CN108058842A - A kind of battery change system of express delivery unmanned plane - Google Patents
A kind of battery change system of express delivery unmanned plane Download PDFInfo
- Publication number
- CN108058842A CN108058842A CN201711448041.7A CN201711448041A CN108058842A CN 108058842 A CN108058842 A CN 108058842A CN 201711448041 A CN201711448041 A CN 201711448041A CN 108058842 A CN108058842 A CN 108058842A
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- CN
- China
- Prior art keywords
- unmanned plane
- battery
- battery pack
- gag lever
- lever post
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- 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.)
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- 230000008859 change Effects 0.000 title claims abstract description 15
- 230000007246 mechanism Effects 0.000 claims abstract description 27
- 239000002184 metal Substances 0.000 claims abstract description 21
- 229910052751 metal Inorganic materials 0.000 claims abstract description 21
- 238000003475 lamination Methods 0.000 claims abstract description 10
- 210000000078 claw Anatomy 0.000 claims description 13
- 230000002459 sustained effect Effects 0.000 claims description 3
- 230000009471 action Effects 0.000 claims description 2
- 230000005484 gravity Effects 0.000 claims description 2
- 238000005516 engineering process Methods 0.000 description 7
- 230000005611 electricity Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 2
- 239000010931 gold Substances 0.000 description 2
- 229910052737 gold Inorganic materials 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 239000000837 restrainer Substances 0.000 description 1
Classifications
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Manipulator (AREA)
Abstract
The present invention discloses a kind of battery change system of express delivery unmanned plane, including the battery pack being arranged on unmanned plane and a manipulator, battery pack is cylindrical structure, the crown center of unmanned plane is provided with cylindrical battery chamber, battery pack is removably inserted in battery cavities, the charging contact around cylinder periphery is provided in battery pack, charging spring lamination is provided on the inside of battery cavities, battery pack further includes the clamping mechanism for being arranged on top and the metal derby that can be attracted by magnet, and manipulator includes the magnechuck for being arranged on end.The battery cavities of the present invention are arranged on the crown center of unmanned plane, the courier packages of lower section carry will not be impacted when replacing battery, in addition battery pack is cylindrical structure and the contact that charges is around cylinder periphery, when battery pack being allowed to be inserted into battery cavities with any angle charging contact can be made to be contacted with charging spring lamination, unmanned plane need to only drop to designated position, special angle is not required, reduces the control requirement to unmanned plane landing.
Description
Technical field
The present invention relates to unmanned air vehicle technique fields, are specifically a kind of battery change system of express delivery unmanned plane.
Background technology
In a kind of entitled patent of unmanned plane charging station, it is automatic to disclose unmanned plane for Application No. 2016213507659
The technology of battery is replaced, by setting landing deck, after UAV Landing, then the battery in unmanned plane is removed with manipulator and is put
Enter the station that charges to charge, then change the battery for filling with electricity.Although this technology can realize the replacement of battery, battery
Uav bottom is arranged on, battery can not be replaced in the case of carry courier packages, it is necessary to be improved, to be suitble to carry fast
The needs of package are passed, while are replaced in cell process, the charging port of battery is needed to pay attention to be matched with charging interface, in the technology
This technology is specifically solved the problems, such as without providing, and specific angle is voluntarily adjusted to when can usually land by unmanned plane to solve
Interface marriage problem when replacing battery, but this way is very high to the control accuracy requirement of unmanned plane, realizes more difficult.
The content of the invention
To solve the deficiencies in the prior art, the present invention provides one kind can replace electricity in the case of carry courier packages
Pond, the battery change system of the express delivery unmanned plane matched convenient for charging port and charging interface.
It is of the present invention solve the problems, such as the technical solution adopted is that：
A kind of battery change system of express delivery unmanned plane, including the battery pack being arranged on unmanned plane and for replacing battery pack
Manipulator, the battery pack is cylindrical structure, and the crown center of the unmanned plane is provided with cylindrical battery chamber, the electricity
Chi Bao is removably inserted in battery cavities, and the charging contact around cylinder periphery is provided in the battery pack, described
It is provided with charging spring lamination on the medial surface of battery cavities, the battery pack further includes the clamping mechanism that is arranged on top and can be by magnet
The metal derby of attraction, the manipulator include the magnechuck for being arranged on end；When battery pack is fully inserted in battery cavities,
The charging spring lamination and charging contact pad, the clamping mechanism and unmanned plane clamping；When magnechuck is moved to manipulator
When above battery pack and being powered, the metal derby is moved up by attraction and clamping mechanism is driven to be unclamped with unmanned plane.
