CN206107593U - Unmanned aerial vehicle electric quantity replenishing device - Google Patents
Unmanned aerial vehicle electric quantity replenishing device Download PDFInfo
- Publication number
- CN206107593U CN206107593U CN201621116405.2U CN201621116405U CN206107593U CN 206107593 U CN206107593 U CN 206107593U CN 201621116405 U CN201621116405 U CN 201621116405U CN 206107593 U CN206107593 U CN 206107593U
- Authority
- CN
- China
- Prior art keywords
- battery
- unmanned plane
- charging panel
- battery charging
- electricity device
- 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.)
- Active
Links
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model provides an unmanned aerial vehicle electric quantity replenishing device, get the mechanism including unmanned aerial vehicle landing platform, battery charging panel and battery dress, the battery dress is got the mechanism and is included the manipulator, the unmanned aerial vehicle landing platform sets up the inside at the battery charging panel to the battery charging panel goes up and down relatively, the equipartition is provided with a plurality of battery depots on the battery charging panel, and a plurality of battery depots can charge for simultaneously a plurality of batteries, machinery handbag draws together the telescopic link and gets the thing claw, getting the thing claw and setting up a tip at the telescopic link, the telescopic link can be followed its length direction and stretched out and drawn back. The utility model provides a pair of unmanned aerial vehicle electric quantity replenishing device can take out the battery that has exhausted when unmanned aerial vehicle electric quantity insufficient supply, put into unmanned aerial vehicle with the battery of having substituted the bad for the good on the battery charging panel again, need not the manual work and changes the battery.
Description
Technical field
This utility model is related to unmanned plane application, in particular to a kind of unmanned plane electricity device for supplying.
Background technology
At present, unmanned air vehicle technique is applied to electric inspection process effect significantly, and it is not limited by topography and geomorphology, is particularly suited for danger
Line walking work under high mountain area, many river morphologies.Airborne high-definition camera equipment can carry out tuning on-line and monitoring to transmission line of electricity
And fact is returned in time, beneficial to exclusion line defct and major hidden danger is found, inspection efficiency is greatly improved, and saves a large amount of manpower things
Power.But, unmanned plane carries the items of equipment high-altitude non-stop flight activity duration and is unable to maintain that oversize, and easily supply is not or not internal electricity
Foot, endurance is restricted, and needs artificial Jing often to change battery, increases labor intensity, and the use for giving people brings not
Just.
Based on this, this utility model provides a kind of unmanned plane electricity device for supplying to solve above-mentioned technical problem.
Utility model content
In view of this, the purpose of this utility model embodiment is to provide a kind of unmanned plane electricity device for supplying, to solve
There is unmanned plane endurance in prior art to be restricted, need artificial Jing often to change battery, increase the skill of labor intensity
Art problem.
This utility model embodiment provides a kind of unmanned plane electricity device for supplying, including UAV Landing platform, battery
Charging panel and battery Zhuan Qu mechanisms, the battery Zhuan Qu mechanisms include mechanical hand；
The UAV Landing platform is arranged on the inside of the battery charging panel, and can relatively described battery charging panel
Rotated and/or lifted；
Multiple battery depots are uniformly arranged on the battery charging panel, multiple battery depots can simultaneously to many
Individual battery charges；
The mechanical hand includes expansion link and takes thing pawl, described to take the end that thing pawl is arranged on the expansion link, institute
Stating expansion link can be stretched along its length.
Preferably, this utility model embodiment provides a kind of unmanned plane electricity device for supplying, wherein, the unmanned plane
Lu Pingtai middle parts are provided with stopper slot, and the stopper slot is engaged by clamping with the base of unmanned plane, for the spacing unmanned plane.
Preferably, this utility model embodiment provides a kind of unmanned plane electricity device for supplying, wherein, the stopper slot bag
Include cell body, two springs and two catch；
Draw-in groove is provided with two side walls of the cell body, two draw-in grooves are symmetrical arranged；
Two springs are located in two draw-in grooves respectively, and one end of two springs is separately fixed at two institutes
State at the bottom land of draw-in groove, the other end of two springs is affixed with two catch respectively；
Two catch are inserted into respectively in the corresponding draw-in groove, and can be slided along groove depth direction.
