CN210882679U

CN210882679U - Charging station

Info

Publication number: CN210882679U
Application number: CN201921644762.XU
Authority: CN
Inventors: 杨祥磊
Original assignee: Beijing Jingdong Qianshi Technology Co Ltd
Current assignee: Beijing Jingdong Qianshi Technology Co Ltd
Priority date: 2019-09-29
Filing date: 2019-09-29
Publication date: 2020-06-30
Anticipated expiration: 2029-09-29

Abstract

The embodiment of the utility model provides a charging station, including shut down platform, charging assembly, support and mechanism of reforming; the aircraft parking device comprises a parking platform, a support, a correcting mechanism and a power supply mechanism, wherein the parking platform is connected with one end of the support, and the correcting mechanism is arranged on the parking platform and used for limiting an aircraft on the parking platform to a target charging position; the charging assembly is arranged on the shutdown platform and used for charging the aircraft. Through setting up a plurality of charging stations at suitable position interval, when aircraft battery electric quantity in flight is not enough, the aircraft can look for apart from nearest charging station, descends on shutting down the platform to restrict the aircraft on the target charging position through the mechanism of reforming, the subassembly that charges the aircraft afterwards, and after the completion of charging, the mechanism of reforming resets, and the aircraft takes off and continues the flight. The problem that the duration of the aircraft is short is solved like this, and the accessible is fallen and is supplemented the electric quantity on the charging station, increases the duration of the aircraft, prolongs the radius of cruising of aircraft.

Description

Charging station

Technical Field

The utility model relates to a technical field that charges, concretely relates to charging station.

Background

With the rapid development of the aircraft industry, various aircrafts are widely applied to the fields of logistics transportation, agricultural production, surveying and mapping and the like. At present, most aircrafts fly by means of fuel oil or battery power supply. For example, the use of drones for the field of logistics transportation has become a new trend, with drones flying on a substantially battery-powered basis.

In the process of implementing the present invention, the inventor finds that there are at least the following problems in the prior art: when the aircraft flies by depending on the power supply of the battery, the battery power storage capacity of the aircraft is limited, so that the endurance time of the aircraft is short, and the cruising radius of the aircraft is small. When the aircraft is used for logistics transportation, the requirement of long-distance logistics transportation cannot be met far away.

SUMMERY OF THE UTILITY MODEL

In view of this, the embodiment of the utility model provides a charging station is provided to solve among the prior art because the battery accumulate ability of aircraft is limited for aircraft duration is short, leads to the problem that aircraft radius is little that cruises.

In order to achieve the above object, an embodiment of the present invention provides a charging station, which includes a shutdown platform, a charging assembly, a bracket, and a return mechanism; the aircraft parking device comprises a parking platform, a support and a correcting mechanism, wherein the parking platform is connected with one end of the support, and the correcting mechanism is arranged on the parking platform and used for limiting an aircraft on the parking platform to a target charging position; the charging assembly is arranged on the shutdown platform and used for charging the aircraft.

Optionally, in the above charging station, the parking platform includes a sun-facing plate, a back-and-back plate, and a side plate; the sun-facing plate and the back-and-back plate are fixedly connected through the side plate, the charging assembly is arranged on the sun-facing plate, and the back-and-back plate is fixedly connected with the bracket; the righting mechanism is arranged on the sun-facing plate in a sliding mode, and a positioning structure is arranged on the sun-facing plate and used for limiting the sliding position of the righting mechanism, so that the aircraft on the parking platform is limited to a target charging position.

Optionally, in the charging station, the righting mechanism includes at least one set of push rod and driving mechanism; each group of push rods comprises a first push rod and a second push rod, the first push rod and the second push rod are arranged on the sun-facing plate in a sliding mode, and the first push rod and the second push rod are arranged oppositely; the driving mechanism is used for driving the first push rod and the second push rod to slide on the sun-facing plate in opposite directions.

Optionally, in the charging station, the number of the push rods is two, and the two groups of the push rods are arranged in a vertical crossing manner.

Optionally, in the charging station, at least one group of sliding openings is formed on the periphery of the sun facing plate, and each group of sliding openings includes a first sliding opening and a second sliding opening; the first push rod penetrates through the sun-facing plate through the first sliding opening and is arranged in the first sliding opening in a sliding mode; the second push rod penetrates through the sun-facing plate through the second sliding opening and is arranged in the second sliding opening in a sliding mode.

