A drone library with assisted landing function

Abstract

The utility model relates to the field of drones, and in particular to a drone hangar with an assisted landing function. The purpose of the utility model is to provide a drone hangar with an assisted landing function that allows drones to land stably. How to design a drone hangar with an assisted landing function, including a drone hangar, a cylinder, a support platform, a guide rail A and a lifting platform; a cylinder is fixedly connected inside the drone hangar, a support platform is fixedly connected on the drone hangar, a guide rail A is fixedly connected on the support platform, a lifting platform is fixedly connected to the top of the push rod of the cylinder, and the push rod of the cylinder is slidably connected to the support platform. By controlling the cylinder to push the lifting platform upward, the windbreak wall moves upward along the guide rail A, and the windbreak wall can pass through the through hole, so that the strong wind flowing from the outside passes through the wall to form an upper and lower interfering airflow on the inner side of the wall, which plays a role in reducing the impact of environmental wind on the landing of the drone, and achieves the effect of increasing the landing stability of the drone.

Description

Technical Field

[0001] The utility model relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle library with an auxiliary landing function. Background Art

[0002] A drone is an unmanned aircraft controlled by a radio remote control device and a self-contained program control device. It is currently used in aerial photography, agriculture, plant protection, micro selfies, express transportation, disaster relief, wildlife observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, and romance creation. After completing the work, the drone needs to return to the drone hangar for charging and storage. However, the drone will be disturbed when returning to the hangar in strong winds and heavy rains, resulting in deviations and even damage to the drone. Therefore, it is of great significance to design a drone hangar with an assisted landing function. Utility Model Content

[0003] In order to overcome the disadvantage of deviation caused by strong wind when the drone is stored, the utility model aims to provide a drone hangar with an auxiliary landing function that allows the drone to land stably.

[0004] Technical solution: A drone hangar with an auxiliary landing function, including a drone hangar, a cylinder, a support platform, a guide rail A, a lifting platform, a windbreak wall and a charging base. The cylinder is fixedly connected inside the drone hangar, the support platform is fixedly connected on the drone hangar, the guide rail A is fixedly connected on the support platform, the top of the cylinder's push rod is fixedly connected to the lifting platform, and the cylinder's push rod is slidably connected to the support platform, the lifting platform is fixedly connected to the windbreak wall, the guide rail A is slidably connected to the windbreak wall, and the lifting platform is fixedly connected to the charging base.

[0005] As an improvement of the above solution, the material of the windbreak wall is aluminum alloy, the shape of the windbreak wall is corrugated, and a plurality of through holes are opened on the windbreak wall.

[0006] As an improvement of the above scheme, it also includes a driver, a brush head and a guide rail B. The driver is fixedly connected to the lifting platform, the brush head is slidably connected to the left side of the driver, the guide rail B is fixedly connected to the charging base, and the brush head cooperates with the guide rail B.

[0007] As an improvement of the above scheme, it also includes a spring, a base groove and a buffer pad, the spring is fixedly connected to the lifting platform, the base groove is fixedly connected to the spring, one end of the spring is fixed to the lifting platform, and the other end is fixed to the bottom of the base groove, and the buffer pad is slidably connected to the base groove.

[0008] As an improvement of the above solution, a camera is also included, and the drone hangar is fixedly connected with the camera.

[0009] As an improvement of the above solution, it also includes an anemometer and a controller. The anemometer is fixedly connected to the drone hangar, and the controller is fixedly connected to the drone hangar.

[0010] 1. By controlling the cylinder to push the lifting platform upward, the windbreak wall moves upward along the guide rail A. The windbreak wall can pass through the through holes so that the strong wind from the outside passes through the wall to form an upward and downward interfering airflow on the inside of the wall, which reduces the effect of environmental wind on the landing of the drone and increases the landing stability of the drone.

[0011] 2. The driver drives the brush head to clean the landing area of ​​the drone, so that the dirt, dust and rain that the drone is stained with when it is on an outdoor mission can be effectively cleaned, which plays a role in cleaning the landing area of ​​the drone and achieves the effect of avoiding foreign objects causing malfunctions and poor contact when the drone is charging.

[0012] 3. The anemometer will judge the ambient wind speed and send a signal to the controller. When the ambient wind speed is high and the drone needs to land, the controller will control the hatch to open and start the cylinder at the same time to push the windbreak upward to complete the assisted landing. This allows the device to judge whether to enable the assisted landing function based on the environment, thereby reducing the energy consumption of the device. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 It is a schematic diagram of the three-dimensional structure of the utility model.

