CN216268756U - Charging system for unmanned aerial vehicle wheel patrol - Google Patents
Charging system for unmanned aerial vehicle wheel patrol Download PDFInfo
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- CN216268756U CN216268756U CN202122619494.XU CN202122619494U CN216268756U CN 216268756 U CN216268756 U CN 216268756U CN 202122619494 U CN202122619494 U CN 202122619494U CN 216268756 U CN216268756 U CN 216268756U
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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
- Y02T90/12—Electric charging stations
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Abstract
The utility model relates to the field of charging equipment of unmanned aerial vehicles, in particular to a charging system for unmanned aerial vehicle polling, which comprises a main charging platform, wherein a plurality of charging piles for charging the unmanned aerial vehicles and wind-solar complementary power generation modules for supplying electric energy to the plurality of charging piles are arranged on the main charging platform; still include a plurality of supplies the sub charging platform that unmanned aerial vehicle continued to sail and charge, sub charging platform is located the terminal point of the ability of continuing to sail after unmanned aerial vehicle uses main charging platform to fly as the starting point, and sub charging platform arranges into the ring form around main charging platform, sets up on the sub charging platform one and supplies the electric pile of charging that unmanned aerial vehicle charges and to should fill the complementary power generation module of scene that electric energy provided. The distribution positions of the sub charging platform and the main charging platform can enable a plurality of unmanned aerial vehicles to simultaneously prolong the cruising ability in the longitudinal depth direction, and enable the unmanned aerial vehicles to carry out wheel patrol in the transverse direction and then charge, so that the wheel patrol range of the unmanned aerial vehicles is enlarged.
Description
Technical Field
The utility model relates to the field of charging equipment of unmanned aerial vehicles, in particular to a charging system for unmanned aerial vehicle polling.
Background
Scenes such as a border unmanned area, forest fire control, lake and river water administration and the like need to be subjected to twenty-four-hour uninterrupted inspection on the scene, and abnormal conditions such as fire, illegal boundary crossing and the like in the scene can be found in time through inspection. At present patrol and examine to the environment and generally use unmanned aerial vehicle to carry and go on like infrared camera etc. for the unmanned aerial vehicle who patrols and examines charges by the power supply platform of concentrating the settling, when carrying out electric power patrol and examine if utilizing unmanned aerial vehicle, carries out distributed energy storage through the mode with the complementary electricity generation of scene on the platform that charges to carry out the electric quantity supply to unmanned aerial vehicle, when the unmanned aerial vehicle electric quantity is not enough, let unmanned aerial vehicle automatic fly back and charge.
However, because of unmanned aerial vehicle's battery duration is limited, when unmanned aerial vehicle rounds to patrol the in-process discovery the place ahead unusual and battery duration exhausts, and unmanned aerial vehicle is limited with backstage communication's distance, and current charging platform can't let unmanned aerial vehicle continue to patrol and examine towards the depth direction, and unmanned aerial vehicle's round is patrolled and examined the ability and is lower.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a charging system for unmanned aerial vehicle polling, and solves the problem that the existing charging platform cannot provide large cruising ability for the unmanned aerial vehicle polling.
The charging system for the unmanned aerial vehicle polling in the scheme comprises a main charging platform, wherein a plurality of charging piles for charging the unmanned aerial vehicle and wind-solar complementary power generation modules for supplying power to the plurality of charging piles are arranged on the main charging platform;
still include a plurality of supply sub charging platform that unmanned aerial vehicle continued to sail and charge, sub charging platform is located the terminal point of the ability of continuing to sail after unmanned aerial vehicle uses main charging platform to fly as the starting point, sub charging platform arranges into the ring form around main charging platform, set up on the sub charging platform and supply the electric pile of charging that unmanned aerial vehicle charges and to this wind-solar complementary power generation module that fills electric pile and provide electric energy.
The beneficial effect of this scheme is:
when unmanned aerial vehicle took place to take turns to patrol to duration ability endpoint from main charging platform, let unmanned aerial vehicle fly back main charging platform according to the information received and charge, perhaps when discovering the place ahead unusual needs continue to fly to take turns to patrol, let unmanned aerial vehicle fly to the son charging platform according to the information received and then continue to patrol, patrol the regional abnormal conditions of target, can charge the back to unmanned aerial vehicle through son charging platform, prolong unmanned aerial vehicle duration in vertical depth direction, let unmanned aerial vehicle can take turns to patrol farther region. The distribution position of sub-charging platform and main charging platform can supply a plurality of unmanned aerial vehicles to prolong duration simultaneously in vertical direction of depth, can also let unmanned aerial vehicle go up the round in the transverse direction and patrol the back and charge, increase unmanned aerial vehicle round the scope of patrolling.
