CN215896575U - Battery with anti-seismic structure for small-sized unmanned aerial vehicle - Google Patents
Battery with anti-seismic structure for small-sized unmanned aerial vehicle Download PDFInfo
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- CN215896575U CN215896575U CN202121784419.2U CN202121784419U CN215896575U CN 215896575 U CN215896575 U CN 215896575U CN 202121784419 U CN202121784419 U CN 202121784419U CN 215896575 U CN215896575 U CN 215896575U
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- battery
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- aerial vehicle
- unmanned aerial
- battery body
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- 238000001125 extrusion Methods 0.000 claims abstract description 33
- 238000013016 damping Methods 0.000 claims abstract description 24
- 230000035939 shock Effects 0.000 claims abstract description 24
- 239000011159 matrix material Substances 0.000 claims abstract description 7
- 238000010521 absorption reaction Methods 0.000 claims description 5
- 238000003825 pressing Methods 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 10
- 238000004880 explosion Methods 0.000 abstract description 3
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000000630 rising effect Effects 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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Abstract
The utility model belongs to the technical field of batteries, and particularly relates to a battery with an anti-seismic structure for a small-sized unmanned aerial vehicle, which comprises a shell assembly, a damping assembly and an adjusting assembly; the shell assembly comprises a bin body, and a fixed cover is rotatably connected to the bottom end of the bin body; through the slide bar of the crowded board one end of extrusion battery body, first spacing ring and first spring all are the matrix and arrange at shock attenuation board and storehouse inboard top, thereby make every department of crowded board the extrusion power degree of battery body the same, thereby the fixed and antidetonation effect to battery body has been improved, thereby prevent that small unmanned aerial vehicle from extrudeing the battery body and leading to the battery body to damage the explosion in the external collision, through screw rod and shock attenuation board sliding connection and the screw rod outside and adjustable ring threaded connection, thereby make adjustable ring extrusion shock attenuation board reciprocate in the screw rod outside through rotating the adjustable ring, thereby adjust the extrusion power degree of crowded board and battery body, thereby adjust the antidetonation effect of battery body.
Description
Technical Field
The utility model belongs to the technical field of batteries, and particularly relates to a battery with an anti-seismic structure for a small unmanned aerial vehicle.
Background
The unmanned aircraft is called an unmanned aerial vehicle for short, and called a UAV in English for short, and is an unmanned aircraft operated by using a radio remote control device and a self-contained program control device, and the definition of the technology can be divided into: unmanned fixed wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned parachute-wing aircraft and the like, wherein the unmanned aerial vehicle can be divided into military and civil according to the application field, the unmanned aerial vehicle can be divided into reconnaissance aircraft and target aircraft according to the military aspect and the civil aspect, the unmanned aerial vehicle is applied in the unmanned aerial vehicle industry and is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, self-shooting, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded.
But current unmanned aerial vehicle is at the in-process that uses, and unmanned aerial vehicle is when colliding the object, and the object is to unmanned aerial vehicle and the inside extrusion battery of unmanned aerial vehicle to lead to the easy explosion of battery.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Aiming at the defects of the prior art, the utility model provides the battery with the anti-seismic structure for the small unmanned aerial vehicle, which has the advantages of battery shock absorption and protection and solves the problem that the battery is easy to damage and explode due to the collision of the battery extruded inside caused by the collision of the small unmanned aerial vehicle.
(II) technical scheme
In order to achieve the purpose, the utility model provides the following technical scheme: a battery with an anti-seismic structure for a small unmanned aerial vehicle comprises a shell assembly, a damping assembly and an adjusting assembly;
the shell assembly comprises a bin body, the bottom end of the bin body is rotatably connected with a fixed cover, the inner side of the fixed cover is in threaded connection with a screw, and the left end of the inner side of the bin body is provided with a socket;
the damping component comprises a damping plate, the damping plate and the top end of the inner side of the bin body are connected with a sliding rod in a sliding mode, one end of the sliding rod is fixedly connected with a squeezing plate, a battery body is placed at one end of the squeezing plate, the left end of the battery body is provided with a connector, the connector is meshed with a socket, a first limiting ring is fixedly connected with one end of the sliding rod, a first spring is fixedly connected with one end of the first limiting ring, a screw rod is fixedly connected with the top end of the inner side of the bin body, and an adjusting ring is in threaded connection with the outer side of the screw rod.