Preferably, this utility model embodiment provides a kind of unmanned plane electricity device for supplying, wherein, the expansion link is remote
It is connected with elevating mechanism from described one end for taking thing pawl, and can vertically moves in the presence of the elevating mechanism.
Preferably, this utility model embodiment provides a kind of unmanned plane electricity device for supplying, wherein, the mechanical hand is also
Including swing arm；
The expansion link is hinged away from described one end for taking thing pawl and one end of the swing arm, the other end of the swing arm with
Elevating mechanism is hinged, and can swing in perpendicular.
Preferably, this utility model embodiment provides a kind of unmanned plane electricity device for supplying, wherein, the battery dress takes
Mechanism also includes that battery pushes position and battery exits position；
The battery pushes position and is arranged on the UAV Landing platform；
The battery exits position and is arranged on the battery charging panel.
Preferably, this utility model embodiment provides a kind of unmanned plane electricity device for supplying, wherein, also including driving
Device；
The driver is arranged on the bottom of the battery charging panel, including motor and gear, the output shaft of the motor
It is connected with the gear；
The battery charging panel is provided with circumferentially extending tooth bar, and the tooth bar is engaged with the gear, the electricity
Machine can drive the tooth bar to rotate, and finally drive the battery charging panel to rotate.
Preferably, this utility model embodiment provides a kind of unmanned plane electricity device for supplying, wherein, also including control mould
Block；
The control module includes the signal acquiring unit being arranged on the UAV Landing platform and is arranged on described
Signal driving unit in battery Zhuan Qu mechanisms；The signal acquiring unit, for obtaining the approaching signal of the unmanned plane, and
Send to the signal driving unit；The signal driving unit, for after the approaching signal is received, driving the electricity
Chi Zhuanqu mechanisms work.
Preferably, this utility model embodiment provides a kind of unmanned plane electricity device for supplying, wherein, the signal acquisition
Unit is GPS locator.
Preferably, this utility model embodiment provides a kind of unmanned plane electricity device for supplying, wherein, the battery supply
Voltage sensor is additionally provided with standing；
The voltage sensor, for judging the battery depot in battery it is whether fully charged, when judged result is
When being, the battery depot stops charging the battery.
A kind of unmanned plane electricity device for supplying that this utility model embodiment is provided, mainly include UAV Landing platform,
Battery charging panel and battery Zhuan Qu mechanisms, battery Zhuan Qu mechanisms include mechanical hand；UAV Landing platform is arranged on battery charging
The inside of plate, and can be lifted with respect to battery charging panel；Multiple battery depots have been uniformly arranged on battery charging panel, it is many
Individual battery depot can charge to multiple batteries simultaneously；Mechanical hand includes expansion link and takes thing pawl；Take thing pawl and be arranged on expansion link
An end, expansion link can be stretched along its length.
A kind of unmanned plane electricity device for supplying that this utility model is provided, can take when the supply of unmanned plane electricity is not enough
Go out the battery for having exhausted, then the battery substituted the bad for the good on battery charging panel is put in unmanned plane, without the need for manually carrying out changing electricity
Pond.
Based on this, this utility model changes battery, so as to reduce the advantage of labor intensity compared with original technology with automatic.
Description of the drawings
In order to be illustrated more clearly that the technical scheme of this utility model embodiment, below will be to use needed for embodiment
Accompanying drawing be briefly described, it will be appreciated that the following drawings illustrate only some embodiments of the present utility model, therefore should not be by
Regard the restriction to scope as, for those of ordinary skill in the art, on the premise of not paying creative work, may be used also
To obtain other related accompanying drawings according to these accompanying drawings.
