Unmanned aerial vehicle transporting, storing and launching integrated device

Abstract

The utility model relates to an unmanned aerial vehicle transportation, storage and launching integrated device, which comprises a box body, and a power supply, a launching assembly, a control assembly and a driving assembly which are arranged in the box body, the box body is provided with a launching port and a launching cover arranged on the launching port, the bottom of the box body is provided with a walking piece, and the driving assembly comprises a first driving piece and a second driving piece. The first driving piece and the second driving piece are in transmission connection with the walking piece and the transmitting cover respectively, the first driving piece, the second driving piece, the transmitting assembly and the control assembly are electrically connected with the power source, and the control assembly is in communication connection with the first driving piece and used for controlling the walking piece to act to drive the box body to move. The control assembly is in communication connection with the second driving part and used for controlling the launching cover to act to open or close the launching opening, and the control assembly is in communication connection with the launching assembly and used for launching the unmanned aerial vehicle arranged in the launching assembly through the launching opening. According to the utility model, the technical problems of unmanned aerial vehicle storage, remote launching and single-multi-tube launching are solved.

Description

Technical Field

[0001] The utility model belongs to the technical field of unmanned aerial vehicle (UAV) launching equipment, and in particular relates to an integrated device for transporting, storing and launching UAVs. Background Art

[0002] Drones (UAVs) have a wide range of applications in military, civilian, communications, and scientific research. Existing technologies, to ensure safe and stable transportation of UAVs, often use a transport-first, assembly-later method, shipping UAV parts and supporting equipment in batches. This is not only expensive but also time-sensitive, significantly impacting operational uncertainty.

[0003] In addition, drones also need to have good concealment during transportation. The existing transport boxes only have a transportation function, a single role, occupy a large area, and require transportation tools for transportation, which is not convenient for subsequent movement.

[0004] To sum up, there is an urgent need to provide a drone transportation, storage and launch integrated device that can realize the transportation, storage and launch of drones, has good stability and concealment in storing and transporting drones, and has a rapid launch response. Utility Model Content

[0005] The purpose of the utility model is to provide a drone transportation, storage and launching integrated device which can realize the transportation, storage and launching of drones, has good stability and concealment when storing and transporting drones, and has a fast launch response.

[0006] The above-mentioned purpose is achieved through the following technical solution: A device for transporting, storing and launching a drone, comprising a box and a power supply, a launching assembly, a control assembly and a driving assembly arranged in the box, the box being provided with a launching port and a launching cover arranged on the launching port, a walking part being provided at the bottom of the box, the driving assembly comprising a first driving part and a second driving part, the first driving part and the second driving part being respectively connected to the walking part and the launching cover in transmission, the first driving part, the second driving part, the launching assembly and the control assembly being electrically connected to the power supply, the control assembly being communicated with the first driving part and being used to control the movement of the walking part to drive the movement of the box, the control assembly being communicated with the second driving part and being used to control the movement of the launching cover to open or close the launching port, the control assembly being communicated with the launching assembly and being used to launch the drone built into the launching assembly through the launching port.

[0007] The utility model is used for the transportation, storage and launch of unmanned aerial vehicles (UAVs), and has the function of self - movement. During the application process, the UAV and the launch component are built into the box for storage. According to the arrangement, the control component controls the first driving part to actuate, driving the bottom walking part to move to a designated position to standby. When launching is required, the control component first controls the second driving part to actuate to open the launch port, and then controls the launch component to launch the UAV as needed. After launching the UAV, when everything inside the box is normal, the UAV launch port is closed to enter the standby state, etc.

[0008] A further technical solution is that the control component is provided with a wireless communication module and a control module. The wireless communication module is used to receive remote control instructions and transmit them to the control module for control operations. With this setting, the utility model can interact remotely with the control personnel through the wireless communication module and can accept remote instructions to perform actions such as walking and UAV launching.

[0009] A further technical solution is that an internal control component is provided inside the box. The internal control component includes multiple sensors. The multiple sensors are used to detect the humidity and temperature inside the box and transmit the detection signals to the control component. The wireless communication module is used to send the detection signals to a predetermined communication party. With this setting, the humidity, temperature inside the box and the UAV status can be detected in real - time.

[0010] A further technical solution is that the internal control component further includes an actuator. The actuator is electrically connected to the control component. After the control component makes a judgment based on the received detection signals, it can control the actuator to perform constant temperature and humidity control and automatic fire extinguishing operations. With this setting, the inside of the box can be kept at a constant temperature and humidity state, ensuring that the UAV can be launched normally. At the same time, if self - ignition and other phenomena occur during launching, automatic fire extinguishing can be carried out.

[0011] A further technical solution is that a solar charging panel is provided on the upper part of the box. The solar charging panel is electrically connected to the power supply. The power supply has the function of charging and energy storage. With this setting, when the utility model is in the standby state after moving to the designated position, the power supply is charged and stored energy through the solar charging panel to ensure normal operation thereafter.