Optionally, in the above charging station, the first sliding port and the second sliding port are intermittently arranged to form the positioning structure.

Optionally, in the above charging station, the bracket includes a column, a reinforcing rib, and a connecting plate, two ends of the reinforcing rib are respectively and fixedly connected to the column and the connecting plate, and the connecting plate is fixedly connected to the shutdown platform.

Optionally, in the charging station, the connecting plate is circular, the reinforcing ribs are circular arc-shaped, the number of the reinforcing ribs is multiple, and the plurality of reinforcing ribs are fixed between the upright post and the connecting plate at equal intervals.

Optionally, in the above charging station, the charging assembly includes a solar panel assembly, a charging electrode and a storage battery; the solar panel component is arranged in the central area of the sun plate, the charging electrode is arranged on the solar panel component, the solar panel component is connected with the storage battery, solar energy is converted into electric energy to be stored in the storage battery, and the charging electrode is connected with the storage battery.

Optionally, in the above charging station, the solar panel assembly includes a transparent plate and a solar panel, the solar panel is disposed on the sunny plate, and the transparent plate is disposed on the sunny side of the solar panel.

According to the technical scheme of the utility model, an embodiment in the above-mentioned utility model has following advantage or beneficial effect: the aircraft can be stopped and dropped on the platform of shutting down, and the support has the take the altitude, makes the platform of shutting down be in the take the altitude like this, has reduced the influence that peripheral facility was descended to the aircraft, makes things convenient for the aircraft to descend. The charging assembly is arranged on the parking platform and used for charging the aircraft parked on the parking platform. The aircraft charging device comprises an aircraft landing position adjusting mechanism, a target charging position adjusting mechanism, a correcting mechanism and a charging mechanism, wherein the aircraft landing position adjusting mechanism is arranged on the aircraft landing position adjusting mechanism, the correcting mechanism is arranged on the aircraft landing platform, and the aircraft landing position adjusting mechanism is used for adjusting the aircraft landing position to be inaccurate. After the aircraft is charged, the righting mechanism resets, and the aircraft takes off and continues flying. Through set up a plurality of charging stations at suitable position interval, when the aircraft was not enough in flight on the way electric quantity, can fall and carry out interim charging on the charging station, increased the time of endurance of aircraft, prolonged the radius of cruising of aircraft.

Further effects of the above-mentioned non-conventional alternatives will be described below in connection with the embodiments.

Drawings

The accompanying drawings are included to provide a better understanding of the present invention and are not intended to constitute an undue limitation on the invention. Wherein:

fig. 1 is a schematic structural diagram of an embodiment of a charging station according to the present invention;

fig. 2 is a schematic structural diagram of a part of a charging station according to an embodiment of the present invention;

fig. 3 is a schematic structural diagram of a charging station according to an embodiment of the present invention after a part of the structure is cut off;

fig. 4 is a schematic structural view of an embodiment of a charging station according to the present invention, wherein an aircraft is parked on a parking platform;

fig. 5 is a schematic structural view of an embodiment of a charging station according to the present invention after the aircraft is returned;

fig. 6 is a schematic structural diagram of a bracket according to an embodiment of the present invention;

fig. 7 is a schematic structural diagram of an electric cabinet in an embodiment of a charging station of the present invention;

fig. 8 is an enlarged view of a portion I of fig. 3 according to an embodiment of the present invention;

fig. 9 is an effect schematic diagram of practical application of an embodiment of the charging station of the present invention.

Wherein the figures include the following reference numerals:

1-a stop platform, 11-a positive plate, 12-a negative plate, 13-a side plate, 14-a positioning structure, 15-a sliding opening, 151-a first sliding opening, 152-a second sliding opening, 2-a charging assembly, 21-a solar panel assembly, 211-a transparent plate, 212-a solar panel, 213-a supporting plate, 22-a charging electrode, 23-a storage battery, 3-a support, 31-a vertical column, 32-a reinforcing rib, 33-a connecting plate, 4-a correcting mechanism, 41-a push rod, 411-a first push rod, 412-a second push rod, 42-a driving mechanism and 5-an electric cabinet.

