CN205811623U - A kind of contact unmanned plane automatic charge device - Google Patents
A kind of contact unmanned plane automatic charge device Download PDFInfo
- Publication number
- CN205811623U CN205811623U CN201620780872.9U CN201620780872U CN205811623U CN 205811623 U CN205811623 U CN 205811623U CN 201620780872 U CN201620780872 U CN 201620780872U CN 205811623 U CN205811623 U CN 205811623U
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- charging
- unmanned plane
- charging inlet
- automatic charge
- charge device
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Abstract
This utility model relates to a kind of contact unmanned plane automatic charge device, including recharging base and charging panel, it is provided with charge controller in described recharging base, some pieces of charging lumps it have been covered with on described charging panel, every piece of charging lump is connected with charge controller respectively, unmanned plane leg is provided with the first charging inlet and the second charging inlet, described first charging inlet and the second charging inlet are conflicted from different charging lumps respectively, thus solve unmanned plane and need artificial unloading to change battery when low-voltage state, or use dock automatically land charger time need to be aided with high-precision positioner problem, achieve unmanned plane in the case of unmanned automatically land charging and continue Mission Operations, there is simple in construction, with low cost, automaticity advantages of higher.
Description
Technical field
This utility model relates to unmanned air vehicle technique field, more specifically refers to a kind of contact unmanned plane automatic charging dress
Put.
Background technology
Unmanned plane is a kind of to realize the most manned of flight operation by wireless control link and onboard flight control system and fly
Machine, be widely used in agricultural plant protection at present, video display are taken photo by plane, power-line patrolling, mapping, environmental monitoring, the neck such as anti-terrorism investigation
Territory.
One main pain spot of current many rotor wing unmanned aerial vehicles industry is that battery life is too short, and average 20-30 minute left
Right battery life seriously constrains unmanned plane in range of application and the expansion in the application degree of depth.In use, one
Denier electricity is not enough, it is necessary to manual control unmanned plane lands, and more renews battery, or is pulled down by original battery, after fully charged
It is loaded on use.In this case, unmanned plane lacks ability of working continuously, and the experience property of whole system is deteriorated, simultaneously need to
Put into more human cost to safeguard.For this present situation, some domestic and international companies are also had to have developed the nothing of dock
Man-machine automatic charge device, by the Dock With Precision Position of unmanned plane charging bayonet socket with charging base station, it is achieved automatic charging, but this dress
Putting and typically require supporting high-precision positioner and use, to revise the error of current GPS location, the usual structure of such device is multiple
Miscellaneous, cost is high, and reliability exist the biggest problem.
Summary of the invention
This utility model provides a kind of contact unmanned plane automatic charge device, to solve many rotor wing unmanned aerial vehicles at low electricity
In the case of need manpower intervention change battery problem, it is achieved unmanned plane in the case of unmanned automatically land charging and
Continue Mission Operations.
This utility model adopts the following technical scheme that
A kind of contact unmanned plane automatic charge device, including recharging base and charging panel, described recharging base is provided with nothing
Man-machine hoistable platform, described charging panel is arranged on hoistable platform, it is characterised in that: it is provided with charging control in described recharging base
Device, described charging panel has been covered with some pieces of charging lumps, and every piece of charging lump is connected with charge controller respectively, on unmanned plane leg
Be provided with the first charging inlet and the second charging inlet, described first charging inlet and the second charging inlet respectively from different chargings
Block is conflicted.
Further, cornerwise length of every piece of charging lump is respectively less than between the first charging inlet and the second charging inlet
Away from.
Further, being provided with insulation projection between every piece of charging lump, described insulation is protruding to be arranged in equilateral triangle.
Further, described first charging inlet and the second charging inlet are that del is arranged.
Further, in described charge controller, be provided with capacitance-sensitive switch, described capacitance-sensitive switch respectively with every piece
Charging lump connects.
Further, described charge controller is nonpolarity charge controller.
Further, described recharging base is provided with a protective enclosure, and described protective enclosure is turning to be hidden in described liter
Above fall platform, or turning it is accommodated in recharging base.
