Unmanned aerial vehicle garage base mounting and fixing structure

Abstract

The utility model relates to the technical field of unmanned aerial vehicle garages, and discloses an unmanned aerial vehicle garage base mounting and fixing structure which comprises a base, a plurality of mounting holes are formed in the upper surface of the base, two supporting plates are fixedly connected to the outer surface of the base, limiting rods are welded to the upper surfaces of the two supporting plates, and the multiple limiting rods are made of metal materials; the outer surfaces of the multiple limiting rods are each sleeved with a plurality of balancing weights, the outer surface of the base is fixedly connected with two bearing plates, and the upper surfaces of the two bearing plates are each fixedly connected with a plurality of inserting rods. According to the unmanned aerial vehicle garage base installing and fixing structure, the self weight of the base can be increased through cooperation of the balancing weight and the sandbag so that large wind power can be resisted, meanwhile, wind resistance can be reduced through the hollowed-out design of the base so that thrust acting on the base can be reduced, and friction force between the supporting plate and the ground and friction force between the bearing plate and the ground can be increased through the arrangement of the anti-skid plate; and therefore, the base can be more stably placed on the ground.

Description

Technical Field

[0001] The present application relates to the technical field of drone hangars, specifically to a fixing structure for installing a drone hangar base. Background Art

[0002] A drone hangar, that is, a drone storage, maintenance, deployment and management site. With the rapid development and wide application of drone technology, drone hangars play an important role in multiple fields. Drone hangars not only provide parking space for drones, but also integrate digital management and intelligent deployment technologies. Through advanced drone equipment and software systems, centralized control and optimized scheduling of drones are achieved.

[0003] When drones are not in use, they are usually placed in the hangar, and the hangar is usually installed on the base. Normally, the installation of the drone hangar base is carried out by piling up a cement platform. Now, in some areas, building owners on the roof are not allowed to use this method, and it is also not possible to directly fix expansion bolts on the roof, which is rather inconvenient to use. Summary of the Utility Model

[0004] Aiming at the deficiencies of the prior art, the present application provides a fixing structure for installing a drone hangar base, which has the advantages of improving wind resistance and solves the problems raised in the background art.

[0005] To achieve the above object, the present application provides the following technical solution: A fixing structure for installing a drone hangar base, including a base. A plurality of mounting holes are provided on the upper surface of the base. Two support plates are fixedly connected to the outer surface of the base. Limiting rods are welded to the upper surfaces of the two support plates. A plurality of the limiting rods are made of metal. A plurality of counterweight blocks are sleeved on the outer surfaces of the plurality of limiting rods. Two bearing plates are fixedly connected to the outer surface of the base. A plurality of insertion rods are fixedly connected to the upper surfaces of the two bearing plates. Sandbags are provided on the upper surfaces of the two bearing plates. A plurality of the insertion rods are inserted into the sandbags adjacent to them.

[0006] Through the above solution, the self-weight of the base can be increased by the cooperation of installing counterweight blocks and sandbags, thereby withstanding greater wind force.

[0007] Further, the base is made of steel structure and undergoes an anti-rust treatment.

[0008] Through the above solution, the anti-rust treatment of the base can prevent the base from being corroded by rainwater and improve its service life.

[0009] Further, the base is designed with a hollow structure.

[0010] Through the above solution, the hollow design of the base can reduce wind resistance and the thrust acting on the base.

[0011] Furthermore, anti-slip plates are installed on the bottom surfaces of the two support plates and the two bearing plates.

[0012] Through the above solution, installing anti-slip plates can increase the resistance between the base and the ground, enabling the base to be placed on the ground more stably.

[0013] Furthermore, stainless steel water tanks are welded on the upper surfaces of the two support plates, and the two stainless steel water tanks are symmetrical.

[0014] Through the above solution, installing stainless steel water tanks can fill them with water to increase the weight of the base, enabling the base to withstand stronger winds.

[0015] Furthermore, multiple counterweight blocks are all made of lead blocks.

[0016] Through the above solution, making the counterweight blocks of lead blocks can prevent the counterweight blocks from rusting and sticking together due to long-term contact with the limiting rods, facilitating the disassembly of the counterweight blocks.

[0017] Furthermore, a plurality of rubber pads are fixedly connected to the upper surface of the base, and the plurality of rubber pads are distributed in a matrix.

[0018] Through the above solution, installing rubber pads can improve the protection of the external hangar, preventing rigid contact between the hangar and the base during installation and causing damage to the hangar.

[0019] Furthermore, water inlet pipes are fixedly connected to the upper surfaces of the two stainless steel water tanks, and valves are installed on the outer surfaces of the two water inlet pipes.

[0020] Through the above solution, installing valves can seal the stainless steel water tanks, preventing the water source in the stainless steel water tanks from volatilizing and affecting the weight of the base.