Detailed Description

Exemplary embodiments of the invention are described below with reference to the accompanying drawings, in which various details of embodiments of the invention are included to assist understanding, and which are to be considered exemplary only. Accordingly, those of ordinary skill in the art will recognize that various changes and modifications of the embodiments described herein can be made without departing from the scope and spirit of the invention. Also, descriptions of well-known functions and constructions are omitted in the following description for clarity and conciseness.

As shown in fig. 1, a charging station provided in an embodiment of the present invention includes a shutdown platform 1, a charging assembly 2, a bracket 3, and a righting mechanism 4; the parking platform 1 is connected with one end of the support 3, and the correcting mechanism 4 is arranged on the parking platform 1 and used for limiting the aircraft on the parking platform 1 to a target charging position; the charging assembly 2 is arranged on the shutdown platform 1 and used for charging the aircraft.

The embodiment of the utility model provides an in the charging station, shut down 1 fixed connection of platform in the one end of support 3, the aircraft can stop and fall on shutting down platform 1, and support 3 has the take the altitude, makes like this shut down platform 1 and is in the take the altitude, has reduced the influence that peripheral facility descended the aircraft, makes things convenient for the aircraft to descend. The charging assembly 2 is arranged on the shutdown platform 1 and used for charging the aircraft parked on the shutdown platform 1, wherein the charging assembly 2 is arranged on the shutdown platform 1, so that the charging station is compact in structure, and occupied space is saved. The correcting mechanism 4 is arranged on the shutdown platform 1, and when the aircraft stops on the shutdown platform 1, the aircraft can be limited to be charged at the target charging position through the adjustment of the correcting mechanism 4 on the aircraft, wherein the correcting mechanism 4 can not only adjust the aircraft with an inaccurate landing position to move to the target charging position, but also fix the aircraft at the target charging position, so that the influence of the external environment on the aircraft in the charging process is prevented, and the aircraft can be smoothly charged. After the aircraft is charged, the righting mechanism 4 is reset, and the aircraft takes off and continues flying. Through setting up a plurality of charging stations at suitable position interval, when aircraft battery electric quantity in flight is not enough, the aircraft can look for apart from nearest charging station, descends on shutting down platform 1 to restrict the aircraft on the target charging position through mechanism 4 that reforms, the subassembly 2 that charges the aircraft afterwards, and the back is accomplished in charging, and mechanism 4 resets that reforms, and the aircraft takes off and continues the flight. Like this the aircraft when the flight on the way electric quantity is not enough, can land and carry out interim charging on the charging station, increased the time of endurance of aircraft, prolonged the radius that cruises of aircraft.

As shown in fig. 2 and 3, in a charging station according to an embodiment of the present invention, a parking platform 1 includes a sun-facing plate 11, a back-facing plate 12, and a side plate 13; the sun-facing plate 11 and the back-shade plate 12 are fixedly connected through a side plate 13, the charging assembly 2 is arranged on the sun-facing plate 11, and the back-shade plate 12 is fixedly connected with the bracket 3; the righting mechanism 4 is arranged on the sun-facing plate 11 in a sliding mode, and the sun-facing plate 11 is provided with a positioning structure 14, wherein the positioning structure 14 is used for limiting the sliding position of the righting mechanism 4, so that the aircraft on the parking platform 1 is limited to the target charging position.

The embodiment of the utility model provides an in the charging station, shut down platform 1 and constitute by sunny board 11, shady board 12 and curb plate 13 of the back of the body, curb plate 13 fixed connection is between sunny board 11 and shady board 12 of the back of the body, shuts down platform 1 like this and forms the box structure, makes and shuts down platform 1 structure more firm, and the aircraft can stop steadily and fall on sunny board 11. Meanwhile, the shutdown platform 1 is designed into an upper layer plate and a lower layer plate of the sun-facing plate 11 and the back-shading plate 12, so that the shutdown platform 1 can be conveniently and fixedly installed on the support 3, and the charging assembly 2 and the correcting mechanism 4 are conveniently installed on the shutdown platform 1, so that the charging station is compact in structure. The righting mechanism 4 can slide on the sun-facing plate 11, and the positioning structure 14 is arranged on the sun-facing plate 11, and the positioning structure 14 is used for limiting the sliding position of the righting mechanism 4, so that the righting mechanism 4 can accurately limit the aircraft on the parking platform 1 to the target charging position through the positioning structure 14.

