CN212751028U - Unmanned aerial vehicle removable battery mounting structure - Google Patents
Unmanned aerial vehicle removable battery mounting structure Download PDFInfo
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- CN212751028U CN212751028U CN202022125643.2U CN202022125643U CN212751028U CN 212751028 U CN212751028 U CN 212751028U CN 202022125643 U CN202022125643 U CN 202022125643U CN 212751028 U CN212751028 U CN 212751028U
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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
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
-
- 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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- Photovoltaic Devices (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
The utility model discloses a detachable battery mounting structure of unmanned aerial vehicle, which comprises a body, a battery component and a solar panel component, wherein the battery component comprises a battery bin, a wiring jack, a battery body, a wiring plug, a connecting block, a first chute, a first spring, a first stop block, a slide block, a baffle plate, a second chute, a first limit groove and a holding tank, the solar panel component comprises a slide rail, a fixing frame, a solar panel body, a second stop block, a limit block, an elastic contact and an opening, compared with the existing unmanned aerial vehicle battery structure, the designed battery is detachable, the designed battery structure is convenient to detach and simple to replace on the premise of ensuring good sealing performance of the body, the solar panel component designed by the utility model can continuously supplement electric energy in the using process of the unmanned aerial vehicle, thereby greatly improving the service life of the unmanned aerial vehicle, the clamping structure design facilitates the disassembly and the maintenance of the assembly.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle removable battery mounting structure.
Background
Unmanned aerial vehicle battery is unmanned aerial vehicle's power supply, current unmanned aerial vehicle battery have be with the fuselage integration, undetachable, or through the screw fixation, inconvenient dismantlement, the former has improved the security of organism, but can't prolong unmanned aerial vehicle's live time through changing the battery, the latter then is inconvenient installation and dismantlement, and twist the screw back many times, cause the screw smooth silk easily, this has just made the battery more difficult to change, current unmanned aerial vehicle lacks solar charging device, can not use on one side to charge.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle removable battery mounting structure to solve the problem that proposes in the above-mentioned background art.
In order to solve the technical problem, the utility model provides a following technical scheme: an unmanned aerial vehicle detachable battery mounting structure comprises a body, a battery assembly and a solar panel assembly, wherein the battery assembly is arranged on the inner wall of one side of the body, the battery assembly comprises a battery bin, a wiring jack, a battery body, a wiring plug, a connecting block, a first sliding groove, a first spring, a first stop block, a sliding block, a baffle plate, a second sliding groove, a first limiting groove and a containing groove, the battery bin is arranged on the inner wall of one side of the body, the battery body is sleeved on the inner wall of one side of the battery bin, the connecting block is fixedly connected to the outer wall of one side of the battery body, the first sliding groove is formed in the inner wall of one side of the connecting block, the first spring is fixedly connected to the inner wall of the bottom end of the first sliding groove, the first stop block is slidably connected to the inner wall of one side of the first sliding groove, and one end of, a sliding block is fixedly connected to the outer wall of one side of the first stop block, a baffle is fixedly connected to the outer wall of one side of the connecting block, a second sliding groove is formed in the outer wall of one side of the baffle in a penetrating mode, the sliding block is connected to the inner wall of one side of the second sliding groove in a sliding mode, and a solar panel assembly is arranged on the outer wall of the top end of the machine body;
the solar panel component comprises a slide rail, a fixed frame, a solar panel body, a second stop block, a pressing block, a second limiting groove, a second spring, a limiting block, a third stop block, an elastic contact and an opening, wherein the second limiting groove is formed in the outer wall of the top end of the machine body, the second spring is fixedly connected to the inner wall of the bottom end of the second limiting groove, the limiting block is slidably connected to the inner wall of one side of the second limiting groove, one end of the second spring is fixedly connected to the outer wall of the bottom end of the limiting block, the third stop block is fixedly connected to the outer wall of the top end of the limiting block, and the third stop block is slidably connected to the inner wall of one side of the second limiting.
Furthermore, wiring jacks are symmetrically arranged on the inner wall of one side of the battery compartment, wiring plugs are symmetrically fixed on the outer wall of one side of the battery body, and the wiring plugs are inserted into the wiring jacks.
Furthermore, a first limit groove is formed in the inner wall of the top end of the battery compartment, and the first stop block is connected to the inner wall of one side of the first limit groove in a clamping mode.
