CN212231135U - Aerial charging device of unmanned aerial vehicle - Google Patents
Aerial charging device of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN212231135U CN212231135U CN202021250202.9U CN202021250202U CN212231135U CN 212231135 U CN212231135 U CN 212231135U CN 202021250202 U CN202021250202 U CN 202021250202U CN 212231135 U CN212231135 U CN 212231135U
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- unmanned aerial
- aerial vehicle
- charging
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- control module
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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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
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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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/16—Information or communication technologies improving the operation of electric vehicles
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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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/16—Information or communication technologies improving the operation of electric vehicles
- Y02T90/167—Systems integrating technologies related to power network operation and communication or information technologies for supporting the interoperability of electric or hybrid vehicles, i.e. smartgrids as interface for battery charging of electric vehicles [EV] or hybrid vehicles [HEV]
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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
- Y04—INFORMATION OR COMMUNICATION TECHNOLOGIES HAVING AN IMPACT ON OTHER TECHNOLOGY AREAS
- Y04S—SYSTEMS INTEGRATING TECHNOLOGIES RELATED TO POWER NETWORK OPERATION, COMMUNICATION OR INFORMATION TECHNOLOGIES FOR IMPROVING THE ELECTRICAL POWER GENERATION, TRANSMISSION, DISTRIBUTION, MANAGEMENT OR USAGE, i.e. SMART GRIDS
- Y04S30/00—Systems supporting specific end-user applications in the sector of transportation
- Y04S30/10—Systems supporting the interoperability of electric or hybrid vehicles
- Y04S30/12—Remote or cooperative charging
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- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model discloses an aerial charging device of unmanned aerial vehicle, it has flexible solar cell panel just to receive unmanned aerial vehicle's surface paste receive unmanned aerial vehicle's inside to be equipped with battery A, receive unmanned aerial vehicle's top to be equipped with the interface that charges, and battery A is communication module and orientation module power supply, and communication module is connected to remote control terminal, and unmanned aerial vehicle's inside of charging is equipped with energy storage module, energy storage module and charging coil electric connection, and unmanned aerial vehicle's bottom of charging is equipped with a bulge just the charging coil is inlayed the bottom of bulge, the charging coil faces receive unmanned aerial vehicle's the interface that charges, the inside of fuselage is equipped with control module and battery B, is equipped with electric quantity detection module between control module and the battery B. The output end of the control module is electrically connected with the communication module and the positioning module. The utility model discloses effectively carry out long-range power supply, still can inform remote control terminal when the electric quantity is not enough.
Description
Technical Field
The utility model relates to an aerial unmanned aerial vehicle technique field especially relates to an aerial charging device of unmanned aerial vehicle.
Background
At present, unmanned aerial vehicles are widely applied in the fields of field construction, exploration, transportation, tourism, rescue and the like, and mainly play roles in observing field conditions, acquiring information, transmitting a small amount of materials and the like. The system has unique advantages, is not limited by terrain, can quickly reach the site of a fault position, even a place with rare occurrence, and can carry out close-range observation; the video and image data are sent to relevant departments through shooting and camera equipment, so that technicians of the relevant departments can analyze and judge the site, or materials can be rapidly conveyed to the site to carry out rescue, and a good effect is achieved.
However, the current unmanned aerial vehicle has the following problems:
firstly, in the process of inspection and observation, as repeated and long-time suspended observation is needed to collect image data, the energy consumption is very high, and the capacity of a battery is limited, the working time is limited; secondly, if the electric quantity of the unmanned aerial vehicle is exhausted, the unmanned aerial vehicle must return to the ground and be recharged or the battery is replaced, and because the operation place of the unmanned aerial vehicle is far away from the landing and charging place, the unmanned aerial vehicle needs to consume a large amount of time in the processes of returning to the ground, charging or replacing the battery and recovering operation in the process of returning to the operation place, and the work is interrupted, so that the normal and continuous operation in the air is delayed.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
The utility model provides a not enough to prior art, the utility model provides an aerial charging device of unmanned aerial vehicle has solved among the prior art unmanned vehicles and is returning ground, charging process or change battery process to and resume the operation again, all need consume a large amount of time, and the work of breaking out delays the normal continuous problem of going on of aerial operation.