Further, the surrounding of the battery cavities has upwardly extended a circle flange collar, is set in the flange collar around periphery
Screens, the clamping mechanism are uniformly distributed including at least two and are hinged on the kelly at the top of battery pack, and the kelly has
The claw that can be clamped with screens is extended downward into, the metal derby is fixedly connected on kelly, the weight of the kelly and metal derby
Power forces claw to be rotated toward inside and is clamped with screens, and when the metal derby is by attracting to move up, the kelly is rotated toward outside.
Further, the clamping mechanism further includes the spring being arranged at the top of battery pack, and the spring withstands kelly and forces
Claw has the trend rotated toward inside.
Further, the battery pack further includes the end cap being arranged at the top of battery pack, the clamping mechanism, metal derby and bullet
Spring is respectively positioned on the inside of end cap.
Further, landing deck and position-limit mechanism are further included, the position-limit mechanism includes motor, fixed with the shaft of motor
The gear of connection, four racks for being uniformly distributed and being engaged with gear with can moving back and forth respectively and it is fixedly connected on rack
On gag lever post, the gag lever post is located at the top on landing deck, and four gag lever posts are arc structure and move
Circular, at least three piece supporting legs of the unmanned plane including being evenly distributed on lower section, the supporting leg are formed among to landing deck
On be provided with block, when four gag lever posts are formed it is circular when, the gag lever post is located at the top of block.
Further, opposite gag lever post is in sustained height, and adjacent gag lever post is in different height, the gag lever post
Circular arc both ends are also respectively provided with extended end, and when gag lever post is moved on the outside of landing deck, four gag lever posts can incite somebody to action
Land deck is trapped among centre, and two layers of block corresponding with the gag lever post of different height respectively is provided on the supporting leg.
Further, the supporting leg bottom of the unmanned plane is provided with universal caster wheel.
Beneficial effects of the present invention：The battery pack of the present invention uses cylindrical structure, can be inserted directly into the top of unmanned plane
Intermediate cylindrical battery chamber, the charging contact in battery pack around cylinder periphery can connect with the charging spring lamination in battery cavities
Touch and be powered, since battery cavities are arranged on the crown center of unmanned plane, when replacing battery will not below unmanned plane carry express delivery
Package impacts, and in addition battery pack is cylindrical structure and the contact that charges is around cylinder periphery, allows battery pack to appoint
During meaning angle insertion battery cavities charging contact can be made to be contacted with charging spring lamination, unmanned plane need to only drop to designated position,
Special angle is not required, reduces the control requirement to unmanned plane landing, interface marriage problem when solving to replace battery, and structure
Simply, it is easy to implement.
Description of the drawings
Fig. 1 is the structure diagram of the present invention；
Fig. 2 is the landing deck of the present invention and the schematic front view of position-limit mechanism；
Fig. 3 is the enlarged diagram at the A of Fig. 2；
Fig. 4 is the landing deck of the present invention and the dimensional structure diagram of position-limit mechanism.
Specific embodiment
The technique effect of the design of the invention, concrete structure and generation is carried out below with reference to embodiment and attached drawing
Clear, complete description, to be completely understood by the purpose of the invention, feature and effect.Each skill in the invention
Art feature, can be with combination of interactions on the premise of not conflicting conflict.