As shown in fig. 2 and 3, in a charging station according to an embodiment of the present invention, the righting mechanism 4 includes at least one set of push rods 41 and a driving mechanism 42; each group of push rods 41 comprises a first push rod 411 and a second push rod 412, the first push rod 411 and the second push rod 412 are arranged on the sun-facing plate 11 in a sliding mode, and the first push rod 411 and the second push rod 412 are arranged oppositely; the driving mechanism 42 is used for driving the first push rod 411 and the second push rod 412 to slide on the sun-facing plate 11 in an opposite direction.

The embodiment of the utility model provides an in the charging station, mechanism 4 comprises at least a set of push rod 41 and actuating mechanism 42 of reforming, and push rod 41 is the executive component of mechanism 4 of reforming, and wherein every group push rod 41 is including relative first push rod 411 and the second push rod 412 that sets up, and first push rod 411 and second push rod 412 can slide on board 11 facing the sun, and the executive component design that will mechanism 4 of reforming is the push rod 41 structure, makes mechanism 4's simple structure, convenient manufacturing. The driving mechanism 42 is fixed on the parking platform 1 and is used for driving the first push rod 411 and the second push rod 412 to slide on the sun-facing plate 11 in the opposite direction, so that an aircraft with an inaccurate landing position can be moved to a target charging position under the pushing of the first push rod 411 and the second push rod 412, the aircraft at the target charging position can be clamped between the first push rod 411 and the second push rod 412, the aircraft is stably located at the target charging position for charging, and the influence of the external environment on the aircraft in the charging process is effectively prevented. After the aircraft is charged, the driving mechanism 42 drives the first push rod 411 and the second push rod 412 to slide on the sun-facing plate 11 in opposite directions, so that the return mechanism 4 is restored to the initial position, and the aircraft takes off and continues flying.

As shown in fig. 2 and fig. 3, in the charging station provided in the embodiment of the present invention, the push rods 41 are two sets, and the two sets of push rods 41 are arranged perpendicularly and crosswise. By arranging the two groups of push rods 41 and arranging the two groups of push rods 41 on the sun-facing plate 11 in a vertically crossed manner in a sliding manner, when the aircraft lands on the sun-facing plate 11, the first push rods 411 and the second push rods 412 in the two groups of push rods 41 simultaneously slide on the sun-facing plate 11 in an opposite direction, so that the aircraft can be more stably limited to a target charging position for charging, and the righting effect of the righting mechanism 4 is better.

As shown in fig. 2 and fig. 3, in the charging station according to the embodiment of the present invention, at least one set of sliding openings 15 is disposed on the periphery of the sun-facing plate 11, and each set of sliding openings 15 includes a first sliding opening 151 and a second sliding opening 152; the first push rod 411 passes through the sun-facing plate 11 through the first sliding opening 151 and is slidably arranged in the first sliding opening 151; the second push rod 412 passes through the sun-facing plate 11 through the second sliding opening 152, and is slidably disposed in the second sliding opening 152. By forming the slide opening 15 on the periphery of the sun-facing plate 11 and arranging the slide opening 15 in correspondence with the push rod 41, the push rod 41 can be slid in the slide opening 15 to restrict the aircraft to the target charging position. Each set of sliding openings 15 includes a first sliding opening 151 and a second sliding opening 152, the first sliding openings 151 and the first push rods 411 are arranged in a one-to-one correspondence manner, the first push rods 411 pass through the sun-facing plate 11 through the first sliding openings 151, so that the first push rods 411 can slide on the sun-facing plate 11 along the first sliding openings 151, and similarly, the second push rods 412 can slide on the sun-facing plate 11 along the second sliding openings 152. The push rod 41 slides on the sun-facing plate 11 by arranging the sliding opening 15, and the scheme is simple and easy to implement and saves cost.

Optionally, in the charging station provided in the embodiment of the present invention, there are various ways in which the first push rod 411 and the second push rod 412 are slidably disposed on the sun exposed plate 11, and the first push rod 411 and the second push rod 412 may be slid on the sun exposed plate 11 by providing a guide rail on the sun exposed plate 11 or by opening the sliding opening 15 on the sun exposed plate 11 to slide the first push rod 411 and the second push rod 412 on the sun exposed plate 11, or other ways that the first push rod 411 and the second push rod 412 can be slid on the sun exposed plate 11. Alternatively, in order to make the solution simple and easy to operate, an embodiment of the present invention provides a charging station, in which the first push rod 411 and the second push rod 412 are slid on the sun-facing plate 11 by opening the sliding opening 15 on the periphery of the sun-facing plate 11.

