CN112736358A - Unmanned aerial vehicle group battery of easy dismouting - Google Patents

Unmanned aerial vehicle group battery of easy dismouting Download PDF

Info

Publication number
CN112736358A
CN112736358A CN202011552411.3A CN202011552411A CN112736358A CN 112736358 A CN112736358 A CN 112736358A CN 202011552411 A CN202011552411 A CN 202011552411A CN 112736358 A CN112736358 A CN 112736358A
Authority
CN
China
Prior art keywords
aerial vehicle
unmanned aerial
battery
main body
clamping
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.)
Withdrawn
Application number
CN202011552411.3A
Other languages
Chinese (zh)
Inventor
王洪明
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN202011552411.3A priority Critical patent/CN112736358A/en
Publication of CN112736358A publication Critical patent/CN112736358A/en
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02Aircraft characterised by the type or position of power plant
    • B64D27/24Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M2220/00Batteries for particular applications
    • H01M2220/20Batteries in motive systems, e.g. vehicle, ship, plane
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries

Abstract

The invention relates to the field of unmanned aerial vehicle battery pack equipment, in particular to an unmanned aerial vehicle battery pack easy to disassemble and assemble, which comprises an unmanned aerial vehicle main body, wherein a mounting seat is fixedly mounted on one side of the bottom end of the unmanned aerial vehicle main body, a battery main body is embedded and mounted on one side of the bottom end of the mounting seat, a camera is fixedly mounted on one side, close to the battery main body, of the bottom end of the unmanned aerial vehicle main body, connecting arms are fixedly mounted on the periphery of the outer wall of the unmanned aerial vehicle main body, propellers are fixedly mounted on one sides of the outer ends of the connecting arms, an access hole is formed in one side of the interior of the battery main body, an access cover is arranged. The unmanned aerial vehicle battery pack disassembling and assembling device can enable the whole device to realize more convenient and efficient unmanned aerial vehicle battery pack disassembling and assembling, effectively improves the working efficiency of users, improves the practicability of the whole device, and brings better use prospect.

