CN110265594A - A kind of graphene battery for unmanned plane - Google Patents
A kind of graphene battery for unmanned plane Download PDFInfo
- Publication number
- CN110265594A CN110265594A CN201910467440.0A CN201910467440A CN110265594A CN 110265594 A CN110265594 A CN 110265594A CN 201910467440 A CN201910467440 A CN 201910467440A CN 110265594 A CN110265594 A CN 110265594A
- Authority
- CN
- China
- Prior art keywords
- battery
- pedestal
- unmanned plane
- graphene
- heating column
- 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.)
- Withdrawn
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/60—Heating or cooling; Temperature control
- H01M10/61—Types of temperature control
- H01M10/613—Cooling or keeping cold
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/60—Heating or cooling; Temperature control
- H01M10/62—Heating or cooling; Temperature control specially adapted for specific applications
- H01M10/625—Vehicles
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/60—Heating or cooling; Temperature control
- H01M10/65—Means for temperature control structurally associated with the cells
- H01M10/653—Means for temperature control structurally associated with the cells characterised by electrically insulating or thermally conductive materials
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M2220/00—Batteries for particular applications
- H01M2220/20—Batteries in motive systems, e.g. vehicle, ship, plane
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Battery Mounting, Suspending (AREA)
- Secondary Cells (AREA)
Abstract
The invention discloses a kind of graphene batteries for unmanned plane, including pedestal and shell；The side of the pedestal is connected with plug, the upper surface of pedestal is connected with the multiple battery packs being distributed in honeycomb, the battery pack includes six battery cores of heating column and circular array distribution, and the surface of the heating column has graphene, and the bottom of heating column is also connected with pedestal；The cross section of the battery core is triangular in shape, and the head of battery core is fitted on heating column；The shell is equipped with the through slot to match with battery pack outer wall, and the bottom of shell is connected with pedestal, present apparatus rapid heat dissipation, stable structure.
Description
Technical field
The present invention relates to a kind of graphene batteries for unmanned plane.
Background technique
Battery is that chemical energy is converted into the device of electric energy chemical cell, commonly abbreviated as battery.It, can after electric discharge
Internal active material is regenerated with the mode of charging --- electric energy is stored as chemical energy；Chemical energy is turned again when needing to discharge
It is changed to electric energy, this kind of battery is known as battery, also referred to as secondary cell；So-called battery is storage chemical energy, in necessity
When release electric energy a kind of electrochemical devices.
It is necessarily required to be powered it using battery in unmanned plane, to guarantee the normal/cruise of unmanned plane, especially
In mission phase, since power consumption rate is fast, battery there is also the bad situation that radiates, when unmanned plane rises and falls, it is also necessary to protect
The structural strength for demonstrate,proving battery pack is enough, to prevent battery pack from damaging the case where revealing.
Graphene is as a kind of novel material, with its good performance by the concern of people, especially in unmanned plane
How flight domain solves the problems such as unmanned plane cruise duration is short, battery is inflammable, battery pack structure is not sufficiently stable, graphene material
Material provides thinking direction well in these fields for researcher.
Summary of the invention
The purpose of the present invention is to solve the above the deficiencies in the prior art, propose a kind of graphene for unmanned plane
Battery.
A kind of graphene battery for unmanned plane, including pedestal and shell；The side of the pedestal is connected with plug, pedestal
Upper surface be connected in honeycomb be distributed multiple battery packs, the battery pack include heating column and circular array distribution
Six battery cores, the surface of the heating column has graphene, and the bottom of heating column is also connected with pedestal；The battery core it is transversal
Face is triangular in shape, and the head of battery core is fitted on heating column；The shell is equipped with the through slot to match with battery pack outer wall,
The bottom of shell is connected with pedestal.
Preferably, the quantity of the battery pack is 7.
Preferably, the material of the shell is hard aluminium alloy.
Preferably, the material of the pedestal is stainless steel.
