CN107128203A - Portable unmanned plane charging station - Google Patents
Portable unmanned plane charging station Download PDFInfo
- Publication number
- CN107128203A CN107128203A CN201710408336.5A CN201710408336A CN107128203A CN 107128203 A CN107128203 A CN 107128203A CN 201710408336 A CN201710408336 A CN 201710408336A CN 107128203 A CN107128203 A CN 107128203A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- magnet
- charging station
- flat board
- board charger
- 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
Links
- 239000011159 matrix material Substances 0.000 description 4
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/30—Constructional details of charging stations
- B60L53/31—Charging columns specially adapted for electric vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
- B60L53/16—Connectors, e.g. plugs or sockets, specially adapted for charging electric vehicles
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/02—Contact members
- H01R13/22—Contacts for co-operating by abutting
- H01R13/24—Contacts for co-operating by abutting resilient; resiliently-mounted
- H01R13/2407—Contacts for co-operating by abutting resilient; resiliently-mounted characterized by the resilient means
- H01R13/2421—Contacts for co-operating by abutting resilient; resiliently-mounted characterized by the resilient means using coil springs
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/62—Means for facilitating engagement or disengagement of coupling parts or for holding them in engagement
- H01R13/6205—Two-part coupling devices held in engagement by a magnet
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
-
- 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
-
- 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
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
-
- 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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/12—Electric charging stations
-
- 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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The present invention discloses a kind of portable unmanned plane charging station, including unmanned plane connector and flat board charger, described unmanned plane connector includes charging module and two elastic electrodes, elastic electrode one end and charging module connection, the other end is conductive flat thin magnet, and the magnetic pole of the flat thin magnet of two elastic electrodes is opposite；Described flat board charger is provided with conductive magnet array, and surface magnetic pole in magnet array between adjacent magnets provides charging service on the contrary, the present invention is not limited by geographic for unmanned plane at any time, and it is swift to operate simply, efficiency high.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, specifically a kind of portable unmanned plane charging station.
Background technology
In recent years, unmanned plane is widely used in the field such as civilian, police, military, because battery is using light,
It can recycle, leading position is commercially occupied using battery powered SUAV, however, the endurance of battery
Always unmanned plane application an important bottlenecks, add it is more multi-functional the need for, the equipment carried on unmanned plane is also got over
Come more, the endurance of battery seems even more important.Usual unmanned plane flies be accomplished by returning to ground after a period of time in the air
Face changes battery or battery is charged, and can just continue executing with aerial mission, but the charging station set at present is mostly fixed
In some region, this is extremely inconvenient for the unmanned plane that field carries out various tasks, and the behaviour charged now
Make also relatively complicated, it is inefficient.
The content of the invention
The technical problems to be solved by the invention are：A kind of portable unmanned plane charging station is provided, it is not by geographical position
Limitation, provide charging service at any time for unmanned plane, and swift to operate simple, efficiency high.
The technical solution adopted in the present invention is：A kind of portable unmanned plane charging station, including unmanned plane connector are provided
With flat board charger, described unmanned plane connector includes charging module and two elastic electrodes, elastic electrode one end and charging
Module is connected, and the other end is conductive flat thin magnet, and the magnetic pole of the flat thin magnet of two elastic electrodes is opposite；Described flat board charger
Surface magnetic pole in magnet array provided with conduction, magnet array between adjacent magnets is opposite.
Described flat board charger is provided with expansion interface.
Described elastic electrode is power spring.
After above structure, portable unmanned plane charging station of the present invention is easy to carry, is not limited by geographical position, at any time
Charged, extremely facilitated for the unmanned plane of operation in the wild to unmanned plane, unmanned plane is using on elastic electrode during charging
The flat thin magnet principle that identical charges repel each other, there is a natural attraction between the sexes corresponding with magnet array magnet carries out adhesive automatically, connect circuit and carry out
Charging, reduces the triviality of charging operations, efficiency high.
Brief description of the drawings
Structural representation when Fig. 1 uses for the unmanned plane connector of the present invention.
Fig. 2 is flat board charger construction schematic diagram of the invention.
Embodiment
The present invention is described in detail below in conjunction with drawings and examples.
As shown in Figure 1 and Figure 2, portable unmanned plane charging station of the present invention, including unmanned plane connector 1 and flat board charger
2.Unmanned plane connector 1 includes charging module 12 and two elastic electrodes 11, and unmanned plane connector 1 is fixed on unmanned motor spindle.
The one end of elastic electrode 11 and charging module 12 are connected, and the other end is conductive flat thin magnet, and elastic electrode 11 uses power spring, two
Individual flat thin magnet opposite polarity in the same direction, the one side of flat thin magnet N poles is connected to inside unmanned plane by power spring and charging module 12
The positive pole of battery, the one side of flat thin magnet S poles connects GND by power spring.On the one hand the effect of power spring makees wire
Flat thin magnet is connected, flat thin magnet is freely shifted under outside magnetic fields, to be parked in flat board charging in unmanned plane
During device 2 can corresponding magnet that closely accurately adhesive is arrived, set back rapidly when leaving flat board charger 2.
