CN211125740U - Unmanned aerial vehicle battery case - Google Patents
Unmanned aerial vehicle battery case Download PDFInfo
- Publication number
- CN211125740U CN211125740U CN201922255125.XU CN201922255125U CN211125740U CN 211125740 U CN211125740 U CN 211125740U CN 201922255125 U CN201922255125 U CN 201922255125U CN 211125740 U CN211125740 U CN 211125740U
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- Prior art keywords
- battery
- inner shell
- shell
- outer shell
- aerial vehicle
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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 discloses an unmanned aerial vehicle battery case, including battery case and battery inner shell, one side of battery case forms the side opening, and in the battery inner shell assembled into battery case from this side opening department, the battery inner shell formed pull formula assembly structure with battery case. The technical scheme provides a drawing type battery box structure which can realize quick disassembly; the locking structure between the battery inner shell and the battery outer shell can be opened without any tool; the battery inner shell is used for loading the battery, and battery case is used for cooperating the fuselage appearance, and both realize stable assembly structure, better utilization the box spatial structure who loads the battery, increased box life, reduced the use of material, and provide double-deck protection to the battery, provide stable operational environment for machine carries the battery.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle power module's technique and specifically relates to a battery case for unmanned aerial vehicle, its mechanical connection structure of in particular to.
Background
Reference, patent application No.: 201910251716.1, Applicant: tanku City, Tanxing aerospace technologies, Inc., filing date: 2019.03.29, the present case discloses "an unmanned aerial vehicle battery case", including battery box body, connector lug and T type bolt, its characterized in that: the battery box is characterized in that two fixed columns are fixed in the battery box body, a sleeve (8) is fixed on the side wall of the battery box body, an adjusting bolt is connected to the top end face of the sleeve, a telescopic rod is connected to one end of the telescopic rod, a movable plate is installed at one end of the telescopic rod, two positioning round hole seats are installed at the center shaft of the movable plate and sleeved on the two fixed columns respectively, a spring piece is installed on the side face of the movable plate and connected with a connector lug through a wire, two stainless steel hinges are installed at the top end of the battery box body and connected with battery box sealing covers through the stainless steel hinges, and wear-resistant sealing strips are fixedly arranged at the edges of the battery box sealing covers and are of rectangular structures.
Present unmanned aerial vehicle machine carries battery case and adopts individual layer box body structure more, and direct shaping on the fuselage, barrier propterty is weak, also does not benefit to the replacement of daily battery module simultaneously, so still need carry out further improvement to current unmanned aerial vehicle battery case mechanism.
Disclosure of Invention
An object of the utility model is to provide an unmanned aerial vehicle battery case designs into inner shell and the shell of mutually assembling with the battery case, can realize quick dismantlement, assembly between the two. Overcomes the defects in the prior art.
In order to realize the purpose, the technical scheme of the utility model is that: an unmanned aerial vehicle battery box comprises a battery outer shell and a battery inner shell, wherein a side opening is formed in one side of the battery outer shell, the battery inner shell is assembled into the battery outer shell from the side opening, a pull-out assembly structure is formed between the battery inner shell and the battery outer shell, an outer shell extending part is formed outwards on the upper edge of the side opening of the battery outer shell, a button hole is formed in the extending part of the outer shell, a battery cavity is formed in the inner cavity of the battery inner shell, an upper opening is formed in the upper part of the battery inner shell, an inner shell extending part matched with the outer shell extending part is formed outwards on the edge of the upper opening of the battery inner shell, the inner shell extending part outwards protrudes out of the side wall of the battery inner shell, a spring is assembled in the inner shell extending part, a button part is assembled on the upper part of the spring, a button part, the height of the buckle is lower than that of the button part.
The utility model discloses an unmanned aerial vehicle battery box, which provides a drawing type battery box structure, and can realize quick disassembly; the locking structure between the battery inner shell and the battery outer shell can be opened without any tool; the battery inner shell is used for loading the battery, and battery case is used for cooperating the fuselage appearance, and both realize stable assembly structure, better utilization the box spatial structure who loads the battery, increased box life, reduced the use of material, and provide double-deck protection to the battery, provide stable operational environment for machine carries the battery.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a sectional view of the present invention.
Fig. 3 is a top view of the present invention.
Fig. 4 is a side view of the present invention.
Fig. 5 is a perspective view of the present invention.
Detailed Description
The invention will be further described with reference to the accompanying drawings.