(II) technical scheme
In order to achieve the above object, the utility model provides a following technical scheme: an aerial charging device of an unmanned aerial vehicle comprises a powered unmanned aerial vehicle and a charging unmanned aerial vehicle, wherein a flexible solar cell panel is stuck on the upper surface of the powered unmanned aerial vehicle, a storage battery A is arranged in the powered unmanned aerial vehicle, the top of the power receiving unmanned aerial vehicle is provided with a charging interface, the storage battery A supplies power for the communication module and the positioning module, the communication module is connected to the remote control terminal, the remote control terminal drives the charging unmanned aerial vehicle, the charging unmanned aerial vehicle is internally provided with an energy storage module, the energy storage module is electrically connected with a charging coil, the bottom of the charging unmanned aerial vehicle is provided with a bulge, the charging coil is embedded at the bottom of the bulge, the charging coil faces the charging interface of the power receiving unmanned aerial vehicle, a control module and a storage battery B are arranged inside the body of the power receiving unmanned aerial vehicle, and an electric quantity detection module is arranged between the control module and the storage battery B. The output end of the control module is electrically connected with the communication module and the positioning module.
Preferably, receive unmanned aerial vehicle and charge unmanned aerial vehicle and all include fuselage and a plurality of rotor, the fuselage is cylindrical structure just the side of fuselage is equipped with a plurality of slope branches along its even interval of circumferencial direction, and the high-end of every slope branch all is equipped with rotates the motor, the output shaft that rotates the motor passes the tip of slope branch just the output shaft fixed connection who rotates the motor is to the rotor.
Preferably, the bilateral symmetry of the bottom of fuselage is equipped with the buffer frame, is buffer frame A and buffer frame B respectively, buffer frame A and buffer frame B are the trapezium structure.
Preferably, the side of fuselage is equipped with a plurality of infrared sensor along its circumferencial direction even interval, is equipped with an infrared sensor between two adjacent slope branches, infrared sensor with control module electric connection, control module's output is connected to the rotating electrical machines.
Preferably, the storage battery B supplies power to the control module and the rotating motor, and the storage battery also supplies power to the communication module and the positioning module.
(III) advantageous effects
The utility model provides an aerial charging device of unmanned aerial vehicle possesses following beneficial effect: the utility model discloses powered unmanned aerial vehicle and charging unmanned aerial vehicle have been set up, powered unmanned aerial vehicle's inside is equipped with control module, battery A and battery B, battery B plays normal power supply effect, battery B supplies power for control module, communication module and orientation module when powered unmanned aerial vehicle normally works, electric quantity detection module detects the electric quantity of battery B, when the electric quantity is not enough, control module enables battery A to supply power for communication module and orientation module, can't inform the remote monitoring terminal when avoiding the electric quantity is not enough, battery A still supplies power through the flexible solar cell panel that sets up at the top of powered unmanned aerial vehicle, thus in time charge battery A when battery A is not enough, keep communication function, charging unmanned aerial vehicle finds powered unmanned aerial vehicle through orientation module and communication module, utilize the charge coil of its bottom to supply power for battery B, avoid the line connection, be convenient for transmit electricity.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a block diagram of the present invention.
In the figure: 1. a powered unmanned aerial vehicle; 2. charging the unmanned aerial vehicle; 3. a charging interface; 4. a projection; 5. a charging coil; 6. an infrared sensor; 7. a rotor; 8. rotating the motor; 9. a remote control terminal; 10. a flexible solar panel; 11. a communication module; 12. a positioning module; 13. a storage battery A; 14. a storage battery B; 15. an electric quantity detection module; 16. a control module; 17. a buffer frame A; 18. and a buffer frame B.
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 work belong to the protection scope of the present invention.
