CN106058591A - Unmanned plane power source quick plugging device and unmanned plane - Google Patents
Unmanned plane power source quick plugging device and unmanned plane Download PDFInfo
- Publication number
- CN106058591A CN106058591A CN201610555511.9A CN201610555511A CN106058591A CN 106058591 A CN106058591 A CN 106058591A CN 201610555511 A CN201610555511 A CN 201610555511A CN 106058591 A CN106058591 A CN 106058591A
- Authority
- CN
- China
- Prior art keywords
- plug
- unmanned plane
- electric energy
- battery
- energy output
- 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.)
- Pending
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R24/00—Two-part coupling devices, or either of their cooperating parts, characterised by their overall structure
- H01R24/66—Two-part coupling devices, or either of their cooperating parts, characterised by their overall structure with pins, blades or analogous contacts and secured to apparatus or structure, e.g. to a wall
-
- 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
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R24/00—Two-part coupling devices, or either of their cooperating parts, characterised by their overall structure
- H01R24/76—Two-part coupling devices, or either of their cooperating parts, characterised by their overall structure with sockets, clips or analogous contacts and secured to apparatus or structure, e.g. to a wall
-
- 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
Abstract
The invention discloses an unmanned plane power source quick plugging device. The unmanned plane power source quick plugging device comprises a power source supplying system and an electrical energy input plug, wherein the power source supplying system is an integrated structure comprising a cell chamber, an electrical energy output plug and cells, the cells are mounted in the cell chamber, the electrical energy output plug is electrically connected with the cells, the electrical energy input plug is fixedly mounted on a body of an unmanned plane, and the electrical energy output plug of the power source supplying system is in plugging connection with the electrical energy input plug on the body of the unmanned plane during use. According to the unmanned plane power source quick plugging device, the power source supplying system is the integrated structure, the power source supplying system is mounted on the body of the unmanned plane only through inserting the electrical energy output plug into the electrical energy input plug on the body, a combined portion of the cell chamber and the body is simple in structure, the cells are convenient and quick to replace, and errors of an assembling process can be avoided.
Description
Technical field
The invention belongs to the part design technical field of light aerocraft and SUAV, particularly relate to a kind of unmanned plane
The fast plug device of power supply, and the unmanned plane of this fast plug device is installed.
Background technology
Unmanned plane is with its use configuration flexible, airborne variation, hang time length, flexible operation, economic and practical, training dimension
Repair low cost and other advantages, succeed fortune in many military fields such as investigation, air-to-ground attack, interference, message interrupts, over the ground support
With.
The battery of unmanned plane is positioned at unmanned aerial vehicle body, mainly provides power to aircraft, it is ensured that aircraft can effectively complete to fly
Row task, battery contact needs to connect reliable in performing task process at aircraft.If the battery contact of aircraft can not obtain
Well fastening, then the safety for in-flight aircraft will have very big hidden danger.The most therefore connector female end is connect
Touch reliability aspect and propose higher requirement, contain male, and can be reliably connected under harsh conditions.Now the most military also
Being civilian, require more and more higher to unmanned plane flying power, the lithium battery on electronic unmanned plane must install high-multiplying power discharge
Lithium battery, because aircraft requirements weight is light as far as possible, output is the biggest.The output of battery is the biggest at battery plug
Plug connection procedure in the easiest plug position produce spark, big electric current by wire cause battery-heating, burning or
Burn out mainboard.
Existing battery compartment is arranged in body, need connect battery time it is generally required to open the Cang Gai of battery compartment, then
The plug being connected with battery is inserted the circuit plug of fuselage, is then shut off the hatchcover of battery compartment.Traditional battery compartment and body
Junction structure complexity loaded down with trivial details, change battery waste time and energy, assembling process is easily made a slip-up, causes serious consequence.
Summary of the invention
The first object of the present invention is to provide a kind of fast plug device of unmanned plane power supply.
The second object of the present invention is to provide a kind of unmanned plane.
In order to realize above-mentioned first purpose, the present invention provides a kind of fast plug device of unmanned plane power supply, comprising:
Power system, described power system is made up of battery compartment, electric energy output plug and battery, is integrated knot
Structure；Battery is arranged in described battery compartment, and electric energy output plug electrically connects with described battery；
Electric energy input plug, described electric energy input plug is fixedly mounted on the body of unmanned plane；
During use, the electric energy output plug of power system is inserted with the electric energy input plug being arranged on unmanned plane body
Pull out connection.
The present invention unmanned plane as above fast plug device of power supply, further, described power system also includes power supply
Switch, described on and off switch is for controlling being switched on or switched off between electric energy output plug and battery.
