CN111017233B - A quick removable battery - Google Patents
A quick removable batteryDownload PDFInfo
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- CN111017233B CN111017233BCN201911341707.8ACN201911341707ACN111017233BCN 111017233 BCN111017233 BCN 111017233BCN 201911341707 ACN201911341707 ACN 201911341707ACN 111017233 BCN111017233 BCN 111017233B
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- battery
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- aerial vehicle
- copper electrode
- copper
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M2220/00—Batteries for particular applications
- H01M2220/20—Batteries in motive systems, e.g. vehicle, ship, plane
- 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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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
Translated fromChinese
Description
Technical Field
The invention relates to a battery capable of being rapidly disassembled, and belongs to the technical field of machinery.
Background
A drone is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device. At present, unmanned aerial vehicles are widely applied in the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, movie and television shooting, and the like, and the unmanned aerial vehicle technology is also actively applied and developed in various countries.
At present, unmanned aerial vehicle battery has developed to the fairly mature stage, continues to improve unmanned aerial vehicle availability factor through the breakthrough in battery field, faces the problem with high costs, the slow progress. Meanwhile, to improve the endurance time of the unmanned aerial vehicle, the battery capacity needs to be increased, and the increase of the battery capacity inevitably leads to the increase of the weight of the battery, so that the power consumption of the unmanned aerial vehicle is increased, and the endurance time is shortened in turn. The battery of the unmanned aerial vehicle has short general endurance time, and the defect seriously hinders the development of industrialization.
The tradition adopts the manual unmanned aerial vehicle battery of carrying on to change, and unmanned aerial vehicle is connected complicacy with the battery, and the battery is changed inconveniently, waste time, inefficiency. Also there is unmanned aerial vehicle battery replacement device in the existing market, but it mostly needs to change battery shape and structure, and the range of application is little, and is with high costs. The shape of the battery is changed in the Rong detachable battery, the application range of the battery is limited, the battery cannot be widely used, and the market needs a device which can be widely applied to various batteries.
Therefore, a new battery replacement method which can improve the cruising ability of the unmanned aerial vehicle, has a wide application range, is low in implementation cost and has no adverse effect on the flight of the unmanned aerial vehicle is urgently needed to be found.
Disclosure of Invention
In order to solve the problems, the invention provides a battery which can be disassembled quickly. The battery provided by the invention has the advantages of simple operation, wide application range, short development period, moderate difficulty, low realization cost and the like.
The technical scheme of the invention is as follows:
the invention provides a battery capable of being rapidly disassembled, which comprises an unmanned aerial vehicle battery connecting device and an unmanned aerial vehicle battery box; the unmanned aerial vehicle battery connecting device is arranged at the bottom of the unmanned aerial vehicle; the unmanned aerial vehicle battery connecting device comprises an unmanned aerial vehicle battery connecting frame, a copper electrode telescopic bin, a first copper electrode, a first limiting block, a reset spring and a second limiting block; the battery connecting device is of a frame body structure and is formed by vertically extending two cuboids at the same side along the longitudinal section of the cuboid at two ends of one cuboid; the copper electrode telescopic bin is located at the first end of the unmanned aerial vehicle battery connecting frame, the first copper electrode is located in the middle of the copper electrode telescopic bin and is divided into a positive copper electrode and a negative copper electrode, the first copper electrode is connected with the bin wall of the copper electrode telescopic bin through a reset spring, the first copper electrode can realize reciprocating motion, the first limiting blocks are symmetrically distributed on the left side and the right side of the first copper electrode, and the second limiting blocks are located on the positive upper side of the first copper electrode; the inner side of the second end of the unmanned aerial vehicle battery connecting frame is not provided with a first copper pole, and a first limiting block and a second limiting block which have the same structure and are distributed with the inner side of the first end of the unmanned aerial vehicle battery connecting frame are arranged; the battery box of the unmanned aerial vehicle comprises a battery bin, a battery box limiting block, a second copper electrode and a clamping block; the clamping block is a rectangular block and is positioned below the second copper electrode, and the length of the clamping block is equal to the width of the battery bin; the battery bin is used for storing batteries; the battery box limiting block is a rectangular block, and the cross section of the battery box limiting block and the longitudinal section of the battery compartment form a certain angle; the second copper electrode is positioned at the first end of the battery bin and is connected with a battery in the battery bin through a lead; and the second end of the battery compartment is not provided with the second copper electrode, and the battery box limiting block and the clamping block which have the same structure and are distributed with the first end of the battery compartment are arranged.
