CN208226632U - A kind of quadrotor drone recharging device - Google Patents
A kind of quadrotor drone recharging device Download PDFInfo
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- CN208226632U CN208226632U CN201820773345.4U CN201820773345U CN208226632U CN 208226632 U CN208226632 U CN 208226632U CN 201820773345 U CN201820773345 U CN 201820773345U CN 208226632 U CN208226632 U CN 208226632U
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model provides a kind of quadrotor drone recharging device, comprising: charging base and the charging mechanism on unmanned plane, charging base include dipping tank and balance charging panel, and equilibrium charging plate is connect with external power supply；Charging mechanism is set on unmanned machine base, including elastic electrode piece is arranged in landing foot prop, conducting wire and charging bracket, charging bracket bottom；Battery charging positive and negative anodes on unmanned plane are drawn by the two arrays of electrodes piece on unmanned machine base；When the elastic electrode piece on the charging bracket is contacted with equilibrium charging plate, two arrays of electrodes piece is wired to the elastic electrode on piece of the charging bracket bottom, and charging current will be input in the battery of unmanned plane by the conducting wire.Present apparatus design is simple, and whole process is participated in without artificial, is capable of the carry out unmanned plane charging of safety；Dipping tank setting structure special simultaneously makes autostop condition loose, without harsh alignment, improves and shuts down efficiency and adaptability.
Description
Technical field
The utility model belongs to unmanned air vehicle technique application field, and in particular to a kind of recharging dress of rotor wing unmanned aerial vehicle
It sets.
Background technique
With the development and progress of science and technology, unmanned plane has obtained extensive popularization in the fields such as civilian, industrial and military
Work, aerial reconnaissance operation are gone on patrol with application, such as security.But due to battery technology, the cruising ability of unmanned plane
It is not strong, battery is just needed replacing after having executed one section of aerial mission.Currently, the mode of replacement battery manually is often mostly used,
This largely limits unmanned plane and further develops and application.Therefore, it is necessary to design a kind of recharging device, work as nothing
When man-machine battery electric power deficiency, unmanned plane finds charging unit nearby, carries out Autonomous landing and charging, takes off after charging complete
Continue aerial mission.
Utility model content
In view of the above technical problems, the utility model provides a kind of quadrotor drone recharging device.Work as unmanned plane
When battery electric power deficiency, unmanned plane finds charging unit nearby, carries out Autonomous landing and charging, continuation of taking off after charging complete
Aerial mission is carried out, the autonomous cruising ability of unmanned plane is improved.
In order to solve the above technical problems, the utility model adopts the following technical solution:
A kind of quadrotor drone recharging device, characterized by comprising: charging base and on unmanned plane
Charging mechanism, the charging base include dipping tank and balance charging panel, and equilibrium charging plate is connect with external power supply；The charging
Mechanism is set on unmanned machine base, including elastic electrode is arranged in landing foot prop, conducting wire and charging bracket, charging bracket bottom
Piece；Battery charging positive and negative anodes on unmanned plane are drawn by the two arrays of electrodes piece on unmanned machine base, when on the charging bracket
When elastic electrode piece and equilibrium charging plate contact, two arrays of electrodes piece is connected to the bullet of the charging bracket bottom by the conducting wire
On property electrode slice, charging current will be input in the battery of unmanned plane by the conducting wire.
In the above scheme, the charging base upper surface set there are four stand upside down funnelform dipping tank, for placing
The landing foot prop of unmanned plane, the dipping tank setting are as follows: unmanned plane need not guarantee when carrying out Autonomous landing accurately to land
Point landing, in the range of landing foot prop falls on the dipping tank, unmanned plane can be under the effect of gravity along landing groove groove wall
It slides into and completes landing in the dipping tank；Landing groove center is the equilibrium charging plate, and equilibrium charging plate is placed on described fill
The center of electric pedestal is equipped with inside and outside two charge coils, the inner ring and outer ring of the charge coil bullet with charging bracket bottom respectively
Property electrode slice it is corresponding up and down, after being respectively communicated with so as to charge coil and the elastic electrode piece, charging current will be led by described
Line is input in the battery of unmanned plane.
In the above scheme, the two arrays of electrodes piece on unmanned machine base is symmetrical two-by-two in unmanned plane base lower surface
In four apexes of oval diagonal line；Two anode electrode pieces in the inner part pass through the conducting wire respectively and equilibrium charging plate charges
The inner ring of coil connects；Two negative electricity pole pieces in the outer part pass through the outer of the conducting wire and equilibrium charging plate charge coil respectively
Circle connection.
In the above scheme, charging bracket includes four support posts, Yi Jiyong in landing foot prop hollow space
In the support construction and balancing frame that support and balance four support posts；It is propped up in the middle part of four support posts by support construction
Balancing frame is arranged close to bottom in support；Anode electrode piece and negative electricity pole piece, four supports are separately connected at the top of four support posts
Elastic electrode piece is arranged in column bottom.