From the above-mentioned description to this utility model structure, compared to the prior art, this utility model has the most excellent
Point:
1, during the automatic charge device operation of this utility model one contact unmanned plane, unmanned plane lands on hoistable platform
Charging panel on, owing to charging panel has been covered with some pieces of charging lumps, cornerwise length of every piece of charging lump is respectively less than unmanned plane
First charging inlet and the spacing of the second charging inlet on leg, so unmanned plane is when landing, the first charging on leg
Mouth can contact charging respectively with the second charging inlet with the charging lump of different masses, thus solves unmanned plane when low-voltage state
Artificial unloading is needed to change battery or need to be aided with high-precision positioner when use dock lands charger automatically
Problem, it is achieved that unmanned plane automatically lands in the case of unmanned and charges and continue Mission Operations, has simple in construction,
With low cost, automaticity advantages of higher.
2, being provided with insulation bulge clearance between every piece of charging lump to divide, insulation is protruding to be arranged in equilateral triangle, unmanned plane the
One charging port and the second charging port are that del is arranged, and thus, unmanned plane is when landing, and charging port will not just drop
Fall within insulation projection, it is ensured that charging port can fully be conflicted with charging lump and is connected.
3, recharging base is provided with a protective enclosure, and protective enclosure is turning to be hidden above hoistable platform, thus to filling
Electroplax or unmanned plane are protected, and reduce the impact of these devices of factor such as ambient weather, extend the service life of charging panel.And
And, protective enclosure is turning to be accommodated in recharging base, facilitates UAV Landing or leaves recharging base.
Accompanying drawing explanation
Fig. 1 is this utility model protective enclosure receiving state structural representation；
Fig. 2 is the enlarged diagram of A in Fig. 1；
Fig. 3 is this utility model charging panel top view；
Fig. 4 is B-B direction sectional view in Fig. 3；
Fig. 5 is that this utility model protective enclosure hides status architecture schematic diagram.
Detailed description of the invention
The detailed description of the invention of this utility model embodiment is described with reference to the accompanying drawings.
With reference to Fig. 1, Fig. 2 and Fig. 5, a kind of contact unmanned plane automatic charge device, including recharging base 1 and charging panel
2, ancillary equipment is unmanned plane 3, and unmanned plane 3 leg is provided with the first charging inlet 31 and the second charging inlet 32, the first charging
Interface 31 and the second charging inlet 32 are arranged in del.Recharging base 1 is provided with the lifting landed for unmanned plane 3 lifting
Platform 11 and protective enclosure 12, protective enclosure 12 is connected with recharging base 1 by rotary shaft 13, and turning covering is put down in lifting
Above platform 11, it is possible to upset is accommodated in recharging base 1.
With reference to Fig. 1, Fig. 3 and Fig. 4, charging panel 2 is arranged on hoistable platform 11.Some pieces of chargings it have been covered with on charging panel 2
Block 21, charging lump 21 can square or regular hexagon setting.Divided, absolutely by protruding 22 intervals of insulation between every piece of charging lump 21
Edge projection 22 is arranged in equilateral triangle, and cornerwise length of every piece of charging lump 21 is respectively less than unmanned plane 3 first charging inlet
31 and second spacing of charging inlet 32.
With reference to Fig. 1, in recharging base 1, be additionally provided with nonpolarity charge controller 4, charge controller 4 respectively with every piece of charging
Block 21 connects, for powering to charging lump 21.Capacitance-sensitive switch 41, capacitance-sensitive switch 41 it is additionally provided with in charge controller 4
It is connected with every piece of charging lump 21 respectively.