[0014] Figure 2 The utility model is a three-dimensional structural schematic diagram of the UAV hangar, anemometer and controller.

[0015] Figure 3 It is a three-dimensional structural schematic diagram of the cylinder, supporting platform and lifting platform of the utility model.

[0016] Figure 4 It is a three-dimensional structural schematic diagram of the driver, brush head and guide rail B of the utility model.

[0017] The numbers in the figure are as follows: 1. UAV hangar, 2. Cylinder, 3. Support platform, 4. Guide rail A, 5. Lifting platform, 6. Windbreak wall, 7. Charging base, 8. Driver, 9. Brush head, 10. Guide rail B, 11. Spring, 12. Base groove, 13. Buffer pad, 14. Camera, 15. Anemometer, 16. Controller. DETAILED DESCRIPTION

[0018] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0019] Embodiment: A drone library with an assisted landing function, such as Figure 1-4 As shown, it includes an unmanned aerial vehicle hangar 1, a cylinder 2, a supporting platform 3, a guide rail A4, a lifting platform 5, a windbreak wall 6 and a charging base 7. The cylinder 2 is fixedly connected in the unmanned aerial vehicle hangar 1, the supporting platform 3 is fixedly connected on the unmanned aerial vehicle hangar 1, the guide rail A4 is fixedly connected on the supporting platform 3, the top of the push rod of the cylinder 2 is fixedly connected to the lifting platform 5, and the push rod of the cylinder 2 is slidably connected to the supporting platform 3, the lifting platform 5 is fixedly connected to the windbreak wall 6, the material of the windbreak wall 6 is aluminum alloy, the shape of the windbreak wall 6 is corrugated, and a number of through holes are opened on the windbreak wall 6, the guide rail A4 is slidably connected to the windbreak wall 6, the lifting platform 5 is fixedly connected to the charging base 7, and also includes a driver 8, a brush head 9 and a guide rail B10, the driver 8 is fixedly connected to the lifting platform 5, the brush head 9 is slidably connected to the left side of the driver 8, the charging base 7 is fixedly connected to the guide rail B10, and the brush head 9 cooperates with the guide rail B10.

[0020] When the UAV needs to land, the operator controls the hatch to open slowly, and at this time the operator starts the cylinder 2, and the cylinder 2 passes through the support platform 3 and drives the lifting platform 5 to rise upward along the guide rail A4, and the lifting platform 5 drives the windbreak wall 6 to move upward. Because the windbreak wall 6 is in a corrugated shape and has a number of through holes, the strong wind from the outside through the wall forms an upward and downward interfering airflow on the inside of the wall, so as to achieve the effect of strong wind on the outside, weak wind on the inside, small wind on the outside, and no wind on the inside. At this time, the UAV lands smoothly under the action of the windbreak wall 6 When the drone is on the lifting platform 5, the driver 8 drives the brush head 9 along the guide rail B10 to clean the mud, dust and rainwater on the bottom of the drone and the charging base 7 when the drone is on an outdoor mission, thereby cleaning the landing area of ​​the drone and avoiding foreign objects from causing failures and poor contact when charging the drone. After the drone completes the landing, the drone docks with the charging base 7 for charging. After the drone is docked, the cylinder 2 controls the lifting platform 5 to move downward along the guide rail A4 to the target position and the hatch is closed.

[0021] like Figure 3As shown, it also includes a spring 11, a base groove 12 and a buffer pad 13. The spring 11 is fixedly connected to the lifting platform 5, and the base groove 12 is fixedly connected to the spring 11. One end of the spring 11 is fixed to the lifting platform 5, and the other end is fixed to the bottom of the base groove 12. The buffer pad 13 is slidably connected to the base groove 12.

[0022] When the drone lands, the base of the drone will first contact the buffer pad 13, and the buffer pad 13 will be affected by the gravity of the drone landing to first alleviate part of the impact force of the drone landing. At this time, the spring 11 will be compressed and further buffer the impact force of the drone landing. When the buffer pad 13 needs to be replaced, the buffer pad 13 can be dragged out backwards through the base groove 12 and replaced with a new buffer pad 13, which plays a role in alleviating the impact force generated when the drone lands and achieves the effect of protecting the drone.