As shown in fig. 1 and 2, the following examples are proposed:
an unmanned aerial vehicle aerial charging device comprises a powered unmanned aerial vehicle 1 and a charging unmanned aerial vehicle 2, wherein a flexible solar cell panel 10 is pasted on the upper surface of the powered unmanned aerial vehicle 1, a storage battery A13 is arranged inside the powered unmanned aerial vehicle 1, a charging interface 3 is arranged at the top of the powered unmanned aerial vehicle 1, the storage battery A13 supplies power to a communication module 11 and a positioning module 12, the communication module 11 is connected to a remote control terminal 9 and the remote control terminal 9 drives the charging unmanned aerial vehicle 2, an energy storage module is arranged inside the charging unmanned aerial vehicle 2 and is electrically connected with a charging coil 5, the bottom of the charging unmanned aerial vehicle 2 is provided with a bulge part 4, the charging coil 5 is embedded at the bottom of the bulge part 4, the charging coil 5 faces the charging interface 3 of the powered unmanned aerial vehicle 1, and the inside of the charging unmanned aerial vehicle 1 and 2 are provided with a control module 16 and a storage battery B14, an electric quantity detection module 15 is arranged between the control module 16 and the storage battery B14. The output end of the control module 16 is electrically connected to the communication module 11 and the positioning module 12.
In this embodiment, receive electric unmanned aerial vehicle 1 and charge unmanned aerial vehicle 2 and all include fuselage and a plurality of rotor 7, the fuselage is cylindrical structure just the side of fuselage is equipped with a plurality of slope branches along its even interval of circumferencial direction, and the high-end of every slope branch all is equipped with rotates motor 8, the output shaft that rotates motor 8 passes the tip of slope branch just the output shaft fixed connection who rotates motor 8 is to rotor 7. The side body of fuselage sets up a plurality of slope branches, and the tip of slope branch is equipped with rotates motor 8, rotates motor 8's output shaft fixed connection to rotor 7, and the rotation that rotates motor 8 drives rotor 7 and rotates, provides lift to receiving unmanned aerial vehicle 1 and unmanned aerial vehicle 2 that charges then.
In this embodiment, the two sides of the bottom of the fuselage are symmetrically provided with a buffer frame, namely a buffer frame a17 and a buffer frame B18, and the buffer frame a17 and the buffer frame B18 are in a trapezoidal structure. When the unmanned aerial vehicle lands, the buffer frame A17 and the buffer frame B18 strengthen the stability of the whole device.
In this embodiment, the side of fuselage is equipped with a plurality of infrared sensor 6 along its circumferencial direction evenly spaced, is equipped with an infrared sensor 6 between two adjacent slope branches, infrared sensor 6 with control module 16 electric connection, control module 16's output is connected to and rotates motor 8. The infrared sensor 6 has a model number GP2Y0a02YK 0F. It should be noted that, the calculation process of determining the position of the target location through the control module, the navigation system and the communication system of the unmanned aerial vehicle belongs to the existing mature technology in the field of unmanned aerial vehicles, and therefore detailed processes are not repeated herein.
In the present exemplary embodiment, the battery B14 supplies power to the control module 16 and to the rotary electric machine 8, the battery B14 also supplies power to the communication module 11 and to the positioning module 12, and the battery B14 serves as the main power supply.
In fig. 1-2, the utility model provides a powered unmanned aerial vehicle 1 and a charging unmanned aerial vehicle 2, the powered unmanned aerial vehicle 1 is internally provided with a control module 16, a storage battery a13 and a storage battery B14, the storage battery B14 plays a normal power supply role, the storage battery B14 supplies power to the control module 16, the communication module 11 and the positioning module 12 when the powered unmanned aerial vehicle 1 is in normal operation, the power detection module 15 detects the power of the storage battery B14, when the power is insufficient, the control module 16 starts the storage battery a13 to supply power to the communication module 11 and the positioning module 12, the remote control terminal 9 cannot be informed when the power is insufficient, the storage battery a13 also supplies power through the flexible solar panel 10 arranged on the top of the powered unmanned aerial vehicle 1, thus, the storage battery a13 is charged in time when the power of the storage battery a13 is insufficient, the communication function is maintained, the charging unmanned aerial vehicle 2 finds the powered unmanned, and the charging coil 5 at the bottom of the battery B is used for supplying power to the storage battery B, so that connection is avoided, and power transmission is facilitated.