Referring to figs. 1 to Fig. 4, a kind of battery change system of express delivery unmanned plane, including the battery pack 1 being arranged on unmanned plane
And the manipulator 2 for replacing battery pack 1, the battery pack 1 are cylindrical structure, the crown center of the unmanned plane is set
There is cylindrical battery chamber, the battery pack 1 is removably inserted in battery cavities, is provided in the battery pack 1 around cylinder
The charging contact 11 of external disc is provided with charging spring lamination 31 on the medial surface of the battery cavities, and the battery pack 1, which further includes, to be set
It puts in the clamping mechanism at top and the metal derby 13 that can be attracted by magnet, electromagnetism suction of the manipulator 2 including being arranged on end
Disk 21；When battery pack 1 is fully inserted in battery cavities, the charging spring lamination 31 is contacted with charging contact 11, the clamping machine
Structure and unmanned plane clamping；When magnechuck 21 is moved to 1 top of battery pack with manipulator 2 and is powered, the metal derby 13
By attracting to move up and clamping mechanism and unmanned plane driven to unclamp, in addition magnechuck 21 hold metal derby 13 can take up it is whole
A battery pack 1.Clamping mechanism enables battery pack 1 to be fixed on unmanned plane, prevents battery pack 1 and unmanned plane point in flight course
From.Generally, the data contact 16 for data transmission around cylinder periphery is additionally provided in battery pack 1, it is corresponding
The shrapnel that can be contacted with data contact 16 is provided on the medial surface of battery cavities.The technology of manipulator is the prior art, can be risen
It is high or reduce and can move back and forth while rotatable, it realizes to remove battery pack 1 from nobody and is then placed within charging station
On 8.
In the present embodiment, with reference to Fig. 3, the surrounding of the battery cavities has upwardly extended a circle flange collar 3, has been set in the flange collar 3
The screens around periphery is put, the clamping mechanism includes at least two cards for being uniformly distributed and being hinged on 1 top of battery pack
Bar 12, kelly 12 are generally three or four, and the kelly 12 has the claw that extends downward into and can be clamped with screens, the gold
Belong to block 13 to be fixedly connected on kelly 12, the gravity of the kelly 12 and metal derby 13 forces claw to rotate and screens card toward inside
It connects, when the metal derby 13 is by attracting to move up, the kelly 12 is rotated toward outside, and metal derby 13 is arranged on same with claw
On the kelly 12 of side, claw can be pulled to rotate when metal derby 13 moves up, claw can separate release with screens at this time.In addition block
Connection mechanism further includes the spring 14 for being arranged on 1 top of battery pack, and the spring 14, which withstands kelly 12, forces claw to have toward inside
The trend of rotation sets spring 14 that claw can preferably be made to keep clamped condition with screens.In addition in being further improved, the electricity
Pond bag 1 further includes the end cap 15 for being arranged on 1 top of battery pack, and the clamping mechanism, metal derby 13 and spring 14 are respectively positioned on end cap
15 inside.The end cap 15 can more preferably protect battery pack 1, and after adding end cap 15, magnechuck 21 can hold gold across end cap 15
Belong to block 13.
Further improved embodiment with reference to Fig. 2 and Fig. 4, further includes landing deck 4 and position-limit mechanism 5, the position restrainer
Structure 5 is uniformly distributed including motor 51, the gear 52, four being fixedly connected with the shaft of motor 51 and can move back and forth ground respectively
The rack 53 engaged with gear 52 and the gag lever post 54 being fixedly connected on rack 53, the gag lever post 54 are located at landing deck
4 top, four gag lever posts 54, which are arc structure and are movable among landing deck 4, forms annular shape, described
Unmanned plane includes at least three supporting legs for being evenly distributed on lower section, which is generally three or four, on the supporting leg
Block 6 is provided with, when four gag lever posts 54 form annular shape, the gag lever post 54 is located at the top of block 6.Landing first
Plate 4 facilitates unmanned plane to land, and position-limit mechanism 5 during movement, can promote unmanned plane to be moved to land deck 4 among landing deck 4
Intermediate position substantially reduces the required precision of unmanned plane landing, and beneficial to raising efficiency, while gag lever post 54 is located at block 6
When top can prevent from removing battery pack 1, the problem of unmanned plane may together be taken up by manipulator.
To being further improved for above-mentioned gag lever post 54, opposite gag lever post 54 is in sustained height, adjacent gag lever post 54
In different height, the circular arc both ends of the gag lever post 54 are also respectively provided with extended end 541, when gag lever post 54 is moved to landing
During 4 outside of deck, landing deck 4 can be trapped among centre by four gag lever posts 54, be provided on the supporting leg two layers respectively with
The 54 corresponding block 6 of gag lever post of different height.The circular arc both ends of gag lever post 54 set extended end 541 that gag lever post 54 can be allowed past
The area bigger surrounded in 4 intermediate moving process of landing deck preferably promotes unmanned plane mobile among landing deck 4, limit
Position bar 54 is divided into two layers of different height, interferes when can avoid being moved to centre.In addition, for ease of movement, it is described nobody
The supporting leg bottom of machine is provided with universal caster wheel 7.