Preferably, it is connected between the pedestal and battery pack by heat conductive silica gel.
The utility model has the advantages that
Multiple battery cores are in first hexagonal annulus array by honey comb like distribution mode by the present apparatus, and utilize centre
The graphene layer on heating column surface carries out hot transmitting, to prevent battery core from radiating in the operating condition undesirable happen.
And whole battery pack is in honeycomb distribution once more, to guarantee the structural stability of battery pack, to realize electricity
High intensity, the high energy source density, high heat dispersion of Chi Bao entirety.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of graphene battery for unmanned plane；
Fig. 2 is the structural schematic diagram of internal battery；
Fig. 3 is the explosive view of battery pack；
1. 41. battery core of pedestal 2. shell, 3. plug, 4. battery pack, 42. heating column.
Specific embodiment
In order to deepen the understanding of the present invention, below in conjunction with embodiment and attached drawing, the invention will be further described, should
The examples are only for explaining the invention, is not intended to limit the scope of the present invention..
A kind of graphene battery for unmanned plane, including pedestal 1 and shell 2；The side of the pedestal 1 is connected with plug,
The upper surface of pedestal 1 is connected with 7 battery packs 4 being distributed in honeycomb, and the battery pack 4 includes heating column 42 and in a ring
Six battery cores 41 of array distribution, the surface of the heating column 42 have a graphene, the bottom of heating column 42 also with 1 phase of pedestal
Even；The cross section of the battery core 41 is triangular in shape, and the head of battery core 41 is fitted on heating column 42；It is set on the shell 2
There is the through slot to match with 4 outer wall of battery pack, the bottom of shell 2 is connected with pedestal, passes through thermal conductive silicon between pedestal 1 and battery pack 4
Glue is connected.The material of the shell 2 is hard aluminium alloy, and the material of the pedestal 1 is stainless steel.
When the battery core in battery pack 4 in a state of use when, the heat that battery core 41 generates passes through the stone on 42 surface of heating column
Black alkene is passed down to pedestal 1, then is distributed outward by pedestal 1.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Within mind and principle, any modification, equivalent replacement, improvement and so on be should all be included in the protection scope of the present invention.
Claims (5)
1. a kind of graphene battery for unmanned plane, which is characterized in that including pedestal and shell；The side of the pedestal is connected with
Plug, the upper surface of pedestal are connected with the multiple battery packs being distributed in honeycomb, and the battery pack includes heating column and is in ring
The surface of six battery cores of shape array distribution, the heating column has graphene, and the bottom of heating column is also connected with pedestal；It is described
The cross section of battery core is triangular in shape, and the head of battery core is fitted on heating column；The shell is equipped with and battery pack outer wall
The bottom of the through slot of matching, shell is connected with pedestal.
2. a kind of graphene battery for unmanned plane according to claim 1, which is characterized in that the number of the battery pack
Amount is 7.
3. a kind of graphene battery for unmanned plane according to claim 1, which is characterized in that the material of the shell
For hard aluminium alloy.
4. a kind of graphene battery for unmanned plane according to claim 1, which is characterized in that the material of the pedestal
For stainless steel.
5. a kind of graphene battery for unmanned plane according to claim 1, which is characterized in that the pedestal and electricity
It is connected between the group of pond by heat conductive silica gel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910467440.0A CN110265594A (en) | 2019-05-31 | 2019-05-31 | A kind of graphene battery for unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910467440.0A CN110265594A (en) | 2019-05-31 | 2019-05-31 | A kind of graphene battery for unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110265594A true CN110265594A (en) | 2019-09-20 |
Family
ID=67916059
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910467440.0A Withdrawn CN110265594A (en) | 2019-05-31 | 2019-05-31 | A kind of graphene battery for unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110265594A (en) |
-
2019
- 2019-05-31 CN CN201910467440.0A patent/CN110265594A/en not_active Withdrawn
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190920 |
|
| WW01 | Invention patent application withdrawn after publication |