As shown in fig. 2, 4 and 5, in a charging station provided in an embodiment of the present invention, the first sliding opening 151 and the second sliding opening 152 are intermittently disposed to form the positioning structure 14. The first sliding port 151 and the second sliding port 152 are arranged intermittently, and when the first push rod 411 and the second push rod 412 slide on the sun-facing plate 11 along the first sliding port 151 and the second sliding port 152 respectively, the first push rod and the second push rod cannot slide at the intermittent positions, so that the positioning structure 14 can be formed by arranging the intermittent positions, and the aircraft can be limited to the target charging position. According to the scheme, the positioning structure 14 is not additionally arranged, so that the processing technology is simplified, and the cost is saved. Optionally, the embodiment of the present invention provides a charging station, wherein the positioning structure 14 is disposed on the sun panel 11 in a plurality of ways, and the righting mechanism 4 can not slide on the sun panel 11 by disposing a protrusion or other obstacle structure on the sun panel 11, even if the first push rod 411 and the second push rod 412 can not slide on the sun panel 11.

As shown in fig. 6, the embodiment of the utility model provides a charging station, support 3 include stand 31, strengthening rib 32 and connecting plate 33, the both ends of strengthening rib 32 respectively with stand 31 and connecting plate 33 fixed connection, connecting plate 33 with shut down platform 1 fixed connection.

The embodiment of the utility model provides an in the charging station, support 3 includes stand 31, strengthening rib 32 and connecting plate 33, and stand 31 passes through strengthening rib 32 and connecting plate 33 fixed connection, is fixed with on the connecting plate 33 and shuts down platform 1, shuts down platform 1 like this and fixes subaerial through stand 31, and stand 31 makes and shuts down platform 1 and be in certain height simultaneously, can reduce the influence that peripheral facility descended to the aircraft like this, makes things convenient for the aircraft to descend. The structure of the bracket 3 is stable, and has the advantages of small occupied area and reasonable control of the height of the shutdown platform 1. Optionally, the embodiment of the utility model provides an in the charging station, the height of stand 31 is decided according to peripheral facility to do not influence the aircraft and descend as the purpose, generally speaking, the height ratio peripheral facility of stand 31 is slightly higher. Optionally, the embodiment of the present invention provides an in the charging station, the quantity of stand 31 is one at least. Optionally, in order to make charging station simple structure compact, save and possess the space, easy to assemble, the embodiment of the utility model provides an in the charging station, the quantity of stand 31 is one.

Optionally, the embodiment of the utility model provides an in the charging station, shut down platform 1 and fix subaerial through stand 31, fixed mode can be welding or bolt fastening, or other fixed modes. For the convenience of charging station installation fixed, optionally, the embodiment of the utility model provides an in the charging station, stand 3 passes through earth anchor and bolt fastening subaerial.

As shown in fig. 6, in the charging station according to the embodiment of the present invention, the connecting plate 33 is circular, the reinforcing ribs 32 are circular arc-shaped, the number of the reinforcing ribs 32 is multiple, and the multiple reinforcing ribs 32 are fixed between the upright 31 and the connecting plate 33 at equal intervals. The shape of the connecting plate 33 is designed to be circular, so that the connecting plate can be uniformly contacted with the shutdown platform 1, and the shutdown platform 1 is more stably installed. The reinforcing ribs 32 are arranged in a circular arc shape, and the plurality of reinforcing ribs 32 are fixed between the upright posts 31 and the connecting plate 33 at equal intervals, so that the overall structure of the charging station is more stable. Optionally, in order to make the platform 1 of shutting down more firm fix on support 3, and make charging station overall structure simple compact, the embodiment of the utility model provides an in the charging station, the quantity of strengthening rib 32 is four.

As shown in fig. 3 and 7, in a charging station according to an embodiment of the present invention, the charging assembly 2 includes a solar panel assembly 21, a charging electrode 22 and a storage battery 23; the solar panel assembly 21 is disposed in the central region of the sun-facing plate 11, the charging electrode 22 is disposed on the solar panel assembly 21, the solar panel assembly 21 is connected to the storage battery 23, the solar panel assembly 21 converts solar energy into electric energy to be stored in the storage battery 23, and the charging electrode 22 is connected to the storage battery 23.