Fig. 1 shows a kind of structure chart of unmanned plane electricity device for supplying that this utility model embodiment is provided；
Fig. 2 shows the structure of stopper slot in a kind of unmanned plane electricity device for supplying that this utility model embodiment is provided
Figure；
Fig. 3 shows a kind of another kind of structure of unmanned plane electricity device for supplying that this utility model embodiment is provided
Figure.
Digitized representation meaning is as follows in accompanying drawing：
10- UAV Landing platforms
11- stopper slots
111- springs
112- cell bodies
113- catch
20- battery charging panels
The full electricity batteries of 21-
22- batteries depot
30- mechanical hands
31- takes thing pawl
32- expansion links
33- swing arms
40- elevating mechanisms
50- battery compartments
60- drivers
61- gears
62- tooth bars
63- motors
Specific embodiment
Below in conjunction with accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out clearly
Chu, it is fully described by, it is clear that described embodiment is only a part of embodiment of this utility model, rather than the reality of whole
Apply example.The component of this utility model embodiment generally described and illustrated in accompanying drawing herein can be come with a variety of configurations
Arrangement and design.Therefore, the detailed description of embodiment of the present utility model below to providing in the accompanying drawings is not intended to limit
Claimed scope of the present utility model, but it is merely representative of selected embodiment of the present utility model.Based on this utility model
Embodiment, the every other embodiment that those skilled in the art are obtained on the premise of creative work is not made, all
Belong to the scope of this utility model protection.
In description of the present utility model, it should be noted that term " " center ", " on ", D score, "left", "right", " perpendicular
Directly ", the orientation or position relationship of the instruction such as " level ", " interior ", " outward " is, based on orientation shown in the drawings or position relationship, to be only
For the ease of describe this utility model and simplify description, rather than indicate or imply indication device or element must have it is specific
Orientation, with specific azimuth configuration and operation, therefore it is not intended that to restriction of the present utility model.Additionally, term " the
One ", " second ", " the 3rd " are only used for describing purpose, and it is not intended that indicating or implying relative importance.
In description of the present utility model, it should be noted that unless otherwise clearly defined and limited, term " peace
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected, or connected using hot plug mode,
Or be integrally connected；Can be mechanically connected, or electrically connect；Can be joined directly together, it is also possible to by intermediary
It is indirectly connected to, can is the connection of two element internals.For the ordinary skill in the art, can be managed with concrete condition
Solve concrete meaning of the above-mentioned term in this utility model.
As shown in figure 1, a kind of unmanned plane electricity device for supplying that this utility model embodiment is provided includes UAV Landing
Platform 10, battery charging panel 20 and battery Zhuan Qu mechanisms, battery Zhuan Qu mechanisms include mechanical hand 30；
UAV Landing platform 10 is arranged on the inside of battery charging panel 20, and can be revolved with respect to battery charging panel 20
Turn and/or lift；
Multiple battery depots 22 are uniformly arranged on battery charging panel 20, multiple battery depots 22 can simultaneously to multiple
Battery charges；
Mechanical hand 30 is including expansion link 32 and takes thing pawl 31, takes the end that thing pawl 31 is arranged on expansion link 32, stretches
Bar 32 can be stretched along its length.
A kind of unmanned plane electricity device for supplying that this utility model is provided, is provided with battery compartment 50, battery inside unmanned plane
Battery in storehouse 50 carries items of equipment and provides electric energy in high-altitude flight operation for unmanned plane, after non-stop flight operation, battery compartment
The easy electricity shortage of battery inside 50, now, is arranged on the detection means inside unmanned plane and is detecting the letter of not enough power supply
Number when, unmanned plane can be driven to fly to disposed proximally unmanned plane electricity device for supplying.
Specific UAV Landing platform 10 is circular plate-like shape platform, and battery charging panel 20 is put down for the tabular of annular
Platform, UAV Landing platform 10 is arranged on the inside of battery charging panel 20, and the external diameter of UAV Landing platform 10 is equal to battery
The internal diameter of charging panel 20.
