CN212556814U - Unmanned aerial vehicle battery quick replacement device - Google Patents
Unmanned aerial vehicle battery quick replacement device Download PDFInfo
- Publication number
- CN212556814U CN212556814U CN202021513465.4U CN202021513465U CN212556814U CN 212556814 U CN212556814 U CN 212556814U CN 202021513465 U CN202021513465 U CN 202021513465U CN 212556814 U CN212556814 U CN 212556814U
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- Prior art keywords
- installation shell
- aerial vehicle
- unmanned aerial
- vehicle battery
- replacement device
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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.)
- Expired - Fee Related
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- 238000009434 installation Methods 0.000 claims abstract description 43
- 230000007306 turnover Effects 0.000 claims description 13
- 239000002184 metal Substances 0.000 claims description 10
- 238000013461 design Methods 0.000 claims description 6
- 238000005192 partition Methods 0.000 claims description 2
- 238000010030 laminating Methods 0.000 claims 1
- 230000000149 penetrating effect Effects 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 12
- 230000002349 favourable effect Effects 0.000 abstract description 12
- 230000005540 biological transmission Effects 0.000 abstract description 7
- 230000008859 change Effects 0.000 abstract description 6
- 238000006073 displacement reaction Methods 0.000 abstract description 6
- 238000004804 winding Methods 0.000 abstract description 6
- 238000000034 method Methods 0.000 description 7
- 230000008878 coupling Effects 0.000 description 4
- 238000010168 coupling process Methods 0.000 description 4
- 238000005859 coupling reaction Methods 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000006872 improvement Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle battery quick replacement device, including the installation shell, the equal fixed mounting in top left and right sides of installation shell has the connection roof, the constant head tank has been seted up to the inside of connecting the roof, inside fixed mounting has the winding displacement to leak the net around the installation shell, the inside block hole of having seted up in middle section around the installation shell, the inside movable mounting in block hole has movable cock stem. This unmanned aerial vehicle battery quick replacement device, it can with unmanned aerial vehicle inter-mounting to connect the roof, conveniently provide the power, the screw rod can be installed to the inside of constant head tank simultaneously, be favorable to improving the installation stability of this device, the inside that the winding displacement leaks the net can be used for alternating the electric wire, be favorable to guaranteeing the mutual transmission of inside electric energy, guarantee this change device's practicality, block hole can peg graft each other with the activity cock stem when not using, keep the stability of upset bottom plate, guarantee the stability of placing of internal battery.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle battery quick replacement device.
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 machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like.
However, current unmanned aerial vehicle is comparatively troublesome when changing the battery, the speed that the improvement battery that can not be fine was changed, and general unmanned aerial vehicle battery is integrative with unmanned aerial vehicle simultaneously, is difficult for dismantling the convenience.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle battery quick replacement device to solve current unmanned aerial vehicle comparatively troublesome when changing the battery among the above-mentioned background, the speed of improvement battery change that can not be fine, general unmanned aerial vehicle battery is integrative with unmanned aerial vehicle simultaneously, is difficult for dismantling the problem of convenience.
In order to achieve the above object, the utility model provides a following technical scheme: a quick change device for an unmanned aerial vehicle storage battery comprises an installation shell, wherein the left side and the right side of the top end of the installation shell are both fixedly provided with a connecting top plate, a positioning groove is arranged inside the connecting top plate, a wire arranging screen is fixedly arranged inside the front and the back of the mounting shell, clamping holes are arranged in the front and rear middle sections of the mounting shell, a movable plug rod is movably arranged in the clamping holes, a connecting spring is fixedly arranged on the inner wall of the right side of the mounting shell, a turnover bottom plate is movably arranged at the bottom end of the mounting shell, side edge connecting plates are fixedly arranged at the front side and the rear side of the turnover bottom plate, a middle section clapboard is fixedly arranged at the middle section of the turnover bottom plate, the left side terminal surface fixed mounting of side connecting plate has the front end baffle, the top right side movable mounting of front end baffle has the bullet piece, the left side inner wall department fixed mounting of installation shell has circular telegram metal sheet.
Preferably, the installation shell is in an opening shape, the installation shell is integrally connected with the connecting top plate, and the connecting top plate and the positioning groove are mutually penetrated.
Preferably, the interior of the flat cable screen is designed to be hollow, the number of the flat cable screens is two, and the mounting shell is integrally connected with the flat cable screen.
Preferably, the clamping holes are connected with the movable plug rod in a clamping mode, the number of the clamping holes is two, and the clamping holes and the middle sections of the side connecting plates are in one-to-one correspondence.
Preferably, the connecting springs correspond to the electrified metal plates in number and position one by one, and the turnover bottom plate is connected with the installation shell through a rotating shaft.