[0012] A further technical solution is that the power supply is a storage battery.

[0013] A further technical solution is that the box is provided with bullet - proof armor. In specific applications, the appearance of the box can be similar to a container, having a certain concealment function. According to actual needs, bullet - proof armor is installed to have a certain good protection function.

[0014] A further technical solution is that the launch component is a multi - tube UAV launcher. With this setting, the control component can control the multi - tube UAV launcher to launch UAVs (single or group launch) to perform tasks.

[0015] A further technical solution is that the first driving member is a motor and the second driving member is a telescopic member.

[0016] A further technical solution is that the walking member is a moving wheel or a crawler.

[0017] Compared with the prior art, the application of the present utility model solves the technical problems of the storage, remote launching, and single / multi-tube launching of unmanned aerial vehicles. Through the present utility model, the transportation, storage, and launching of unmanned aerial vehicles are realized. It has good stability and concealment during the storage and transportation of unmanned aerial vehicles, and has advantages such as rapid response during launching. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] The accompanying drawings constituting a part of the present utility model are used to provide a further understanding of the present utility model. The schematic embodiments of the present utility model and their descriptions are used to explain the present utility model and do not constitute an improper limitation to the present utility model.

[0019] Figure 1 FIG. is a schematic structural diagram of an integrated device for transporting, storing, and launching unmanned aerial vehicles according to an embodiment of the present utility model;

[0020] Figure 2 is Figure 1 a schematic structural diagram of the integrated device for transporting, storing, and launching unmanned aerial vehicles after opening the launch port as involved in ;

[0021] Figure 3 FIG. is a schematic internal structural diagram of the integrated device for transporting, storing, and launching unmanned aerial vehicles according to an embodiment of the present utility model;

[0022] Figure 4 is Figure 1 a schematic structural diagram of another perspective of the integrated device for transporting, storing, and launching unmanned aerial vehicles as involved in.

[0023] In the figure:

[0024] 1 box body, 2 solar charging panel, 3 launch cover, 4 multi-tube launcher

[0025] 5 walking member, 6 internal control component, 7 control component, 8 power supply

[0026] 9 second driving member, 10 launch port DETAILED DESCRIPTION OF THE EMBODIMENTS

[0027] The present utility model will be described in detail below with reference to the accompanying drawings. The description in this part is only exemplary and explanatory, and should not have any restrictive effect on the protection scope of the present utility model. In addition, those skilled in the art can make corresponding combinations of the features in the embodiments in this document and in different embodiments according to the description of this document.

[0028] The embodiments of the present utility model are as follows. Refer to Figures 1 to 4 , a device for transporting, storing, and launching a drone integrally, which includes a box body 1 and a power supply 8, a launching component, a control component 7, and a driving component arranged inside the box body 1. The box body 1 is provided with a launching port 10 and a launching cover 3 arranged on the launching port 10. The bottom of the box body 1 is provided with a walking component 5. The driving component includes a first driving part and a second driving part 9. The first driving part and the second driving part 9 are respectively in transmission connection with the walking component 5 and the launching cover 3. The first driving part, the second driving part 9, the launching component, and the control component 7 are electrically connected to the power supply 8. The control component 7 is in communication connection with the first driving part and is used to control the movement of the walking component 5 to drive the box body 1 to move. The control component 7 is in communication connection with the second driving part 9 and is used to control the action of the launching cover 3 to open or close the launching port 10. The control component 7 is in communication connection with the launching component and is used to launch the drone built in the launching component through the launching port 10.

[0029] The present utility model is used for transporting, storing, and launching a drone and has a self - moving function. During the application process, the drone and the launching component are built in the box body 1 for storage. According to the arrangement, the control component 7 controls the first driving part to drive the bottom walking component 5 to move to a designated position for standby. When launching is required, the control component 7 first controls the second driving part 9 to open the launching port 10, and then controls the launching component to launch the drone as needed. After launching the drone, when everything inside the box body 1 is normal, the drone launching port 10 is closed to enter the standby state, etc.

[0030] Based on the above - mentioned embodiment, in another embodiment of the present utility model, as Figure 3 , the control component 7 is provided with a wireless communication module and a control module. The wireless communication module is used to receive a remote control instruction and transmit it to the control module for control operations. With such a setting, the present utility model can remotely interact with the control personnel through the wireless communication module and can receive remote instructions to perform actions such as walking and drone launching.

[0031] Based on the above - mentioned embodiment, in another embodiment of the present utility model, as Figure 3 , an internal control component 6 is arranged inside the box body 1. The internal control component 6 includes multiple sensors. The multiple sensors are used to detect the humidity and temperature inside the box body 1 and transmit the detection signals to the control component 7. The wireless communication module is used to send the detection signals to a predetermined communication party. With such a setting, the humidity and temperature inside the box body 1 and the state of the drone can be detected in real time.