It is flat with UAV Landing platform 10 at the opening of battery compartment 50 after unmanned plane is dropped on UAV Landing platform 10
Together, thus, the battery in battery compartment 50 clog-free can be slided out on UAV Landing platform 10 from battery compartment 50.Nobody
Machine landing platform 10 is rotated and is lifted relative to battery charging panel 20, and rotation causes the battery compartment 50 of unmanned plane in flexible
In the telescopic direction of bar 32, lifting cause UAV Landing platform 10 higher than battery charging panel 20 or less than battery charging panel 20 or
It is concordant with battery charging panel 20.
Further, the middle part of UAV Landing platform 10 is provided with the base clamping of stopper slot 11, stopper slot 11 and unmanned plane
Coordinate, for spacing unmanned plane.Preferably, stopper slot 11 includes 112, two springs 111 of cell body and two catch 113；Cell body
Draw-in groove is provided with 112 two side walls, two draw-in grooves are symmetrical arranged；Two springs 111 are located at respectively in two draw-in grooves, and two
One end of individual spring 111 is separately fixed at the bottom land of two draw-in grooves, the other end of two springs 111 respectively with two catch
113 is affixed；Two catch 113 are inserted into respectively in corresponding draw-in groove, and can be slided along groove depth direction, as shown in Figure 2.Unmanned plane
After landing, base and the cell body 112 of unmanned plane coordinate, and contact with two catch 113, and unmanned plane is continued traveling downwardly, to two gears
113 1 downward power of piece, catch 113 pushes under this force the spring 111 with the corresponding connection of two catch 113 open, so far,
Complete fixation of the stopper slot 11 to unmanned plane.
Unmanned plane is dropped on UAV Landing platform 10 and after fixation, and the battery compartment 50 on unmanned plane may face machine
Thing pawl 31 is taken on tool handss 30, it is also possible to towards other directions.When battery compartment 50 faces taking on mechanical hand 30 on unmanned plane
During thing pawl 31, UAV Landing platform 10 is lifted as needed without the need for rotation with respect to battery charging panel 20；When nobody
Towards other directions, UAV Landing platform 10 needs rotation to battery compartment 50 on machine, so that battery compartment 50 faces mechanical hand
Taking in thing pawl 31, the i.e. telescopic direction in expansion link 32 on 30.
Multiple battery depots 22 are along the circumferential direction uniformly arranged on battery charging panel 20, multiple battery depots 22 can
Charge to multiple batteries simultaneously.Before battery altering is carried out to unmanned plane, one is at least should be ensured that on battery charging panel 20
Battery above is in fully charged state, and the fully charged battery is in a perpendicular, for replacing with battery compartment 50
Change the battery exhausted on unmanned plane.
Mechanical hand 30 is including expansion link 32 and takes thing pawl 31, takes the end that thing pawl 31 is arranged on expansion link 32.As
One preferred version of the present embodiment, the other end and the elevating mechanism 40 of expansion link 32 are slidably connected, and can be in elevating mechanism
Vertically move in the presence of 40, therefore, taking thing pawl 31 can also follow expansion link 32 on elevating mechanism 40 along vertically
Slide in direction.Battery Zhuan Qu mechanisms also include that battery pushes position and battery exits position；Battery pushes position and is arranged on UAV Landing
On platform 10；Battery exits position and is arranged on battery charging panel 20.