The present invention unmanned plane as above fast plug device of power supply, further, described electric energy output plug is female end, institute
Stating electric energy input plug is male end；Or, described electric energy output plug is male end, and described electric energy input plug is female
End.
The present invention unmanned plane as above fast plug device of power supply, further, described female end includes cathode metal terminal
With negative metal terminal, described male end includes cathode metal terminal and negative metal terminal.
The present invention unmanned plane as above fast plug device of power supply, further, described battery is rechargeable battery, described electricity
Pond is detachably arranged in described battery compartment.
In order to realize above-mentioned second purpose, the present invention provides a kind of unmanned plane, and described unmanned plane includes that body and power supply are fast
Plug device, the fast plug device of power supply includes power system, and described power system is by battery compartment, electric energy output plug and electricity
Pond forms, and is structure as a whole；Battery is arranged in described battery compartment, and electric energy output plug electrically connects with described battery；Electric energy is defeated
Entering plug, described electric energy input plug is fixedly mounted on the body of unmanned plane；During use, the electric energy output of power system
Plug is connected with the electric energy input plug plug being arranged on unmanned plane body.
Present invention unmanned plane as above, further, described power system also includes on and off switch, described power supply
Switch is for controlling being switched on or switched off between electric energy output plug and battery.
Present invention unmanned plane as above, further, described electric energy output plug is female end, and the input of described electric energy is inserted
Head is male end；Or, described electric energy output plug is male end, and described electric energy input plug is female end.
Present invention unmanned plane as above, further, described female end includes cathode metal terminal and negative metal end
Son, described male end includes cathode metal terminal and negative metal terminal.
Present invention unmanned plane as above, further, described battery is rechargeable battery, the peace of described battery-disassembled
It is contained in described battery compartment.
The invention has the beneficial effects as follows:
Stable connection and assembling are quick.Owing to power system is integral structure, power system is being installed
Only need to insert electric energy output plug the electric energy input plug of body, battery compartment and the knot of body time on unmanned plane body
Simple in construction at conjunction, changes battery convenient and swift, it is to avoid make mistakes in assembling process.
Additionally, on and off switch is for controlling being switched on or switched off between electric energy output plug and battery.By power supply supply
System turns off the power switch before being installed to unmanned plane body, it is to avoid battery plug produces spark, greatly electricity in plug connection procedure
Stream is caused battery-heating by wire, burn or is burnt out mainboard.
Accompanying drawing explanation
By the detailed description made in conjunction with the following drawings, above-mentioned and/or other aspects of the present invention and advantage will become
Becoming apparent from and be easier to understand, these accompanying drawings the most schematically, are not limiting as the present invention, wherein:
Fig. 1 is the power system schematic diagram of an embodiment of the present invention；
Fig. 2 is the electric energy input plug body scheme of installation with unmanned plane of an embodiment of the present invention；
Fig. 3 is the electric energy output plug of an embodiment of the present invention, battery and on and off switch connection diagram.
In accompanying drawing, the list of parts representated by each label is as follows:
1, electric energy input plug, 11, plug body, 12, metal terminal；
2, power system, 21, electric energy output plug, 22, battery compartment, 23, battery, 24, on and off switch；
3, the body of unmanned plane；
4, bolt.
Detailed description of the invention
Hereinafter, the embodiment of the fast plug device of unmanned plane power supply of the present invention is described with reference to the accompanying drawings.
The embodiment recorded at this is the specific detailed description of the invention of the present invention, for the design of the present invention being described, all
It is explanatory and exemplary, should not be construed as the restriction to embodiment of the present invention and the scope of the invention.Except record at this
Outside embodiment, those skilled in the art can also based on the application claims and description disclosure of that use aobvious and
Other technical scheme being clear to, these technical schemes include use to the embodiment recorded at this make any obviously
The technical scheme of substitutions and modifications.
The accompanying drawing of this specification is schematic diagram, aids in illustrating the design of the present invention, it is schematically indicated the shape of each several part
And mutual relation.Note that the structure of each parts for the ease of clearly showing the embodiment of the present invention, between each accompanying drawing
Do not draw according to identical ratio.Identical reference marker is used for representing identical part.
The fast plug device of unmanned plane power supply of an embodiment of the present invention is described below in conjunction with attached Fig. 1 and 2, comprising:
Power system 2, as it is shown in figure 1, described power system is by battery compartment 22, electric energy output plug 21 and electricity
Pond 23 forms, and is structure as a whole；Battery 23 is arranged in described battery compartment 22, and electric energy output plug 21 is electrically connected with described battery 23
Connect；
Electric energy input plug 1, as in figure 2 it is shown, described electric energy input plug 1 is fixedly mounted on the body 3 of unmanned plane；
During use, the electric energy output plug 21 of power system 2 is inserted with the electric energy input being arranged on unmanned plane body 3
1 plug connects.