Furthermore, an accommodating groove is formed in the inner wall of one side of the battery compartment, and the baffle is arranged on the inner wall of one side of the accommodating groove.
Further, fixedly connected with slide rail on the top outer wall of fuselage, sliding connection has fixed frame on one side inner wall of slide rail, fixedly connected with solar panel body on one side inner wall of fixed frame, fixedly connected with second dog on one side outer wall of fixed frame, the opening has been seted up on one side outer wall of second dog, fixedly connected with briquetting on one side outer wall of fixed frame.
Furthermore, elastic contacts are symmetrically arranged on the outer wall of the top end of the machine body.
Compared with the prior art, the utility model discloses the beneficial effect who reaches is: the utility model discloses a compare in current unmanned aerial vehicle battery structure, the battery of design is detachable, under the prerequisite of having guaranteed the good leakproofness of organism, the battery structure of design dismantles conveniently, changes simply, the utility model discloses a solar panel component can be at the in-process that unmanned aerial vehicle used, the supplementary electric energy that lasts, very big improvement unmanned aerial vehicle's live time, the structural design of its snap-on, the dismantlement and the maintenance of the subassembly of being convenient for.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
fig. 1 is a schematic view of the overall three-dimensional structure of the present invention;
fig. 2 is a schematic side view and sectional structure diagram of the battery assembly of the present invention;
FIG. 3 is a side view and sectional structural diagram of the body of the present invention;
FIG. 4 is a side view and sectional structure of the fixing frame of the present invention;
in the figure: 1. a body; 2. a battery assembly; 3. a solar panel assembly; 21. a battery compartment; 22. a wiring jack; 23. a battery body; 24. a wiring plug; 25. connecting blocks; 26. a first chute; 27. a first spring; 28. a first stopper; 29. a slider; 210. a baffle plate; 211. a second chute; 212. a first limit groove; 213. accommodating grooves; 31. a slide rail; 32. a fixing frame; 33. a solar panel body; 34. a second stopper; 35. briquetting; 36. a second limit groove; 37. a second spring; 38. a limiting block; 39. a third stopper; 310. an elastic contact; 311. and (6) opening.
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 efforts belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: an unmanned aerial vehicle detachable battery mounting structure comprises a machine body 1, a battery component 2 and a solar panel component 3, wherein the battery component 2 is arranged on the inner wall of one side of the machine body 1, the battery component 2 comprises a battery compartment 21, a wiring jack 22, a battery body 23, a wiring plug 24, a connecting block 25, a first sliding chute 26, a first spring 27, a first stop dog 28, a sliding block 29, a baffle 210, a second sliding chute 211, a first limiting groove 212 and a holding groove 213, the battery compartment 21 is arranged on the inner wall of one side of the machine body 1, the battery body 23 is sleeved on the inner wall of one side of the battery compartment 21, the connecting block 25 is fixedly connected on the outer wall of one side of the battery body 23, the first sliding chute 26 is arranged on the inner wall of one side of the connecting block 25, the first spring 27 is fixedly connected on the inner wall of the bottom end of the first sliding chute 26, the first stop dog 28 is slidably connected on the inner wall of one side of the first, the outer wall of one side of the first stop block 28 is fixedly connected with a sliding block 29, the outer wall of one side of the connecting block 25 is fixedly connected with a baffle 210, the outer wall of one side of the baffle 210 is provided with a second sliding groove 211 in a penetrating manner, the sliding block 29 is connected to the inner wall of one side of the second sliding groove 211 in a sliding manner, and the outer wall of the top end of the machine body 1 is provided with a solar panel assembly 3;
the solar panel component 3 comprises a slide rail 31, a fixing frame 32, a solar panel body 33, a second stopper 34, a pressing block 35, a second limiting groove 36, a second spring 37, a limiting block 38, a third stopper 39, an elastic contact 310 and a notch 311, wherein the outer wall of the top end of the machine body 1 is provided with the second limiting groove 36, the inner wall of the bottom end of the second limiting groove 36 is fixedly connected with the second spring 37, the inner wall of one side of the second limiting groove 36 is slidably connected with the limiting block 38, one end of the second spring 37 is fixedly connected to the outer wall of the bottom end of the limiting block 38, the outer wall of the top end of the limiting block 38 is fixedly connected