Further, the wind-solar hybrid power generation module comprises a solar power generation unit, a wind power generation unit, a battery unit and a charging control unit, wherein the charging control unit controls the solar power generation unit and/or the wind power generation unit to start to generate power, and the charging control unit controls the battery unit to store electric energy.
The beneficial effects are that: wind power generation and solar energy power generation through the wind-solar hybrid power generation module generate electricity, can increase the battery unit and guarantee the required probability of unmanned aerial vehicle flight, let unmanned aerial vehicle can the continuation round of patrolling.
Further, the wind power generation unit comprises a fan, the fan comprises a tower column, two groups of crosses are fixedly arranged at the top end of the tower column, the crosses are coaxially arranged on a central shaft of the tower column, and the end parts of the two crosses, which are located on the same vertical line, are fixedly provided with blades which are rectangular plate-shaped.
The beneficial effects are that: the fan is provided with four blades, and the rectangular plate-shaped blades are used, so that the fan can rotate under the condition of low wind speed, such as breeze.
Further, be equipped with the electromagnetism actuation unit that is used for counterpointing the actuation of charging to unmanned aerial vehicle on filling electric pile, the control unit that charges controls electromagnetism actuation unit circular telegram when unmanned aerial vehicle charges.
The beneficial effects are that: through the electromagnetic attraction unit, can be when unmanned aerial vehicle charges automatic switch-on and actuation unmanned aerial vehicle, avoid unmanned aerial vehicle not to drop during charging, the holding current is stable.
Further, all be equipped with on sub-charging platform and the main charging platform and carry out the first communicator of unmanned aerial vehicle information interaction with backend server, all be equipped with on sub-charging platform and the main charging platform and carry out the second communicator of charging information interaction with unmanned aerial vehicle.
The beneficial effects are that: unmanned aerial vehicle directly carries out the information interaction with sub charging platform and main charging platform, and sub charging platform and main charging platform directly carry out the information interaction with backend server, are convenient for inquire mutual information.
Further, the ground size of the main charging platform is 6m × 24m, and the ground size of the sub-charging platform is 3m × 5 m.
The beneficial effects are that: the size of main charging platform can supply a plurality of unmanned aerial vehicles to use simultaneously, and sub-charging platform's size is less, is convenient for set up to different positions according to the topography.
Further, the rain shelter of L type has set firmly on main charging platform and the sub-charging platform, the horizontal segment of rain shelter is located the top of filling electric pile.
The beneficial effects are that: can avoid filling electric pile rain through rainshelter, keep the continuation of charging.
Further, still include a plurality of limiters that set up on main charging platform and sub-charging platform, the limiter includes a plurality of flexible power pack, flexible power pack is located and can carries out spacing position department to the unmanned aerial vehicle wheel, flexible power signal connection charging control unit, be equipped with on the flexible power pack and carry out spacing gag lever post to the unmanned aerial vehicle wheel, electromagnetism actuation unit is equipped with photosensitive unit towards ground one side department, photosensitive unit signal connection charging control unit.
The beneficial effects are that: after the electromagnetism actuation unit adsorbs unmanned aerial vehicle, unmanned aerial vehicle can shelter from photosensitive unit's illumination to triggering photosensitive unit and sending the illumination signal to the control unit that charges, letting the control unit that charges control flexible power pack when receiving the illumination signal and drive the stop lever and carry on spacingly to the unmanned aerial vehicle wheel, prevent that unmanned aerial vehicle from shifting or being blown because of factors such as wind-force influence in the charging process.
Furthermore, the limiting rod is sleeved with an anti-skidding sleeve, the anti-skidding sleeve is wavy in shape, and the anti-skidding sleeve is located at the end part close to the limiting rod.
The beneficial effects are that: the antiskid cover that the gag lever post overcoat was established to and the wave shape of antiskid cover appearance can improve the gag lever post to the spacing stability of unmanned aerial vehicle wheel.