When UAV Landing platform 10 is higher than battery charging panel 20, expansion link 32 can drive and take thing pawl 31 along vertical side
To the position slided into the sustained height of battery compartment 50, now expansion link 32 goes out battery and pushes on position, and expansion link 32 extends forward,
So that the thing pawl 31 that takes for being arranged on the end of expansion link 32 captures the battery exhausted inside battery compartment 50, the receding of expansion link 32
It is short, that is, return to battery and push on position, take out from battery compartment 50 so as to take thing pawl 31 and will exhaust battery, expansion link 32 drives
The battery for having exhausted that thing pawl 31 is taken together with crawl is moved downward to the position contour with battery charging panel 20, in battery charging panel
Battery on 20 exits release at position and takes thing pawl 31, so that the battery for having exhausted falling to exited on position in battery.Because battery charges
It has been used to replace the full battery 21 for having exhausted battery on plate 20, and the full electricity battery 21 is perpendicular in one with battery compartment 50
In straight plane, now, mechanical hand 30 can accurately capture full electricity battery 21 by expansion link 32, and rear telescopic rod 32 drives and takes thing
Pawl 31 is moved upward to the position contour with UAV Landing platform 10 together with the full battery 21 of crawl, and now expansion link 32 goes out
Battery is pushed on position, and expansion link 32 extends forward, takes thing pawl 31 and is pushed into full battery 21 in the battery compartment 50 of unmanned plane, extremely
This, completes the automatic replacement of unmanned machine battery.
When UAV Landing platform 10 drops to it is concordant with battery charging panel 20 when, battery pushes position and battery and exits position and exist
Straight line, the position that full electricity battery 21 is in battery push and battery is exited between position are in horizontal direction.Mechanical hand
During 30 replacement battery, take thing pawl 31 and push on position in battery, expansion link 32 extends, and be arranged on the end of expansion link 32 takes thing pawl
The battery exhausted inside 31 crawl battery compartments 50, expansion link 32 shortens backward, that is, return to battery and push on position, so as to take thing
Pawl 31 will exhaust battery and take out in the battery compartment 50, expansion link 32 drive the battery for having exhausted that takes thing pawl 31 together with crawl to
After upper movement, expansion link 32 shortens and is displaced downwardly to the position (with across full battery 21) contour with battery charging panel 20 again, in electricity
Battery exits release at position and takes thing pawl 31 on pond charging panel 20, so that the battery for having exhausted falling to exited on position in battery.Due to electricity
It has been used to replace the full battery 21 for having exhausted battery on pond charging panel 20, and the full electricity battery 21 pushes in battery and is
And the position that battery is exited between position, now, mechanical hand 30 can accurately capture full electricity battery 21 by expansion link 32, then stretch
Full battery 21 is pushed to battery and is pushed on position by contracting bar 32, and expansion link 32 continues to extend forward, and taking thing pawl 31 will full electricity battery
21 are pushed in the battery compartment 50 of unmanned plane, so far, complete the automatic replacement of unmanned machine battery.
When UAV Landing platform 10 is less than battery charging panel 20, mechanical hand 30 replaces battery and UAV Landing platform
10 are similar to less than the situation of battery charging panel 20, repeat no more here.
As shown in figure 3, of a kind of unmanned plane electricity device for supplying provided as this utility model embodiment is preferred
Scheme, mechanical hand 30 also includes swing arm 33；
Expansion link 32 is hinged away from the one end for taking thing pawl 31 with one end of swing arm 33, the other end and elevating mechanism of swing arm 33
40 are hinged, and can swing in perpendicular.
Specifically, because expansion link 32 is hinged away from the one end for taking thing pawl 31 with one end of swing arm 33, swing arm 33 it is another
End be hinged with elevating mechanism 40, expansion link 32 can opposed swing arms 33 rotate in perpendicular, swing arm 33 being capable of OQ t
Mechanism 40 rotates in perpendicular.Compare the side that aforementioned expansion link 32 can slide along the in the vertical direction of elevating mechanism 40
Case, swing arm 33 in this programme instead of movement of the expansion link about 32 along the rotation of elevating mechanism 40, as shown in Figure 3.When nobody
When machine landing platform 10 is higher than battery charging panel 20, swing arm 33 is rotated up, so that expansion link 32 is in same with battery compartment 50
The position of height, now expansion link 32 go out battery push position on, expansion link 32 extends forward, so as to be arranged on the end of expansion link 32
Take the battery that exhausted inside the crawl battery compartment 50 of thing pawl 31, expansion link 32 shortens backward, that is, return to battery and push on position,
Take out from battery compartment 50 so as to take thing pawl 31 and will exhaust battery, swing arm 33 is rotated down, and expansion link 32 drives and takes thing pawl 31
The position contour with battery charging panel 20, the electricity on battery charging panel 20 are moved downward to together with the battery for having exhausted of crawl
Pond exits release at position and takes thing pawl 31, so that the battery for having exhausted falling to exited on position in battery.Due on battery charging panel 20
Have for replacing the full battery 21 for having exhausted battery, and the full electricity battery 21 is in a perpendicular with battery compartment 50
Interior, now, mechanical hand 30 can pass through the accurately full electricity battery 21 of crawl of expansion link 32, and the drive of rear telescopic rod 32 takes thing pawl 31 and connects
The position contour with UAV Landing platform 10 is moved upward to the full battery 21 of crawl, now expansion link 32 goes out battery and pushes away
Send on position, expansion link 32 extends forward, take thing pawl 31 and full battery 21 is pushed in the battery compartment 50 of unmanned plane, it is so far, complete
Into the automatic replacement of unmanned machine battery.