Preferably, the slide bar, the first limiting ring and the first spring are arranged on the top ends of the inner sides of the damping plate and the cabin body in a matrix manner.
Through adopting above-mentioned scheme, all be the matrix through slide bar, first spacing ring and first spring at damper plate and storehouse inboard top and arrange to improved the fixed and antidetonation effect to battery body, thereby prevented that battery body from damaging at the inboard collision in storehouse.
Preferably, the number of the screws is two, the two screws are respectively positioned on the left side and the right side of the top end of the inner side of the bin body, and the extrusion plate and the battery body are positioned between the two screws.
Through adopting above-mentioned scheme, lie in crowded board and battery body left and right sides respectively through two screws to improve the extrusion effect to the shock attenuation board to battery body.
Preferably, the screw rod is connected with the damping plate in a sliding mode, and the outer side of the screw rod is connected with the adjusting ring in a threaded mode.
Through adopting above-mentioned scheme, through screw rod and shock attenuation board sliding connection and screw rod outside and adjustable ring threaded connection to thereby make adjustable ring extrusion shock attenuation board reciprocate in the screw rod outside through rotating the adjustable ring, thereby adjust the extrusion pressure degree of crowded board and battery body, thereby adjust battery body's antidetonation effect.
Preferably, the adjusting assembly comprises an extrusion ring, the extrusion ring is connected with the screw in a sliding manner, the top end of the adjusting ring is fixedly connected with a connecting ring, the outer side of the connecting ring is fixedly connected with a clamping plate, the bottom end of the extrusion ring is fixedly connected with a hollow tube, the bottom end of the extrusion ring is fixedly connected with a second spring, and the bottom end of the second spring is fixedly connected with the connecting ring.
Through adopting above-mentioned scheme, make the go-between slide in the spout inboard through rotating the adjustable ring to make the go-between slide in the adjustable ring inboard, thereby make the go-between extrude the second spring, make the extrusion ring drive the shock attenuation board through the second spring and upwards slide in the screw rod outside, prevent through the second spring that the shock attenuation board rises to extrude and damage battery body.
Preferably, a placing groove is formed in the inner side of the damping plate, and the extrusion ring and the hollow pipe are located on the inner side of the placing groove.
Through adopting above-mentioned scheme, all be located the inboard standing groove of shock attenuation board through extrusion ring and hollow tube to reduce the occupation space to the storehouse body, the shock attenuation board of being convenient for simultaneously goes up and down.
Preferably, the inner side of the hollow tube is provided with a sliding groove, and the sliding groove is in sliding connection with the clamping plate.
Through adopting above-mentioned scheme, through cardboard and spout sliding connection to when preventing to rotate the adjustable ring, the go-between drives the second spring rotatory, thereby damages the second spring.
(III) advantageous effects
Compared with the prior art, the utility model provides a battery with an anti-seismic structure for a small unmanned aerial vehicle, which has the following beneficial effects:
this small-size unmanned aerial vehicle is with battery that has antidetonation structure, the slide bar of crowded board one end through the extrusion battery body, first spacing ring and first spring all are the matrix arrangement on shock attenuation board and storehouse inboard top, thereby make every department of crowded board the extrusion power degree of battery body the same, thereby the fixed and antidetonation effect to the battery body has been improved, thereby prevent that small-size unmanned aerial vehicle from extruding the battery body and leading to the battery body to damage the explosion in the external collision, through screw rod and shock attenuation board sliding connection and the screw rod outside and adjustable ring threaded connection, thereby make adjustable ring extrusion shock attenuation board reciprocate in the screw rod outside through rotating the adjustable ring, thereby adjust the extrusion power degree of crowded board and battery body, thereby adjust the antidetonation effect of battery body.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the structure at position A in the present invention;
FIG. 3 is a schematic view of the external structure of the present invention;
FIG. 4 is a schematic view of the structure at B in the present invention;
FIG. 5 is a schematic cross-sectional view at B in the present invention;
