrogen fuel cell pile;
The side of hydrogen fuel cell pile is provided with DC/DC converters and controller, and DC/DC converters and controller are input into End connection hydrogen fuel cell pile, its output end connection unmanned plane dynamical system;
Hydrogen fuel cell pile connects a hydrogen storage bottle, and hydrogen storage bottle provides hydrogen for hydrogen fuel cell pile, and hydrogen storage is bottled to be had Hydrogen, delivery outlet is connected with hydrogen fuel cell pile.
Used as preferred technical scheme, also including a battery, battery connects DC/DC converters and controller, radiating Fan input connects the battery and by the storage battery power supply.
Used as preferred technical scheme, there is electrochemistry by hydrogen fuel cell pile in the hydrogen being input into the oxygen in air Reaction produces electric energy.
The beneficial effects of the utility model are:For the relatively general battery of hydrogen fuel cell power-supply system, with cleaning Environmental protection, output power, the features such as noise is less, the hydrogen fuel cell power supply used by the utility model overcomes the continuous of conventional power source The short problem of ETS estimated time of sailing, to realize multi-rotor unmanned aerial vehicle cruising time length, rational in infrastructure, easy to operate advantage.
Description of the drawings
In order to be illustrated more clearly that the utility model embodiment or technical scheme of the prior art, below will be to embodiment Or the accompanying drawing to be used needed for description of the prior art is briefly described, it should be apparent that, drawings in the following description are only It is some embodiments of the present utility model, for those of ordinary skill in the art, in the premise for not paying creative work Under, can be with according to these other accompanying drawings of accompanying drawings acquisition.
Fig. 1 is configuration schematic diagram of the present utility model.
Specific embodiment
All features disclosed in this specification, or disclosed all methods or during the step of, except mutually exclusive Feature and/or step beyond, can combine by any way.
Any feature disclosed in this specification (including any accessory claim, summary and accompanying drawing), except non-specifically is chatted State, can alternative features equivalent by other or with similar purpose replaced.I.e., unless specifically stated otherwise, each feature It is an example in a series of equivalent or similar characteristics.
As shown in figure 1, including the fuel cell being installed on unmanned plane, the fuel cell is hydrogen fuel cell pile 1, hydrogen The bottom of fuel cell pile 1 has a radiator fan 5, and the outlet air surface of radiator fan 5 is just to hydrogen fuel cell pile 1;
The side of hydrogen fuel cell pile 1 is provided with DC/DC converters and controller 4, DC/DC converters and controller 4 Input connection hydrogen fuel cell pile 1, its output end connection unmanned plane dynamical system;
Hydrogen fuel cell pile connects a hydrogen storage bottle 2, and hydrogen storage bottle 2 provides hydrogen for hydrogen fuel cell pile, and hydrogen storage is bottled There is hydrogen, delivery outlet is connected with hydrogen fuel cell pile.
Also include a battery 3, battery connection DC/DC converters and controller, radiator fan input connects the storage Battery simultaneously passes through the storage battery power supply.
There is electrochemical reaction generation electric energy by hydrogen fuel cell pile in the hydrogen being input into, and pass through with the oxygen in air DC/DC converters and controller export the part electric energy that hydrogen fuel cell pile is produced after conversion gives unmanned plane dynamical system System.Meanwhile, the battery in the utility model can increase due to connecting unmanned plane dynamical system as standby Emergency use Flight safety.
The beneficial effects of the utility model are:For the relatively general battery of hydrogen fuel cell power-supply system, with cleaning Environmental protection, output power, the features such as noise is less, the hydrogen fuel cell power supply used by the utility model overcomes the continuous of conventional power source The short problem of ETS estimated time of sailing, to realize multi-rotor unmanned aerial vehicle cruising time length, rational in infrastructure, easy to operate advantage.
The above, specific embodiment only of the present utility model, but protection domain of the present utility model do not limit to In this, any change or replacement expected without creative work all should be covered within protection domain of the present utility model. Therefore, the protection domain that protection domain of the present utility model should be limited by claims is defined.

Claims (3)

1. a kind of hydrogen fuel cell power supply in unmanned plane field, it is characterised in that:Including the fuel cell being installed on unmanned plane, The fuel cell is hydrogen fuel cell pile, and the bottom of hydrogen fuel cell pile has a radiator fan, the air-out of radiator fan Face is just to hydrogen fuel cell pile;
The side of hydrogen fuel cell pile is provided with DC/DC converters and controller, and DC/DC converters and controller input connect Hydrogen fuel cell pile is connect, its output end connection unmanned plane dynamical system;
Hydrogen fuel cell pile connects a hydrogen storage bottle, and hydrogen storage bottle provides hydrogen for hydrogen fuel cell pile, and hydrogen storage is bottled hydrogen, Delivery outlet is connected with hydrogen fuel cell pile.
2. the hydrogen fuel cell power supply in unmanned plane field as claimed in claim 1, it is characterised in that:Also include a battery, Battery connects unmanned plane dynamical system and DC/DC converters and controller, and radiator fan input connects the battery simultaneously By the storage battery power supply.
3. the hydrogen fuel cell power supply in unmanned plane field as claimed in claim 1, it is characterised in that:Hydrogen fuel cell pile will There is electrochemical reaction generation electric energy with the oxygen in air in the hydrogen of input.
CN201621079848.9U 2016-09-26 2016-09-26 Hydrogen cell power in unmanned aerial vehicle field Expired - Fee Related CN206098554U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201621079848.9U CN206098554U (en) 2016-09-26 2016-09-26 Hydrogen cell power in unmanned aerial vehicle field

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201621079848.9U CN206098554U (en) 2016-09-26 2016-09-26 Hydrogen cell power in unmanned aerial vehicle field

Publications (1)

Publication Number Publication Date
CN206098554U true CN206098554U (en) 2017-04-12

Family

ID=58479731

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201621079848.9U Expired - Fee Related CN206098554U (en) 2016-09-26 2016-09-26 Hydrogen cell power in unmanned aerial vehicle field

Country Status (1)

Country Link
CN (1) CN206098554U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107193285A (en) * 2017-04-20 2017-09-22 湖北工业大学 Many rotor fuel cell plant protection unmanned aerial vehicle control systems and its method of work
CN113193209A (en) * 2021-04-25 2021-07-30 电子科技大学 Air-cooled type fuel cell dual-stack integrated power system of fixed-wing unmanned aerial vehicle

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107193285A (en) * 2017-04-20 2017-09-22 湖北工业大学 Many rotor fuel cell plant protection unmanned aerial vehicle control systems and its method of work
CN107193285B (en) * 2017-04-20 2020-11-10 湖北工业大学 Multi-rotor-wing fuel cell plant protection unmanned aerial vehicle control system and working method thereof
CN113193209A (en) * 2021-04-25 2021-07-30 电子科技大学 Air-cooled type fuel cell dual-stack integrated power system of fixed-wing unmanned aerial vehicle
CN113193209B (en) * 2021-04-25 2022-07-26 电子科技大学 Air cooling type fuel cell double-stack integrated power system of fixed-wing unmanned aerial vehicle

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Granted publication date: 20170412