Drawings
Fig. 1 is a schematic distribution diagram of a main charging platform and sub-charging platforms in a first embodiment of a charging system for unmanned aerial vehicle polling according to the present invention;
fig. 2 is a front view of a tower column in a charging system for unmanned aerial vehicle polling according to an embodiment of the present invention;
fig. 3 is a diagram showing a positional relationship between a retractable power unit and wheels of an unmanned aerial vehicle in a second embodiment of the charging system for the unmanned aerial vehicle polling of the present invention.
Detailed Description
The following is a more detailed description of the present invention by way of specific embodiments.
Reference numerals in the drawings of the specification include: the main charging platform 1, the sub-charging platform 2, the charging pile 3, the tower column 4, the cross 5, the blades 6, the telescopic power unit 7, the limiting rod 8 and the anti-skid sleeve 9.
Example one
A charging system for unmanned aerial vehicle is tourd, as shown in fig. 1: including main charging platform 1, install a plurality of confession unmanned aerial vehicle on the main charging platform 1 and carry out the electric pile 3 that fills that charges and to a plurality of wind-solar complementary power generation modules that fill electric pile 3 and provide the electric energy, the product of the product that the usable current SH-300H model of wind-solar complementary power generation module or the product of selecting other models fills electric pile 3 and corresponds uses current product, no longer gives unnecessary details here.
The unmanned aerial vehicle continuous-flight charging system further comprises a plurality of sub charging platforms 2 for unmanned aerial vehicle continuous-flight charging, the ground size of the main charging platform 1 is 6m multiplied by 24m, the ground size of the sub charging platforms 2 is 3m multiplied by 5m, the ground size refers to the width multiplied by the length of the main charging platform 1 and the sub charging platforms 2, and the main charging platform 1 and the sub charging platforms 2 can be carried out through a cement concrete platform body which is integrated in advance; the sub-charging platform 2 is located close to a subsequent navigation capability end point of the unmanned aerial vehicle from the main charging platform 1, for example, the unmanned aerial vehicle is used for a 30-kilometer cruising (the unmanned aerial vehicle flies for 30 kilometers and must fly back to charge), the sub-charging platform 2 is located 30 kilometers away from the main charging platform 1, the sub-charging platform 2 is arranged into a circular ring shape around the main charging platform 1, namely, the sub-charging platform 2 is distributed around the circular ring shape with the main charging platform 1 as a circle center, and the sub-charging platform 2 is provided with a charging pile 3 for charging the unmanned aerial vehicle and a wind-solar hybrid power generation module for providing electric energy for the charging pile 3.
The wind-solar hybrid power generation module comprises a solar power generation unit, a wind power generation unit, a battery unit and a charging control unit, wherein the solar power generation unit can use a conventional 20KVA solar device, the wind power generation unit can use a conventional 10KVA electromagnetic wind power generation device, the charging control unit controls the solar power generation unit and/or the wind power generation unit to start to generate power, the charging control unit can use a conventional wind-solar hybrid controller, such as HECR series, the charging control unit controls the battery unit to store electric energy, and the battery unit is a conventional storage battery pack.
As shown in fig. 2, the wind power generation unit includes a fan, the fan includes a tower 4, two sets of crosses 5 are fixedly mounted on the top end of the tower 4 through screws and nuts, the crosses 5 are coaxially arranged on the central shaft of the tower 4, the distance between the centers of the crosses 5 is 50cm, the end portions of the two crosses 5 on the same vertical line are fixed with blades 6 through screws, and the blades 6 are rectangular plate-shaped.
The installation is used for counterpointing the electromagnetism actuation unit that charges the actuation on charging pile 3, counterpoint the actuation that charges is set up on charging pile 3 and is gone on with the electromagnetism actuation unit that the actuation position is located same horizontal position on the unmanned aerial vehicle to let unmanned aerial vehicle's the interface that charges and the interface that charges on charging pile 3 charge to closing, electromagnetism actuation unit can use current electro-magnet, the electro-magnet of MZS1 series model for example, the control unit that charges controls electromagnetism actuation unit circular telegram when unmanned aerial vehicle charges.
Install on sub charging platform 2 and the main charging platform 1 and carry out the first communicator of unmanned aerial vehicle information interaction with backend server, backend server can be the PC host computer that the backstage is used for the management, the available current satellite communication ware of first communicator, buy according to actual demand, install on sub charging platform 2 and the main charging platform 1 and carry out the second communicator of charging information interaction with unmanned aerial vehicle, the current wireless video transmitting system of second communicator accessible carries out wireless interaction.