Description

Unmanned aerial vehicle group battery of easy dismouting
Technical Field
The invention relates to the field of unmanned aerial vehicle battery pack equipment, in particular to an unmanned aerial vehicle battery pack easy to disassemble and assemble.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The unmanned aerial vehicle has no cockpit, but is provided with an automatic pilot, a program control device and other equipment, the power supply of the unmanned aerial vehicle in flight mainly comes from a storage battery inside the unmanned aerial vehicle, the storage battery has a certain service life, and therefore the battery of the unmanned aerial vehicle needs to be replaced regularly.
There is certain drawback in current unmanned aerial vehicle group battery when using, and current unmanned aerial vehicle group battery structure is comparatively simple, then dismantles whole unmanned aerial vehicle after the change, and dismantlement and installation process are comparatively complicated to comparatively inconvenient, at the in-process that uses, brought certain influence. Therefore, the technical personnel in the field provide an unmanned aerial vehicle group battery of easy dismouting to solve the problem that proposes in the above-mentioned background art.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle battery pack easy to disassemble and assemble so as to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme:
an unmanned aerial vehicle battery pack easy to disassemble and assemble comprises an unmanned aerial vehicle main body, wherein a mounting seat is fixedly arranged on one side of the bottom end of the unmanned aerial vehicle main body, a battery main body is embedded and installed at one side of the bottom end of the installation seat, a camera is fixedly installed at one side of the bottom end of the unmanned aerial vehicle main body, which is close to the battery main body, the connecting arms are fixedly arranged on the periphery of the outer wall of the unmanned aerial vehicle main body, propellers are fixedly arranged on one sides of the outer ends of the connecting arms, an access hole is arranged on one side of the interior of the battery main body, an access cover is arranged on one side of the interior of the access hole, one side of the top end of the battery main body, which corresponds to the mounting seat, is fixed on a connecting seat, one side of the top end of the connecting seat is fixedly provided with a connecting plug, the battery is characterized in that a charging port is embedded in one side of the interior of the battery main body, and connecting clamping blocks are fixedly mounted at four corners of the bottom end of the battery main body.
As a further scheme of the invention: one side of the top end of the battery main body, which is close to the connecting clamping block, is fixedly provided with a sponge cushion, and one side of the interior of the battery main body is embedded with a power switch.
As a still further scheme of the invention: the utility model discloses a power switch's output one side fixed mounting has a set of connection antenna, the equal fixed mounting in outer end one side of connecting the antenna has the electric wire, a set of conductive sleeve is installed to inside one side gomphosis of connecting plug, it passes through electric wire and conductive sleeve electric connection to connect the antenna.
As a still further scheme of the invention: the battery pack is characterized in that a plurality of groups of storage batteries are arranged on one side of the inside of the battery body, a fixing clamp is fixedly mounted on one side, close to the storage batteries, of the inner wall of the battery body, the battery body is fixedly connected with the storage batteries through the fixing clamp, and heat dissipation holes are formed in one side of the inner bottom of the battery body in a penetrating mode.
As a still further scheme of the invention: the utility model discloses an unmanned aerial vehicle, including unmanned aerial vehicle main part, the inside one side of unmanned aerial vehicle main part is provided with circuit control board, circuit control board's input one side is provided with the conducting block, and the conducting block gomphosis is installed in the interior bottom of unmanned aerial vehicle main part and is corresponded one side of conductive sleeve.
As a still further scheme of the invention: connecting clamping grooves are formed in one side, corresponding to the connecting clamping block, of the inside of the mounting seat, the connecting seat is connected with the connecting clamping grooves in a clamping mode through the connecting clamping block, a mounting groove is formed in one side, corresponding to the connecting seat, of the inside of the mounting seat, and the mounting seat is connected with the connecting seat in a clamping mode through the mounting groove.
As a still further scheme of the invention: the inside both sides of connecting seat all run through and have seted up the standing groove, the kelly has been seted up to inner wall one side of standing groove, and the equal gomphosis in inside one side of kelly installs the slip ball.
As a still further scheme of the invention: one side that the inside of standing groove is close to the kelly all is provided with first spring, and the connecting seat passes through first spring and kelly fixed connection, the draw-in groove has all been seted up to one side that the inside of mount pad corresponds the kelly, and the connecting seat passes through the kelly to be connected with the draw-in groove block.
As a still further scheme of the invention: the inside of mount pad corresponds one side of kelly and all is provided with the ejector pin, and the ejector pin setting is in inner wall one side of draw-in groove, the equal fixed mounting in surface both sides of ejector pin has the stopper.
As a still further scheme of the invention: one side that the inside of mount pad corresponds the stopper all is provided with the second spring, equal fixed mounting in outer end one side of ejector pin has the button.
Compared with the prior art, the invention has the beneficial effects that:
1. through the arranged mounting seat, when a user needs to mount the battery main body, the connecting seat can be inserted into the mounting groove, the conductive sleeve arranged on the connecting plug is sleeved into the conductive block, and the conductive sleeve is clamped into the connecting clamping groove through the connecting clamping block, so that the connection stability of the mounting seat and the connecting seat can be improved, the clamping rod is pushed into the clamping groove through the first spring arranged in the placing groove, the mounting seat and the connecting seat can be clamped and connected through the matching between the clamping rod and the clamping groove, the convenient mounting of the battery main body is realized, otherwise, when the user needs to dismount the battery main body, the button can be pressed, the clamping rod is pushed out from the clamping groove through the ejector rod, so that the battery main body can be quickly dismounted for use, the limiting block is pushed through the second spring, so that the ejector rod can be reset, the practicability of the device during use is effectively improved, and the use of the user is facilitated, better than the traditional way.
2. Through the access cover that sets up, in order to be convenient for the better maintenance battery of user of service, then can be through opening the access cover that the access hole set up, with the back of pulling down the access cover, user of service need pull down the battery from the fixation clamp, realize convenient maintenance and use, the accuracy when effectual improvement the device uses, convenient to use person uses, and is better for traditional mode.
Drawings
Fig. 1 is a schematic structural diagram of an easy-to-disassemble battery pack of an unmanned aerial vehicle;
fig. 2 is a schematic structural diagram of a battery main body in an unmanned aerial vehicle battery pack easy to disassemble and assemble;