When UAV Landing platform 10 drops to or UAV Landing platform 10 concordant with battery charging panel 20 less than battery
The situation of charging panel 20, the replacement battery of mechanical hand 30 is similar with preceding method, repeats no more here.
A kind of one preferred version of the unmanned plane electricity device for supplying provided as this utility model embodiment, also includes
Driver 60；
Driver 60 is arranged on the bottom of battery charging panel 20, including motor 63 and gear 61, the output shaft of motor 63 with
Gear 61 connects；
Battery charging panel 20 is provided with circumferentially extending tooth bar 62, and tooth bar 62 is engaged with gear 61, and motor 63 can band
Carry-over bar 62 rotates, final to drive battery charging panel 20 to rotate.
Specifically, it is often that a unmanned plane changes battery when the battery depot 22 on battery charging panel 20 is multiple
Afterwards, driver 60 can drive battery charging panel 20 to rotate, and next full electricity battery 21 is moved to into correspondence UAV Landing
The position of battery compartment 50 afterwards, is that replacing battery next time is prepared.
It is emphasized that driver 60 drive battery charging panel 20 to carry out rotation can also be during battery be changed
Use.If by battery exit position and full battery 21 along the circumferencial direction of battery charging panel 20 arrange when, replace to unmanned plane
Before battery, battery exits the lower section that position is arranged on battery compartment 50, mechanical hand 30 will the battery that exhausted take out after be placed on electricity
Pond is exited on position, and battery charging panel 20 is rotated under the driving of driver 60, and full battery 21 is rotated to battery compartment
50 lower section, mechanical hand 30 is again placed into full electricity battery 21 crawl in battery compartment 50, so far, completes the replacement of battery.
A kind of one preferred version of the unmanned plane electricity device for supplying provided as this utility model embodiment, also includes
Control module；
Control module includes that the signal acquiring unit being arranged on UAV Landing platform 10 takes machine with battery dress is arranged on
Signal driving unit on structure；Signal acquiring unit, for obtaining the approaching signal of unmanned plane, and sending to signal list is driven
Unit；Signal driving unit, for after approaching signal is received, driving the work of battery Zhuan Qu mechanisms.Specifically, above-mentioned signal is obtained
Unit is taken for GPS locator.
A kind of one preferred version of the unmanned plane electricity device for supplying provided as this utility model embodiment, battery is mended
To station 22 on be additionally provided with voltage sensor；
Voltage sensor, for judging battery depot 22 in battery it is whether fully charged, when judged result is to be
Wait, battery depot 22 stops charging the battery.
More than, specific embodiment only of the present utility model, but protection domain of the present utility model is not limited thereto,
Any those familiar with the art can readily occur in change or replace in the technical scope that this utility model is disclosed
Change, all should cover within protection domain of the present utility model.Therefore, protection domain of the present utility model should be with claim
Protection domain is defined.