Owing to power system is integral structure, only need when power system is installed on unmanned plane body
Electric energy output plug is inserted the electric energy input plug of body, the junction simple in construction of battery compartment and body, changes electricity
Pond is convenient and swift, it is to avoid make mistakes in assembling process.
In the embodiment improved further, as it is shown on figure 3, described power system 2 also includes on and off switch 24, institute
State on and off switch 24 for controlling being switched on or switched off between electric energy output plug 21 and battery 23.Power system is being pacified
Turn off the power switch before installing to unmanned plane body, it is to avoid battery plug produces spark in plug connection procedure, and big electric current passes through
Wire causes battery-heating, burns or burns out mainboard.Illustrate only a wire being connected with switch in figure 3, it is only
For signal effect, actually include double joint wire, respectively as both positive and negative polarity.On and off switch can control solid conductor disconnection or
Connect, it is also possible to disconnect while controlling double joint wire or connect.
In embodiment as shown in figures 1 and 2, electric energy output plug 21 is female end, and electric energy input plug 1 is male
End, inserts male end by female end when assembling uses.According to product needed can also be electric energy output plug 21 be male
End, electric energy input plug 1 is female end.In a preferred embodiment, described female end includes cathode metal terminal and negative pole gold
Belonging to terminal, described male end includes cathode metal terminal and negative metal terminal.In a kind of specific embodiment, described male end
Being XT90 plug with female end, material the most easily selects.In the embodiment illustrated in figure 2, electric energy input plug is male end, its bag
Including plug body 11 and metal terminal 12, electric energy input plug 1 is fixed on the body 3 of unmanned plane by bolt 4.
In the present invention unmanned plane as above fast plug device of power supply, described battery 23 is rechargeable battery, such as lithium electricity
Pond.Described battery 23 is detachably arranged in described battery compartment 22.
The embodiment of the present invention also provides for a kind of unmanned plane, and described unmanned plane includes body 3 and the fast plug device of power supply, and power supply is fast
Plug device includes power system 2, and described power system is by battery compartment 22, electric energy output plug 21 and 23 groups of battery
Become, be structure as a whole；Battery 23 is arranged in described battery compartment 22, and electric energy output plug 21 electrically connects with described battery 23；Electricity
Energy input plug 1, described electric energy input plug 1 is fixedly mounted on the body 3 of unmanned plane；During use, power system 2
Electric energy output plug 21 is connected with electric energy input plug 1 plug being arranged on unmanned plane body 3.
The fast plug device of power supply in above-mentioned unmanned plane can also be carried out according to the embodiment of the fast plug device of above-mentioned power supply accordingly
Improvement, do not repeat them here.
Each technical characteristic of above-mentioned disclosure is not limited to disclosed and further feature combination, and those skilled in the art are also
Other combination between each technical characteristic can be carried out according to the purpose of invention, be as the criterion realizing the purpose of the present invention.
Claims (10)
1. the fast plug device of unmanned plane power supply, it is characterised in that including:
Power system, described power system is made up of battery compartment, electric energy output plug and battery, is structure as a whole；
Battery is arranged in described battery compartment, and electric energy output plug electrically connects with described battery；
Electric energy input plug, described electric energy input plug is fixedly mounted on the body of unmanned plane；
During use, the electric energy output plug of power system is with the electric energy input plug plug being arranged on unmanned plane body even
Connect.
The fast plug device of unmanned plane power supply the most according to claim 1, it is characterised in that described power system also includes
On and off switch, described on and off switch is for controlling being switched on or switched off between electric energy output plug and battery.
The fast plug device of unmanned plane power supply the most according to claim 1 and 2, it is characterised in that described electric energy output plug is
Female end, described electric energy input plug is male end；Or, described electric energy output plug is male end, and the input of described electric energy is inserted
Head is female end.
The fast plug device of unmanned plane power supply the most according to claim 3, it is characterised in that described female end includes cathode metal
Terminal and negative metal terminal, described male end includes cathode metal terminal and negative metal terminal.
The fast plug device of unmanned plane power supply the most according to claim 1, it is characterised in that described battery is rechargeable battery,
Being arranged in described battery compartment of described battery-disassembled.
6. a unmanned plane, described unmanned plane includes body and the fast plug device of power supply, it is characterised in that the fast plug device of power supply includes
Power system, described power system is made up of battery compartment, electric energy output plug and battery, is structure as a whole；Battery
Being arranged in described battery compartment, electric energy output plug electrically connects with described battery；Electric energy input plug, described electric energy input plug
It is fixedly mounted on the body of unmanned plane；During use, the electric energy output plug of power system be arranged on unmanned plane body
On electric energy input plug plug connect.
