阅读说明：本技术 一种无人机起落充电装置及无人机任务交接方法 (Unmanned aerial vehicle landing and landing charging device and unmanned aerial vehicle task handover method ) 是由 段春艳 赖华景 许继源 辛少权 李颖 冯泽君 陈潇跃 连佳生 于 2019-09-20 设计创作，主要内容包括：本发明公开一种无人机起落充电装置,其特征在于,包括支架、供电装置、设在所述支架上的若干充电机舱；各所述充电机舱包括舱门、舱体以及设在所述舱体内的蓄电池、与所述蓄电池电连接的电源分配模块、分别与所述电源分配模块电连接的机载ARM嵌入式系统、数据传输模块、充电模块、舱门开启模块、无人机传输模块；所述蓄电池与所述供电装置电连接,所述无人机传输模块用于将无人机输送进出所述充电机舱,所述机载ARM嵌入式系统与所述无人机传输模块、所述舱门开启模块、所述数据传输模块连接,用于控制所述无人机传输模块、所述舱门开启模块运行或停止运行并通过所述数据传输模块与所述监控后台、无人机进行数据传输。(The invention discloses a landing and landing charging device for an unmanned aerial vehicle, which is characterized by comprising a support, a power supply device and a plurality of charging cabins arranged on the support; each charging cabin comprises a cabin door, a cabin body, a storage battery arranged in the cabin body, a power distribution module electrically connected with the storage battery, an airborne ARM embedded system respectively electrically connected with the power distribution module, a data transmission module, a charging module, a cabin door opening module and an unmanned aerial vehicle transmission module; the battery with the power supply unit electricity is connected, unmanned aerial vehicle transmission module is used for carrying unmanned aerial vehicle business turn over the cabin of charging, machine carries ARM embedded system with unmanned aerial vehicle transmission module the module is opened to the hatch door data transmission module connects, is used for control unmanned aerial vehicle transmission module the hatch door is opened the module and is moved or the stall and pass through data transmission module with control backstage, unmanned aerial vehicle carry out data transmission.)

1. An unmanned aerial vehicle landing and charging device is characterized by comprising a support, a monitoring background, a plurality of charging cabins arranged on the support, and a power supply device for supplying power to the charging cabins; each of the charging bays includes: the unmanned aerial vehicle comprises a cabin body with a cabin door, a storage battery arranged in the cabin body, a power distribution module electrically connected with the storage battery, an airborne ARM embedded system, a data transmission module, a charging module, a cabin door opening module and an unmanned aerial vehicle transmission module, wherein the airborne ARM embedded system, the data transmission module, the charging module, the cabin door opening module and the unmanned aerial vehicle transmission module are respectively electrically connected with the power distribution module; the battery with the power supply unit electricity is connected, unmanned aerial vehicle transmission module is used for carrying unmanned aerial vehicle business turn over the cabin of charging, machine carries ARM embedded system with unmanned aerial vehicle transmission module the module is opened to the hatch door, data transmission module connects, is used for control unmanned aerial vehicle transmission module, the hatch door is opened the module and is moved or the bring to rest, and pass through data transmission module with the control backstage unmanned aerial vehicle carries out data transmission.

2. The unmanned aerial vehicle landing and charging device of claim 1, wherein the unmanned aerial vehicle transmission module comprises a hydraulic telescoping rod and a platform disposed on the hydraulic telescoping rod and configured to enter and exit the charging cabin under the action of the hydraulic telescoping rod.

3. An unmanned aerial vehicle landing and landing charging device according to claim 1, wherein the power supply means comprises: one or more of a photovoltaic power generation device, a wind-solar hybrid power generation device and an external power grid.

4. The landing and landing charging device for unmanned aerial vehicles of claim 3, wherein the photovoltaic power generation device comprises a photovoltaic module fixed on the periphery of the support and the cabin door, and a photovoltaic controller connected with the photovoltaic module.

5. The landing and landing charger for unmanned aerial vehicles according to claim 1, wherein the battery supplies 9V to the onboard ARM embedded system and the data transmission module, respectively, supplies 36V to the wireless charging module, and supplies 12V to the door opening module and the unmanned aerial vehicle transmission module, respectively, through the power distribution module.

6. The landing and landing charging device for unmanned aerial vehicles of claim 1, wherein the charging module is a wireless charging device or a contact charging device.

7. The landing and charging device for unmanned aerial vehicle as claimed in claim 1, wherein one end of the cabin door is hinged to the cabin body, the cabin door opening module is a cylinder, the cylinder is disposed below the cabin door, and a cylinder shaft of the cylinder is connected to the cabin door;

or one end of the cabin door is rotatably connected with the cabin body through a rotating shaft, the cabin door opening module is a motor, and an output shaft of the motor is connected with the rotating shaft through a gear transmission mechanism.

