CN211858717U - Quick-falling battery box for unmanned aerial vehicle - Google Patents
Quick-falling battery box for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN211858717U CN211858717U CN202020397750.8U CN202020397750U CN211858717U CN 211858717 U CN211858717 U CN 211858717U CN 202020397750 U CN202020397750 U CN 202020397750U CN 211858717 U CN211858717 U CN 211858717U
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- Prior art keywords
- aerial vehicle
- unmanned aerial
- casing
- battery
- seat
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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.)
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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
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
The utility model provides an unmanned aerial vehicle is with battery case that drops fast, including unmanned aerial vehicle body and battery case. The unmanned aerial vehicle body is fixedly provided with two body rods, four rotors and a controller box body, the control box body is provided with an upper cover and a lower cover, the middle part of the upper cover is provided with a battery box seat, the periphery of the battery box seat is provided with a transverse buckling seat and a longitudinal buckling seat, buckles are arranged inside the battery box seat, the lower part of the upper cover is provided with a tray, and four corners of the tray are fixedly provided with power plugs; the battery case includes the casing, the battery frame, gasket and lithium cell, the casing includes casing and lower casing, it is equipped with locking knot to go up the casing counterpoint both sides, the casing is equipped with horizontal bayonet socket and vertical bayonet socket down, the casing bottom is equipped with supply socket down, this unmanned aerial vehicle helps coming off fast with the battery case structure that drops fast, when unmanned aerial vehicle striking ground or barrier, the fuselage frame can make it shake off the buckle constraint for the reverse impact force of battery case, launch out the battery case seat, cause the battery case to break away from unmanned aerial vehicle, ensure unmanned aerial vehicle's safety.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, more specifically relates to a battery case drops fast for unmanned aerial vehicle.
Background
The unmanned aerial vehicle technology has good application prospects in various application fields, such as aerial reconnaissance, aerial photography, remote material conveying, agricultural medicine spreading and the like. Unmanned aerial vehicle's power supply system is mostly lithium battery powered, has the battery less because its power supply load ratio is lower, however the carrying of lithium cell, and the great load of weight increase that will probably give unmanned aerial vehicle, when dangerous the taking place, unmanned aerial vehicle when hitting bottom surface or barrier, the risk of exploding very easily takes place for the existence of battery, destroys whole unmanned aerial vehicle software and hardware structure, early inestimable's loss.
The prior art is as follows: CN 205355106U discloses a battery and a fixing structure thereof, the battery comprises a battery box, a battery unit and a metal sheet, wherein the battery unit is assembled inside the battery box, and the metal sheet is arranged on the outer surface of the battery box and used for being adsorbed with an external magnetic block structure to fix the battery. The fixing structure of the battery comprises a support main body, wherein a magnet is arranged on the support main body, and the position of the magnet corresponds to the position of a metal sheet in the battery. This technical scheme's battery and fixed knot construct through adsorbing each other between magnet and the sheetmetal for when the battery was installed in fixed establishment, can enough fix the battery effectively and prevent to drop on the battery frame, also can take place to vibrate the back through the quick playback of magnetic force absorption at the battery, can also make things convenient for the quick assembly disassembly of battery and battery structure.
However, if the battery is applied to the unmanned aerial vehicle technology, the stability is not high, the battery is very easy to fall off or misplace in the acceleration and deceleration process, and the danger of crash explosion can occur when the connection power supply is disconnected.
Disclosure of Invention
The utility model relates to a purpose is: in order to make further improvement by combining the technical scheme provided by the prior art, a quick-release battery box for an unmanned aerial vehicle is designed and provided, wherein multiple interfaces are used for butt joint and power supply at the same time, and preliminary positioning is carried out; and then the clamping is positioned and clamped for the second time by a buckle.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a battery case that drops fast for unmanned aerial vehicle, includes unmanned aerial vehicle body and battery case.
The unmanned aerial vehicle body is fixedly provided with two body rods, four rotors and a controller box, the two body rods are arranged in a cross manner, and four lifting frames are symmetrically arranged at the lower part of the unmanned aerial vehicle body;
the control box body is provided with an upper cover and a lower cover, a battery box seat is arranged in the middle of the upper cover, a transverse buckling seat and a longitudinal buckling seat are arranged on the periphery of the battery box seat, buckles are arranged in the transverse buckling seat and the longitudinal buckling seat respectively, a tray is arranged on the lower portion of the upper cover, and power plugs are fixedly arranged at four corners of the tray;
the battery case includes casing, battery frame, gasket and lithium cell, the casing includes casing and lower casing, it is equipped with the locking knot to go up casing counterpoint both sides, with casing cooperation locking down, the casing is equipped with horizontal bayonet socket and vertical bayonet socket down, the casing bottom is equipped with supply socket down, with power plug cooperates, gives unmanned aerial vehicle control circuit power supply, the battery frame set up in inside the casing, the gasket attached with the upper and lower portion of battery frame, the lithium cell with supply socket electric connection, the battery case possesses charge-discharge function.
Furthermore, a plurality of reinforcing ribs are arranged on the periphery of the battery box seat.
Furthermore, the transverse bayonet and the longitudinal bayonet correspond to the clamping positions of the transverse clamping seat and the longitudinal clamping seat one by one.
Furthermore, six sides of the battery rack are provided with heat dissipation openings.