in the figure:
1. a housing assembly; 101. a bin body; 102. a fixed cover; 103. a screw; 104. a socket;
2. a shock absorbing assembly; 201. a damper plate; 202. a slide bar; 203. extruding a plate; 204. a battery body; 205. a connector; 206. a first limit ring; 207. a first spring; 208. a screw; 209. an adjusting ring;
3. an adjustment assembly; 301. an extrusion ring; 302. a connecting ring; 303. clamping a plate; 304. a hollow tube; 305. a second spring; 306. a placement groove; 307. a chute.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example one
A battery with an anti-seismic structure for a small unmanned aerial vehicle comprises a shell component 1, a damping component 2 and an adjusting component 3;
the shell assembly 1 comprises a bin body 101, the bottom end of the bin body 101 is rotatably connected with a fixed cover 102, the inner side of the fixed cover 102 is in threaded connection with a screw 103, and the left end of the inner side of the bin body 101 is provided with a socket 104;
the damping component 2 comprises a damping plate 201, the damping plate 201 and the top end of the inner side of the bin body 101 are both connected with a sliding rod 202 in a sliding manner, one end of the sliding rod 202 is fixedly connected with a squeezing plate 203, one end of the squeezing plate 203 is provided with a battery body 204, the left end of the battery body 204 is provided with a connector 205, the connector 205 is meshed with a socket 104, one end of the sliding rod 202 is fixedly connected with a first limiting ring 206, one end of the first limiting ring 206 is fixedly connected with a first spring 207, the top end of the inner side of the bin body 101 is fixedly connected with a screw 208, and the outer side of the screw 208 is in threaded connection with an adjusting ring 209;
Referring to fig. 1-5, during installation, the battery body 204 is placed on the squeezing plates 203 on the shock absorption plate 201, the battery body 204 is connected with the cabin 101 of the small unmanned aerial vehicle, the shock absorption plate 201 moves upwards along the screw 208, so that the squeezing plates 203 on the upper and lower sides can squeeze the battery body 204 at the same time, thereby fixing the battery body, when in use, the battery body 204 is squeezed through the two squeezing plates 203, when the small unmanned aerial vehicle collides with an object, the object squeezes the battery body 204 inside the small unmanned aerial vehicle and the small unmanned aerial vehicle, the sliding rods 202 on the two sides of the battery body 204 drive the first limiting rings 206 to squeeze the first springs 207 through the first limiting rings 206, the squeezing plates 203 squeeze the battery body 204 through the sliding rods 202, thereby damping the battery body 204, through the sliding rods 202, the first limiting rings 206 and the first springs 207 are arranged in a matrix form on the top ends of the shock absorption plate 201 and the cabin 101, therefore, the extrusion force of each position of the extrusion plate 203 on the battery body 204 is the same, the fixation and the anti-seismic effect on the battery body 204 are improved, the battery body 204 is prevented from being damaged by collision at the inner side of the bin body 101 and the joint of the battery body 204 and the bin body 101 is prevented from being loosened, the adjustment ring 209 is connected with the damping plate 201 in a sliding mode through the screw 208 and is in threaded connection with the adjusting ring 209 on the outer side of the screw 208, the damping plate 201 is extruded by the adjusting ring 209 to move up and down on the outer side of the screw 208 through rotation of the adjusting ring 209, the extrusion force of the extrusion plate 203 and the battery body 204 is adjusted, and the anti-seismic effect of the battery body 204 is adjusted.
Example two
The adjusting component 3 for preventing the battery body 204 from being damaged by extrusion when the damping plate 201 is lifted is added on the basis of the first embodiment.
The adjusting assembly 3 comprises an extrusion ring 301, the extrusion ring 301 is slidably connected with the screw 208, the top end of the adjusting ring 209 is fixedly connected with a connecting ring 302, the outside of the connecting ring 302 is fixedly connected with a clamping plate 303, the bottom end of the extrusion ring 301 is fixedly connected with a hollow tube 304, the bottom end of the extrusion ring 301 is fixedly connected with a second spring 305, the bottom end of the second spring 305 is fixedly connected with the connecting ring 302, the inner side of the damping plate 201 is provided with a placing groove 306, the extrusion ring 301 and the hollow tube 304 are both located on the inner side of the placing groove 306, the inner side of the hollow tube 304 is provided with a sliding groove 307, and the sliding groove 307 is slidably connected with the clamping plate 303.