Unmanned plane the most according to claim 6, it is characterised in that described power system also includes on and off switch, institute
State on and off switch for controlling being switched on or switched off between electric energy output plug and battery.
8. according to the unmanned plane described in claim 6 or 7, it is characterised in that described electric energy output plug is female end, described electricity
Can input plug be male end；Or, described electric energy output plug is male end, and described electric energy input plug is female end.
Unmanned plane the most according to claim 8, it is characterised in that described female end includes cathode metal terminal and negative pole gold
Belonging to terminal, described male end includes cathode metal terminal and negative metal terminal.
Unmanned plane the most according to claim 6, it is characterised in that described battery is rechargeable battery, and described battery is removable
That unloads is arranged in described battery compartment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610555511.9A CN106058591A (en) | 2016-07-15 | 2016-07-15 | Unmanned plane power source quick plugging device and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610555511.9A CN106058591A (en) | 2016-07-15 | 2016-07-15 | Unmanned plane power source quick plugging device and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106058591A true CN106058591A (en) | 2016-10-26 |
Family
ID=57186835
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610555511.9A Pending CN106058591A (en) | 2016-07-15 | 2016-07-15 | Unmanned plane power source quick plugging device and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106058591A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628105A (en) * | 2017-02-28 | 2017-05-10 | 天峋（常州）智能科技有限公司 | Unmanned aerial vehicle with rod-shaped plug batteries |
| CN108807032A (en) * | 2017-04-27 | 2018-11-13 | 南京福尔摩斯智能科技有限公司 | Low-voltage forceful electric power streaming high power switch |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103701163A (en) * | 2013-12-06 | 2014-04-02 | 深圳市大疆创新科技有限公司 | Battery, aircraft with battery and battery control method |
| CN204415738U (en) * | 2014-12-29 | 2015-06-24 | 深圳一电科技有限公司 | Battery and unmanned plane |
| CN204998786U (en) * | 2015-08-06 | 2016-01-27 | 广州极飞电子科技有限公司 | Power module and unmanned aerial vehicle who has this power module |
| CN205081532U (en) * | 2015-11-13 | 2016-03-09 | 深圳高科新农技术有限公司 | Power for unmanned aerial vehicle |
| CN205131686U (en) * | 2015-08-05 | 2016-04-06 | 北京韦加天地通航空科技有限公司 | A prevent striking sparks wiring circuit and unmanned aerial vehicle for unmanned aerial vehicle power battery |
| WO2016074134A1 (en) * | 2014-11-10 | 2016-05-19 | 深圳市大疆创新科技有限公司 | Battery, heat management apparatus thereof and uav having the battery |
| CN205790804U (en) * | 2016-07-15 | 2016-12-07 | 天峋（常州）智能科技有限公司 | A kind of fast plug device of unmanned plane power supply and unmanned plane |
-
2016
- 2016-07-15 CN CN201610555511.9A patent/CN106058591A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103701163A (en) * | 2013-12-06 | 2014-04-02 | 深圳市大疆创新科技有限公司 | Battery, aircraft with battery and battery control method |
| WO2016074134A1 (en) * | 2014-11-10 | 2016-05-19 | 深圳市大疆创新科技有限公司 | Battery, heat management apparatus thereof and uav having the battery |
| CN204415738U (en) * | 2014-12-29 | 2015-06-24 | 深圳一电科技有限公司 | Battery and unmanned plane |
| CN205131686U (en) * | 2015-08-05 | 2016-04-06 | 北京韦加天地通航空科技有限公司 | A prevent striking sparks wiring circuit and unmanned aerial vehicle for unmanned aerial vehicle power battery |
| CN204998786U (en) * | 2015-08-06 | 2016-01-27 | 广州极飞电子科技有限公司 | Power module and unmanned aerial vehicle who has this power module |
| CN205081532U (en) * | 2015-11-13 | 2016-03-09 | 深圳高科新农技术有限公司 | Power for unmanned aerial vehicle |
| CN205790804U (en) * | 2016-07-15 | 2016-12-07 | 天峋（常州）智能科技有限公司 | A kind of fast plug device of unmanned plane power supply and unmanned plane |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628105A (en) * | 2017-02-28 | 2017-05-10 | 天峋（常州）智能科技有限公司 | Unmanned aerial vehicle with rod-shaped plug batteries |
| CN108807032A (en) * | 2017-04-27 | 2018-11-13 | 南京福尔摩斯智能科技有限公司 | Low-voltage forceful electric power streaming high power switch |
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Application publication date: 20161026 |