Flat board charger 2 is made up of magnet matrix 21, plastic plate 22, battery 23 and connection circuit 24, magnet matrix 21
On the surface for being embedded in plastic plate 22, magnet is electrically conductive in magnet matrix 21, and adjacent magnets polarity phase in the same direction is pressed in direction in length and breadth
Instead, the mode of the spacing of two flat thin magnets in the equivalent elastic electrode 11 of spacing is arranged, and connection circuit 24 is then by magnet matrix 21
In the S poles magnet of one side upwards be linked to the positive pole of battery 23, the magnet of N poles is connected to the negative pole of battery 23.
In the specific implementation, flat board charger 2 is provided with expansion interface to the present invention, using expansion interface, can extend connection
The charging platform that polylith flat board charger 2 is constituted.When unmanned plane needs charging, as long as resting in any position of charging platform
Put, the N poles and S poles of unmanned plane connector 1 respectively with the S poles on flat board charger 2 and the extremely close adhesives of N, be connected to exactly
The both positive and negative polarity of battery 23 in flat board charger 2, realizes unmanned plane automatic charging function.
Claims (3)
1. a kind of portable unmanned plane charging station, it is characterised in that：Including unmanned plane connector and flat board charger, described nothing
Man-machine connector includes charging module and two elastic electrodes, elastic electrode one end and charging module connection, and the other end is conduction
Flat thin magnet, the magnetic pole of the flat thin magnet of two elastic electrodes is opposite；Magnet array of the described flat board charger provided with conduction,
Surface magnetic pole in magnet array between adjacent magnets is opposite.
2. portable unmanned plane charging station according to claim 1, it is characterised in that：Described flat board charger is provided with expansion
Open up interface.
3. portable unmanned plane charging station according to claim 1, it is characterised in that：Described elastic electrode is conductive bullet
Spring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710408336.5A CN107128203A (en) | 2017-06-02 | 2017-06-02 | Portable unmanned plane charging station |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710408336.5A CN107128203A (en) | 2017-06-02 | 2017-06-02 | Portable unmanned plane charging station |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107128203A true CN107128203A (en) | 2017-09-05 |
Family
ID=59734363
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710408336.5A Pending CN107128203A (en) | 2017-06-02 | 2017-06-02 | Portable unmanned plane charging station |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107128203A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101971453A (en) * | 2007-05-08 | 2011-02-09 | 莫琼移动股份有限公司 | System and method for inductive charging of portable devices |
| CN106033826A (en) * | 2015-03-17 | 2016-10-19 | 李昊阳 | Multi-rotary-wing unmanned aerial vehicle returning automatic charging method |
| CN106130113A (en) * | 2016-07-20 | 2016-11-16 | 中国电子科技集团公司第四十八研究所 | A kind of portable rotor wing unmanned aerial vehicle charging device |
| CN205986293U (en) * | 2016-08-03 | 2017-02-22 | 中国电子科技集团公司第四十八研究所 | A solar energy wireless charging device for unmanned aerial vehicle |
| CN106450880A (en) * | 2016-08-17 | 2017-02-22 | 杭州美思特智能科技股份有限公司 | Elastic contact device for electric connection |
| CN106787000A (en) * | 2017-02-27 | 2017-05-31 | 无锡龙翼智能科技有限公司 | A kind of unmanned plane charging device and its charging method based on magnetic bodies |
-
2017
- 2017-06-02 CN CN201710408336.5A patent/CN107128203A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101971453A (en) * | 2007-05-08 | 2011-02-09 | 莫琼移动股份有限公司 | System and method for inductive charging of portable devices |
| CN106033826A (en) * | 2015-03-17 | 2016-10-19 | 李昊阳 | Multi-rotary-wing unmanned aerial vehicle returning automatic charging method |
| CN106130113A (en) * | 2016-07-20 | 2016-11-16 | 中国电子科技集团公司第四十八研究所 | A kind of portable rotor wing unmanned aerial vehicle charging device |
| CN205986293U (en) * | 2016-08-03 | 2017-02-22 | 中国电子科技集团公司第四十八研究所 | A solar energy wireless charging device for unmanned aerial vehicle |
| CN106450880A (en) * | 2016-08-17 | 2017-02-22 | 杭州美思特智能科技股份有限公司 | Elastic contact device for electric connection |
| CN106787000A (en) * | 2017-02-27 | 2017-05-31 | 无锡龙翼智能科技有限公司 | A kind of unmanned plane charging device and its charging method based on magnetic bodies |
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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 | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170905 |