The embodiment of the utility model provides an in the charging station, solar panel component 21 sets up in the central zone to positive plate 11, can not only guarantee to receive the sun and shine, makes charging station simple structure compact moreover, sparingly occupies the space. The solar panel assembly 21 is connected to a battery 23, and converts solar energy into electric energy to be stored in the battery 23. Charging electrode 22 sets up on solar panel assembly 21, and is connected with battery 23, makes things convenient for the aircraft to charge. As shown in fig. 4, after the aircraft is parked on the parking platform 1, the righting mechanism 4 performs a righting adjustment on the aircraft to accurately limit the aircraft to the target charging position, so that the charging electrode 22 contacts the contact point on the aircraft. The accumulator 23 then charges the aircraft via the charging electrode 22 under the control of the charge management system. Optionally, the embodiment of the utility model provides an in the charging station that provides, the quantity and the mounted position of charging electrode 22 are decided according to the model of aircraft, guarantee to charge for the aircraft. Optionally, the embodiment of the present invention provides a charging station, wherein four charging electrodes 22 are disposed on the solar panel assembly 21.

As shown in fig. 3 and 8, in a charging station provided in an embodiment of the present invention, the solar panel assembly 21 includes a transparent plate 211 and a solar panel 212, the solar panel 212 is disposed on the sun-facing plate 11, and the transparent plate 211 is disposed on the sun-facing surface of the solar panel 212. The solar panel 212 is arranged on the sun-facing plate 11 and used for receiving sunlight, the transparent plate 211 is fixedly arranged on the sun-facing surface of the solar panel 212 and used for protecting the solar panel 212, the aircraft can be prevented from directly stopping on the solar panel 212 and being damaged by the solar panel 212, the aircraft can directly stop on the transparent plate 211, and the transparent plate 211 is transparent and good in light transmission and cannot influence the normal work of the solar panel 212.

Optionally, the embodiment of the utility model provides an in the charging station, the material of transparent plate 211 can be transparent toughened glass or transparent organic material, or other transparent materials. In order to make protection and transparent effect better, optionally, the embodiment of the utility model provides an in the charging station, transparent plate 211 adopts toughened glass to make and forms, and the toughened glass that transparent plate 211 adopted has waterproof, sealed effect simultaneously, plays fine guard action to solar panel 212 and other structures.

As shown in fig. 3 and 8, an embodiment of the present invention provides a charging station, further including a supporting plate 213; the supporting plate 213 is fixed on the shadow side of the solar panel 212, and supports the solar panel 212, so that the structure of the solar panel assembly 21 is more stable. Optionally, in the charging station provided in the embodiment of the present invention, the material of the supporting plate 213 may be a steel plate or an aluminum plate, or other materials. In order to make the supporting effect better, optionally, the embodiment of the present invention provides a charging station, the supporting plate 213 is made of steel plate.

Optionally, the embodiment of the utility model provides an in the charging station, still including the mechanism controller that reforms, the mechanism controller that reforms is used for controlling mechanism 4 that reforms. After the aircraft is parked on the parking platform 1, the righting mechanism controller accurately restrains the aircraft at the target charging position by controlling the righting mechanism 4, causes the charging electrode 22 to contact a contact on the aircraft, and then charges the aircraft. After the charging is finished, the restoring mechanism controller controls the restoring mechanism 4 to reset. Optionally, the embodiment of the utility model provides an in the charging station, still include difference GPS module and charging station control system, difference GPS module can be to the coordinate position information of charging station control system transmission charging station, and charging station control system can be to the coordinate position information of the communication module transmission charging station on the aircraft. When the electric quantity of the battery of the flying aircraft is insufficient, the flying aircraft can search for the charging station closest to the flying aircraft, the charging station can send the position information of the flying aircraft to the flying aircraft, and the flying aircraft can land on the charging station closest to the flying aircraft for charging. The charging station control system also has the functions of controlling and storing electric energy, charging and the like. Optionally, the embodiment of the utility model provides an in the charging station, still including the balanced module of charging, the balanced module of charging is connected with solar panel 212 and battery 23 respectively, and solar panel 212 produces the electric current under the illumination condition, and the electric current change that leads to producing because of the change of illumination condition is great, and the balanced module of charging can be with the electric current output of change for the certain electric current of size, for the battery 23 power supply. As shown in fig. 7, the embodiment of the utility model provides an in the charging station, still include electric cabinet 5, wherein battery 23, mechanism controller, balanced charging module, difference GPS module and charging station control system etc. all install in electric cabinet 5.