Preferably, the length of the turnover bottom plate is the same as the length of the bottom end of the installation shell, the front end baffle is attached to the left end face of the installation shell, and the elastic block is connected with the inside of the left side of the installation shell in a clamping manner.
Compared with the prior art, the beneficial effects of the utility model are that: this unmanned aerial vehicle battery quick replacement device, it can with unmanned aerial vehicle inter-mounting to connect the roof, conveniently provide the power, the screw rod can be installed to the inside of constant head tank simultaneously, be favorable to improving the installation stability of this device, the inside that the winding displacement leaks the net can be used for alternating the electric wire, be favorable to guaranteeing the mutual transmission of inside electric energy, guarantee this change device's practicality, block hole can peg graft each other with the activity cock stem when not using, keep the stability of upset bottom plate, guarantee the stability of placing of internal battery, coupling spring and circular telegram metal sheet and battery interconnect, be favorable to keeping the normal transmission effect of battery electric energy, the upset bottom plate can overturn, help the battery on its top to overturn, be favorable to increasing the swift effect that the battery was dismantled, the stable effect of installation that the upset bottom plate has also been improved.
Drawings
FIG. 1 is an overall structure diagram of the present invention;
FIG. 2 is a top view of the structure of the present invention;
FIG. 3 is a side view of the present invention;
fig. 4 is a front structural view of the present invention.
In the figure: 1. installing a shell; 2. connecting the top plate; 3. positioning a groove; 4. wire arrangement and net leakage; 5. a clamping hole; 6. a movable stopper rod; 7. a connecting spring; 8. turning over the bottom plate; 9. side edge connecting plates; 10. a middle partition plate; 11. a front end baffle; 12. a spring block; 13. and electrifying the metal plate.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle battery quick replacement device, including installation shell 1, the equal fixed mounting in the top left and right sides of installation shell 1 has connection roof 2, constant head tank 3 has been seted up to the inside of connecting roof 2, inside fixed mounting has the winding displacement to leak net 4 around installation shell 1, inside block hole 5 has been seted up in the middle section around installation shell 1, the inside movable mounting of block hole 5 has movable cock stem 6, the right side inner wall department fixed mounting of installation shell 1 has coupling spring 7, the bottom movable mounting of installation shell 1 has upset bottom plate 8, both sides fixed mounting has side connecting plate 9 around upset bottom plate 8, the middle section fixed mounting of upset bottom plate 8 has middle section baffle 10, the left side terminal surface fixed mounting of side connecting plate 9 has front end baffle 11, the top right side movable mounting of front end baffle 11 has bullet piece 12, the left side inner wall department fixed mounting of installation shell 1 has.
The utility model discloses in: the installation shell 1 is in an open design, the installation shell 1 is integrally connected with the connecting top plate 2, and the connecting top plate 2 and the positioning groove 3 are in a mutually-penetrating design; connect roof 2 can with unmanned aerial vehicle inter-erection, conveniently provide the power, the screw rod can be installed to the inside of constant head tank 3 simultaneously, is favorable to improving the installation stability of this device.
The utility model discloses in: the interior of the flat cable leakage net 4 is designed in a hollow shape, the number of the flat cable leakage nets 4 is two, and the installation shell 1 is integrally connected with the flat cable leakage net 4; the wire arranging leakage net 4 can be used for inserting wires, so that mutual transmission of internal electric energy is guaranteed, and the practicability of the replacing device is guaranteed.
The utility model discloses in: the clamping holes 5 are connected with the movable plug rod 6 in a clamping manner, the number of the clamping holes 5 is two, and the clamping holes 5 and the middle sections of the side connecting plates 9 are in one-to-one correspondence design; when the battery turnover device is not used, the clamping hole 5 can be mutually inserted with the movable plug rod 6, so that the stability of the turnover bottom plate 8 is kept, and the placing stability of the internal battery is ensured.
The utility model discloses in: the connecting springs 7 correspond to the electrified metal plates 13 in number and position one by one, and the turnover bottom plate 8 is connected with the mounting shell 1 as a rotating shaft; the connecting spring 7 and the electrifying metal plate 13 are connected with the battery, so that the normal transmission effect of the electric energy of the battery can be kept.
The utility model discloses in: the length of the turnover bottom plate 8 is the same as that of the bottom end of the installation shell 1, the front baffle 11 is in fit connection with the left end face of the installation shell 1, and the elastic block 12 is in clamping connection with the inside of the left side of the installation shell 1; the upset bottom plate 8 can overturn, and the battery on help its top overturns, is favorable to increasing the swift effect that the battery was dismantled, and the design of bullet piece 12 has also improved the installation stable effect of upset bottom plate 8 simultaneously.