In the above-mentioned technical solutions, a control switch is set also on unmanned plane, charging is cut off in unmanned plane during flying
Circuit, and the charging circuit connecting with elastic electrode piece is opened when landing touches equilibrium charging plate.
The utility model devises a kind of quadrotor drone recharging device, and structure is simple, for realizing unmanned plane
Recharging after Autonomous landing and landing.Improve the voyage of unmanned plane.Present apparatus design is simple, and whole process is without artificial
It participates in, is capable of the carry out unmanned plane charging of safety；Dipping tank setting structure special simultaneously makes autostop condition loose, does not have to
Harsh alignment improves and shuts down efficiency and adaptability.
Detailed description of the invention
The utility model is described further below in conjunction with the drawings and specific embodiments.
Fig. 1 is the schematic perspective view of the utility model；
Fig. 2 is the schematic perspective view of charging base in the utility model；
Fig. 3 is the schematic perspective view of charging mechanism in the utility model；
Fig. 4 is the floor map of charging bracket in the utility model.
In figure: 1, charging base, 2, charging mechanism, 3, unmanned machine base, 11, dipping tank, 12, equilibrium charging plate, 13, fill
Electric coil, 21, landing foot prop, 22, conducting wire, 23, support post, 23-1, negative electricity pole piece, 23-2, anode electrode piece, 24, flat
Weigh disk, 25, support construction.
Specific embodiment
The selected example of the utility model is illustrated with reference to the accompanying drawing, example described herein is merely to illustrate
With explanation the utility model, it is not limited to the utility model.
A kind of embodiment 1: quadrotor drone recharging device, comprising: charging base 1 and charging mechanism 2, it is described to fill
Electric pedestal 1 includes dipping tank 11 and balance charging panel 12；The charging mechanism 2 includes landing foot prop 21, conducting wire 22 and charging
Bracket, the charging mechanism 2 are fixed on the bottom of unmanned machine base 3, on the lower surface of the unmanned machine base 3, anode electricity
Pole piece 23-2 and negative electricity pole piece 23-1 (is not shown by the elastic electrode piece that transfer wire 22 is connected to the charging bracket bottom
On out).It contacts and charges on the charging bracket bottom and the equilibrium charging plate 12 of charging base 1.
In the present embodiment, the charging base 1 set there are four stand upside down funnelform dipping tank 11, for placing unmanned plane
Landing foot prop 21, the unmanned machine base 3 when carrying out Autonomous landing need not guarantee accurately to landing point land, as long as institute
Stating landing foot prop 21 can fall in the range of the dipping tank 11, and the unmanned machine base 3 can edge under gravity
Cell wall slide into the dipping tank 11, complete landing.
In the present embodiment, the charging bracket include positioned at landing 21 hollow space of foot prop in four support posts 23,
And it is used to support and balances the support construction 25 and balancing frame 24 of four support posts 23.Pass through in the middle part of four support posts 23
Support construction 25 is supported, and balancing frame 24 is arranged close to bottom.Anode electrode piece is separately connected at the top of four support posts 23
Elastic electrode piece (not shown) is arranged in 23-2 and negative electricity pole piece 23-1, four 23 bottoms of support post；In unmanned machine base 3
On lower surface, four apexes of oval diagonal line are symmetrical arranged the anode electrode piece 23-2 and negative electricity pole piece 23-1 two-by-two,
Two anode electrode piece 23-2 and two negative electricity pole piece 23-1 pass through the conducting wire 22 and four 23 bottoms of support post respectively
Elastic electrode piece is set and realizes connection in charging.
In the present embodiment, equilibrium charging plate 12,12 center of equilibrium charging plate and four are placed at the center of the charging base 1
A 23 bottom corresponding position of support post is respectively equipped with inside and outside two charge coils 13, and inner ring connects positive electricity by the conducting wire 22
Pole piece 23-2, outer ring connect negative electricity pole piece 23-1 by the conducting wire 22, vertical with two pairs of supports of the charging bracket respectively
Column 23 is corresponding, when the charge coil 13 on the equilibrium charging plate 12 is connected to the elastic electrode piece on the charging bracket 23
Afterwards, charging current will be input in the battery of unmanned machine base 3 along the conducting wire 22.
One control switch can also be set, by remote control mode, charging circuit is cut off in unmanned plane during flying, and
Charging circuit is opened when landing touches equilibrium charging plate 12.Reinforce the safety in flight course.
The foregoing is merely the selected example of the utility model, the implementation model that is not intended to limit the utility model
It encloses.All any modification, equivalent replacements etc. made within principle and content of the invention, should be included in the utility model
Within protection scope.
Claims (5)
1. a kind of quadrotor drone recharging device, characterized by comprising: charging base and filling on unmanned plane
Motor structure, the charging base include dipping tank and balance charging panel, and equilibrium charging plate is connect with external power supply；The charger
Structure is set on unmanned machine base, including elastic electrode is arranged in landing foot prop, conducting wire and charging bracket, charging bracket bottom
Piece；Battery charging positive and negative anodes on unmanned plane are drawn by the two arrays of electrodes piece on unmanned machine base, when on the charging bracket
When elastic electrode piece and equilibrium charging plate contact, two arrays of electrodes piece is connected to the bullet of the charging bracket bottom by the conducting wire
On property electrode slice, charging current will be input in the battery of unmanned plane by the conducting wire.