with the third stopper 39, and the third stopper 39 is slidably connected to the inner wall of one side of the second limiting groove; the inner wall of one side of the battery compartment 21 is symmetrically provided with wiring jacks 22, the outer wall of one side of the battery body 23 is symmetrically fixed with wiring plugs 24, and the wiring plugs 24 are inserted into the wiring jacks 22 and used for conducting a circuit; a first limit groove 212 is formed on the inner wall of the top end of the battery compartment 21, and the first stopper 28 is connected to the inner wall of one side of the first limit groove 212 in a clamping manner and used for fixing the battery body 23; an accommodating groove 213 is formed in the inner wall of one side of the battery compartment 21, and the baffle 210 is arranged on the inner wall of one side of the accommodating groove 213, so that the baffle 210 and the machine body 1 are integrated, the appearance of the machine body 1 is attractive, and the waterproof performance is improved; the sliding rail 31 is fixedly connected to the outer wall of the top end of the machine body 1, the fixing frame 32 is slidably connected to the inner wall of one side of the sliding rail 31, the solar panel body 33 is fixedly connected to the inner wall of one side of the fixing frame 32 and used for charging the battery body 23, the second stopper 34 is fixedly connected to the outer wall of one side of the fixing frame 32, the opening 311 is formed in the outer wall of one side of the second stopper 34 and convenient for taking down the fixing frame 32, and the pressing block 35 is fixedly connected to the outer wall of one side of the fixing frame 32 and used for pressing the third stopper 39 when the fixing frame 32 is; elastic contacts 310 are symmetrically arranged on the outer wall of the top end of the machine body 1 and used for being connected with wiring contacts below the solar panel body 33 to realize circuit putting-in and conducting;
when the battery assembly 2 of the present invention is disassembled, the sliding block 29 slides downwards along the second sliding groove 211 on the baffle 210, at this time, the first stopper 28 slides downwards along the first sliding groove 26 on the connecting block 25 to separate from the first limiting groove 212, and compresses the first spring 27, the battery body 23 is drawn out along the battery compartment 21, the wiring plug 24 separates from the wiring jack 22, the baffle 210 separates from the accommodating groove 213, and the disassembly of the battery assembly 2 is completed; during installation, the sliding block 29 slides downwards along the second sliding groove 211 on the baffle 210, the battery body 23 is inserted inwards along the battery compartment 21, after the battery body is completely inserted, the sliding block 29 is loosened, and under the reset action of the first spring 27, the first stop block 28 pops out and is clamped with the first limiting groove 212, so that the installation is completed; when the solar panel assembly 3 is installed, the pressing block 35 is inserted into a gap between the third stopper 39 and the slide rail 31, the fixing frame 32 and the solar panel body 33 thereon are inserted along the slide rail 31, at this time, the fixing frame 32 presses down the third stopper 39, the third stopper 39 drives the stopper 38 to compress the second spring 37 along the second limiting groove 36, when the pressing block 35 reaches the bottom end of the slide rail 31, under the resetting action of the second spring 37, the stopper 38 drives the third stopper 39 to pop out along the second limiting groove 36 and abut against the second stopper 34, the fixing frame 32 is clamped in the slide rail 31, and at this time, the elastic contact 310 is conducted with the bottom end of the solar panel body 33, and installation is completed; when the fixing frame is disassembled, the third stop block 39 in the notch 311 is pressed, the second stop block 34 is drawn out along the slide rail 31, the fixing frame 32 is driven to slide out, and the disassembling is completed.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle removable battery mounting structure, includes fuselage (1), battery pack (2) and solar panel component (3), its characterized in that: the battery pack comprises a machine body (1), wherein a battery assembly (2) is arranged on the inner wall of one side of the machine body (1), the battery assembly (2) comprises a battery bin (21), a wiring jack (22), a battery body (23), a wiring plug (24), a connecting block (25), a first sliding groove (26), a first spring (27), a first stop block (28), a sliding block (29), a baffle (210), a second sliding groove (211), a first limiting groove (212) and a containing groove (213), the battery bin (21) is arranged on the inner wall of one side of the machine body (1), the battery body (23) is sleeved on the inner wall of one side of the battery bin (21), the connecting block (25) is fixedly connected on the outer wall of one side