CN108725820A - Unmanned plane automatic charging platform - Google Patents
Unmanned plane automatic charging platform Download PDFInfo
- Publication number
- CN108725820A CN108725820A CN201810341154.5A CN201810341154A CN108725820A CN 108725820 A CN108725820 A CN 108725820A CN 201810341154 A CN201810341154 A CN 201810341154A CN 108725820 A CN108725820 A CN 108725820A
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- China
- Prior art keywords
- charging
- unmanned plane
- row
- charging platform
- electrode
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- 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
Abstract
The invention discloses a kind of unmanned plane automatic charging platforms, it is related to unmanned plane charging technique field, charging plane is divided into multiple " charge point " arrays by the unmanned plane automatic charging platform, each the positive-negative polarity of " charge point " can be by circuit control, the mounting anode and cathode contact below aircraft tripod.After aircraft is placed in charging plane, detect which " charge point " is connected with the contact of aircraft tripod by certain method, then by the positive-negative polarity of these contacts of circuit control, to establish charging path.
Description
Technical field
The present invention relates to unmanned plane charging technique fields, in particular it relates to which a kind of unmanned plane automatic charging is flat
Platform.
Background technology
At present common unmanned plane automatic charging technology be required for by mechanical mechanism either robot move aircraft or
Electrode on charging platform establishes charging path, and the system is higher to position accuracy demand of the aircraft on charging platform, together
When mechanical mechanism increase the complexity of system, reduce the reliability of system.When existing unmanned plane charging technique requires charging
Aircraft is in the specific position of platform, and only charging path could be established on this position, has complexity height, reliability low
Defect.
Invention content
Technical problem to be solved by the invention is to provide a kind of unmanned plane automatic charging platforms, are controllably charged using array
Electrode technology, may be implemented highly reliable unmanned plane automatic charging function, and unmanned plane may be at any position of charging platform.
To achieve the above object, the present invention provides technical solution below：
The unmanned plane automatic charging platform includes charging platform, and the charge point of 10 rows 10 row, nothing are dispersed on charging platform
Charging electrode anode is installed in man-machine left front tripod bottom, and charging electrode cathode, charging are installed in unmanned plane right back tripod bottom
When, charging platform makes " charge point " that the 5th row the 3rd row, the 6th row the 3rd arrange to be used as charging anode by circuit control, by the 7th
" charge point " that the row of row the 9th, the 7th row the 10th arrange is flown to constitute current supply circuit by image recognition as charging cathode
Elaborate position and accurate course of the machine on charging platform, thus known to unmanned aerial vehicle rack mechanical structure relationship,
Position of the positive and negative anodes contact on charging platform on unmanned plane tripod, the electricity on unmanned plane tripod can be obtained by geometric operation
Extremely sufficiently large, each electrode can be connected with multiple charge points simultaneously, so that these charge points are being electrically connections,
Which charge point charge point adjacent thereto is obtained by the method for rank scanning to be connected, may thereby determine that on charging platform
Which charge point is connected with the electrode on unmanned plane tripod.
Preferably, the charging electrode anode on the unmanned plane tripod and minus 2 of charging electrode cathode at least one positive one,
But 2 are not limited to, can there is multiple anodes and cathode.
Preferably, the charge point quantity on the charging platform and arrangement mode are unlimited.
It is using the advantageous effect of above technical scheme：The unmanned plane automatic charging platform is drawn by the plane that will entirely charge
It is divided into " charge point " of multiple array distributions, the positive-negative polarity and break-make of each " charge point " are individually controllable, under aircraft tripod
Side's installation contact electrode can charge, from anywhere in being in charging platform but regardless of aircraft without machinery
Mechanism realizes that electrode alignment contacts, and unmanned plane may be at any position of charging platform.
Description of the drawings
The specific implementation mode of the present invention is described in further detail below in conjunction with the accompanying drawings.
Fig. 1 is the structure principle chart of unmanned plane automatic charging platform of the present invention.
Wherein, 1- charging platforms, 2- charge points, 3- charging electrodes anode, 4- charging electrode cathode.
Specific implementation mode
The preferred embodiment of the invention will now be described in detail with reference to the accompanying drawings unmanned plane automatic charging platform.
Fig. 1 shows the specific implementation mode of unmanned plane automatic charging platform of the present invention：
As shown in Figure 1, the unmanned plane automatic charging platform includes charging platform 1,10 rows 10 row are dispersed on charging platform 1
Charge point 2, charging electrode anode 3, the installation charging of unmanned plane right back tripod bottom are installed in unmanned plane left front tripod bottom
Electrode Negative 4, when charging, charging platform 1 makes " charge point " that the 5th row the 3rd row, the 6th row the 3rd arrange to be used as by circuit control
Charging anode passes through " charge point " of the 7th row the 9th row, the 7th row the 10th row as charging cathode to constitute current supply circuit
Image recognition obtains elaborate position and accurate course of the aircraft on charging platform, in unmanned aerial vehicle rack mechanical structure relationship
In the case of known, position of the positive and negative anodes contact on charging platform 1, nothing on unmanned plane tripod can be obtained by geometric operation
Electrode on man-machine tripod is sufficiently large, and each electrode can be connected with multiple charge points simultaneously, so that these charge points exist
It is electrically connection, the charge point adjacent thereto of which charge point 2 is obtained by the method for rank scanning on charging platform 1
2 are connected, and may thereby determine which charge point 2 is connected with the electrode on unmanned plane tripod.It solves unmanned plane and necessarily is in and fill
The problem of specific position on level platform 1 could charge, eliminates the machine added in order to which unmanned plane is moved to this position
Tool device.