Compared with the prior art, implement the utility model discloses a battery case drops fast for unmanned aerial vehicle has following beneficial effect:
1. the quick-release battery box for the unmanned aerial vehicle utilizes multiple interfaces to supply power with the unmanned aerial vehicle control circuit at the same time, is positioned and clamped by the buckle, and is convenient and practical;
2. the reinforcing ribs arranged on the periphery of the battery box seat can ensure the firmness and stability of the unmanned aerial vehicle control box body structure, and the design is reasonable;
3. this unmanned aerial vehicle is with battery case structure that drops fast helps dropping fast, and when unmanned aerial vehicle striking ground or barrier, the fuselage frame can make it shake off the buckle constraint for the reverse impact force of battery case, launches out the battery case seat, causes the battery case to break away from unmanned aerial vehicle, ensures unmanned aerial vehicle's safety.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly described below.
Fig. 1 is a perspective view of the unmanned aerial vehicle according to the embodiment;
fig. 2 is a perspective view of the unmanned aerial vehicle according to the embodiment after a battery box is removed;
FIG. 3 is a partial enlarged view of FIG. 2A;
fig. 4 is a perspective view of the unmanned aerial vehicle of the embodiment with the upper case removed by the quick-release battery box;
FIG. 5 is a schematic structural diagram of a battery box for a rapid detachment of the unmanned aerial vehicle according to the embodiment;
the airplane comprises a fuselage rod 1, a rotor 2, a landing gear 3, an upper cover 4, a longitudinal buckle seat 41, a longitudinal buckle 411, a transverse buckle seat 42, a transverse buckle 421, a supporting plate 43, a power plug 44, a reinforcing rib 45, a battery box 5, an upper shell 51, a locking buckle 511, a lower shell 52, a longitudinal bayonet 521, a transverse bayonet 522, a battery rack 53, a lithium battery 54, a gasket 55 and a battery socket 56.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.
Example (b):
as shown in fig. 1-5, the present embodiment provides a quick-release battery box for an unmanned aerial vehicle, which includes an unmanned aerial vehicle body and a battery box 5.
Be fixed with two fuselage poles 1, four rotors 2, controller box on the unmanned aerial vehicle body, two fuselage pole 1 cross is arranged, and the lower part symmetry is equipped with four and props up the landing frame 3.
The control box is equipped with upper cover 4 and lower cover, 4 middle parts of upper cover are equipped with the battery box seat, the battery box seat periphery is equipped with horizontal buckle seat 42 and vertical buckle seat 41, horizontal buckle seat 42 with vertical buckle seat 41 is inside all to be equipped with buckle (421, 411), 3 lower parts of upper cover are equipped with tray 43, the fixed power plug 44 that is equipped with in tray 43 four corners.
In a further embodiment, the battery box base is provided with a plurality of reinforcing ribs 45 at the periphery.
In a further embodiment, the transverse bayonet 522 and the longitudinal bayonet 521 correspond to the positions of the buckles (421, 411) of the transverse buckle seat 42 and the longitudinal buckle seat 41 one by one.
In a further embodiment, six sides of the battery holder 53 are provided with heat dissipation openings.
The embodiments of the present invention have been described in detail with reference to the accompanying drawings, but the present invention is not limited to the above embodiments, and various changes, modifications, substitutions and alterations can be made without departing from the spirit of the present invention within the knowledge of those skilled in the art, and the scope of the present invention is defined by the appended claims and their equivalents.
Claims (4)
1. The utility model provides an unmanned aerial vehicle is with battery case that drops fast, includes unmanned aerial vehicle body and battery case, its characterized in that:
the unmanned aerial vehicle body is fixedly provided with two body rods, four rotors and a controller box, the two body rods are arranged in a cross manner, and four lifting frames are symmetrically arranged at the lower part of the unmanned aerial vehicle body;
the controller box is provided with an upper cover and a lower cover, a battery box seat is arranged in the middle of the upper cover, a transverse buckling seat and a longitudinal buckling seat are arranged on the periphery of the battery box seat, buckles are arranged in the transverse buckling seat and the longitudinal buckling seat respectively, a tray is arranged on the lower portion of the upper cover, and power plugs are fixedly arranged at four corners of the tray;
the battery case includes casing, battery frame, gasket and lithium cell, the casing includes casing and lower casing, it is equipped with the locking knot to go up casing counterpoint both sides, with casing cooperation locking down, the casing is equipped with horizontal bayonet socket and vertical bayonet socket down, the casing bottom is equipped with supply socket down, with power plug cooperates, gives unmanned aerial vehicle control circuit power supply, the battery frame set up in inside the casing, the gasket attached with the upper and lower portion of battery frame, the lithium cell with supply socket electric connection.
2. The quick-release battery pack for the unmanned aerial vehicle as claimed in claim 1, wherein: and a plurality of reinforcing ribs are arranged on the periphery of the battery box seat.
3. The quick-release battery pack for the unmanned aerial vehicle as claimed in claim 1, wherein: the transverse bayonet and the longitudinal bayonet correspond to the clamping positions of the transverse clamping seat and the longitudinal clamping seat one by one.
4. The quick-release battery pack for the unmanned aerial vehicle as claimed in claim 1, wherein: six sides of the battery frame are provided with heat dissipation openings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020397750.8U CN211858717U (en) | 2020-03-25 | 2020-03-25 | Quick-falling battery box for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020397750.8U CN211858717U (en) | 2020-03-25 | 2020-03-25 | Quick-falling battery box for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211858717U true CN211858717U (en) | 2020-11-03 |
Family
ID=73136812
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020397750.8U Expired - Fee Related CN211858717U (en) | 2020-03-25 | 2020-03-25 | Quick-falling battery box for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211858717U (en) |
-
2020
- 2020-03-25 CN CN202020397750.8U patent/CN211858717U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201103 Termination date: 20210325 |
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| CF01 | Termination of patent right due to non-payment of annual fee |