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. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
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 invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides an aerial charging device of unmanned aerial vehicle which characterized in that: the unmanned aerial vehicle charging system comprises a power receiving unmanned aerial vehicle and a charging unmanned aerial vehicle, wherein a flexible solar cell panel is pasted on the upper surface of the power receiving unmanned aerial vehicle, a storage battery A is arranged in the power receiving unmanned aerial vehicle, a charging interface is arranged at the top of the power receiving unmanned aerial vehicle, the storage battery A supplies power for a communication module and a positioning module, the communication module is connected to a remote control terminal and drives the charging unmanned aerial vehicle by the remote control terminal, an energy storage module is arranged in the charging unmanned aerial vehicle and is electrically connected with a charging coil, a bulge part is arranged at the bottom of the charging unmanned aerial vehicle, the charging coil is embedded at the bottom of the bulge part, the charging coil faces the charging interface of the power receiving unmanned aerial vehicle, a control module and a storage battery B are arranged in the body of the power receiving unmanned aerial, the output end of the control module is electrically connected with the communication module and the positioning module.
2. An aerial charging device for unmanned aerial vehicles according to claim 1, wherein: receive unmanned aerial vehicle and charge unmanned aerial vehicle and all include fuselage and a plurality of rotor, the fuselage is cylindrical structure just the side of fuselage is equipped with a plurality of slope branches along its even interval of circumferencial direction, and the high-end of every slope branch all is equipped with rotates the motor, the output shaft that rotates the motor passes the tip of slope branch just the output shaft fixed connection who rotates the motor is to the rotor.
3. An aerial charging device for unmanned aerial vehicles according to claim 2, wherein: the two sides of the bottom of the machine body are symmetrically provided with buffer frames, namely a buffer frame A and a buffer frame B, and the buffer frames A and B are of a trapezoidal structure.
4. An aerial charging device for unmanned aerial vehicles according to claim 2, wherein: the side of fuselage is equipped with a plurality of infrared sensor along its circumferencial direction even interval, is equipped with an infrared sensor between two adjacent slope branches, infrared sensor with control module electric connection, control module's output is connected to the rotation motor.
5. An aerial charging device for unmanned aerial vehicles according to claim 1, wherein: the storage battery B supplies power to the control module and the rotating motor, and the storage battery also supplies power to the communication module and the positioning module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021250202.9U CN212231135U (en) | 2020-06-30 | 2020-06-30 | Aerial charging device of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021250202.9U CN212231135U (en) | 2020-06-30 | 2020-06-30 | Aerial charging device of unmanned aerial vehicle |
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| Publication Number | Publication Date |
|---|---|
| CN212231135U true CN212231135U (en) | 2020-12-25 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021250202.9U Expired - Fee Related CN212231135U (en) | 2020-06-30 | 2020-06-30 | Aerial charging device of unmanned aerial vehicle |
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| CN (1) | CN212231135U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20210217318A1 (en) * | 2018-01-25 | 2021-07-15 | Dushan Kandasamy | Autonomous aerial vehicle system |
| CN114044140A (en) * | 2021-11-22 | 2022-02-15 | 北部湾大学 | Unmanned aerial vehicle for water operation |
-
2020
- 2020-06-30 CN CN202021250202.9U patent/CN212231135U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20210217318A1 (en) * | 2018-01-25 | 2021-07-15 | Dushan Kandasamy | Autonomous aerial vehicle system |
| CN114044140A (en) * | 2021-11-22 | 2022-02-15 | 北部湾大学 | Unmanned aerial vehicle for water operation |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201225 Termination date: 20210630 |
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| CF01 | Termination of patent right due to non-payment of annual fee |