The utility model discloses an unmanned aerial vehicle battery case, it is different from prior art and lies in: the battery comprises a battery outer shell 1 and a battery inner shell 2, wherein a side opening is formed on one side of the battery outer shell 1, the battery inner shell 2 is assembled into the battery outer shell 1 from the side opening, a pull-out assembly structure is formed between the battery inner shell 2 and the battery outer shell 1, an outer shell extension part 3 is formed outwards on the upper edge of the side opening of the battery outer shell 1, a button hole 4 is formed at the beginning of the outer shell extension part 3, a battery cavity 5 is formed in an inner cavity of the battery inner shell 2, an upper opening is formed on the upper part of the battery inner shell 2, an inner shell extension part 6 matched with the outer shell extension part 3 is formed outwards on the edge of the upper opening of the battery inner shell 2, the inner shell extension part 6 outwards protrudes out of the side wall of the battery inner shell 2, a spring 7 is assembled in the inner shell extension part 6, a button part 8 is assembled on the, the top of the battery shell 1 is provided with a slot 11 matched with the buckle 10, and the height of the buckle 10 is lower than that of the button part 8.
In specific implementation, the inner walls of the two sides of the battery outer casing 1 are formed with horizontally distributed guide rail convex strips 12, and the outer walls of the left and right sides of the battery inner casing 2 are formed with sliding grooves 13 matched with the guide rail convex strips 12.
In specific implementation, a convex mounting box 14 is formed at the top of the battery shell 1, a mounting plate 15 is arranged at the top of the mounting box 14, and a threading opening 16 is formed at the mounting plate 15.
In practical implementation, the bottom of the inner shell extension part 6 is provided with a handle groove 17.
During specific implementation, a plurality of damping rubber sheets 18 are distributed at the bottom of the inner cavity of the battery outer shell 1 and used for providing damping protection for the battery inner shell and the battery module in the shell.
When the battery inner shell is implemented, the button is pressed down, the spring is compressed, the buckle slips from the clamping groove firstly, then the button is pressed down along the same trend, the button slips from the button hole, and an operator pulls the handle groove with hand to pull out the battery inner shell.
The foregoing is a more detailed description of the invention, taken in conjunction with the accompanying preferred embodiments, and it is not intended that the invention be limited to the specific embodiments described above. To the utility model belongs to the technical field of ordinary technical personnel, do not deviate from the utility model discloses under the prerequisite of design, can also make a plurality of simple deductions or replacement, all should regard as belonging to the utility model discloses a protection scope.
Claims (5)
1. Unmanned aerial vehicle battery case, its characterized in that: the battery comprises a battery outer shell (1) and a battery inner shell (2), wherein a side opening is formed in one side of the battery outer shell (1), the battery inner shell (2) is assembled into the battery outer shell (1) from the side opening, a drawing type assembly structure is formed between the battery inner shell (2) and the battery outer shell (1), an outer shell extending part (3) is outwards formed on the upper edge of the side opening of the battery outer shell (1), a button hole (4) is formed in the outer shell extending part (3), a battery cavity (5) is formed in the inner cavity of the battery inner shell (2), an upper opening is formed in the upper part of the battery inner shell (2), an inner shell extending part (6) matched with the outer shell extending part (3) is outwards formed on the edge of the upper opening of the battery inner shell (2), the inner shell extending part (6) outwards protrudes out of the side wall of the battery inner shell (2), a spring (7) is assembled in, the front side and the rear side of the button part (8) are respectively provided with a button (9) and a buckle (10) which are protruded upwards, the button (9) is arranged corresponding to the button hole (4), the top of the battery shell (1) is provided with a clamping groove (11) matched with the buckle (10), and the height of the buckle (10) is lower than that of the button part (8).
2. The unmanned aerial vehicle battery box of claim 1, characterized in that: the inner walls of the two sides of the battery outer shell (1) are provided with guide rail convex strips (12) which are horizontally distributed, and the outer walls of the left side and the right side of the battery inner shell (2) are provided with sliding grooves (13) matched with the guide rail convex strips (12).
3. The unmanned aerial vehicle battery box of claim 1, characterized in that: the battery case (1) top upwards forms protruding mounting box (14), and the top of mounting box (14) is equipped with mounting panel (15), and mounting panel (15) department has seted up through wires mouth (16).
4. The unmanned aerial vehicle battery box of claim 1, characterized in that: the bottom of the inner shell extension part (6) is provided with a handle groove (17).
5. The unmanned aerial vehicle battery box of claim 1, characterized in that: the bottom of the inner cavity of the battery shell (1) is distributed with a plurality of damping rubber sheets (18).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201922255125.XU CN211125740U (en) | 2019-12-16 | 2019-12-16 | Unmanned aerial vehicle battery case |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201922255125.XU CN211125740U (en) | 2019-12-16 | 2019-12-16 | Unmanned aerial vehicle battery case |
Publications (1)
Publication Number | Publication Date |
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CN211125740U true CN211125740U (en) | 2020-07-28 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201922255125.XU Active CN211125740U (en) | 2019-12-16 | 2019-12-16 | Unmanned aerial vehicle battery case |
Country Status (1)
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CN (1) | CN211125740U (en) |
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2019
- 2019-12-16 CN CN201922255125.XU patent/CN211125740U/en active Active
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