8. An unmanned aerial vehicle landing and charging device according to claim 1, wherein the charging bays are hexagonal pillar cavities or square pillar cavities, and each charging bay is formed into a honeycomb structure.

9. An unmanned aerial vehicle task handover method is characterized in that the unmanned aerial vehicle landing and charging device as claimed in any one of claims 1 to 8 is adopted, a task handover distribution system is arranged on the airborne ARM embedded system, the airborne ARM embedded system distributes work to an unmanned aerial vehicle X through the task handover distribution system after receiving a task instruction issued by the monitoring background through the data transmission module, when the unmanned aerial vehicle X returns to the charging cabin for charging, if the task handover distribution system receives the work information and the operation data of the unmanned aerial vehicle X in an unfinished state, the task handover distribution system continuously distributes the unfinished task to an unmanned aerial vehicle X +1 with a full electric quantity state, and the process is circulated until the task is completed.

10. The method according to claim 9, wherein the number of the drones X is 2 or more.

Technical Field

The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle landing and charging device and an unmanned aerial vehicle task handover method.

Background

With the progress of science and technology, the era of intellectualization, informatization and automation has come, and the unmanned aerial vehicle is a child under new science and technology. Present unmanned aerial vehicle has functions such as artificial intelligence, autopilot and signal processing, because of its advantage such as small, can unmanned driving, has been widely used in fields such as military affairs, electric power patrol and examine, oil pipe patrol and examine, photovoltaic power plant operation and maintenance, public safety patrol and examine, fire control is supplementary, the agricultural is supplementary, topography reconnaissance.

However, the cruising ability of the unmanned aerial vehicle is poor, and the cruising ability is always an important factor for restricting the application of the unmanned aerial vehicle. At present, most of unmanned aerial vehicle charging platforms applied outdoors are provided with solar charging devices so as to save energy and improve environmental adaptability; see the patent application with the publication number of CN108110883A and the patent with the publication numbers of CN204947630U and CN 208411468U. In the prior art, one platform can only correspond to one unmanned aerial vehicle, can not many unmanned aerial vehicles charge together. When the electric quantity is insufficient in the process of executing the task by the unmanned aerial vehicle, the unmanned aerial vehicle can start to continue to work after the charging platform is returned to charge, and the working efficiency is seriously influenced.

Disclosure of Invention

Aiming at the problems in the prior art, the invention aims to provide the unmanned aerial vehicle landing charging device which can meet the requirement of simultaneously charging a plurality of unmanned aerial vehicles.

Another object of the present invention is to provide a method for task handover of an unmanned aerial vehicle.

In order to achieve the above purpose, the invention adopts the following technical scheme:

an unmanned aerial vehicle landing and charging device is characterized by comprising a support, a monitoring background, a plurality of charging cabins arranged on the support, and a power supply device for supplying power to the charging cabins; each of the charging bays includes: the unmanned aerial vehicle comprises a cabin body with a cabin door, a storage battery arranged in the cabin body, a power distribution module electrically connected with the storage battery, an airborne ARM embedded system, a data transmission module, a charging module, a cabin door opening module and an unmanned aerial vehicle transmission module, wherein the airborne ARM embedded system, the data transmission module, the charging module, the cabin door opening module and the unmanned aerial vehicle transmission module are respectively electrically connected with the power distribution module; the battery with the power supply unit electricity is connected, unmanned aerial vehicle transmission module is used for carrying unmanned aerial vehicle business turn over the cabin of charging, machine carries ARM embedded system with unmanned aerial vehicle transmission module the module is opened to the hatch door, data transmission module connects, is used for control unmanned aerial vehicle transmission module, the hatch door is opened the module and is moved or the bring to rest, and pass through data transmission module with the control backstage unmanned aerial vehicle carries out data transmission.

As a further explanation of the above scheme, the unmanned aerial vehicle transmission module comprises a hydraulic telescopic rod and a platform which is arranged on the hydraulic telescopic rod and can enter and exit the charging cabin under the action of the hydraulic telescopic rod.

As a further explanation of the above aspect, the power supply device includes: one or more of a photovoltaic power generation device, a wind-solar hybrid power generation device and an external power grid.

As a further explanation of the above scheme, the photovoltaic power generation device includes a photovoltaic module fixedly disposed on the periphery of the support and the cabin door, and a photovoltaic controller connected to the photovoltaic module.

As a further explanation of the above scheme, the storage battery supplies 9V voltage to the airborne ARM embedded system and the data transmission module through the power distribution module, supplies 36V voltage to the wireless charging module, and supplies 12V voltage to the cabin door opening module and the unmanned aerial vehicle transmission module.

As a further explanation of the above scheme, the charging module is a wireless charging device or a contact type charging device.