Use unmanned aerial vehicle to be used for the commodity circulation transportation as the example below, explain the embodiment of the utility model provides a use of charging station.

As shown in fig. 9, when the charging station is used, a plurality of charging stations are first installed at appropriate positions at intervals, and the column 31 is fixed to the ground by the ground anchor and the bolt, thereby completing installation of the charging station. Under light conditions, the solar panels 212 generate electricity and power the battery 23 through the balanced charging module, thus converting solar energy into electrical energy for storage in the battery 23. When unmanned aerial vehicle is not enough in the commodity circulation transportation flight electric quantity, control system among the unmanned aerial vehicle begins to look for apart from nearest charging station, and the charging station sends positional information to unmanned aerial vehicle through self difference GPS module and charging station control system, and according to positional information, unmanned aerial vehicle looks for apart from nearest charging station to stop on the transparent plate 211 of shutting down platform 1. At this time, the righting mechanism controller controls the first push rod 411 and the second push rod 412 in the righting mechanism 4 to slide oppositely on the sun-facing plate 11 along the first sliding port 151 and the second sliding port 152 respectively, and the unmanned aerial vehicle is accurately limited on the target charging position through the positioning of the positioning structure 14, so that the charging electrode 22 contacts with a contact on the unmanned aerial vehicle. Then, under the control of the charging management system, the storage battery 23 charges the unmanned aerial vehicle through the charging electrode 22. After charging is completed, the first push rod 411 and the second push rod 412 in the righting mechanism 4 are controlled by the righting mechanism controller to slide on the sun-facing plate 11 in opposite directions along the first sliding port 151 and the second sliding port 152 respectively, and then the unmanned aerial vehicle returns to the initial position and continues flying. Through setting up a plurality of charging stations at suitable position interval, when unmanned aerial vehicle battery power in flight is not enough, the nearest charging station of distance is look for to unmanned aerial vehicle, descends and is shutting down platform 1 to restrict unmanned aerial vehicle on the target charging position through mechanism 4 of reforming, charge subassembly 2 afterwards and charge unmanned aerial vehicle, charge and accomplish the back, mechanism 4 resets of reforming, and unmanned aerial vehicle takes off and continues the flight. Unmanned aerial vehicle when the flight on the way electric quantity is not enough like this, can land and carry out interim charging on the charging station, has increased unmanned aerial vehicle's time of endurance, has prolonged unmanned aerial vehicle's radius of cruising.

Therefore, the embodiment of the utility model provides an in the charging station, shut down 1 fixed connection of platform in the one end of support 3, the aircraft can stop and fall on shutting down platform 1, and support 3 has the take the altitude, makes like this and shuts down platform 1 and be in the take the altitude, has reduced the influence that peripheral facility descended to the aircraft, makes things convenient for the aircraft to descend. The charging assembly 2 is arranged on the shutdown platform 1 and used for charging the aircraft parked on the shutdown platform 1, wherein the charging assembly 2 is arranged on the shutdown platform 1, so that the charging station is compact in structure, and occupied space is saved. The correcting mechanism 4 is arranged on the shutdown platform 1, and when the aircraft stops on the shutdown platform 1, the aircraft can be limited to be charged at the target charging position through the adjustment of the correcting mechanism 4 on the aircraft, wherein the correcting mechanism 4 can not only adjust the aircraft with an inaccurate landing position to move to the target charging position, but also fix the aircraft at the target charging position, so that the influence of the external environment on the aircraft in the charging process is prevented, and the aircraft can be smoothly charged. After the aircraft is charged, the righting mechanism 4 is reset, and the aircraft takes off and continues flying. Through setting up a plurality of charging stations at suitable position interval, when aircraft battery electric quantity in flight is not enough, the aircraft can look for apart from nearest charging station, lands on shutting down platform 1 to make the aircraft restriction on the target charging position through mechanism 4 that reforms, the subassembly 2 that charges the aircraft afterwards, and the back is accomplished in charging, and mechanism 4 resets that reforms, and the aircraft takes off and continues the flight. Like this the aircraft when the flight on the way electric quantity is not enough, can land and carry out interim charging on the charging station, increased the time of endurance of aircraft, prolonged the radius that cruises of aircraft.