Referring to fig. 1 to 5, when the adjusting ring 209 is rotated to enable the adjusting ring 209 to press the damping plate 201 to move up and down outside the screw 208, the adjusting ring 209 drives the connecting ring 302 to slide inside the sliding groove 307 through the snap plate 303, so that the connecting ring 302 slides inside the adjusting ring 209, so that the connecting ring 302 presses the second spring 305, the pressing ring 301 drives the damping plate 201 to slide upwards outside the screw 208 through the second spring 305, the damping plate 201 is prevented from rising and pressing to damage the battery body 204 through the second spring 305, and the snap plate 303 is slidably connected with the sliding groove 307 through the snap plate 303, so that when the adjusting ring 209 is prevented from being rotated, the connecting ring 302 drives the second spring 305 to rotate, so that the second spring 305 is damaged.
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 utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides a battery that small-size unmanned aerial vehicle used has shock-resistant structure which characterized in that: comprises a shell component (1), a shock absorption component (2) and an adjusting component (3);
the shell assembly (1) comprises a bin body (101), the bottom end of the bin body (101) is rotatably connected with a fixed cover (102), the inner side of the fixed cover (102) is in threaded connection with a screw (103), and the left end of the inner side of the bin body (101) is provided with a socket (104);
damping component (2) are including shock attenuation board (201), the equal sliding connection in shock attenuation board (201) and the inboard top of the storehouse body (101) has slide bar (202), the crowded board (203) of slide bar (202) one end fixedly connected with, battery body (204) have been placed to crowded board (203) one end, battery body (204) left end is provided with connector (205), connector (205) and socket (104) meshing, the first spacing ring (206) of slide bar (202) one end fixedly connected with, the first spring (207) of first spacing ring (206) one end fixedly connected with, the inboard top fixedly connected with screw rod (208) of the storehouse body (101), screw rod (208) outside threaded connection has adjustable ring (209).
2. The battery with an earthquake-proof structure for the small-sized unmanned aerial vehicle according to claim 1, wherein: the top ends of the sliding rod (202), the first limiting ring (206) and the first spring (207) on the inner sides of the damping plate (201) and the cabin body (101) are arranged in a matrix manner.
3. The battery with an earthquake-proof structure for the small-sized unmanned aerial vehicle according to claim 1, wherein: the number of the screw rods (208) is two, the two screw rods (208) are respectively positioned at the left side and the right side of the top end of the inner side of the bin body (101), and the extrusion plate (203) and the battery body (204) are positioned between the two screw rods (208).
4. The battery with an earthquake-proof structure for the small-sized unmanned aerial vehicle according to claim 1, wherein: the screw rod (208) is connected with the damping plate (201) in a sliding mode, and the outer side of the screw rod (208) is connected with the adjusting ring (209) in a threaded mode.
5. The battery with an earthquake-proof structure for the small-sized unmanned aerial vehicle according to claim 1, wherein: adjusting part (3) is including pressing ring (301), press ring (301) and screw rod (208) sliding connection, adjusting ring (209) top fixedly connected with go-between (302), go-between (302) outside fixedly connected with cardboard (303), press ring (301) bottom fixedly connected with hollow tube (304), press ring (301) bottom fixedly connected with second spring (305), second spring (305) bottom and go-between (302) fixed connection.
6. The battery with an earthquake-proof structure for the small-sized unmanned aerial vehicle according to claim 5, wherein: a placing groove (306) is formed in the inner side of the damping plate (201), and the extrusion ring (301) and the hollow pipe (304) are located on the inner side of the placing groove (306).
7. The battery with an earthquake-proof structure for the small-sized unmanned aerial vehicle according to claim 5, wherein: a sliding groove (307) is formed in the inner side of the hollow pipe (304), and the sliding groove (307) is connected with the clamping plate (303) in a sliding mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121784419.2U CN215896575U (en) | 2021-08-02 | 2021-08-02 | Battery with anti-seismic structure for small-sized unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121784419.2U CN215896575U (en) | 2021-08-02 | 2021-08-02 | Battery with anti-seismic structure for small-sized unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215896575U true CN215896575U (en) | 2022-02-22 |
Family
ID=80343380
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121784419.2U Expired - Fee Related CN215896575U (en) | 2021-08-02 | 2021-08-02 | Battery with anti-seismic structure for small-sized unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215896575U (en) |
-
2021
- 2021-08-02 CN CN202121784419.2U patent/CN215896575U/en not_active Expired - Fee Related
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Legal Events
| 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: 20220222 |