It should be noted that it is above simply in conjunction with the embodiments further elucidated above to the present invention, it does not form to the present invention
The limitation of protection domain if simply being changed to this technology, simply realizes the invention with essentially identical means
Purpose, should all belong to the scope of protection of the present invention.
Claims (7)
1. a kind of battery change system of express delivery unmanned plane, including the battery pack being arranged on unmanned plane（1）And for replacing
Battery pack（1）Manipulator（2）, it is characterised in that：The battery pack（1）For cylindrical structure, in the top of the unmanned plane
Between be provided with cylindrical battery chamber, the battery pack（1）It is removably inserted in battery cavities, the battery pack（1）Upper setting
There is the charging contact of circular cylinder periphery（11）, charging spring lamination is provided on the medial surface of the battery cavities（31）, it is described
Battery pack（1）Further include the clamping mechanism for being arranged on top and the metal derby that can be attracted by magnet（13）, the manipulator（2）Bag
Include the magnechuck for being arranged on end（21）；Work as battery pack（1）When being fully inserted in battery cavities, the charging spring lamination（31）With
Charging contact（11）Contact, the clamping mechanism and unmanned plane clamping；Work as magnechuck（21）With manipulator（2）It is moved to battery
Bag（1）Top and when being powered, the metal derby（13）It is moved up by attraction and clamping mechanism is driven to be unclamped with unmanned plane.
2. the battery change system of a kind of express delivery unmanned plane according to claim 1, it is characterised in that the battery cavities
Surrounding has upwardly extended a circle flange collar（3）, the flange collar（3）The upper screens set around periphery, the clamping mechanism include
At least two are uniformly distributed and are hinged on battery pack（1）The kelly at top（12）, the kelly（12）With extending downward into
The claw that can be clamped with screens, the metal derby（13）It is fixedly connected on kelly（12）On, the kelly（12）And metal derby
（13）Gravity force claw toward inside rotate with screens be clamped, the metal derby（13）During by attracting to move up, the card
Bar（12）It is rotated toward outside.
A kind of 3. battery change system of express delivery unmanned plane according to claim 2, it is characterised in that the clamping mechanism
It further includes and is arranged on battery pack（1）The spring at top（14）, the spring（14）Withstand kelly（12）Claw is forced to have inside
The trend that side rotates.
A kind of 4. battery change system of express delivery unmanned plane according to claim 3, it is characterised in that the battery pack（1）
It further includes and is arranged on battery pack（1）The end cap at top（15）, the clamping mechanism, metal derby（13）And spring（14）It is respectively positioned on end
Lid（15）Inside.
5. the battery change system of a kind of express delivery unmanned plane according to claim 1, it is characterised in that further include landing first
Plate（4）And position-limit mechanism（5）, the position-limit mechanism（5）Including motor（51）With motor（51）The gear that is fixedly connected of shaft
（52）, four pieces be uniformly distributed and can move back and forth respectively and gear（52）The rack of engagement（53）And it is fixedly connected on tooth
Item（53）On gag lever post（54）, the gag lever post（54）Positioned at landing deck（4）Top, four gag lever posts（54）
For arc structure and it is movable to landing deck（4）Centre forms annular shape, and the unmanned plane includes being evenly distributed on lower section
At least three supporting legs, be provided with block on the supporting leg（6）, when four gag lever posts（54）It is described when forming circular
Gag lever post（54）Positioned at block（6）Top.
A kind of 6. battery change system of express delivery unmanned plane according to claim 5, it is characterised in that opposite gag lever post
（54）In sustained height, adjacent gag lever post（54）In different height, the gag lever post（54）Circular arc both ends also distinguish
It is provided with extended end（541）, work as gag lever post（54）It is moved to landing deck（4）During outside, four gag lever posts（54）It can incite somebody to action
Landing deck（4）Centre is trapped among, two layers of gag lever post with different height respectively is provided on the supporting leg（54）Corresponding block
（6）.