fig. 3 is a schematic cross-sectional view of a battery body in an easily detachable battery pack of an unmanned aerial vehicle;
fig. 4 is a schematic structural diagram of a mounting seat and a connecting seat in an easily detachable battery pack of an unmanned aerial vehicle;
fig. 5 is a partial enlarged view of a portion a in fig. 4.
In the figure: 1. an unmanned aerial vehicle main body; 2. a mounting seat; 3. a battery main body; 4. a camera; 5. a connecting arm; 6. a propeller; 7. an access hole; 8. an access cover; 9. a connecting seat; 10. a connecting plug; 11. a charging port; 12. connecting a clamping block; 13. a sponge cushion; 14. a power switch; 15. connecting an antenna; 16. an electric wire; 17. a conductive sleeve; 18. a storage battery; 19. a fixing clip; 20. heat dissipation holes; 21. a circuit control board; 22. a conductive block; 23. a connecting clamping groove; 24. mounting grooves; 25. a placement groove; 26. a clamping rod; 27. a first spring; 28. a card slot; 29. a top rod; 30. a limiting block; 31. a second spring; 32. a button.
Detailed Description
Referring to fig. 1 to 5, in the embodiment of the invention, an unmanned aerial vehicle battery pack easy to disassemble and assemble comprises an unmanned aerial vehicle main body 1, a mounting seat 2 is fixedly mounted on one side of the bottom end of the unmanned aerial vehicle main body 1, a battery main body 3 is installed on one side of the bottom end of the mounting seat 2 in an embedded mode, a camera 4 is fixedly mounted on one side, close to the battery main body 3, of the bottom end of the unmanned aerial vehicle main body 1, connecting arms 5 are fixedly mounted on the periphery of the outer wall of the unmanned aerial vehicle main body 1, propellers 6 are fixedly mounted on one side of the outer end of each connecting arm 5, an access hole 7 is formed in one side of the inside of the battery main body 3, an access cover 8 is arranged on one side of the inside of the access hole 7, a connecting seat 9 is fixed on one side, corresponding to the mounting seat 2, a connecting plug 10 is fixedly mounted.
In FIGS. 1-2: one side fixed mounting that battery body 3's top one side is close to connecting fixture block 12 has foam-rubber cushion 13, and switch 14 is installed in the inside one side gomphosis of battery body 3 to make the overall device can improve the effect of being connected between mount pad 2 and the connecting seat 9 through foam-rubber cushion 13.
In fig. 2-3: a set of connecting antenna 15 is fixedly installed on one side of the output end of the power switch 14, an electric wire 16 is fixedly installed on one side of the outer end of the connecting antenna 15, a set of conductive sleeve 17 is installed on one side of the inside of the connecting plug 10 in an embedded mode, the connecting antenna 15 is electrically connected with the conductive sleeve 17 through the electric wire 16, and therefore the whole device can be connected and electrified with the storage battery 18 and the conductive sleeve 17 through the electric wire 16.
In fig. 1 and 3: the inside one side of battery body 3 is provided with multiunit battery 18, and one side fixed mounting that the inner wall of battery body 3 is close to battery 18 has fixation clamp 19, and battery body 3 passes through fixation clamp 19 and battery 18 fixed connection, and louvre 20 has been seted up in running through to interior bottom one side of battery body 3 to make the overall device can keep battery body 3 to dispel the heat through louvre 20.
In fig. 1, 3 and 4: inside one side of unmanned aerial vehicle main part 1 is provided with circuit control panel 21, and input one side of circuit control panel 21 is provided with conducting block 22, and the conducting block 22 gomphosis is installed in the one side of the interior bottom correspondence conducting sleeve 17 of unmanned aerial vehicle main part 1 to make the integrated device can realize that battery 18 carries out the circular telegram and uses through conducting block 22 and the cooperation of conducting sleeve 17.
In fig. 1, 2 and 4: connecting slot 23 has all been seted up to the inside one side that corresponds connecting fixture block 12 of mount pad 2, and connecting seat 9 is connected with connecting slot 23 block through connecting fixture block 12, and mounting groove 24 has been seted up to the inside one side that corresponds connecting seat 9 of mount pad 2, and mount pad 2 has connecting seat 9 block to connect through mounting groove 24 to make the integrated device can drive mount pad 2 more stable and be connected with connecting seat 9 through connecting fixture block 12 and connecting slot 23's cooperation.
In fig. 2 and 5: the inside both sides of connecting seat 9 have all been run through and have been seted up standing groove 25, and jamming rod 26 has been seted up to inner wall one side of standing groove 25, and the equal gomphosis in inside one side of jamming rod 26 installs the slip ball to make the integrated device can store jamming rod 26 through standing groove 25 and use.
In fig. 1, 2 and 5: one side that the inside of standing groove 25 is close to kelly 26 all is provided with first spring 27, and connecting seat 9 is through first spring 27 and kelly 26 fixed connection, draw-in groove 28 has all been seted up to one side that the inside of mount pad 2 corresponds kelly 26, and connecting seat 9 is connected through kelly 26 and draw-in groove 28 block, thereby make the overall device can push kelly 26 into draw-in groove 28 through first spring 27, through the cooperation between kelly 26 and the draw-in groove 28, then can carry out the block with mount pad 2 and connecting seat 9 and be connected.
In fig. 1 and 5: the inside of mount pad 2 corresponds one side of kelly 26 and all is provided with ejector pin 29, and ejector pin 29 sets up in the inner wall one side of draw-in groove 28, and the equal fixed mounting in surface both sides of ejector pin 29 has stopper 30 to make integrated device ejecting from draw-in groove 28 with kelly 26 through ejector pin 29, thereby can be swift pull down battery body 3 and use.
In fig. 1 and 5: one side that the stopper 30 is corresponded to in the inside of mount pad 2 all is provided with second spring 31, and the equal fixed mounting in outer end one side of ejector pin 29 has button 32 to make the integrated device can withstand stopper 30 through second spring 31, thereby can reset by ejector pin 29, the practicality when effectual improvement the device uses.
The working principle of the invention is as follows: when a user needs to install the battery body 3, the connecting seat 9 can be inserted into the mounting groove 24, the conductive sleeve 17 arranged on the connecting plug 10 is sleeved into the conductive block 22, and is clamped into the connecting clamping groove 23 through the connecting clamping block 12, so that the connection stability of the mounting seat 2 and the connecting seat 9 can be improved, the clamping rod 26 is pushed into the clamping groove 28 through the first spring 27 arranged in the placing groove 25, the mounting seat 2 and the connecting seat 9 can be clamped and connected through the matching between the clamping rod 26 and the clamping groove 28, so that the battery body 3 can be conveniently installed and used, otherwise, when the user needs to detach the battery body 3, the button 32 can be pressed, the clamping rod 26 is pushed out of the clamping groove 28 through the ejector rod 29, so that the battery body 3 can be rapidly detached and used, the limiting block 30 is pushed through the second spring 31, so that the ejector rod 29 can reset, and the practicability of the device when in use is effectively improved, in order to be convenient for the better maintenance battery 18 of user of service, then can be through opening the access cover 8 that access hole 7 set up, with the back of pulling down access cover 8, the user of service need pull down battery 18 from fixation clamp 19, realizes convenient maintenance and uses, and the precision when effectual improvement the device uses, convenient to use person uses comparatively practically.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.