The canopy that is fixed with the L type is pour through cement on main charging platform 1 and the sub-charging platform 2, and the horizontal segment of canopy is located the top of filling electric pile 3, and the canopy can be made with current PVC material.
The specific implementation process is as follows:
in the process of the unmanned aerial vehicle polling, the wind-solar complementary power generation module converts solar or wind energy into electric energy and stores the electric energy in the battery unit for charging the unmanned aerial vehicle; meanwhile, the unmanned aerial vehicle receives the control information of the main platform to carry out flying round inspection, when the unmanned aerial vehicle starts from the main charging platform 1 to carry out round inspection to the end point of cruising ability, namely the unmanned aerial vehicle flies to a position 130 kilometers away from the main charging platform, if the unmanned aerial vehicle does not need to go forward continuously, the unmanned aerial vehicle flies back to the main charging platform 1 to carry out charging according to the received information, or when the flying round inspection is needed continuously when the front abnormity is found, the unmanned aerial vehicle flies to the sub-charging platform 2 according to the received information and then carries out round inspection, the information received by the unmanned aerial vehicle can be flight control information or charging information and the like, the unmanned aerial vehicle can be communicated with the main platform in a satellite communication mode after the sub-charging platform 2 is charged, or is communicated with the main charging platform 1 by the sub-charging platform 2 after being communicated with the sub-charging platform 2 to inspect the abnormal condition of the target area, the unmanned aerial vehicle can be charged by the sub-charging platform 2, the cruising ability of the unmanned aerial vehicle in the longitudinal depth direction is prolonged, and the unmanned aerial vehicle can be wheeled to a farther area. The distribution position of sub charging platform 2 and main charging platform 1 can supply a plurality of unmanned aerial vehicles to prolong duration simultaneously on vertical direction of depth, can also let unmanned aerial vehicle go up the round in the transverse direction and patrol the back and charge, and the scope that increase unmanned aerial vehicle round was patrolled.
Example two
The difference from the first embodiment is that, as shown in fig. 3, the system further comprises a plurality of position limiters arranged on the main charging platform 1 and the sub-charging platform 2, each position limiter comprises a plurality of telescopic power units 7, the number of the telescopic power units 7 is set according to the wheels of the unmanned aerial vehicle, for example, four telescopic power units can be arranged for rod-shaped wheels of the unmanned aerial vehicle, every two telescopic power units 7 are in a group, the position limitation is performed from two sides of the unmanned aerial vehicle, the telescopic power units 7 can use telescopic cylinders of the existing CDJ2B type, the telescopic power units 7 are located at positions capable of limiting the wheels of the unmanned aerial vehicle, for example, piston rods of the telescopic cylinders are arranged perpendicular to the central axis of the electromagnetic suction unit from two sides of the unmanned aerial vehicle, the telescopic power units are connected with the charging control unit, limiting rods 8 for limiting the wheels of the unmanned aerial vehicle are welded on the telescopic power units 7, that is the limiting rods 8 are welded on the piston rods of the telescopic cylinders, the electromagnetic attraction unit is provided with a photosensitive unit at one side facing the ground, the photosensitive unit can use the existing photosensitive resistor, the photosensitive unit is in signal connection with the charging control unit, the photosensitive unit sends an illumination signal to the charging control unit when the received illumination intensity changes, and the illumination signal is an electric signal received by a pin of the charging control unit; the outer bonding cover of gag lever post 8 is equipped with anti-skidding cover 9, and the appearance of anti-skidding cover 9 is the wave shape, anti-skidding cover 9 is located the tip department that is close to gag lever post 8.
After the electromagnetism actuation unit adsorbs unmanned aerial vehicle, the illumination of photosensitive unit is sheltered from to unmanned aerial vehicle chance to trigger photosensitive unit and send the illumination signal to the control unit that charges, let the control unit that charges control flexible power pack 7 and drive gag lever post 8 and carry on spacingly to the unmanned aerial vehicle wheel when receiving the illumination signal, prevent that unmanned aerial vehicle from shifting or being blown because of factors such as wind-force influence in the charging process.
The foregoing is merely an example of the present invention and common general knowledge of known specific structures and features of the embodiments is not described herein in any greater detail. It should be noted that, for those skilled in the art, without departing from the structure of the present invention, several changes and modifications can be made, which should also be regarded as the protection scope of the present invention, and these will not affect the effect of the implementation of the present invention and the practicability of the patent. The scope of the claims of the present application shall be determined by the contents of the claims, and the description of the embodiments and the like in the specification shall be used to explain the contents of the claims.