Claims (10)
1. a kind of unmanned plane electricity device for supplying, it is characterised in that including UAV Landing platform, battery charging panel and battery dress
Mechanism is taken, the battery Zhuan Qu mechanisms include mechanical hand；
The UAV Landing platform is arranged on the inside of the battery charging panel, and can relatively described battery charging panel carry out
Rotation and/or lifting；
Multiple battery depots are uniformly arranged on the battery charging panel, multiple battery depots can simultaneously give multiple electricity
Charge in pond；
The mechanical hand includes expansion link and takes thing pawl, described to take the end that thing pawl is arranged on the expansion link, described to stretch
Contracting bar can be stretched along its length.
2. a kind of unmanned plane electricity device for supplying according to claim 1, it is characterised in that the UAV Landing platform
Middle part is provided with stopper slot, and the stopper slot is engaged by clamping with the base of unmanned plane, for the spacing unmanned plane.
3. a kind of unmanned plane electricity device for supplying according to claim 2, it is characterised in that the stopper slot includes groove
Body, two springs and two catch；
Draw-in groove is provided with two side walls of the cell body, two draw-in grooves are symmetrical arranged；
Two springs are located in two draw-in grooves respectively, and one end of two springs is separately fixed at two cards
At the bottom land of groove, the other end of two springs is affixed with two catch respectively；
Two catch are inserted into respectively in the corresponding draw-in groove, and can be slided along groove depth direction.
4. a kind of unmanned plane electricity device for supplying according to claim 1, it is characterised in that the expansion link is away from described
The one end for taking thing pawl is connected with elevating mechanism, and can vertically move in the presence of the elevating mechanism.
5. a kind of unmanned plane electricity device for supplying according to claim 1, it is characterised in that the mechanical hand also includes pendulum
Arm；
The expansion link is hinged away from described one end for taking thing pawl and one end of the swing arm, the other end and the lifting of the swing arm
Mechanism is hinged, and can swing in perpendicular.
6. a kind of unmanned plane electricity device for supplying according to claim 1, it is characterised in that the battery Zhuan Qu mechanisms are also
Position is pushed including battery and battery exits position；
The battery pushes position and is arranged on the UAV Landing platform；
The battery exits position and is arranged on the battery charging panel.
7. a kind of unmanned plane electricity device for supplying according to claim 1, it is characterised in that also including driver；
The driver is arranged on the bottom of the battery charging panel, including motor and gear, the output shaft of the motor and institute
State gear connection；
The battery charging panel is provided with circumferentially extending tooth bar, and the tooth bar is engaged with the gear, and the motor can
Drive the tooth bar to rotate, finally drive the battery charging panel to rotate.
8. a kind of unmanned plane electricity device for supplying according to claim 1, it is characterised in that also including control module；
The control module includes the signal acquiring unit being arranged on the UAV Landing platform and is arranged on the battery
Signal driving unit in Zhuan Qu mechanisms；The signal acquiring unit, for obtaining the approaching signal of the unmanned plane, and sends
To the signal driving unit；The signal driving unit, for after the approaching signal is received, driving the battery dress
Take mechanism's work.
9. a kind of unmanned plane electricity device for supplying according to claim 8, it is characterised in that the signal acquiring unit is
GPS locator.