of the battery body (23), the first sliding groove (26) is arranged on the inner wall of one side of the connecting block (25), and the first spring (27) is fixedly connected on the, a first stop block (28) is connected to the inner wall of one side of the first sliding groove (26) in a sliding mode, one end of a first spring (27) is fixedly connected to the outer wall of the bottom end of the first stop block (28), a sliding block (29) is fixedly connected to the outer wall of one side of the first stop block (28), a baffle (210) is fixedly connected to the outer wall of one side of the connecting block (25), a second sliding groove (211) is formed in the outer wall of one side of the baffle (210) in a penetrating mode, the sliding block (29) is connected to the inner wall of one side of the second sliding groove (211) in a sliding mode, and a solar panel assembly (3) is arranged on the outer wall of the;
the solar panel component (3) comprises a slide rail (31), a fixed frame (32), a solar panel body (33), a second stop block (34), a pressing block (35), a second limiting groove (36), a second spring (37), a limiting block (38), a third stop block (39), an elastic contact (310) and a notch (311), a second limit groove (36) is arranged on the outer wall of the top end of the machine body (1), a second spring (37) is fixedly connected on the inner wall of the bottom end of the second limit groove (36), a limiting block (38) is connected on the inner wall of one side of the second limiting groove (36) in a sliding way, one end of the second spring (37) is fixedly connected to the outer wall of the bottom end of the limiting block (38), a third stop block (39) is fixedly connected on the outer wall of the top end of the limiting block (38), and the third stop block (39) is connected on the inner wall of one side of the second limit groove (36) in a sliding way.
2. The detachable battery installation structure of an unmanned aerial vehicle according to claim 1, wherein: the battery box is characterized in that wiring jacks (22) are symmetrically arranged on the inner wall of one side of the battery bin (21), wiring plugs (24) are symmetrically fixed on the outer wall of one side of the battery body (23), and the wiring plugs (24) are inserted into the wiring jacks (22).
3. The detachable battery installation structure of an unmanned aerial vehicle according to claim 1, wherein: a first limit groove (212) is formed in the inner wall of the top end of the battery bin (21), and the first stop block (28) is connected to the inner wall of one side of the first limit groove (212) in a clamping mode.
4. The detachable battery installation structure of an unmanned aerial vehicle according to claim 1, wherein: holding tank (213) have been seted up on one side inner wall of battery compartment (21), and baffle (210) set up on one side inner wall of holding tank (213).
5. The detachable battery installation structure of an unmanned aerial vehicle according to claim 1, wherein: fixedly connected with slide rail (31) on the top outer wall of fuselage (1), sliding connection has fixed frame (32) on the one side inner wall of slide rail (31), fixedly connected with solar panel body (33) on the one side inner wall of fixed frame (32), fixedly connected with second dog (34) on the one side outer wall of fixed frame (32), opening (311) have been seted up on the one side outer wall of second dog (34), fixedly connected with briquetting (35) on the one side outer wall of fixed frame (32).
6. The detachable battery installation structure of an unmanned aerial vehicle according to claim 1, wherein: elastic contacts (310) are symmetrically arranged on the outer wall of the top end of the machine body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022125643.2U CN212751028U (en) | 2020-09-25 | 2020-09-25 | Unmanned aerial vehicle removable battery mounting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022125643.2U CN212751028U (en) | 2020-09-25 | 2020-09-25 | Unmanned aerial vehicle removable battery mounting structure |
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| Publication Number | Publication Date |
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| CN212751028U true CN212751028U (en) | 2021-03-19 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202022125643.2U Active CN212751028U (en) | 2020-09-25 | 2020-09-25 | Unmanned aerial vehicle removable battery mounting structure |
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| CN (1) | CN212751028U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023168885A1 (en) * | 2022-03-10 | 2023-09-14 | 惠州亿纬锂能股份有限公司 | Quickly installable/detachable unmanned aerial vehicle battery pack and unmanned aerial vehicle |
-
2020
- 2020-09-25 CN CN202022125643.2U patent/CN212751028U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023168885A1 (en) * | 2022-03-10 | 2023-09-14 | 惠州亿纬锂能股份有限公司 | Quickly installable/detachable unmanned aerial vehicle battery pack and unmanned aerial vehicle |
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