In an embodiment of the present invention, the longitudinal section of the first stopper is a rectangle with a rounded corner.
In an embodiment of the present invention, the longitudinal section of the second stopper is a rectangle with two corners being rounded.
In an embodiment of the present invention, 2 battery box limiting blocks are disposed above the second copper electrode, and are symmetrically distributed along a vertical symmetry axis of the second copper electrode, and the two battery box limiting blocks are spaced apart from each other by a certain distance.
In one embodiment of the present invention, the battery compartment has a hollow rectangular parallelepiped structure.
In one embodiment of the invention, the bottom of the battery compartment is provided with a pattern which can be identified by a visual module.
In an embodiment of the invention, two side walls of the battery compartment are rectangular hollow structures, and the hollow structures can reduce the weight of the battery compartment.
In an embodiment of the invention, the battery box limiting block is a rectangular block, and a certain angle is formed between the cross section and the longitudinal section of the battery compartment, so that the battery box of the unmanned aerial vehicle can be screwed out and taken out more smoothly.
Has the advantages that:
(1) according to the quick-disassembly battery, the copper poles are arranged in the battery bin, one end of the copper pole is divided into the positive copper pole and the negative copper pole, the battery in the battery bin can be connected with the electrodes on the unmanned aerial vehicle connecting device through one end of the battery, the side wall of the battery bin is of a hollow structure, and the quick-disassembly battery is simple in structure, small in size, light and convenient to manufacture.
(2) According to the rapid battery dismounting device, the battery box can be accurately positioned on the connecting device by matching the limiting blocks at the two ends of the unmanned aerial vehicle battery connecting device with the limiting blocks on the battery box, the clamping blocks on the battery box can be matched with the corresponding rotating devices, rapid rotation dismounting of the unmanned aerial vehicle battery can be performed, the operation is simple, the consumed time is short, and the efficiency is high.
Drawings
Fig. 1 is a schematic diagram of connection between a battery box of an unmanned aerial vehicle and a battery connecting device of the unmanned aerial vehicle.
Fig. 2 is a schematic diagram of a battery box of the unmanned aerial vehicle.
Fig. 3 is a schematic diagram of a battery connection device of an unmanned aerial vehicle.
Fig. 4 is a cross-sectional view of unmanned aerial vehicle battery connecting device a-a.
Fig. 5 is a view of the drone battery connection device a 1.
Fig. 6 is a cross-sectional view of the connection between the battery box of the unmanned aerial vehicle and the battery connecting device of the unmanned aerial vehicle.
Fig. 7 is a schematic view of a detachable battery change-over swivel device.
Fig. 8 is a B-B cross-sectional view of the removable battery exchange rotary device.
Fig. 9 is a schematic view showing the detachable battery locked by the switching rotating device.
Fig. 10 is a schematic view showing the detachable battery being unfastened by the switching rotating means.
Fig. 11 is a schematic view of an omni-directional mobile platform truck.
Fig. 12 is a flow chart of the unmanned aerial vehicle battery change-over charging system.
In the figure:
unmanned aerial vehiclebattery connecting device 1, unmanned aerialvehicle battery case 2, battery transpositionrotary device 3, battery transposition rotary device frame 4,battery rotary drive 5, omnidirectionalmovement platform truck 6, omnidirectional movementplatform truck shell 7, unmanned aerialvehicle battery link 11, theflexible storehouse 12 of copper pole,first copper pole 13,first stopper 14,reset spring 15,second stopper 16,battery compartment 21,battery case stopper 22,second copper pole 23,joint piece 24, the transpositionrotary disk 31,jack catch 32, jackcatch reset spring 33.
Detailed Description
For better understanding of the present invention, the following examples are given for further illustration of the present invention, but the present invention is not limited to the following examples.
As shown in fig. 1, the present invention provides a detachable battery for a drone, comprising: unmanned aerial vehiclebattery connecting device 1, unmanned aerialvehicle battery case 2.
As shown in fig. 2, thebattery box 2 of the drone includes: the battery comprises abattery compartment 21, a batterybox limiting block 22, asecond copper electrode 23 and aclamping block 24; thebattery compartment 21 is of a hollow cuboid structure and can store unmanned aerial vehicle batteries, and two side walls of thebattery compartment 21 are of rectangular hollow structures which can reduce the weight of the battery compartment; thesecond copper electrode 23 is positioned at the first end of thebattery compartment 21 and is connected with the battery inside thebattery compartment 21 through a lead; the batterybox limiting blocks 22 are of a cuboid structure, 2 batterybox limiting blocks 22 are arranged above thesecond copper electrode 23 and are symmetrically distributed along a vertical symmetrical axis of thesecond copper electrode 23, a certain distance is reserved between the two battery box limiting blocks, and a certain angle is reserved between the cross section of each batterybox limiting block 22 and the longitudinal section of thebattery compartment 21, so that the battery box of the unmanned aerial vehicle can be screwed out and taken out more smoothly; theclamping block 24 is positioned below thesecond copper electrode 23, the length of the clamping block is equal to the width of the battery compartment, and the clamping block is of a cuboid structure; the second end of the battery compartment is not provided with asecond copper electrode 23, and a batterybox limiting block 22 and aclamping block 24 which have the same structure and are distributed with the first end of the battery compartment are arranged; the bottom of thebattery compartment 21 is provided with a pattern which can be identified by a vision module.
As shown in fig. 3, 4, 5, and 6, the unmanned aerial vehiclebattery connection apparatus 1 includes: the device comprises an unmanned aerial vehiclebattery connecting frame 11, a copper electrodetelescopic bin 12, afirst copper electrode 13, a first limitingblock 14, areturn spring 15 and a second limitingblock 16; thebattery connecting frame 11 is of a frame body structure and is formed by vertically extending two cuboids at the same side along the longitudinal section of the cuboid at two ends of one cuboid; the copper poletelescopic bin 12 is located at the first end of the unmanned aerial vehiclebattery connecting frame 11, is hollow in the middle, is of a cuboid structure, and is provided with afirst copper pole 13 storage hole, thefirst copper pole 13 is located in the middle of the copper poletelescopic bin 12 and is divided into a positive copper pole and a negative copper pole, one end of thefirst copper pole 13 is connected with the bin wall of the copper poletelescopic bin 12 through areset spring 15, thefirst copper pole 13 can realize reciprocating motion, and when the unmanned aerialvehicle battery box 2 is connected with the unmanned aerial vehiclebattery connecting device 1, thefirst copper pole 13 can be connected with thesecond copper pole 23 through compression of thereset spring 15; the first limitingblocks 14 are symmetrically distributed on the left side and the right side of thefirst copper electrode 13, the longitudinal section of each first limiting block is a rectangle with one corner being a rounded corner, the second limitingblocks 16 are positioned on the right upper side of thefirst copper electrode 13, and the longitudinal section of each second limiting block is a rectangle with two corners being rounded corners; thefirst copper electrode 13 is not disposed at the inner side of the second end of thebattery connecting frame 11, and a first limitingblock 14 and a second limitingblock 16 which have the same structure and distribution as the inner side of the first end of thebattery connecting frame 11 are disposed.
The detachable battery provided by the invention can be used for replacing the battery box of the unmanned aerial vehicle by using the battery replacing and rotatingdevice 3 shown in figures 7, 8, 9 and 10. The battery switching rotatingdevice 3 comprises a switching rotatingdisc 31, a storage position of thebattery box 2 of the unmanned aerial vehicle, aclaw 32 and aclaw return spring 33; the switching rotatingdisc 31 is of a cylindrical structure with a symmetrical center, and a hole for installing a rotating shaft is reserved in the central shaft; the storage positions for the unmanned aerialvehicle battery box 2 are circumferentially and uniformly distributed on the rotatingdisc 31, and the number of the storage positions is 5; the storage position of the unmanned aerialvehicle battery box 2 is of a cuboid structure and is used for storing the unmanned aerialvehicle battery box 2, theclaws 32 are symmetrically distributed at two ends of the storage position of the unmanned aerialvehicle battery box 2 and are of an L-shaped structure, theclaw reset springs 33 are positioned inside the switching rotatingdisc 31, theclaws 32 are connected with theclaw reset springs 33, theclaws 32 are folded and dispersed by stretching of theclaw reset springs 33, and when theclaws 32 are folded, the claws can be matched with theclamping blocks 24, so that the unmanned aerialvehicle battery box 2 can be clamped and fixed; when theclaws 32 are spread apart, thedrone battery box 2 can be moved in and out in the vertical direction as shown by the arrow in fig. 8.
The detachable battery provided by the invention can be applied to an unmanned aerial vehicle battery replacement system. As shown in fig. 11, the battery replacing system of the unmanned aerial vehicle comprises an unmanned aerial vehicle (not shown in the drawings), a detachable battery changing and charging device (not shown in the drawings), an unmanned aerial vehicle battery connecting device 1 (not shown in the drawings), an unmanned aerialvehicle battery box 2, a battery changing androtating device 3, a battery changing and rotating device frame 4, a battery rotating anddriving device 5, an omni-directionalmobile platform truck 6 and a mobileplatform truck shell 7; the unmanned aerial vehiclebattery connecting device 1 is installed at the bottom of an unmanned aerial vehicle, and the unmanned aerialvehicle battery box 2 is tightly connected to the battery changing-overrotating device 3 through theclamping jaws 32; the battery change-over rotating device frame 4 is of a thin plate structure and is provided with an opening; the batteryrotation driving device 5 internally comprises a driving motor, and is connected with a rotating shaft of the rotatingdisc 31 through a battery changing and rotating device frame 4, and the batteryrotation driving device 5 can rotate through the internal motor so as to control the battery changing and rotatingdevice 3 to rotate; the battery switching rotary device frame 4 and the mobileplatform car shell 7 are carried on the omnibearingmobile platform car 6, and the omnibearing mobileplatform car shell 7 is positioned on the upper side of the omnibearingmobile platform car 6; the bottom of the omnibearing movingplatform truck 6 is provided with four universal castors; a flight control system is arranged in the unmanned aerial vehicle and comprises a gyroscope, a satellite positioning module and a control circuit, the gyroscope can sense the flight posture of the unmanned aerial vehicle, and the satellite positioning module can control the hovering horizontal position and height of the unmanned aerial vehicle; the detachable battery switching charging device is internally provided with a device control system, the device control system comprises a visual identification module, a motion control system and a battery switching charging control system, the visual identification module can identify the position of the unmanned aerial vehicle, and the battery switching charging control system can control the detachable battery switching charging device to operate inside.
The following specifically explains the replacement process of the detachable battery with the unmanned aerial vehicle as an example and with reference to fig. 12:
(1) the unmanned aerial vehiclebattery connecting device 1 is installed at the bottom of the unmanned aerial vehicle, the unmanned aerial vehiclebattery connecting device 1 is connected with an unmanned aerialvehicle battery box 2, and thesecond copper electrode 23 supplies energy of a battery in thebattery bin 21 to the unmanned aerial vehicle through thefirst copper electrode 13 on the unmanned aerial vehiclebattery connecting device 1 through a wire;
(2) the unmanned aerial vehicle takes off, and the satellite positioning module can roughly record the position of the omnibearing movingplatform truck 6;
(3) when the unmanned aerial vehicle loses the signal of the remote controller or receives a return command of one key of the remote controller, a flight control system in the unmanned aerial vehicle controls the unmanned aerial vehicle to automatically return to the position above the omnibearing movingplatform car 6 and start to slowly descend;
(4) when the unmanned aerial vehicle navigates back to the position above the omnibearingmoving platform car 6, the camera on the detachable battery change-over charging device captures and shoots the special pattern at the bottom of thebattery bin 21 and transmits the special pattern to the visual identification module in the detachable battery change-over charging device;
(5) the device control system controls four universal casters under the omnibearing movingplatform truck 6 to move, the storage positions of the unmanned aerialvehicle battery boxes 2 which are idle on the circumference of the switchingrotary disc 31 are ensured to be under thebattery bin 21 and the directions of the storage positions are consistent, and theclaws 32 at two ends of the storage positions of the unmanned aerialvehicle battery boxes 2 which are idle under the storage positions are in a dispersed state;
(6) a visual identification module in the detachable battery switching charging device can judge whether thebattery box 2 of the unmanned aerial vehicle falls into a free storage position of thebattery box 2 of the unmanned aerial vehicle right below thebattery box 2 or not according to the picture, and if thebattery box 2 of the unmanned aerial vehicle falls into the storage position, the next operation is carried out;
(7) the device control system controls the jackcatch reset spring 33 to reset, so that thejack catch 32 is folded, the unmanned aerialvehicle battery box 2 is clamped, the flight control system enables the unmanned aerial vehicle to descend, the unmanned aerialvehicle battery box 2 moves upwards for a short distance relative to the unmanned aerial vehiclebattery connecting device 1, the device control system controls the change-over rotatingdisc 31 to rotate for a certain angle around the axial direction, the unmanned aerialvehicle battery box 2 is screwed out of the unmanned aerial vehiclebattery connecting device 1 and screwed into a new unmanned aerial vehicle battery box to the unmanned aerial vehiclebattery connecting device 1, and thecopper electrode 13 is compressed at the moment, so that the newdetachable battery device 2 is connected with thecopper electrode 23;
(8) flight control system control unmanned aerial vehicle is vertical takes off, take off in-process unmanned aerialvehicle battery case 2 and for 1 short distance of downshifting of unmanned aerial vehicle battery connecting device, 16 blocks of card of second stopper this moment are gone into the centre of twobattery case stoppers 22,battery case stopper 22 and firststopper 14 looks butt, can restrict the relative 1 vertical decurrent removal of unmanned aerial vehicle battery connecting device of battery case throughfirst stopper 14, can restrict the relative 1 direction of rotation of unmanned aerial vehicle battery connecting device of battery case and the ascending removal of horizontal side through battery case stopper 22 and the 16 cooperations of second stopper, thereby be fixed in unmanned aerial vehiclebattery connecting device 1 with unmanned aerialvehicle battery case 2 on, tear open and trade the process completion, unmanned aerial vehicle can work once more.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.
Claims (7)
1. A battery capable of being rapidly disassembled is characterized by comprising an unmanned aerial vehicle battery connecting device (1) and an unmanned aerial vehicle battery box (2); the unmanned aerial vehicle battery connecting device (1) is arranged at the bottom of the unmanned aerial vehicle;
the unmanned aerial vehicle battery connecting device (1) comprises an unmanned aerial vehicle battery connecting frame (11), a copper electrode telescopic bin (12), a first copper electrode (13), a first limiting block (14), a return spring (15) and a second limiting block (16); the battery connecting device (1) is of a frame body structure and is formed by vertically extending two cuboids at the same side along the longitudinal section of the cuboid at two ends of one cuboid; the copper electrode telescopic bin (12) is located at the first end of the unmanned aerial vehicle battery connecting frame, and the first copper electrode (13) is located in the middle of the copper electrode telescopic bin (12) and is divided into a positive copper electrode and a negative copper electrode; the first copper pole (13) is connected with the bin wall of the copper pole telescopic bin (12) through a return spring (15), and can realize reciprocating motion; the first limiting blocks (14) are symmetrically distributed on the left side and the right side of the first copper pole (13), and the second limiting blocks (16) are located on the right upper side of the first copper pole (13); the inner side of the second end of the unmanned aerial vehicle battery connecting frame (11) is not provided with a first copper electrode (13), and a first limiting block (14) and a second limiting block (16) which have the same structure and distribution with the inner side of the first end of the unmanned aerial vehicle battery connecting frame (11) are arranged;
the unmanned aerial vehicle battery box (2) comprises a battery bin (21), a battery box limiting block (22), a second copper pole (23) and a clamping block (24); the clamping block (24) is a rectangular block and is positioned below the second copper electrode (23), and the length of the clamping block is equal to the width of the battery bin (21); the battery can be stored in the battery compartment (21); the second copper electrode (23) is positioned at the first end of the battery bin (21) and is connected with a battery in the battery bin (21) through a lead; the second end of the battery compartment (21) is not provided with the second copper electrode (23), and the battery box limiting block (22) and the clamping block (24) which have the same structure and are distributed with the first end of the battery compartment (21) are arranged; two battery box limiting blocks (22) are arranged above the second copper pole (23), and the two battery box limiting blocks (22) are symmetrically distributed along the vertical symmetrical axis of the second copper pole (23) and are separated by a certain distance;
second stopper (16) can block into two the centre of battery case stopper (22), battery case stopper (22) with first stopper (14) looks butt, through first stopper (14) can restrict the battery case relative the vertical decurrent removal of unmanned aerial vehicle battery connecting device (1), through battery case stopper (22) with second stopper (16) cooperation can restrict the battery case relative unmanned aerial vehicle battery connecting device (1) direction of rotation and the ascending removal of horizontal side.
2. A quick detachable battery according to claim 1, wherein the first stopper (14) has a rectangular shape with a rounded corner in longitudinal section.
3. A quick detachable battery according to claim 1, wherein the second stopper (16) has a rectangular shape in longitudinal section with rounded corners at both corners.
4. A quick-release battery as claimed in claim 1, wherein the battery compartment (21) is of hollow rectangular parallelepiped structure.
5. A quick-release battery according to claim 1, characterized in that the bottom of the battery compartment (21) is provided with a pattern for visual module identification.
6. The battery as claimed in claim 1 or 5, wherein two side walls of the battery compartment (21) are rectangular hollow structures, which can reduce the weight of the battery compartment.
7. The battery capable of being disassembled quickly as claimed in claim 1, wherein the battery box limiting block (22) is a rectangular block, and the cross section of the rectangular block is at a certain angle with the longitudinal section of the battery compartment (21), so that the battery box (2) of the unmanned aerial vehicle can be screwed out and taken out more smoothly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911341707.8ACN111017233B (en) | 2019-12-24 | 2019-12-24 | A quick removable battery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911341707.8ACN111017233B (en) | 2019-12-24 | 2019-12-24 | A quick removable battery |
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| Publication Number | Publication Date |
|---|---|
| CN111017233A CN111017233A (en) | 2020-04-17 |
| CN111017233Btrue CN111017233B (en) | 2022-03-15 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911341707.8AActiveCN111017233B (en) | 2019-12-24 | 2019-12-24 | A quick removable battery |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104882575A (en)* | 2015-05-26 | 2015-09-02 | 苏州绿农航空植保科技有限公司 | Battery mounting box of multi-rotor unmanned aerial vehicle |
| WO2017119803A1 (en)* | 2016-01-09 | 2017-07-13 | 김성호 | Automatic battery replacement system for drone |
| CN206900672U (en)* | 2017-06-26 | 2018-01-19 | 山东萌萌哒航空科技有限公司 | Unmanned plane with Detachable battery structure |
| CN207038588U (en)* | 2017-07-28 | 2018-02-23 | 长春草莓科技有限公司 | A kind of lithium battery mounting structure |
| CN110444707A (en)* | 2018-11-08 | 2019-11-12 | 苏州乐轩科技有限公司 | Battery assembly, battery assembly and disassembly system and method |
- 2019
- 2019-12-24CNCN201911341707.8Apatent/CN111017233B/enactiveActive
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104882575A (en)* | 2015-05-26 | 2015-09-02 | 苏州绿农航空植保科技有限公司 | Battery mounting box of multi-rotor unmanned aerial vehicle |
| WO2017119803A1 (en)* | 2016-01-09 | 2017-07-13 | 김성호 | Automatic battery replacement system for drone |
| CN206900672U (en)* | 2017-06-26 | 2018-01-19 | 山东萌萌哒航空科技有限公司 | Unmanned plane with Detachable battery structure |
| CN207038588U (en)* | 2017-07-28 | 2018-02-23 | 长春草莓科技有限公司 | A kind of lithium battery mounting structure |
| CN110444707A (en)* | 2018-11-08 | 2019-11-12 | 苏州乐轩科技有限公司 | Battery assembly, battery assembly and disassembly system and method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN111017233A (en) | 2020-04-17 |
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