Referring to figs. 1 through Fig. 5, when unmanned plane 3 needs charging, unmanned plane 3 flies to nearest recharging base 1.Recharging base 1
On protective enclosure 12 upset be accommodated in recharging base 1, expose hoistable platform 11.Unmanned plane 3 is dropped by landing bootstrap technique
Fall within the charging panel 2 on hoistable platform 11, owing to charging panel 2 is provided with several charging lumps 21, every piece of charging lump 21 right
The length of linea angulata is respectively less than the first charging inlet 31 and spacing of the second charging inlet 32 on unmanned plane 3 leg, so unmanned plane 3
When landing, the first charging inlet 31 on leg and the second charging inlet 32 can charging lump 21 with different masses be conflicted respectively
Connect.After unmanned plane 3 comes to a complete stop, nonpolarity charge controller 4 senses the first charging inlet 31 by capacitance-sensitive switch 41
With any two block charging lumps 21 conflict respectively with the second charging inlet 32 and be connected, by the switching of relay, make these two pieces chargings
Block 21 becomes positive pole and the negative pole of power supply respectively, is charged for unmanned plane 3.Thus, unmanned plane 3 is landing on charging panel 2,
First charging port and the second charging port one connect from different charging lumps 21 the most respectively, solve existing unmanned plane 3 in fall
Fall and when charging, need precise positioning, or complete the problems such as charging manually.Meanwhile, on charging panel 2 every piece of charging lump 21 it
Between be provided with protruding 22 intervals of insulation and divide, protruding 22 settings triangular in shape of this insulation, unmanned plane 3 first charging inlet 31 and second
Charging inlet 32 is arranged in del, and thus, unmanned plane 3 is when landing on charging panel 2, and the first charging port and second fills
Electricity port will not just fall within insulation protruding 22, it is ensured that the first charging port and the second charging port can fill with charging lump 21
Dividing conflicts connects.
Above are only detailed description of the invention of the present utility model, but design concept of the present utility model be not limited thereto,
All changes utilizing this design that this utility model carries out unsubstantiality, all should belong to the row invading this utility model protection domain
For.
Claims (7)
1. a contact unmanned plane automatic charge device, including recharging base and charging panel, described recharging base is provided with unmanned
Machine hoistable platform, described charging panel is arranged on hoistable platform, it is characterised in that: it is provided with charging control in described recharging base
Device, described charging panel has been covered with some pieces of charging lumps, and every piece of charging lump is connected with charge controller respectively, on unmanned plane leg
Be provided with the first charging inlet and the second charging inlet, described first charging inlet and the second charging inlet respectively from different chargings
Block is conflicted.
2. according to a kind of contact unmanned plane automatic charge device described in claim 1, it is characterised in that: every piece of charging lump
Cornerwise length be respectively less than the first charging inlet and the spacing of the second charging inlet.
3. according to a kind of contact unmanned plane automatic charge device described in claim 1, it is characterised in that: every piece of charging lump
Between be provided with insulation projection, described insulation is protruding to be arranged in equilateral triangle.
4. according to a kind of contact unmanned plane automatic charge device described in claim 3, it is characterised in that: described first fills
Electrical interface and the second charging inlet are that del is arranged.
5. according to a kind of contact unmanned plane automatic charge device described in claim 1, it is characterised in that: described charging control
Being provided with capacitance-sensitive switch in device processed, described capacitance-sensitive switch is connected with every piece of charging lump respectively.
6. according to a kind of contact unmanned plane automatic charge device described in claim 1, it is characterised in that: described charging control
Device processed is nonpolarity charge controller.
7. according to a kind of contact unmanned plane automatic charge device described in claim 1, it is characterised in that: described charging base
Seat is provided with a protective enclosure, and described protective enclosure is turning to be hidden above described hoistable platform, or turning being accommodated in is filled