The above detailed description does not limit the scope of the present invention. Those skilled in the art will appreciate that various modifications, combinations, sub-combinations, and substitutions can occur, depending on design requirements and other factors. Any modification, equivalent replacement, and improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. A charging station is characterized by comprising a shutdown platform (1), a charging assembly (2), a bracket (3) and a righting mechanism (4);

the shutdown platform (1) is connected with one end of the bracket (3), and the correcting mechanism (4) is arranged on the shutdown platform (1) and used for limiting an aircraft on the shutdown platform (1) to a target charging position;

the charging assembly (2) is arranged on the shutdown platform (1) and used for charging the aircraft.

2. The charging station according to claim 1, characterized in that the shutdown platform (1) comprises a sun-facing plate (11), a back-facing plate (12) and a side plate (13);

the sun-facing plate (11) and the back-and-back plate (12) are fixedly connected through the side plate (13), the charging assembly (2) is arranged on the sun-facing plate (11), and the back-and-back plate (12) is fixedly connected with the bracket (3);

the righting mechanism (4) is arranged on the sun-facing plate (11) in a sliding mode, a positioning structure (14) is arranged on the sun-facing plate (11), and the positioning structure (14) is used for limiting the sliding position of the righting mechanism (4) so as to limit the aircraft on the parking platform (1) to a target charging position.

3. The charging station according to claim 2, characterized in that the righting mechanism (4) comprises at least one set of a push rod (41) and a drive mechanism (42);

each group of push rods (41) comprises a first push rod (411) and a second push rod (412), the first push rod (411) and the second push rod (412) are arranged on the sun-facing plate (11) in a sliding mode, and the first push rod (411) and the second push rod (412) are arranged oppositely;

the driving mechanism (42) is used for driving the first push rod (411) and the second push rod (412) to slide oppositely on the sun-facing plate (11).

4. The charging station according to claim 3, characterized in that the push rods (41) are in two groups, and the two groups of push rods (41) are arranged perpendicularly across.

5. The charging station according to claim 3, characterized in that at least one group of sliding openings (15) is opened on the periphery of the sun-facing plate (11), each group of sliding openings (15) comprises a first sliding opening (151) and a second sliding opening (152);

the first push rod (411) penetrates through the sun-facing plate (11) through the first sliding opening (151) and is arranged in the first sliding opening (151) in a sliding mode;

the second push rod (412) penetrates through the sun-facing plate (11) through the second sliding opening (152) and is arranged in the second sliding opening (152) in a sliding mode.

6. The charging station according to claim 5, characterized in that the first and second sliding mouths (151, 152) are arranged discontinuously to form the positioning structure (14).

7. The charging station according to claim 1, characterized in that the bracket (3) comprises a column (31), a reinforcing rib (32) and a connecting plate (33), wherein both ends of the reinforcing rib (32) are fixedly connected with the column (31) and the connecting plate (33), respectively, and the connecting plate (33) is fixedly connected with the shutdown platform (1).

8. The charging station according to claim 7, wherein the shape of the connecting plate (33) is circular, the shape of the reinforcing rib (32) is circular arc, and the number of the reinforcing ribs (32) is plural, and the plural reinforcing ribs (32) are fixed between the pillar (31) and the connecting plate (33) at equal intervals.

9. The charging station according to claim 2, wherein the charging assembly (2) comprises a solar panel assembly (21), a charging electrode (22) and a storage battery (23);

the solar panel component (21) is arranged in the central area of the sun-facing plate (11), the charging electrode (22) is arranged on the solar panel component (21), the solar panel component (21) is connected with the storage battery (23), solar energy is converted into electric energy to be stored in the storage battery (23), and the charging electrode (22) is connected with the storage battery (23).

10. The charging station according to claim 9, wherein the solar panel assembly (21) comprises a transparent plate (211) and a solar panel (212), the solar panel (212) being disposed on the sun-facing plate (11), the transparent plate (211) being disposed on the sun-facing side of the solar panel (212).