CN218917644U - Beidou unmanned aerial vehicle tracker - Google Patents
Beidou unmanned aerial vehicle tracker Download PDFInfo
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- CN218917644U CN218917644U CN202222798483.7U CN202222798483U CN218917644U CN 218917644 U CN218917644 U CN 218917644U CN 202222798483 U CN202222798483 U CN 202222798483U CN 218917644 U CN218917644 U CN 218917644U
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- beidou
- aerial vehicle
- unmanned aerial
- vehicle tracker
- solar cell
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Abstract
The utility model discloses a Beidou unmanned aerial vehicle tracker, which relates to the technical field of unmanned aerial vehicle trackers and aims to solve the problems that only one storage battery is available in the existing unmanned aerial vehicle tracker, the endurance performance of the storage battery is limited, the storage battery does not have a photovoltaic charging structure and function, and the practicability is to be improved. The photovoltaic charging device has the advantages of being capable of conducting photovoltaic charging and high in endurance performance.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle trackers, in particular to a Beidou unmanned aerial vehicle tracker.
Background
Unmanned aerial vehicle is as an aircraft, and its technological content is high, belongs to high-tech product commodity, and unmanned aerial vehicle can real-time control unmanned aerial vehicle's position in the monitoring website on ground when flying, and the flight state of unmanned aerial vehicle is convenient for be mastered, and unmanned aerial vehicle tracker even realizes one of unmanned aerial vehicle position monitoring's equipment, extensively installs on unmanned aerial vehicle's of contemporary fuselage.
Only one storage battery is arranged in the existing unmanned aerial vehicle tracker, the endurance performance of the unmanned aerial vehicle tracker is limited, the unmanned aerial vehicle tracker does not have a photovoltaic charging structure and function, and the practicability is to be improved.
Disclosure of Invention
The utility model aims to provide a Beidou unmanned aerial vehicle tracker which can be subjected to photovoltaic charging and has high endurance performance.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
the utility model provides a big dipper unmanned aerial vehicle tracker, includes the fixing base, be provided with the battery mounting groove on the inside bottom end face of fixing base, and the inside fixed mounting of battery mounting groove has the battery, the battery is provided with two, fixedly connected with a plurality of connecting blocks on the surface of fixing base, fixedly mounted with solar cell panel on the connecting block surface of corresponding position department, solar cell panel and battery electric connection, the inside fixed mounting of fixing base has the circuit board, circuit board and battery electric connection, the inside of fixing base is provided with big dipper multimode antenna.
Through adopting above-mentioned technical scheme, can utilize two batteries to provide the power for inner structure in turn, utilize solar cell panel to supply the electric energy for idle battery simultaneously, the effectual continuation of the journey performance that improves this tracker.
Further, two solar panels are arranged and symmetrically distributed on two sides of the fixing seat.
By adopting the technical scheme, the electric energy supplementing order can be stably ensured.
Further, the Beidou multimode antenna is electrically connected with the circuit board.
By adopting the technical scheme, the stability of positioning and short message sending is ensured.
Further, the circuit board comprises a Beidou positioning module, a GPS positioning module, a Bluetooth module and a 4G full-network communication module.
By adopting the technical scheme, the Beidou positioning module and the GPS positioning module can be utilized to perform double-star positioning, and meanwhile, the 4G full-network communication module can be utilized to perform communication operation.
Further, an electrical connection seat is fixedly arranged on the side surface of the fixing seat.
By adopting the technical scheme, the data can be conveniently conducted to the tracker.
Further, an upper cover is buckled on the upper port cover of the fixed seat.
By adopting the technical scheme, the structural firmness and the working stability of the tracker are ensured.
In summary, the beneficial technical effects of the utility model are as follows:
according to the utility model, by arranging the two storage batteries and the two solar panels, the two storage batteries can be used for supplying electric energy to the tracker in turn, meanwhile, the solar panels are used for supplementing electric energy to the other storage battery, the structure can effectively improve the cruising performance of the tracker, meanwhile, the 4G full-network communication module arranged on the circuit board can enable the tracker to realize 4G network communication in a 4G network coverage area, when the tracker is out of coverage, the Beidou multimode antenna can be used for transmitting position data in a short message mode, and the Beidou positioning module and the GPS positioning module in the circuit board can enable the tracker to realize double-star positioning operation.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
fig. 2 is a schematic bottom view of a three-dimensional structure according to the present utility model.
In the figure: 1. a fixing seat; 2. a connecting block; 3. a solar cell panel; 4. a storage battery; 5. a battery limit bracket; 6. an antenna mounting bracket; 7. a Beidou multimode antenna; 8. an upper cover; 9. an electrical connection base; 10. a circuit board.
Detailed Description
The process according to the utility model is described in further detail below with reference to the accompanying drawings.