In electricity pedestal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620780872.9U CN205811623U (en) | 2016-07-25 | 2016-07-25 | A kind of contact unmanned plane automatic charge device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620780872.9U CN205811623U (en) | 2016-07-25 | 2016-07-25 | A kind of contact unmanned plane automatic charge device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205811623U true CN205811623U (en) | 2016-12-14 |
Family
ID=57509389
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620780872.9U Active CN205811623U (en) | 2016-07-25 | 2016-07-25 | A kind of contact unmanned plane automatic charge device |
Country Status (1)
| Country | Link |
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| CN (1) | CN205811623U (en) |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106992574A (en) * | 2017-05-18 | 2017-07-28 | 北京科技大学 | Multi-rotor unmanned aerial vehicle charging system and method |
| CN106992573A (en) * | 2017-05-18 | 2017-07-28 | 北京科技大学 | Multi-rotor unmanned aerial vehicle charging system and method |
| CN107044218A (en) * | 2017-06-15 | 2017-08-15 | 杭州迪洛智能设备有限公司 | A kind of base station equipment for unmanned plane automatic charging |
| CN107247453A (en) * | 2017-07-21 | 2017-10-13 | 杭州迪洛智能设备有限公司 | A kind of day eye detecting system |
| CN107512188A (en) * | 2017-09-07 | 2017-12-26 | 哈尔滨工业大学 | A kind of rotor wing unmanned aerial vehicle recharging device and its optimized parameter determine method |
| WO2018157461A1 (en) * | 2017-03-01 | 2018-09-07 | 广东百事泰电子商务股份有限公司 | Intelligent surface contact charging apparatus, system and method |
| CN108725820A (en) * | 2018-04-08 | 2018-11-02 | 北京领航智能科技发展有限公司 | Unmanned plane automatic charging platform |
| CN109774521A (en) * | 2019-01-18 | 2019-05-21 | 河北科技大学 | Unmanned plane docking system |
| CN110104195A (en) * | 2019-05-14 | 2019-08-09 | 广东电网有限责任公司 | A kind of unmanned plane automatic charging system with solar panel |
| CN110816327A (en) * | 2019-10-18 | 2020-02-21 | 西北工业大学 | Contact unmanned aerial vehicle autonomous charging system |
| CN111404239A (en) * | 2020-04-28 | 2020-07-10 | 上海交通大学 | A porous charging panel of antiskid for unmanned aerial vehicle descending charges |
| EP4139763A4 (en) * | 2021-02-01 | 2023-10-18 | Sagar Defence Engineering Private Limited | Method and system to ascertain location of drone box for stabilized landing and charging of drone |
-
2016
- 2016-07-25 CN CN201620780872.9U patent/CN205811623U/en active Active
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018157461A1 (en) * | 2017-03-01 | 2018-09-07 | 广东百事泰电子商务股份有限公司 | Intelligent surface contact charging apparatus, system and method |
| CN106992573B (en) * | 2017-05-18 | 2023-06-20 | 北京科技大学 | Multi-rotor unmanned aerial vehicle charging system and method |
| CN106992573A (en) * | 2017-05-18 | 2017-07-28 | 北京科技大学 | Multi-rotor unmanned aerial vehicle charging system and method |
| CN106992574A (en) * | 2017-05-18 | 2017-07-28 | 北京科技大学 | Multi-rotor unmanned aerial vehicle charging system and method |
| CN107044218A (en) * | 2017-06-15 | 2017-08-15 | 杭州迪洛智能设备有限公司 | A kind of base station equipment for unmanned plane automatic charging |
| CN107247453A (en) * | 2017-07-21 | 2017-10-13 | 杭州迪洛智能设备有限公司 | A kind of day eye detecting system |
| CN107512188A (en) * | 2017-09-07 | 2017-12-26 | 哈尔滨工业大学 | A kind of rotor wing unmanned aerial vehicle recharging device and its optimized parameter determine method |
| CN107512188B (en) * | 2017-09-07 | 2019-09-13 | 哈尔滨工业大学 | A kind of rotor wing unmanned aerial vehicle recharging device and its optimized parameter determine method |
| CN108725820A (en) * | 2018-04-08 | 2018-11-02 | 北京领航智能科技发展有限公司 | Unmanned plane automatic charging platform |
| CN109774521A (en) * | 2019-01-18 | 2019-05-21 | 河北科技大学 | Unmanned plane docking system |
| CN110104195A (en) * | 2019-05-14 | 2019-08-09 | 广东电网有限责任公司 | A kind of unmanned plane automatic charging system with solar panel |
| CN110816327B (en) * | 2019-10-18 | 2023-04-14 | 西北工业大学 | Contact unmanned aerial vehicle autonomous charging system |
| CN110816327A (en) * | 2019-10-18 | 2020-02-21 | 西北工业大学 | Contact unmanned aerial vehicle autonomous charging system |
| CN111404239A (en) * | 2020-04-28 | 2020-07-10 | 上海交通大学 | A porous charging panel of antiskid for unmanned aerial vehicle descending charges |
| CN111404239B (en) * | 2020-04-28 | 2022-06-10 | 上海交通大学 | A porous charging panel of antiskid for unmanned aerial vehicle descending charges |
| EP4139763A4 (en) * | 2021-02-01 | 2023-10-18 | Sagar Defence Engineering Private Limited | Method and system to ascertain location of drone box for stabilized landing and charging of drone |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |