CN210296468U - High-rate special battery for unmanned aerial vehicle - Google Patents
High-rate special battery for unmanned aerial vehicle Download PDFInfo
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- CN210296468U CN210296468U CN201921625230.1U CN201921625230U CN210296468U CN 210296468 U CN210296468 U CN 210296468U CN 201921625230 U CN201921625230 U CN 201921625230U CN 210296468 U CN210296468 U CN 210296468U
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- battery
- wire
- aerial vehicle
- unmanned aerial
- fixed
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- 238000003825 pressing Methods 0.000 claims description 18
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 16
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 8
- 229910052759 nickel Inorganic materials 0.000 claims description 8
- WABPQHHGFIMREM-UHFFFAOYSA-N lead(0) Chemical compound [Pb] WABPQHHGFIMREM-UHFFFAOYSA-N 0.000 claims description 5
- 239000003292 glue Substances 0.000 claims description 2
- 238000005452 bending Methods 0.000 abstract description 5
- 238000001125 extrusion Methods 0.000 abstract description 4
- 238000011068 loading method Methods 0.000 abstract description 4
- 230000001771 impaired effect Effects 0.000 abstract description 2
- 238000009434 installation Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- 241001391944 Commicarpus scandens Species 0.000 description 2
- 238000004026 adhesive bonding Methods 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000002002 slurry Substances 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 239000002904 solvent Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 241000196324 Embryophyta Species 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000011889 copper foil Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 239000007772 electrode material Substances 0.000 description 1
- 239000003792 electrolyte Substances 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002985 plastic film Substances 0.000 description 1
- 229920006255 plastic film Polymers 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
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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
Landscapes
- Connection Of Batteries Or Terminals (AREA)
Abstract
The utility model discloses a high-rate special battery for unmanned aerial vehicle, including negative pole piece, battery case body, positive pole piece, connector lug and wire, negative pole piece and positive pole piece are fixed to be set up in the one end of battery case body, the connector lug is connected with negative pole piece and positive pole piece through the wire, the lower fixed surface of battery case body is provided with first fixed box, the one end of first fixed box is provided with the opening, and the inside of first fixed box is fixed and is provided with the slide bar, and the surface sliding sleeve of slide bar is equipped with first reset spring and slider, the slider is with first fixed box sliding fit, and the surface fixing of slider is provided with two cylinders, the wire slides around establishing at the surface of cylinder; through designing first fixed box, the wire can be according to the tensile shrink of grafting needs, avoids the wire extrusion impaired when loading and unloading battery, has effectively protected the wire to avoid bending and friction loss, prolongs its life.
Description
Technical Field
The utility model belongs to the technical field of the unmanned aerial vehicle battery, concretely relates to high magnification special battery for unmanned aerial vehicle.
Background
Along with the development of unmanned aerial vehicle technique, unmanned aerial vehicle all has extensive application in each field, and wherein plant protection unmanned aerial vehicle and unmanned aerial vehicle such as take photo by plane all are equipped with the battery of high magnification high capacity.
The conventional high-rate special battery for the unmanned aerial vehicle has the problems that in order to facilitate the installation and the disassembly of the battery, a long lead is reserved on a connector lug of the battery, the space of a battery box is limited, the lead needs to be extruded into a gap of the battery box, and the lead is easily damaged by frequent bending and extrusion, so that the high-rate special battery for the unmanned aerial vehicle is provided.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a special battery of high magnification for unmanned aerial vehicle to solve the special battery of high magnification for unmanned aerial vehicle of the current that proposes in the above-mentioned background art, there is the installation and the dismantlement of the battery for the ease, the connector lug of battery generally reserves longer wire, and places firmly for making the battery, and the battery case space is limited, need extrude the wire to the battery case gap in, frequent extrusion of buckling easily causes the problem that the wire damaged.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a special battery of high magnification for unmanned aerial vehicle, includes negative pole piece, battery case body, positive plate, connector lug and wire, the fixed one end that sets up at the battery case body of negative pole piece and positive plate, the connector lug is connected with negative pole piece and positive plate through the wire, the lower fixed surface of battery case body is provided with first fixed box, the one end of first fixed box is provided with the opening, and the fixed slide bar that is provided with in inside of first fixed box, and the surface slip cover of slide bar is equipped with first reset spring and slider, slider and first fixed box sliding fit, and the fixed surface of slider is provided with two cylinders, the wire slides around establishing at cylindrical surface.
Preferably, the opening end of the first fixing box is fixedly provided with two internal thread cylinders, a second fixing box is fixedly arranged between the two internal thread cylinders, two first press blocks are arranged in the second fixing box in a sliding mode, the adjacent surfaces of the two first press blocks are arranged to be inclined surfaces, a second press block is arranged in the middle of the second fixing box in a sliding mode, the second press block is tightly pressed with the two first press blocks, the upper end of the second press block is provided with a lead screw in a pressing mode, the lead screw extends out of the upper surface of the second fixing box in a screwing mode through threads, a clamping block is fixedly arranged on the surface, away from the first press block, of the lead screw extends out of the outer surface of the second fixing box in a sliding mode, the lead wire penetrates through a gap between the internal thread cylinders and the second fixing box in a sliding mode, and the clamping.
Preferably, the outer surface of the clamping block is slidably sleeved with a second return spring, and one end of the second return spring is fixedly provided with the outer surface of the first pressing block.
Preferably, the end part of the extending end of the clamping block is provided with an arc groove, and the inner surface of the arc groove is provided with a soft pad through glue adhesion.
Preferably, the upper end of the screw rod is provided with an inner hexagonal sliding cavity, the upper surface of the first fixing box is provided with a through hole, and the through hole corresponds to the inner hexagonal sliding cavity.
Preferably, a rubber pad is fixedly arranged on the outer surface of the battery outer shell, and the rubber pad and the first fixing box are on the same horizontal plane.
Preferably, the negative plate comprises an aluminum plate and a nickel plate, and the aluminum plate and the nickel plate are welded and fixed.
Compared with the prior art, the beneficial effects of the utility model are that:
(1) through designing first fixed box, the wire can be according to the tensile shrink of grafting needs, avoids the wire extrusion impaired when loading and unloading battery, has effectively protected the wire to avoid bending and friction loss, prolongs its life.
(2) Through the fixed box of design second, realize the spacing fixed to the wire, avoid vibrations to lead to the connector lug to take place to drop, improve equipment's fail safe nature sets up the circular arc groove, and the clamp splice pressfitting of being convenient for fixes the wire, sets up the rubber pad, and the battery installation of being convenient for is placed firmly, through welded fastening nickel piece, makes its electrode slice be difficult for the rupture.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a rear view of the battery case of the present invention;
fig. 3 is a top cross-sectional view of a first fixing box of the present invention;
fig. 4 is a top cross-sectional view of a second fixing box of the present invention;
fig. 5 is a front sectional view of a second fixing case of the present invention;
in the figure: 1. a negative plate; 2. a battery outer case; 3. a positive plate; 4. a connector lug; 5. a first stationary box; 6. a rubber pad; 7. an internal threaded barrel; 8. a wire; 9. a slide bar; 10. a first return spring; 11. a slider; 12. a cylinder; 13. a second stationary box; 14. a clamping block; 15. a first pressing block; 16. a second pressing block; 17. a screw rod; 18. a second return spring.
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.
Examples
Referring to fig. 1-5, the present invention provides a technical solution: a high-magnification special battery for an unmanned aerial vehicle comprises a negative plate 1, a battery shell body 2, a positive plate 3, a connector lug 4 and a lead 8, wherein the negative plate 1 and the positive plate 3 are fixedly arranged at one end of the battery shell body 2, the connector lug 4 is connected with the negative plate 1 and the positive plate 3 through the lead 8, a first fixing box 5 is fixedly arranged on the lower surface of the battery shell body 2 through glue bonding, one end of the first fixing box 5 is provided with an opening, a slide rod 9 is fixedly arranged inside the first fixing box 5, a first reset spring 10 and a slide block 11 are slidably sleeved on the outer surface of the slide rod 9, the slide block 11 is in sliding fit with the first fixing box 5, two cylinders 12 are fixedly arranged on the outer surface of the slide block 11, the lead 8 is slidably wound on the outer surface of the cylinders 12, the connector lug 4 is pulled out of the first fixing box 5 when the battery is installed, at the moment, the lead 8 pulls the slide block 11 to slide towards the opening, treat that connector lug 4 pegs graft on unmanned aerial vehicle's power source, slider 11 resets under the effect of first reset spring 10, and will follow redundant wire 8 that stretches out in the first fixed box 5 and draw back to in the first fixed box 5, avoid wire 8 to pile up in the outside of first fixed box 5, effectively protected wire 8 to avoid bending and friction loss, prolong its life.
In this embodiment, two internal thread cylinders 7 are fixedly arranged at the opening end of the first fixing box 5, a second fixing box 13 is fixedly arranged between the two internal thread cylinders 7, two first pressing blocks 15 are slidably arranged inside the second fixing box 13, the adjacent surfaces of the two first pressing blocks 15 are arranged as inclined surfaces, a second pressing block 16 is slidably arranged in the middle of the second fixing box 13, the second pressing block 16 is tightly pressed against the two first pressing blocks 15, a lead screw 17 is press-fitted at the upper end of the second pressing block 16, the lead screw 17 extends out of the upper surface of the second fixing box 13 through screw thread screwing, a clamping block 14 is fixedly arranged at the surface of the two first pressing blocks 15, the clamping block 14 slidably extends out of the outer surface of the second fixing box 13, the lead wire 8 slidably penetrates through the gap between the internal thread cylinders 7 and the second fixing box 13, the clamping block 14 tightly presses against the lead wire 8, after the connector 4 is fixedly inserted into the power interface of the unmanned aerial vehicle, the rotary screw rod 17 is screwed, the second pressing block 16 is tightly pressed through the screw rod 17, so that the second pressing block 16 moves downwards and extrudes the first pressing blocks 15 on two sides, the first pressing blocks 15 push the clamping blocks 14 to slide and extrude the lead 8, the limit fixation of the lead 8 is realized, the falling of the connector lug 4 caused by the elasticity of the first reset spring 10 and the vibration in the flight is avoided, and the safety and reliability of the device are improved.
In this embodiment, the outer surface of the clamping block 14 is slidably sleeved with a second return spring 18, one end of the second return spring 18 is fixedly provided with the outer surface of the first pressing block 15, and the second return spring 18 is provided, so that the clamping block 14 can automatically contract and return to the second fixing box 13 after the screw rod 17 is loosened by rotation.
In this embodiment, the arc groove has been seted up to the end portion that stretches out of clamp splice 14, and the internal surface in arc groove is provided with the cushion through the glue bonding, sets up the arc groove, and the fixed wire 8 of 14 pressfitting of clamp splice of being convenient for sets up the cushion, increases frictional force, reduces wearing and tearing.
In this embodiment, the upper end of the screw rod 17 is provided with an inner hexagonal sliding cavity, the upper surface of the first fixing box 5 is provided with a through hole, the through hole corresponds to the inner hexagonal sliding cavity, and the through hole and the inner hexagonal sliding cavity are arranged, so that the screw rod 17 can be conveniently inserted into the inner hexagonal sliding cavity through a hexagonal wrench to control the rotation of the screw rod 17, and the battery loading and unloading are not affected.
In this embodiment, the outer fixed surface of battery case body 2 is provided with rubber pad 6, and rubber pad 6 and first fixed box 5 set up rubber pad 6 at same horizontal plane, and the battery installation of being convenient for is placed firmly.
In the embodiment, the negative electrode plate 1 comprises an aluminum plate and a nickel plate, the aluminum plate and the nickel plate are welded and fixed, the negative electrode plate 1 needs to be frequently folded in the production process, the common aluminum plate is easy to break, and the nickel plate is fixed by welding and is not easy to break.
The utility model discloses a theory of operation and use flow:
mixing electrode active materials, a binder, a solvent and the like together, fully stirring and dispersing to form slurry, then uniformly coating the slurry prepared in the first step on a current collector with a specified thickness, wherein the current collector is an aluminum foil or a copper foil, drying the solvent, then punching and cutting the pole piece prepared in the last step into a specified size and shape, assembling a positive pole piece, a negative pole piece and a diaphragm together, forming a pole core after finishing rubberizing, then loading the pole core produced in the last step into an aluminum-plastic film with punched pits, finishing top sealing, side sealing and the like, reserving a liquid injection port at the same time, forming a soft package battery without liquid injection, then injecting a specified amount of electrolyte into the soft package battery core in a low-humidity environment, then baking the battery core, and finally extracting gas in the battery core in a vacuum environment and finishing sealing.
Before the installation battery, slider 11 slides to the interior diapire of first fixed box 5 under the effect of first reset spring 10, make connector lug 4 by the pulling shrink to the opening part of first fixed box 5, during the installation battery, pull out connector lug 4 from first fixed box 5, wire 8 passes through cylinder 12 pulling slider 11 this moment and slides to the open end of first fixed box 5, after connector lug 4 pegs graft on unmanned aerial vehicle's power source, slider 11 resets under the effect of first reset spring 10, draw back unnecessary wire 8 that stretches out in first fixed box 5 into first fixed box 5, avoid wire 8 to pile up in the outside of first fixed box 5, effectively protected wire 8 to avoid bending and friction loss.
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 (7)
1. The utility model provides a special battery of high magnification for unmanned aerial vehicle, includes negative pole piece (1), battery case body (2), positive plate (3), connector lug (4) and wire (8), the fixed one end that sets up in battery case body (2) of negative pole piece (1) and positive plate (3), connector lug (4) are connected its characterized in that with negative pole piece (1) and positive plate (3) through wire (8): the lower fixed surface of battery case body (2) is provided with first fixed box (5), the one end of first fixed box (5) is provided with the opening, and the inside of first fixed box (5) is fixed and is provided with slide bar (9), and the surface slip cover of slide bar (9) is equipped with first reset spring (10) and slider (11), slider (11) and first fixed box (5) sliding fit, and the fixed surface of slider (11) is provided with two cylinders (12), wire (8) slide around establishing the surface at cylinder (12).
2. The battery for the unmanned aerial vehicle, according to claim 1, is characterized in that: the opening end of the first fixing box (5) is fixedly provided with two internal thread cylinders (7), a second fixing box (13) is fixedly arranged between the two internal thread cylinders (7), two first press blocks (15) are arranged in the second fixing box (13) in a sliding manner, the adjacent surfaces of the two first press blocks (15) are arranged to be inclined surfaces, a second press block (16) is arranged in the middle of the second fixing box (13) in a sliding manner, the second press block (16) is tightly pressed with the two first press blocks (15), the upper end of the second press block (16) is provided with a lead screw (17) in a pressing manner, the lead screw (17) is screwed and extends out of the upper surface of the second fixing box (13) through threads, a clamping block (14) is fixedly arranged on the surface of the two first press blocks (15) which is deviated from each other, the clamping block (14) is slidably extended out of the outer surface of the second fixing box (13), and the lead wire (8) slidably penetrates through a gap between the internal thread cylinders (7) and the, the clamping block (14) is tightly pressed with the lead (8).
3. The battery as claimed in claim 2, wherein the battery is used for unmanned aerial vehicle, and comprises: the outer surface of the clamping block (14) is slidably sleeved with a second return spring (18), and one end of the second return spring (18) is fixedly provided with the outer surface of the first pressing block (15).
4. The battery as claimed in claim 2, wherein the battery is used for unmanned aerial vehicle, and comprises: an arc groove is formed in the end portion of the extending end of the clamping block (14), and a soft pad is arranged on the inner surface of the arc groove in a bonding mode through glue.
5. The battery as claimed in claim 2, wherein the battery is used for unmanned aerial vehicle, and comprises: an inner hexagonal sliding cavity is formed in the upper end of the screw rod (17), a through hole is formed in the upper surface of the first fixing box (5), and the through hole corresponds to the inner hexagonal sliding cavity.
6. The battery for the unmanned aerial vehicle, according to claim 1, is characterized in that: the outer surface of the battery outer shell (2) is fixedly provided with a rubber pad (6), and the rubber pad (6) and the first fixing box (5) are on the same horizontal plane.
7. The battery for the unmanned aerial vehicle, according to claim 1, is characterized in that: the negative plate (1) comprises an aluminum plate and a nickel plate, and the aluminum plate and the nickel plate are fixedly welded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921625230.1U CN210296468U (en) | 2019-09-27 | 2019-09-27 | High-rate special battery for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921625230.1U CN210296468U (en) | 2019-09-27 | 2019-09-27 | High-rate special battery for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210296468U true CN210296468U (en) | 2020-04-10 |
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ID=70065901
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921625230.1U Active CN210296468U (en) | 2019-09-27 | 2019-09-27 | High-rate special battery for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210296468U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112435589A (en) * | 2020-12-15 | 2021-03-02 | 合肥维信诺科技有限公司 | Display panel and display terminal |
-
2019
- 2019-09-27 CN CN201921625230.1U patent/CN210296468U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112435589A (en) * | 2020-12-15 | 2021-03-02 | 合肥维信诺科技有限公司 | Display panel and display terminal |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240511 Address after: 518051 room 1601, block B, building 7, Shenzhen International Innovation Valley (Building 9, Zone C, phase III, Vanke Yuncheng), Dali community, Xili street, Nanshan District, Shenzhen, Guangdong Patentee after: Shenzhen Romoss Technology Co.,Ltd. Country or region after: China Address before: No. 15 Dayi Road, Xiacun Industrial Base, Yushui District, Xinyu City, Jiangxi Province, 338019 Patentee before: XINYU ETERNAL ENERGY Co.,Ltd. Country or region before: China |
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| TR01 | Transfer of patent right |