10. a kind of unmanned plane electricity device for supplying according to claim 1, it is characterised in that in the battery depot
It is additionally provided with voltage sensor；
The voltage sensor, for judging the battery depot in battery it is whether fully charged, when judged result is for yes
When, the battery depot stops charging the battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621116405.2U CN206107593U (en) | 2016-10-12 | 2016-10-12 | Unmanned aerial vehicle electric quantity replenishing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621116405.2U CN206107593U (en) | 2016-10-12 | 2016-10-12 | Unmanned aerial vehicle electric quantity replenishing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206107593U true CN206107593U (en) | 2017-04-19 |
Family
ID=58529348
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621116405.2U Active CN206107593U (en) | 2016-10-12 | 2016-10-12 | Unmanned aerial vehicle electric quantity replenishing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206107593U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN107380464A (en) * | 2017-07-28 | 2017-11-24 | 长春草莓科技有限公司 | A kind of unmanned plane battery rotary formula changes structure |
| CN108275283A (en) * | 2018-03-30 | 2018-07-13 | 上海拓攻机器人有限公司 | A kind of unmanned plane charging pile |
| CN108515866A (en) * | 2018-04-04 | 2018-09-11 | 江南大学 | A kind of detachable battery changing-over charging unit |
| CN109774959A (en) * | 2019-01-10 | 2019-05-21 | 山东理工大学 | The unmanned plane landing platform of the automatic replacement cell apparatus of band |
| CN111942604A (en) * | 2020-07-13 | 2020-11-17 | 李隆锦 | Unmanned aerial vehicle battery replacement system |
-
2016
- 2016-10-12 CN CN201621116405.2U patent/CN206107593U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN107380464A (en) * | 2017-07-28 | 2017-11-24 | 长春草莓科技有限公司 | A kind of unmanned plane battery rotary formula changes structure |
| CN107380464B (en) * | 2017-07-28 | 2023-08-04 | 深圳草莓创新技术有限公司 | Unmanned aerial vehicle battery rotation type changes structure |
| CN108275283A (en) * | 2018-03-30 | 2018-07-13 | 上海拓攻机器人有限公司 | A kind of unmanned plane charging pile |
| CN108515866A (en) * | 2018-04-04 | 2018-09-11 | 江南大学 | A kind of detachable battery changing-over charging unit |
| CN109774959A (en) * | 2019-01-10 | 2019-05-21 | 山东理工大学 | The unmanned plane landing platform of the automatic replacement cell apparatus of band |
| CN111942604A (en) * | 2020-07-13 | 2020-11-17 | 李隆锦 | Unmanned aerial vehicle battery replacement system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206107593U (en) | Unmanned aerial vehicle electric quantity replenishing device | |
| CN106428602A (en) | Unmanned aerial vehicle electricity supplementing device | |
| CN104973263B (en) | Automatically cell apparatus and method are changed | |
| CN110667870B (en) | Unmanned aerial vehicle is energy autonomous base station of independently taking off and land trading battery based on solar energy power supply | |
| CN102909540B (en) | Battery automatic replacement system of small-sized multi-rotor-wing unmanned aerial vehicle | |
| CN108237934A (en) | Charging station and charging station module | |
| CN202922160U (en) | Battery automatic changing system of small sized multi-rotor unmanned aerial vehicle | |
| CN205178593U (en) | Unmanned aerial vehicle platform that charges | |
| CN106043247A (en) | Modular extensible electrical changing station equipment and charging rack | |
| CN106787105A (en) | Unmanned plane vehicle-mounted charging device and vehicle | |
| CN107672817A (en) | A kind of intelligent landing system of mobile vehicle-mounted unmanned plane | |
| CN204835618U (en) | Quick charging system of unmanned aerial vehicle | |
| CN107344628A (en) | A kind of structure for changing unmanned machine battery | |
| CN202481049U (en) | Battery changing equipment | |
| CN209719932U (en) | Double-deck more rotor power transmission line inspection devices | |
| CN207842906U (en) | Unmanned plane battery replacement device and unmanned plane battery altering equipment | |
| CN107733365A (en) | The EL automatic testing equipments and system of a kind of photovoltaic module | |
| CN108945500A (en) | Quadrotor drone movable type landing platform and battery methods are replaced automatically | |
| CN108919080A (en) | A kind of solar cell Performance Test System and its test method | |
| CN108012825A (en) | One kind automation hydrojet control method | |
| CN112171680A (en) | Primary and secondary inspection robot for mountain photovoltaic power station | |
| CN108460954A (en) | A kind of monitoring of freezing disaster and early alarming and forecasting method | |
| CN206569272U (en) | A kind of intelligent charge duration flight device system | |
| CN108460953A (en) | A kind of monitoring of freezing disaster and early-warning and predicting system | |
| CN205793080U (en) | A kind of full-automatic four station Camera Test machines |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |