CN205810964U - A kind of high temperature early warning system of unmanned plane fuel cell - Google Patents

A kind of high temperature early warning system of unmanned plane fuel cell Download PDF

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Publication number
CN205810964U
CN205810964U CN201620601208.3U CN201620601208U CN205810964U CN 205810964 U CN205810964 U CN 205810964U CN 201620601208 U CN201620601208 U CN 201620601208U CN 205810964 U CN205810964 U CN 205810964U
Authority
CN
China
Prior art keywords
fuel cell
main fuel
pcb board
unmanned plane
standby lithium
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
CN201620601208.3U
Other languages
Chinese (zh)
Inventor
卢致辉
陈金颖
袁琦
田伟程
侯磊
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
Original Assignee
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 CN201620601208.3U priority Critical patent/CN205810964U/en
Application granted granted Critical
Publication of CN205810964U publication Critical patent/CN205810964U/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
    • Y02BCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
    • Y02B90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02B90/10Applications of fuel cells in buildings
    • 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 the high temperature early warning system of a kind of unmanned plane fuel cell, including the main fuel cell being installed in unmanned plane body and the standby lithium pond being arranged at main fuel cell side, a pcb board is installed in the upper end in main fuel cell and standby lithium pond, rectify under pcb board and main fuel cell is respectively provided with a power supply with standby lithium pond is connected post, the main fuel cell that power supply is just connecting post is provided with the first metal contact piece and the second metal contact piece with upper surface, standby lithium pond, one micromachine is installed between main fuel cell and standby lithium pond, one driving lever is set on the motor shaft of micromachine, one end of driving lever is insulating segment, the other end is conductive segment.This utility model is by the way of using one lithium battery reserve battery of a fuel cell, when main fuel cell thermo-field thoery, automatically switch to reserve battery, prevent main fuel cell because the blast occurred when the too high heat radiation of temperature is inadequate or leakage situation, use safer.

Description

A kind of high temperature early warning system of unmanned plane fuel cell
Technical field
This utility model relates to the high temperature early warning system of a kind of unmanned plane fuel cell.
Background technology
Unmanned plane is after flying for long time, and the temperature of fuel cell will rise, and temperature aggravating reason is failed to understand, probably due to The temperature that cooling system problem occurs is too high, it is also possible to because the temperature that short circuit causes is too high, so when fuel cell temperature When spending height and be continuing with, then there will be the situation that fuel cell explodes, the most existing unmanned plane because temperature is too high It is also faced with that temperature is too high in use and situation about damaging.
Summary of the invention
Technical problem to be solved in the utility model is to provide a kind of automatic switchover when main fuel cell temperature is too high To standby lithium pond, effectively play the high temperature early warning system of the unmanned plane fuel cell of a high temperature warning function.
This utility model is achieved through the following technical solutions: the high temperature early warning system of a kind of unmanned plane fuel cell System, including the main fuel cell being installed in unmanned plane body and the standby lithium pond being arranged at main fuel cell side, main combustion A pcb board is installed in the upper end in material battery and standby lithium pond, rectifies and be respectively provided with main fuel cell with standby lithium pond under pcb board One power supply connects post, just power supply is connected main fuel cell and the upper surface, standby lithium pond of post be provided with the first metal contact piece with Second metal contact piece, the first metal contact piece, the second metal contact piece are connected between post all at a distance of 3mm, position with the power supply of pcb board lower end One micromachine is installed between main fuel cell and standby lithium pond, the motor shaft of micromachine arranges a driving lever, driving lever One end be insulating segment, the other end is conductive segment, and conductive segment is inserted in the first metal contact piece and is connected post with the power supply of pcb board lower end Between, it is achieved main fuel cell is connected with the power supply of pcb board.
As preferred technical scheme, described pcb board is also equipped with the first temperature detection chip and the second temperature detection Chip, main fuel cell upper surface, the temperature of the second temperature detection chip are close in the temperature detection face of the first temperature detection chip Detection faces is close to the upper surface in standby lithium pond.
As preferred technical scheme, described main fuel cell is sealed by a battery cover with the bottom in standby lithium pond.
As preferred technical scheme, the input of described micromachine passes through connecting line connecting PCB board, and micromachine leads to Crossing pcb board and control switch, micromachine is connected with stand-by power supply by power line.
As preferred technical scheme, described pcb board also being installed a temperature indicator, temperature indicator is arranged at a lamp Intracavity, outside arranges a transparent sealing panel.
The beneficial effects of the utility model are: this utility model is by using one lithium battery standby electricity of a fuel cell The mode in pond, when main fuel cell thermo-field thoery, automatically switches to reserve battery, prevents main fuel cell because temperature is too high The blast occurred when dispelling the heat inadequate or leakage situation, use safer.
Accompanying drawing explanation
In order to be illustrated more clearly that this utility model embodiment or technical scheme of the prior art, below will be to embodiment Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, the accompanying drawing in describing below is only It is embodiments more of the present utility model, for those of ordinary skill in the art, in the premise not paying creative work Under, it is also possible to other accompanying drawing is obtained according to these accompanying drawings.
Fig. 1 is structural representation of the present utility model.
Detailed description of the invention
All features disclosed in this specification, or disclosed all methods or during step, except mutually exclusive Feature and/or step beyond, all can combine by any way.
Any feature disclosed in this specification (including any accessory claim, summary and accompanying drawing), unless chatted especially State, all can be by other equivalences or there is the alternative features of similar purpose replaced.I.e., unless specifically stated otherwise, each feature is only It it is an example in a series of equivalence or similar characteristics.
As it is shown in figure 1, the high temperature early warning system of a kind of unmanned plane fuel cell of the present utility model, unmanned including being installed on Main fuel cell 12 in machine body and the standby lithium pond 7 being arranged at main fuel cell 12 side, main fuel cell 12 is with standby Installing a pcb board 1 with the upper end of lithium battery 7, pcb board is rectified for 1 time main fuel cell 12 and standby lithium pond 7 is respectively provided with an electricity Source connects post 8, and the main fuel cell 12 that power supply just connects post 8 is provided with the first metal contact piece with upper surface, standby lithium pond 7 13 and second metal contact piece 4, first metal contact piece the 13, second metal contact piece 4 is connected between post 8 all with the power supply of pcb board 1 lower end At a distance of 3mm, a micromachine 9 is installed between main fuel cell 12 and standby lithium pond 7, on the motor shaft of micromachine 9 Arranging a driving lever 15, one end of driving lever 15 is insulating segment, and the other end is conductive segment 14, and conductive segment 14 is inserted in the first metal contact piece 13 are connected between post 8 with the power supply of pcb board lower end, it is achieved main fuel cell is connected with the power supply of pcb board.
Wherein, pcb board 1 is also equipped with the first temperature detection chip 3 and the second temperature detection chip 2, the first temperature inspection Main fuel cell 12 upper surface is close in the temperature detection face surveying chip 3, and the temperature detection face of the second temperature detection chip 2 is close to standby With the upper surface of lithium battery 7, by temperature detection chip effect, detection main fuel cell and the temperature on standby lithium pond in real time Spend, and the control chip being transferred on pcb board by temperature data is made next step and processed.
Wherein, main fuel cell 12 seals 11 with the bottom in standby lithium pond 7 by a battery cover.
In the present embodiment, the input of micromachine 9 passes through connecting line connecting PCB board, and micromachine is controlled by pcb board Switch, micromachine is connected with stand-by power supply, when the temperature detected on main fuel cell is too high, now by power line Pcb board automatically controls micromachine and rotates, and micromachine rotates and drives driving lever and conductive segment to rotate, and is originally realized by conductive segment Main fuel cell electrically connects with pcb board, due to the rotation of micromachine, enters into the second metal and touch after conductive segment rotation turnback The upper end position of sheet, now conductive segment conducting standby lithium pond and pcb board, disconnect main fuel cell, and now main fuel cell can Temporary transient radiating and cooling.
Also installing a temperature indicator 5 on pcb board, temperature indicator 5 is arranged in a lamp chamber 6, and it is transparent that outside arranges one Sealing panel.Show redness when temperature is too high, when temperature is relatively low, show green, to user one prompting.
The beneficial effects of the utility model are: this utility model is by using one lithium battery standby electricity of a fuel cell The mode in pond, when main fuel cell thermo-field thoery, automatically switches to reserve battery, prevents main fuel cell because temperature is too high The blast occurred when dispelling the heat inadequate or leakage situation, use safer.
The above, detailed description of the invention the most of the present utility model, but protection domain of the present utility model does not limit to In this, any change expected without creative work or replacement, all should contain within protection domain of the present utility model. Therefore, protection domain of the present utility model should be as the criterion with the protection domain that claims are limited.

Claims (5)

1. the high temperature early warning system of a unmanned plane fuel cell, it is characterised in that: include the master being installed in unmanned plane body The upper end in fuel cell and the standby lithium pond being arranged at main fuel cell side, main fuel cell and standby lithium pond installs one Pcb board, rectifies under pcb board and with standby lithium pond, main fuel cell is respectively provided with a power supply is connected post, just to power supply connection post Main fuel cell and upper surface, standby lithium pond are provided with the first metal contact piece and the second metal contact piece, the first metal contact piece, the Two metal contact pieces are connected between post all at a distance of 3mm with the power supply of pcb board lower end, between main fuel cell and standby lithium pond Installing a micromachine, the motor shaft of micromachine arranges a driving lever, one end of driving lever is insulating segment, and the other end is conduction Section, conductive segment is inserted in the first metal contact piece and is connected between post with the power supply of pcb board lower end, it is achieved main fuel cell and pcb board Power supply connect.
The high temperature early warning system of unmanned plane fuel cell the most according to claim 1, it is characterised in that: on described pcb board Being also equipped with the first temperature detection chip and the second temperature detection chip, the temperature detection face of the first temperature detection chip is close to main Fuel cell upper surface, the upper surface in standby lithium pond is close in the temperature detection face of the second temperature detection chip.
The high temperature early warning system of unmanned plane fuel cell the most according to claim 1, it is characterised in that: described main fuel electricity Pond is sealed by a battery cover with the bottom in standby lithium pond.
The high temperature early warning system of unmanned plane fuel cell the most according to claim 1, it is characterised in that: described micromachine Input by connecting line connecting PCB board, micromachine controls switch by pcb board, micromachine by power line with standby Connect with power supply.
The high temperature early warning system of unmanned plane fuel cell the most according to claim 1, it is characterised in that: on described pcb board Also installing a temperature indicator, temperature indicator is arranged in a lamp chamber, and outside arranges a transparent sealing panel.
CN201620601208.3U 2016-06-16 2016-06-16 A kind of high temperature early warning system of unmanned plane fuel cell Expired - Fee Related CN205810964U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620601208.3U CN205810964U (en) 2016-06-16 2016-06-16 A kind of high temperature early warning system of unmanned plane fuel cell

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620601208.3U CN205810964U (en) 2016-06-16 2016-06-16 A kind of high temperature early warning system of unmanned plane fuel cell

Publications (1)

Publication Number Publication Date
CN205810964U true CN205810964U (en) 2016-12-14

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Application Number Title Priority Date Filing Date
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CN (1) CN205810964U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115363413A (en) * 2022-09-22 2022-11-22 广东威王集团有限公司 Safe electric rice cooker with good sealing performance

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115363413A (en) * 2022-09-22 2022-11-22 广东威王集团有限公司 Safe electric rice cooker with good sealing performance

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C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20161214