Claims (10)

1. An unmanned aerial vehicle battery pack easy to disassemble and assemble comprises an unmanned aerial vehicle main body (1) and is characterized in that a mounting seat (2) is fixedly mounted on one side of the bottom end of the unmanned aerial vehicle main body (1), a battery main body (3) is installed on one side of the bottom end of the mounting seat (2) in an embedded mode, a camera (4) is fixedly mounted on one side, close to the battery main body (3), of the bottom end of the unmanned aerial vehicle main body (1), connecting arms (5) are fixedly mounted on the periphery of the outer wall of the unmanned aerial vehicle main body (1), propellers (6) are fixedly mounted on one side of the outer end of each connecting arm (5), an access hole (7) is formed in one side of the interior of the battery main body (3), an access cover (8) is arranged on one side of the interior of the access hole (7), one side, corresponding to, the battery charging device is characterized in that a connecting plug (10) is fixedly mounted on one side of the top end of the connecting seat (9), a charging port (11) is installed on one side of the interior of the battery body (3) in an embedded mode, and connecting clamping blocks (12) are fixedly mounted at four corners of the bottom end of the battery body (3).
2. The unmanned aerial vehicle group battery of easy dismouting of claim 1, characterized in that, the top one side of battery main part (3) is close to the one side fixed mounting who connects fixture block (12) and is had a foam-rubber cushion (13), switch (14) are installed to inside one side gomphosis of battery main part (3).
3. The unmanned aerial vehicle group battery of easy dismouting of claim 2, characterized in that, switch (14) output one side fixed mounting has a set of connection antenna (15), the outer end one side of connecting antenna (15) all fixed mounting has electric wire (16), a set of conductive cover (17) is installed in inside one side gomphosis of connecting plug (10), connect antenna (15) through electric wire (16) and conductive cover (17) electric connection.
4. The unmanned aerial vehicle group battery of claim 1, characterized in that, inside one side of cell main body (3) is provided with multiunit battery (18), the inner wall of cell main body (3) is close to one side fixed mounting of battery (18) has fixation clamp (19), and cell main body (3) passes through fixation clamp (19) and battery (18) fixed connection, louvre (20) have run through to interior bottom one side of cell main body (3).
5. The unmanned aerial vehicle group battery of easy dismouting of claim 3, characterized in that, the inside one side of unmanned aerial vehicle main part (1) is provided with circuit control board (21), input one side of circuit control board (21) is provided with conducting block (22), and conducting block (22) gomphosis is installed in the interior bottom of unmanned aerial vehicle main part (1) and is corresponded one side of conducting sleeve (17).
6. The unmanned aerial vehicle battery pack easy to disassemble and assemble according to claim 1, wherein one side of the mounting seat (2) corresponding to the connecting clamping block (12) is provided with a connecting clamping groove (23), the connecting seat (9) is connected with the connecting clamping groove (23) in a clamping manner through the connecting clamping block (12), one side of the mounting seat (2) corresponding to the connecting seat (9) is provided with a mounting groove (24), and the mounting seat (2) is connected with the connecting seat (9) in a clamping manner through the mounting groove (24).
7. The unmanned aerial vehicle battery pack easy to disassemble and assemble according to claim 1, wherein a placing groove (25) is formed in each of two inner sides of the connecting seat (9), a clamping rod (26) is formed on one side of the inner wall of each placing groove (25), and sliding balls are installed on each of the inner sides of the clamping rods (26) in a matched mode.
8. The unmanned aerial vehicle battery pack easy to disassemble and assemble according to claim 6, wherein a first spring (27) is arranged on one side of the inside of the placing groove (25) close to the clamping rod (26), the connecting seat (9) is fixedly connected with the clamping rod (26) through the first spring (27), a clamping groove (28) is formed in the inside of the mounting seat (2) corresponding to one side of the clamping rod (26), and the connecting seat (9) is connected with the clamping groove (28) in a clamping mode through the clamping rod (26).
9. The unmanned aerial vehicle group battery of easy dismouting of claim 8, characterized in that, the inside of mount pad (2) corresponds one side of kelly (26) and all is provided with ejector pin (29), and ejector pin (29) sets up in the inner wall one side of draw-in groove (28), the equal fixed mounting in surface both sides of ejector pin (29) has stopper (30).
10. The unmanned aerial vehicle group battery of easy dismouting of claim 9, characterized in that, the inside one side that corresponds stopper (30) of mount pad (2) all is provided with second spring (31), all fixed mounting has button (32) in outer end one side of ejector pin (29).
CN202011552411.3A 2020-12-24 2020-12-24 Unmanned aerial vehicle group battery of easy dismouting Withdrawn CN112736358A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202011552411.3A CN112736358A (en) 2020-12-24 2020-12-24 Unmanned aerial vehicle group battery of easy dismouting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202011552411.3A CN112736358A (en) 2020-12-24 2020-12-24 Unmanned aerial vehicle group battery of easy dismouting