Charging electrode anode 3 on unmanned plane tripod and minus 2 of charging electrode cathode 4 at least one positive one, but it is unlimited
In 2, can there are multiple anodes and cathode.2 quantity of charge point and arrangement mode on charging platform 1 is unlimited.
The above are merely the preferred embodiment of the present invention, it is noted that for those of ordinary skill in the art,
Without departing from the concept of the premise of the invention, various modifications and improvements can be made, these belong to the guarantor of the present invention
Protect range.
Claims (3)
1. a kind of unmanned plane automatic charging platform, it is characterised in that：The unmanned plane automatic charging platform includes charging platform 1,
The charge point 2 of 10 rows 10 row is dispersed on charging platform 1, charging electrode anode 3 is installed in unmanned plane left front tripod bottom, nobody
Charging electrode cathode 4 is installed in machine right back tripod bottom, when charging, charging platform 1 by circuit control make the 5th row the 3rd row,
" charge point " of 6th row the 3rd row is negative as charging by " charge point " of the 7th row the 9th row, the 7th row the 10th row as charging anode
Pole obtains elaborate position and accurate course of the aircraft on charging platform to constitute current supply circuit by image recognition, to
Known to unmanned aerial vehicle rack mechanical structure relationship, positive and negative anodes on unmanned plane tripod can be obtained by geometric operation and are touched
Position of the point on charging platform 1, the electrode on unmanned plane tripod is sufficiently large, each electrode can simultaneously with multiple charge point phases
Even, so that these charge points are being electrically connections, which is obtained by the method for rank scanning on charging platform 1
The charge point 2 adjacent thereto of charge point 2 is connected, and may thereby determine which charge point 2 is connected with the electrode on unmanned plane tripod.
2. unmanned plane automatic charging platform according to claim 1, it is characterised in that：Charging on the unmanned plane tripod
Electrode anode 3 and minus 2 of charging electrode cathode 4 at least one positive one, but 2 are not limited to, can there are multiple anodes and cathode.
3. unmanned plane automatic charging platform according to claim 1, it is characterised in that：Charging on the charging platform 1
2 quantity of point and arrangement mode are unlimited.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810341154.5A CN108725820A (en) | 2018-04-08 | 2018-04-08 | Unmanned plane automatic charging platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810341154.5A CN108725820A (en) | 2018-04-08 | 2018-04-08 | Unmanned plane automatic charging platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108725820A true CN108725820A (en) | 2018-11-02 |
Family
ID=63939663
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810341154.5A Pending CN108725820A (en) | 2018-04-08 | 2018-04-08 | Unmanned plane automatic charging platform |
Country Status (1)
| Country | Link |
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| CN (1) | CN108725820A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110065645A (en) * | 2019-04-23 | 2019-07-30 | 河南三和航空工业有限公司 | High-precision UAV Flight Control System |
| CN111762040A (en) * | 2020-06-07 | 2020-10-13 | 中国葛洲坝集团第一工程有限公司 | Near-field continuous navigation unmanned aerial vehicle dangerous rock monitoring system and method |
| CN111861982A (en) * | 2020-06-07 | 2020-10-30 | 中国葛洲坝集团第一工程有限公司 | Visual image monitoring and identifying system |
| CN114285110A (en) * | 2021-11-19 | 2022-04-05 | 国网浙江省电力有限公司江山市供电公司 | Unmanned aerial vehicle automatic charging platform, system and method |
| 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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| CN110065645A (en) * | 2019-04-23 | 2019-07-30 | 河南三和航空工业有限公司 | High-precision UAV Flight Control System |
| CN111762040A (en) * | 2020-06-07 | 2020-10-13 | 中国葛洲坝集团第一工程有限公司 | Near-field continuous navigation unmanned aerial vehicle dangerous rock monitoring system and method |
| CN111861982A (en) * | 2020-06-07 | 2020-10-30 | 中国葛洲坝集团第一工程有限公司 | Visual image monitoring and identifying system |
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| 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 |
| CN114285110A (en) * | 2021-11-19 | 2022-04-05 | 国网浙江省电力有限公司江山市供电公司 | Unmanned aerial vehicle automatic charging platform, system and method |
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Effective date of registration: 20210202 Address after: 100101 room 332, 3 / F, building 1, courtyard a 11, Anxiang Beili, Chaoyang District, Beijing Applicant after: Beijing Jiexiang Tiandi Information Technology Co.,Ltd. Address before: Room 302, 3 / F, building a 11, Anxiang Beili, Chaoyang District, Beijing Applicant before: BEIJING LINGHANG INTELLIGENT TECHNOLOGY DEVELOPMENT Co.,Ltd. |
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