Claims (9)
1. The charging system for the unmanned aerial vehicle polling comprises a main charging platform, wherein a plurality of charging piles for charging the unmanned aerial vehicle and a wind-solar complementary power generation module for providing power for the plurality of charging piles are arranged on the main charging platform; the method is characterized in that:
still include a plurality of supply sub charging platform that unmanned aerial vehicle continued to sail and charge, sub charging platform is located the terminal point of the ability of continuing to sail after unmanned aerial vehicle uses main charging platform to fly as the starting point, sub charging platform arranges into the ring form around main charging platform, set up on the sub charging platform and supply the electric pile of charging that unmanned aerial vehicle charges and to this wind-solar complementary power generation module that fills electric pile and provide electric energy.
2. The charging system for unmanned aerial vehicle rounds as claimed in claim 1, characterized in that: the wind-solar hybrid power generation module comprises a solar power generation unit, a wind power generation unit, a battery unit and a charging control unit, wherein the charging control unit controls the solar power generation unit and/or the wind power generation unit to start to generate power, and the charging control unit controls the battery unit to store electric energy.
3. The charging system for unmanned aerial vehicle rounds as claimed in claim 2, characterized in that: the wind power generation unit comprises a fan, the fan comprises a tower column, two groups of crosses are fixedly arranged at the top end of the tower column, the crosses are coaxially arranged on a central shaft of the tower column, and blades are fixedly arranged on the end parts, located on the same vertical line, of the two crosses and are rectangular plate-shaped.
4. The charging system for unmanned aerial vehicle rounds as claimed in claim 3, characterized in that: the unmanned aerial vehicle charging system is characterized in that an electromagnetic attraction unit used for aligning, charging and attracting the unmanned aerial vehicle is arranged on the charging pile, and the charging control unit controls the electromagnetic attraction unit to be electrified when the unmanned aerial vehicle is charged.
5. The charging system for unmanned aerial vehicle rounds as claimed in claim 4, characterized in that: all be equipped with on sub-charging platform and the main charging platform and carry out the first communicator of unmanned aerial vehicle information interaction with backend server, all be equipped with on sub-charging platform and the main charging platform and carry out the second communicator of charging information interaction with unmanned aerial vehicle.
6. The charging system for unmanned aerial vehicle rounds as claimed in claim 5, characterized in that: the ground size of the main charging platform is 6m multiplied by 24m, and the ground size of the sub charging platform is 3m multiplied by 5 m.
7. The charging system for unmanned aerial vehicle rounds as claimed in claim 5, characterized in that: the main charging platform and the sub-charging platform are fixedly provided with L-shaped rain shelters, and the horizontal sections of the rain shelters are located above the charging piles.
8. The charging system for unmanned aerial vehicle rounds as claimed in claim 4, characterized in that: still include a plurality of limiters of setting on main charging platform and sub-charging platform, the limiter includes a plurality of flexible power pack, flexible power pack is located and can carries out spacing position department to the unmanned aerial vehicle wheel, flexible power signal connection charging control unit, be equipped with on the flexible power pack and carry out spacing gag lever post to the unmanned aerial vehicle wheel, electromagnetism actuation unit is equipped with photosensitive unit towards ground one side department, photosensitive unit signal connection charging control unit.
9. The charging system for unmanned aerial vehicle rounds as claimed in claim 8, characterized in that: the limiting rod is sleeved with an anti-slip sleeve, the anti-slip sleeve is wavy, and the anti-slip sleeve is located at the end part close to the limiting rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122619494.XU CN216268756U (en) | 2021-10-28 | 2021-10-28 | Charging system for unmanned aerial vehicle wheel patrol |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122619494.XU CN216268756U (en) | 2021-10-28 | 2021-10-28 | Charging system for unmanned aerial vehicle wheel patrol |
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| Publication Number | Publication Date |
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| CN216268756U true CN216268756U (en) | 2022-04-12 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202122619494.XU Active CN216268756U (en) | 2021-10-28 | 2021-10-28 | Charging system for unmanned aerial vehicle wheel patrol |
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2021
- 2021-10-28 CN CN202122619494.XU patent/CN216268756U/en active Active
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