As a further explanation of the above scheme, one end of the cabin door is hinged to the cabin body, the cabin door opening module is an air cylinder, the air cylinder is arranged below the cabin door, and an air cylinder shaft of the air cylinder is connected with the cabin door; or one end of the cabin door is rotatably connected with the cabin body through a rotating shaft, the cabin door opening module is a motor, and an output shaft of the motor is connected with the rotating shaft through a gear transmission mechanism.

As a further explanation of the above scheme, the charging machine cabins are hexagonal column cavities or square column cavities, and each charging machine cabin forms a honeycomb structure.

The utility model provides an unmanned aerial vehicle task handing-over method, its characterized in that has adopted as above arbitrary unmanned aerial vehicle rises and falls charging device be equipped with task handing-over distribution system on the airborne ARM embedded system, airborne ARM embedded system passes through after the task instruction that the control backstage was issued is received to data transmission module, pass through task handing-over distribution system distributes work for unmanned aerial vehicle X, works as unmanned aerial vehicle X returns unmanned aerial vehicle cabin charges, if task handing-over distribution system receives unmanned aerial vehicle X's work information and operational data are not accomplished the state, task handing-over distribution system continues to distribute the task that does not accomplish to unmanned aerial vehicle X +1 that the electric quantity state is full of electricity, so circulate to the task completion.

As a further explanation of the above scheme, the number of the unmanned aerial vehicles X is more than 2.

The invention has the beneficial effects that:

firstly, a plurality of unmanned aerial vehicles can be charged simultaneously by adopting a plurality of charging cabins, so that the charging efficiency is improved; the charging process is automatic and convenient to use through the airborne ARM embedded system.

Secondly, charge for unmanned aerial vehicle through photovoltaic module with solar energy transformation for unmanned aerial vehicle no longer need rely on external grid power to charge, applicable in unmanned area of remote.

And thirdly, a task handover system is adopted, if the situation that the task is not completed occurs to the unmanned aerial vehicle which returns to charge, the task handover system sends out another fully charged unmanned aerial vehicle to arrive at the task place to continue to complete the task which is not completed by the previous unmanned aerial vehicle.

Drawings

Fig. 1 is a structural diagram of a landing and landing charging device for an unmanned aerial vehicle according to the present invention.

Fig. 2 is a structural diagram of a charging device main body of the landing and landing charging device for the unmanned aerial vehicle provided by the invention.

Fig. 3 is a flow chart illustrating an autonomous power supply of the landing and landing charging device for an unmanned aerial vehicle according to the present invention.

Fig. 4 is a flowchart of the unmanned aerial vehicle task handover method provided by the present invention.

Description of reference numerals:

101: photovoltaic module, 102: photovoltaic controller, 103: a bracket, 2: charging cabin, 201: storage battery, 202: power distribution module, 203: airborne ARM embedded system, 204: data transmission module, 205: charging module, 206: hatch opening module, 207: unmanned aerial vehicle transmission module.

Detailed Description

In the description of the present invention, it should be noted that, for the terms of orientation, such as "central", "lateral", "longitudinal", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", etc., it indicates that the orientation and positional relationship shown in the drawings are based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, but does not indicate or imply that the device or element referred to must have a specific orientation, be constructed in a specific orientation, and be operated without limiting the specific scope of protection of the present invention.

Furthermore, if the terms "first" and "second" are used for descriptive purposes only, they are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features. Thus, a definition of "a first" or "a second" feature may explicitly or implicitly include one or more of the feature, and in the description of the invention, "at least" means one or more unless specifically defined otherwise.

In the present invention, unless otherwise expressly specified or limited, the terms "assembled", "connected", and "connected" are to be construed broadly, e.g., as meaning fixedly connected, detachably connected, or integrally connected; or may be a mechanical connection; the two elements can be directly connected or connected through an intermediate medium, and the two elements can be communicated with each other. The specific meanings of the above terms in the present invention can be understood by those of ordinary skill in the art according to specific situations.

In the present invention, unless otherwise specified and limited, "above" or "below" a first feature may include the first and second features being in direct contact, and may also include the first and second features not being in direct contact but being in contact with each other through another feature therebetween. Also, the first feature being "above," "below," and "above" the second feature includes the first feature being directly above and obliquely above the second feature, or simply an elevation which indicates a level of the first feature being higher than an elevation of the second feature. The first feature being "above", "below" and "beneath" the second feature includes the first feature being directly below or obliquely below the second feature, or merely means that the first feature is at a lower level than the second feature.

The following describes the embodiments of the present invention with reference to the drawings of the specification, so that the technical solutions and the advantages thereof are more clear and clear. The embodiments described below are exemplary and are intended to be illustrative of the invention, but are not to be construed as limiting the invention.