Referring to fig. 1 and 2, big dipper unmanned aerial vehicle tracker, including fixing base 1, be provided with the battery mounting groove on the inside bottom end face of fixing base 1, and the inside fixed mounting of battery mounting groove has battery 4, battery 4 is provided with two, fixedly connected with a plurality of connecting blocks 2 on the surface of fixing base 1, fixedly mounted with solar cell panel 3 on the connecting block 2 surface of corresponding position department, solar cell panel 3 and battery 4 electric connection, solar cell panel 3 is provided with two, and two solar cell panel 3 symmetric distributions are in the both sides of fixing base 1, wherein through setting up two battery 4 and two solar cell panel 3, can utilize two battery 4 to provide the electric energy for this tracker in turn, utilize solar cell panel 3 to supply the electric energy for another battery 4 simultaneously, this structure can effectually promote the continuation of the journey performance of tracker.
Referring to fig. 1, the circuit board 10 is fixedly installed in the interior of the fixing base 1, the circuit board 10 is electrically connected with the storage battery 4, the Beidou multimode antenna 7 is arranged in the interior of the fixing base 1 and electrically connected with the circuit board 10, the Beidou multimode antenna 7 comprises a Beidou positioning module, a GPS positioning module, a Bluetooth module and a 4G full-network communication module, the 4G full-network communication module arranged on the circuit board 10 can enable the tracker to realize 4G network communication in a 4G network coverage area, when the coverage area is exceeded, the Beidou multimode antenna 7 can be utilized to send position data in a short message mode, and the Beidou positioning module and the GPS positioning module in the circuit board 10 can enable the tracker to realize double-star positioning operation.
Referring to fig. 1 and 2, an electrical socket 9 is fixedly installed on a side surface of the fixing base 1, and an upper cover 8 is installed to an upper port cover button of the fixing base 1, wherein the upper cover 8 can be utilized to improve the working stability and firmness of the tracker.
Working principle: when the intelligent tracking instrument is used, the tracking instrument is firstly installed at a designated position, normal work can be carried out at the moment, the two storage batteries 4 supply power for the circuit board 10 and the Beidou multimode antenna 7 in turn during the work, meanwhile, the solar cell panel 3 arranged outside the fixing seat 1 can supplement electric energy for the idle storage battery 4, the cruising performance of the tracking instrument can be effectively improved, the 4G full-network communication module in the circuit board 10 can enable the tracking instrument to realize 4G network communication in a 4G network coverage area, position information can be stably transmitted to a ground monitoring site, when the coverage area is exceeded, the Beidou multimode antenna 7 can be utilized to send position data in a short message mode, and the Beidou positioning module and the GPS positioning module in the circuit board 10 can enable the tracking instrument to realize double-star positioning operation.
The embodiments of the present utility model are all preferred embodiments of the present utility model, and are not intended to limit the scope of the present utility model in this way, therefore: all equivalent changes in structure, shape and principle of the utility model should be covered in the scope of protection of the utility model.
Claims (6)
1. Big dipper unmanned aerial vehicle tracker, including fixing base (1), its characterized in that: the solar cell panel is characterized in that a cell mounting groove is formed in the inner bottom end face of the fixing seat (1), a storage battery (4) is fixedly mounted in the cell mounting groove, two storage batteries (4) are arranged, a plurality of connecting blocks (2) are fixedly connected to the outer surface of the fixing seat (1), a solar cell panel (3) is fixedly mounted on the outer surface of each connecting block (2) at the corresponding position, the solar cell panel (3) is electrically connected with the storage battery (4), a circuit board (10) is fixedly mounted in the fixing seat (1), the circuit board (10) is electrically connected with the storage battery (4), and a Beidou multimode antenna (7) is arranged in the fixing seat (1).
2. The beidou unmanned aerial vehicle tracker according to claim 1, characterized in that: the solar cell panels (3) are arranged in two, and the two solar cell panels (3) are symmetrically distributed on two sides of the fixing seat (1).
3. The beidou unmanned aerial vehicle tracker according to claim 1, characterized in that: the Beidou multimode antenna (7) is electrically connected with the circuit board (10).
4. The beidou unmanned aerial vehicle tracker according to claim 1, characterized in that: the inside of circuit board (10) includes big dipper positioning module, GPS positioning module, bluetooth module, 4G full network module.
5. The beidou unmanned aerial vehicle tracker according to claim 1, characterized in that: an electrical connection seat (9) is fixedly arranged on the side surface of the fixing seat (1).
6. The beidou unmanned aerial vehicle tracker according to claim 1, characterized in that: an upper cover (8) is buckled on the upper port cover of the fixed seat (1).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202222798483.7U CN218917644U (en) | 2022-10-24 | 2022-10-24 | Beidou unmanned aerial vehicle tracker |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202222798483.7U CN218917644U (en) | 2022-10-24 | 2022-10-24 | Beidou unmanned aerial vehicle tracker |
Publications (1)
Publication Number | Publication Date |
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CN218917644U true CN218917644U (en) | 2023-04-25 |
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Family Applications (1)
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CN202222798483.7U Active CN218917644U (en) | 2022-10-24 | 2022-10-24 | Beidou unmanned aerial vehicle tracker |
Country Status (1)
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CN (1) | CN218917644U (en) |
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2022
- 2022-10-24 CN CN202222798483.7U patent/CN218917644U/en active Active
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