The working principle is as follows: when using this change device, at first need utilize the screw rod to aim at the inside of constant head tank 3, the coupling part interconnect who will connect roof 2 and unmanned aerial vehicle, at the internal connection electric wire of this device afterwards, can pass winding displacement hourglass net 4 and installation shell 1 interconnect with the electric wire, bullet piece 12 is installed to the block, the battery that will need to use is placed on the top of upset bottom plate 8, its some that connects the power needs and circular telegram metal sheet 13 interconnect, it can to utilize movable cock stem 6 to carry out the block with upset bottom plate 8 at last and connect, then take out movable cock stem 6 when needing to dismantle, upset bottom plate 8 takes out the battery.
In summary, the following steps: the quick storage battery replacing device of the unmanned aerial vehicle has the advantages that the connecting top plate 2 can be mutually installed with the unmanned aerial vehicle, the power supply is convenient to provide, simultaneously the screw rod can be installed to the inside of constant head tank 3, be favorable to improving the installation stability of this device, the inside that the winding displacement leaks net 4 can be used for interlude electric wire, be favorable to guaranteeing the mutual transmission of inside electric energy, guarantee this change device's practicality, block hole 5 can peg graft each other with activity cock stem 6 when not using, the stability of bottom plate 8 keeps overturning, guarantee the stability of placing of inside battery, coupling spring 7 and circular telegram metal sheet 13 and battery interconnect, be favorable to keeping the normal transmission effect of battery electric energy, upset bottom plate 8 can overturn, help the battery on its top to overturn, be favorable to increasing the swift effect that the battery was dismantled, simultaneously the design of bullet piece 12 has also improved the installation stable effect of upset bottom plate 8.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an unmanned aerial vehicle battery quick replacement device, includes installation shell (1), its characterized in that: the cable fixing device is characterized in that connecting top plates (2) are fixedly mounted on the left side and the right side of the top end of the mounting shell (1), positioning grooves (3) are formed in the connecting top plates (2), flat cable draining nets (4) are fixedly mounted on the front inner side and the rear inner side of the mounting shell (1), clamping holes (5) are formed in the front middle section and the rear middle section of the mounting shell (1), movable plug rods (6) are movably mounted in the clamping holes (5), connecting springs (7) are fixedly mounted on the right inner wall of the mounting shell (1), a turnover bottom plate (8) is movably mounted at the bottom end of the mounting shell (1), side connecting plates (9) are fixedly mounted on the front side and the rear side of the turnover bottom plate (8), a middle section partition plate (10) is fixedly mounted on the middle section of the turnover bottom plate (8), and a front end, the top right side movable mounting of front end baffle (11) has bullet piece (12), the left side inner wall department fixed mounting of installation shell (1) has circular telegram metal sheet (13).
2. The rapid unmanned aerial vehicle battery replacement device of claim 1, wherein: the installation shell (1) is in an opening shape, the installation shell (1) is connected with the connection top plate (2) in an integrated mode, and the connection top plate (2) and the positioning groove (3) are in a mutually penetrating design.
3. The rapid unmanned aerial vehicle battery replacement device of claim 1, wherein: the interior of the flat cable screen (4) is designed to be hollow, the number of the flat cable screen (4) is two, and the installation shell (1) is integrally connected with the flat cable screen (4).
4. The rapid unmanned aerial vehicle battery replacement device of claim 1, wherein: the clamping holes (5) are connected with the movable plug rods (6) in a clamping mode, the number of the clamping holes (5) is two, and the clamping holes (5) and the middle sections of the side connecting plates (9) are in one-to-one correspondence.
5. The rapid unmanned aerial vehicle battery replacement device of claim 1, wherein: the connecting springs (7) correspond to the electrified metal plates (13) in number and position one by one, and the turnover bottom plate (8) is connected with the installation shell (1) through a rotating shaft.
6. The rapid unmanned aerial vehicle battery replacement device of claim 1, wherein: the length of upset bottom plate (8) is the same with the bottom length of installation shell (1), front end baffle (11) are connected for the laminating with the left side terminal surface of installation shell (1), bullet piece (12) are connected for the block with the inside block that is in installation shell (1) left side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021513465.4U CN212556814U (en) | 2020-07-28 | 2020-07-28 | Unmanned aerial vehicle battery quick replacement device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021513465.4U CN212556814U (en) | 2020-07-28 | 2020-07-28 | Unmanned aerial vehicle battery quick replacement device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212556814U true CN212556814U (en) | 2021-02-19 |
Family
ID=74631910
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021513465.4U Expired - Fee Related CN212556814U (en) | 2020-07-28 | 2020-07-28 | Unmanned aerial vehicle battery quick replacement device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212556814U (en) |
-
2020
- 2020-07-28 CN CN202021513465.4U patent/CN212556814U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210219 |