Publications (1)

Publication Number Publication Date
CN112736358A true CN112736358A (en) 2021-04-30

Family

ID=75615437

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202011552411.3A Withdrawn CN112736358A (en) 2020-12-24 2020-12-24 Unmanned aerial vehicle group battery of easy dismouting

Country Status (1)

Country Link
CN (1) CN112736358A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102460831B1 (en) * 2022-04-27 2022-10-31 주식회사 유맥에어 Drone Battery Mounting Device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102460831B1 (en) * 2022-04-27 2022-10-31 주식회사 유맥에어 Drone Battery Mounting Device

Similar Documents

Publication Publication Date Title
CN112736358A (en) Unmanned aerial vehicle group battery of easy dismouting
CN208690981U (en) A kind of charging cabinet that can give multiple quickly charging batteries simultaneously
CN214280119U (en) Unmanned aerial vehicle group battery fixing device
CN216818502U (en) New energy automobile power storage equipment
CN212112385U (en) Computer air guide cover
CN213151694U (en) Formula portable power source module is inhaled to magnetism
CN115604962A (en) Rapid disassembly and assembly structure of unmanned aerial vehicle interference unit and implementation method thereof
CN216146133U (en) Direct power supply unit of unmanned aerial vehicle remote controller
CN208707364U (en) A kind of onboard wireless charger
CN111555385A (en) Portable power source of removable battery package
CN206505955U (en) A kind of unmanned plane battery case
CN209216279U (en) A kind of communication module group with positioning function
CN114221419B (en) Multifunctional charger and application method thereof
CN217215603U (en) Portable 400Hz inverter power supply
CN214124867U (en) Wireless charger that long duration of a journey of high heat dissipation was used
CN219980503U (en) Quick-dismantling type power supply assembly for solar umbrella
CN216509146U (en) Camera link for unmanned vehicles
CN217789375U (en) Safe and stable UPS power supply device
CN114784417B (en) Heat dissipation shell for unmanned aerial vehicle battery
CN214070494U (en) LED power supply with multidirectional heat dissipation shell
CN108317372A (en) A kind of LED drive power controller
CN216666015U (en) Fan flabellum structure convenient to dismouting
CN216532050U (en) Eight-way network power supply controller
CN219535680U (en) Portable pull rod power supply
CN215584000U (en) Outdoor window cleaning machine

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
WW01 Invention patent application withdrawn after publication
WW01 Invention patent application withdrawn after publication

Application publication date: 20210430