2. quadrotor drone recharging device according to claim 1, it is characterised in that: table on the charging base
Face is set there are four the funnelform dipping tank to stand upside down, for placing the landing foot prop of unmanned plane, the dipping tank setting are as follows: nobody
Machine need not guarantee accurately to land to landing point when carrying out Autonomous landing, when landing foot prop falls on the range of the dipping tank
Interior, unmanned plane can slide under the effect of gravity along landing groove groove wall and complete to land in the dipping tank；Landing groove center be
The equilibrium charging plate, equilibrium charging plate are placed on the center of the charging base, are equipped with inside and outside two charge coils, charging
The inner ring and outer ring of coil is corresponding up and down with the elastic electrode piece of charging bracket bottom respectively, so as to charge coil and the elasticity
After electrode slice is respectively communicated with, charging current will be input in the battery of unmanned plane by the conducting wire.
3. quadrotor drone recharging device according to claim 2, it is characterised in that: two on unmanned machine base
Group electrode slice is symmetrically distributed in four apexes of oval diagonal line two-by-two in unmanned plane base lower surface；Two in the inner part are just
Pole electrode slice passes through the conducting wire respectively and connect with the inner ring of equilibrium charging plate charge coil；Two negative electricity pole pieces in the outer part
It is connect respectively by the conducting wire with the outer ring of equilibrium charging plate charge coil.
4. quadrotor drone recharging device according to claim 2 or 3, it is characterised in that: charging bracket includes
Four support posts in landing foot prop hollow space and it is used to support and balances the support constructions of four support posts
And balancing frame；It is supported in the middle part of four support posts by support construction, balancing frame is set close to bottom；Four support posts
Top is separately connected anode electrode piece and negative electricity pole piece, and elastic electrode piece is arranged in four support post bottoms.
5. quadrotor drone recharging device described in one of -3 according to claim 1, it is characterised in that: also in unmanned plane
One control switch of upper setting, cuts off charging circuit in unmanned plane during flying, and the opening when landing touches equilibrium charging plate
The charging circuit being connect with elastic electrode piece.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820773345.4U CN208226632U (en) | 2018-05-23 | 2018-05-23 | A kind of quadrotor drone recharging device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820773345.4U CN208226632U (en) | 2018-05-23 | 2018-05-23 | A kind of quadrotor drone recharging device |
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| Publication Number | Publication Date |
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| CN208226632U true CN208226632U (en) | 2018-12-11 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201820773345.4U Active CN208226632U (en) | 2018-05-23 | 2018-05-23 | A kind of quadrotor drone recharging device |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109808530A (en) * | 2019-02-20 | 2019-05-28 | 武汉理工大学 | A kind of vehicle-mounted multi-rotor unmanned aerial vehicle charging unit |
| 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 |
| CN110979673A (en) * | 2019-12-18 | 2020-04-10 | 武汉飞流智能技术有限公司 | Unmanned aerial vehicle aligning device |
| CN113147448A (en) * | 2021-02-24 | 2021-07-23 | 广东工业大学 | Unmanned aerial vehicle take-off and landing charging equipment |
| CN113264198A (en) * | 2021-06-11 | 2021-08-17 | 广州优飞智能设备有限公司 | Unmanned aerial vehicle landing automatic centering charging device and method based on slope principle |
| CN114228521A (en) * | 2021-12-20 | 2022-03-25 | 歌尔科技有限公司 | Unmanned aerial vehicle equipment and wireless charging device thereof |
-
2018
- 2018-05-23 CN CN201820773345.4U patent/CN208226632U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109808530A (en) * | 2019-02-20 | 2019-05-28 | 武汉理工大学 | A kind of vehicle-mounted multi-rotor unmanned aerial vehicle charging unit |
| 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 |
| CN110979673A (en) * | 2019-12-18 | 2020-04-10 | 武汉飞流智能技术有限公司 | Unmanned aerial vehicle aligning device |
| CN113147448A (en) * | 2021-02-24 | 2021-07-23 | 广东工业大学 | Unmanned aerial vehicle take-off and landing charging equipment |
| CN113147448B (en) * | 2021-02-24 | 2023-08-08 | 广东工业大学 | Unmanned aerial vehicle takes off and land charging equipment |
| CN113264198A (en) * | 2021-06-11 | 2021-08-17 | 广州优飞智能设备有限公司 | Unmanned aerial vehicle landing automatic centering charging device and method based on slope principle |
| CN114228521A (en) * | 2021-12-20 | 2022-03-25 | 歌尔科技有限公司 | Unmanned aerial vehicle equipment and wireless charging device thereof |
| CN114228521B (en) * | 2021-12-20 | 2024-03-12 | 歌尔科技有限公司 | Unmanned aerial vehicle equipment and wireless charging device thereof |
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