[0023] like Figure 1 As shown, a camera 14 is also included, and the camera 14 is fixedly connected to the drone hangar 1.

[0024] The operator can observe the outside world through the camera 14, which plays the role of remotely observing the landing of the drone, thereby increasing the flexibility of the use of the drone hangar 1.

[0025] like Figure 1 As shown, it also includes an anemometer 15 and a controller 16. The anemometer 15 is fixedly connected to the drone hangar 1, and the controller 16 is fixedly connected to the drone hangar 1.

[0026] The anemometer 15 will make a judgment based on the ambient wind speed and send a signal to the controller 16. When the ambient wind speed is high and the drone needs to land, the controller 16 will control the cabin door to open and at the same time start the cylinder 2 to push the windbreak 6 upward to complete the assisted landing. This allows the device to judge whether to enable the assisted landing function based on the environment, thereby reducing the energy consumption of the device.

[0027] The above description is only an example of the implementation of the present invention and is not intended to limit the present invention. Any equivalent replacement made within the principle of the present invention shall be included in the protection scope of the present invention. The contents not elaborated in the present invention belong to the existing technology known to the technicians in this professional field.

[0028] In order to explain in detail the possible application scenarios, technical principles, specific schemes that can be implemented, and the purposes and effects that can be achieved of this application, the following is a detailed description in combination with the specific embodiments listed and the accompanying drawings. The embodiments recorded in this article are only used to more clearly illustrate the technical solutions of this application, and are therefore only used as examples, and cannot be used to limit the scope of protection of this application.

[0029] Reference to "embodiment" herein means that the specific features, structures or characteristics described in conjunction with the embodiment may be included in at least one embodiment of the present application. The term "embodiment" appearing in various places in the specification does not necessarily refer to the same embodiment, nor does it particularly limit its independence or association with other embodiments. In principle, in the present application, as long as there is no technical contradiction or conflict, the various technical features mentioned in the embodiments can be combined in any way to form a corresponding implementable technical solution.

Claims

1. An unmanned aerial vehicle hangar with an auxiliary landing function, comprising an unmanned aerial vehicle hangar (1), a cylinder (2) and a support platform (3), wherein the cylinder (2) is fixedly connected inside the unmanned aerial vehicle hangar (1), and the support platform (3) is fixedly connected on the unmanned aerial vehicle hangar (1), characterized in that: The invention also comprises a guide rail A (4), a lifting platform (5), a windbreak wall (6) and a charging base (7); the guide rail A (4) is fixedly connected to the support platform (3); the top of the push rod of the cylinder (2) is fixedly connected to the lifting platform (5); the push rod of the cylinder (2) is slidably connected to the support platform (3); the windbreak wall (6) is fixedly connected to the lifting platform (5); the guide rail A (4) is slidably connected to the windbreak wall (6); and the charging base (7) is fixedly connected to the lifting platform (5).

2. The drone hangar with assisted landing function as claimed in claim 1, characterized in that: The material of the windproof wall (6) is an aluminum alloy material, the shape of the windproof wall (6) is a corrugated shape, and a plurality of through holes are opened on the windproof wall (6).

3. The drone hangar with assisted landing function as claimed in claim 1, characterized in that: The utility model also comprises a driver (8), a brush head (9) and a guide rail B (10); the driver (8) is fixedly connected to the lifting platform (5); the brush head (9) is slidably connected to the left side of the driver (8); the guide rail B (10) is fixedly connected to the charging base (7); and the brush head (9) cooperates with the guide rail B (10).

4. The drone hangar with assisted landing function as claimed in claim 1, characterized in that: It also includes a spring (11), a base groove (12) and a buffer pad (13); the spring (11) is fixedly connected to the lifting platform (5); the spring (11) is fixedly connected to the base groove (12); one end of the spring (11) is fixed to the lifting platform (5) and the other end is fixed to the bottom of the base groove (12); and the buffer pad (13) is slidably connected to the base groove (12).

5. The drone hangar with assisted landing function as claimed in claim 1, characterized in that: It also includes a camera (14), and the camera (14) is fixedly connected to the drone hangar (1).

6. The drone hangar with assisted landing function as claimed in claim 1, characterized in that: It also includes an anemometer (15) and a controller (16). The anemometer (15) is fixedly connected to the drone hangar (1), and the controller (16) is fixedly connected to the drone hangar (1).

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