[0032] Based on the above embodiments, in another embodiment of the present utility model, the internal control component 6 further includes an actuator, and the actuator is electrically connected to the control component 7. After the control component 7 makes a judgment based on the received detection signal, it can control the actuator to perform constant temperature and humidity control and automatic fire extinguishing operations. With such a setting, it can ensure that the interior of the box body 1 reaches a constant temperature and humidity state, ensuring that the unmanned aerial vehicle can be launched normally. At the same time, in case of spontaneous combustion or other phenomena during the launch, automatic fire extinguishing can be carried out.

[0033] Based on the above embodiments, in another embodiment of the present utility model, Figure 1 and Figure 4 , a solar charging panel 2 is provided on the upper part of the box body 1, and the solar charging panel 2 is electrically connected to the power supply 8, and the power supply 8 has a charging and energy storage function. With such a setting, when the present utility model is in the standby state after moving to the designated position, the solar charging panel 2 charges and stores energy for the power source, ensuring that it can operate normally thereafter.

[0034] Based on the above embodiments, in another embodiment of the present utility model, Figure 3 , the power supply 8 is a storage battery.

[0035] Based on the above embodiments, in another embodiment of the present utility model, the box body 1 is provided with bulletproof armor. In specific applications, the appearance of the box body 1 can be similar to that of a container, having a certain concealment function, and bulletproof armor can be installed according to actual needs to have a certain good protection function.

[0036] Based on the above embodiments, in another embodiment of the present utility model, Figure 2 and Figure 3 , the launch component is a multi-tube launcher 4 for unmanned aerial vehicles. With such a setting, the control component 7 can control the multi-tube launcher 4 for unmanned aerial vehicles to launch unmanned aerial vehicles (single or group launch) to perform tasks.

[0037] Based on the above embodiments, in another embodiment of the present utility model, Figure 2 , the first driving member is a motor, and the second driving member 9 is a telescopic member.

[0038] Based on the above embodiments, in another embodiment of the present utility model, Figure 4 , the walking member 5 is a mobile wheel or a track.

[0039] The above are only the preferred embodiments of the present utility model. It should be noted that for those of ordinary skill in the art, without departing from the principle of the present utility model, several improvements and refinements can be made, and these improvements and refinements should also be regarded as the protection scope of the present utility model.

Claims

1. An integrated device for transporting, storing and launching an unmanned aerial vehicle, characterized in that, The invention comprises a box body and a power supply, a launching assembly, a control assembly and a driving assembly arranged in the box body, the box body is provided with a launching port and a launching cover arranged on the launching port, a walking part is provided at the bottom of the box body, the driving assembly comprises a first driving member and a second driving member, the first driving member and the second driving member are respectively connected to the walking part and the launching cover in transmission connection, the first driving member, the second driving member, the launching assembly and the control assembly are electrically connected to the power supply, the control assembly is communicatively connected to the first driving member and is used to control the movement of the walking member to drive the movement of the box body, the control assembly is communicatively connected to the second driving member and is used to control the movement of the launching cover to open or close the launching port, the control assembly is communicatively connected to the launching assembly and is used to launch the drone built into the launching assembly through the launching port.

2. The integrated device for transporting, storing, and launching a drone according to claim 1, characterized in that, The control component is provided with a wireless communication module and a control module. The wireless communication module is used to receive remote control instructions and transmit them to the control module for control operations.

3. The integrated device for transporting, storing, and launching a drone according to claim 2, characterized in that, An internal control component is provided in the box, and the internal control component includes multiple sensors. The multiple sensors are used to detect the humidity and temperature in the box and transmit the detection signals to the control component. The wireless communication module is used to send the detection signals to a predetermined communication party.

4. The integrated device for transporting, storing and launching a drone according to claim 3, characterized in that, The internal control component also includes an actuator, which is electrically connected to the control component. The control component can control the actuator to perform constant temperature and humidity and automatic fire extinguishing operations after making a judgment based on the received detection signal.

5. The integrated device for transporting, storing, and launching a drone according to any one of claims 1 to 4, characterized in that, A solar charging panel is provided on the upper portion of the box body. The solar charging panel is electrically connected to the power supply, and the power supply has a charging and energy storage function.

6. The integrated device for transporting, storing and launching of the unmanned aerial vehicle according to claim 5, wherein, The power source is a battery.

7. The integrated device for transporting, storing and launching an unmanned aerial vehicle according to any one of claims 1 to 4, characterized in that, The box body is provided with bulletproof armor.

8. The integrated device for transporting, storing and launching an unmanned aerial vehicle according to any one of claims 1 to 4, characterized in that The launching assembly is a multi-tube launcher for a UAV.

9. The integrated device for transporting, storing and launching an unmanned aerial vehicle according to claim 1, wherein The first driving member is a motor, and the second driving member is a telescopic member.

10. The integrated device for transporting, storing and launching of an unmanned aerial vehicle according to claim 9, characterized in that, The walking parts are moving wheels or crawlers.

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