7. the battery change system of a kind of express delivery unmanned plane according to claim 5, it is characterised in that the unmanned plane
Supporting leg bottom is provided with universal caster wheel（7）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711448041.7A CN108058842A (en) | 2017-12-27 | 2017-12-27 | A kind of battery change system of express delivery unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711448041.7A CN108058842A (en) | 2017-12-27 | 2017-12-27 | A kind of battery change system of express delivery unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108058842A true CN108058842A (en) | 2018-05-22 |
Family
ID=62140438
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711448041.7A Withdrawn CN108058842A (en) | 2017-12-27 | 2017-12-27 | A kind of battery change system of express delivery unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108058842A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945489A (en) * | 2018-08-01 | 2018-12-07 | 深圳市旭发智能科技有限公司 | A kind of installation method of unmanned machine battery |
| CN110697059A (en) * | 2019-10-22 | 2020-01-17 | 国网安徽省电力有限公司蚌埠供电公司 | Unmanned aerial vehicle battery dismouting cabin |
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| CN202922160U (en) * | 2012-10-19 | 2013-05-08 | 南京信息工程大学 | Battery automatic changing system of small sized multi-rotor unmanned aerial vehicle |
| CN104981403A (en) * | 2014-08-08 | 2015-10-14 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle base station and battery change device therefor |
| CN104973263A (en) * | 2015-06-23 | 2015-10-14 | 广东溢达纺织有限公司 | Automatic battery replacement device and method |
| US9481458B2 (en) * | 2013-04-29 | 2016-11-01 | The Boeing Company | Device and method for use with unmanned aerial vehicles |
| CN106428602A (en) * | 2016-10-12 | 2017-02-22 | 北京中飞艾维航空科技有限公司 | Unmanned aerial vehicle electricity supplementing device |
| US20170174091A1 (en) * | 2015-12-16 | 2017-06-22 | Skycatch, Inc. | Unmanned aerial vehicle battery replacement arm |
| CN206569262U (en) * | 2016-12-09 | 2017-10-20 | 华南理工大学广州学院 | A kind of UAS |
| CN206569272U (en) * | 2016-12-09 | 2017-10-20 | 华南理工大学广州学院 | A kind of intelligent charge duration flight device system |
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2017
- 2017-12-27 CN CN201711448041.7A patent/CN108058842A/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202922160U (en) * | 2012-10-19 | 2013-05-08 | 南京信息工程大学 | Battery automatic changing system of small sized multi-rotor unmanned aerial vehicle |
| US9481458B2 (en) * | 2013-04-29 | 2016-11-01 | The Boeing Company | Device and method for use with unmanned aerial vehicles |
| CN104981403A (en) * | 2014-08-08 | 2015-10-14 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle base station and battery change device therefor |
| CN104973263A (en) * | 2015-06-23 | 2015-10-14 | 广东溢达纺织有限公司 | Automatic battery replacement device and method |
| US20170174091A1 (en) * | 2015-12-16 | 2017-06-22 | Skycatch, Inc. | Unmanned aerial vehicle battery replacement arm |
| CN106428602A (en) * | 2016-10-12 | 2017-02-22 | 北京中飞艾维航空科技有限公司 | Unmanned aerial vehicle electricity supplementing device |
| CN206569262U (en) * | 2016-12-09 | 2017-10-20 | 华南理工大学广州学院 | A kind of UAS |
| CN206569272U (en) * | 2016-12-09 | 2017-10-20 | 华南理工大学广州学院 | A kind of intelligent charge duration flight device system |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108945489A (en) * | 2018-08-01 | 2018-12-07 | 深圳市旭发智能科技有限公司 | A kind of installation method of unmanned machine battery |
| CN110697059A (en) * | 2019-10-22 | 2020-01-17 | 国网安徽省电力有限公司蚌埠供电公司 | Unmanned aerial vehicle battery dismouting cabin |
| CN110697059B (en) * | 2019-10-22 | 2024-11-12 | 国网安徽省电力有限公司蚌埠供电公司 | A battery disassembly and assembly cabin for drone |
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180522 |
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