[0021] Compared with the prior art, the technical solution of the present application has the following beneficial effects:

[0022] For the installation and fixing structure of the drone hangar base, by installing counterweight blocks and sandbags in cooperation, the self-weight of the base can be increased, thereby withstanding greater winds. At the same time, the base is designed with a hollow structure to reduce wind resistance, thereby reducing the thrust acting on the base, and by setting anti-slip plates, the friction between the support plates, bearing plates and the ground can be increased, enabling the base to be placed on the ground more stably. BRIEF DESCRIPTION OF THE DRAWINGS

[0023] Figure 1 It is a schematic diagram of the overall structure of the present application Figure 1 ;

[0024] Figure 2 It is a schematic diagram of the insertion rod structure of the present application;

[0025] Figure 3 Schematic diagram of the overall structure of this application Figure 2 ;

[0026] Figure 4 Schematic diagram of the base structure of this application

[0027] In the figure:

[0028] 1. Base; 2. Mounting holes; 3. Support plates; 4. Limiting rods; 5. Counterweight blocks; 6. Bearing plates; 7. Insertion rods; 8. Sandbags; 9. Anti-slip plates; 10. Stainless steel water tank; 11. Rubber pads; 12. Water inlet pipes; 13. Valves Specific implementation manners

[0029] Next, the technical solutions in the embodiments of this application will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of this application. Obviously, the described embodiments are only a part of the embodiments of this application, rather than all the embodiments. Based on the embodiments in this application, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of this application

[0030] Please refer to Figure 1 , Figure 2 and Figure 3 , the base mounting and fixing structure of the drone hangar in this embodiment includes a base 1. A plurality of mounting holes 2 are provided on the upper surface of the base 1. Two support plates 3 are fixedly connected to the outer surface of the base 1. Limiting rods 4 are welded to the upper surfaces of the two support plates 3. A plurality of limiting rods 4 are made of metal. A plurality of counterweight blocks 5 are sleeved on the outer surfaces of the plurality of limiting rods 4. Two bearing plates 6 are fixedly connected to the outer surface of the base 1. A plurality of insertion rods 7 are fixedly connected to the upper surfaces of the two bearing plates 6. Sandbags 8 are provided on the upper surfaces of the two bearing plates 6. A plurality of insertion rods 7 are inserted into the sandbags 8 adjacent to them. By cooperating with the installation of the counterweight blocks 5 and the sandbags 8, the self-weight of the base 1 can be increased, thereby resisting greater wind forces. At the same time, the base 1 is designed with a hollow structure to reduce wind resistance, thereby reducing the thrust acting on the base 1. And by setting the anti-slip plates 9, the friction between the support plates 3, the bearing plates 6 and the ground can be increased, so that the base 1 can be placed on the ground more stably

[0031] Please refer to Figure 1 , Figure 2 and Figure 3 , the base 1 is made of steel structure and undergoes rust prevention treatment. The rust prevention treatment of the base 1 can prevent the base 1 from being corroded by rainwater and improve its service life. The base 1 is designed with a hollow structure, which can reduce wind resistance and the thrust acting on the base 1. Anti-slip plates 9 are installed on the bottom surfaces of the two support plates 3 and the two bearing plates 6. Installing the anti-slip plates 9 can increase the resistance between the base 1 and the ground, so that the base 1 can be placed on the ground more stably

[0032] Please refer to Figure 1 、 Figure 2 and Figure 4 . On the upper surfaces of both support plates 3, stainless steel water tanks 10 are welded. The two stainless steel water tanks 10 are symmetrical. Installing the stainless steel water tanks 10 can inject water into their interiors to increase the weight of the base 1, so that the base 1 can resist stronger winds. A plurality of counterweight blocks 5 are all made of lead blocks. Making the counterweight blocks 5 of lead blocks can prevent the counterweight blocks 5 from rusting and sticking together due to long-term contact with the limiting rods 4, which is convenient for disassembling the counterweight blocks 5. On the upper surface of the base 1, a plurality of rubber pads 11 are fixedly connected. The plurality of rubber pads 11 are distributed in a matrix. Installing the rubber pads 11 can improve the protection against the external hangar and prevent rigid contact between the hangar and the base 1 during installation, resulting in damage to the hangar. On the upper surfaces of both stainless steel water tanks 10, water inlet pipes 12 are fixedly connected. Valves 13 are installed on the outer surfaces of both water inlet pipes 12. Installing the valves 13 can seal the stainless steel water tanks 10 and prevent the water source in the stainless steel water tanks 10 from volatilizing and affecting the weight of the base 1.

[0033] In the installation and fixing structure of the UAV hangar base in this embodiment, by installing the counterweight blocks 5 and sandbags 8 in cooperation, the self-weight of the base 1 can be increased, so as to resist greater winds. At the same time, the base 1 is designed with a hollow structure to reduce wind resistance, thereby reducing the thrust acting on the base 1, and by setting the anti-slip plates 9, the friction between the support plates 3, the bearing plates 6 and the ground can be increased, so that the base 1 can be placed on the ground more stably.

[0034] The working principle of the above embodiment is as follows: When installing the hangar, the hangar is installed on the base 1 by using the cooperation of bolts and the mounting holes 2. By installing the rubber pad 11, the protection of the external hangar can be improved, avoiding rigid contact between the hangar and the base 1 during installation, which may cause damage to the hangar, thus enhancing the protection of the hangar. Subsequently, the sandbag 8 is placed on the bearing plate 6, and the stainless steel water tank 10 is filled with water through the water inlet pipe 12. After the water injection is completed, the stainless steel water tank 10 is closed by closing the valve 13. Then, multiple counterweight blocks 5 are sleeved on the limiting rod 4. By installing the counterweight blocks 5 and the sandbags 8 in cooperation, the self-weight of the base 1 can be increased, thereby withstanding stronger winds. At the same time, the base 1 is designed with a hollow structure to reduce wind resistance, thereby reducing the thrust acting on the base 1. By setting the anti-slip plate 9, the friction between the support plate 3, the bearing plate 6 and the ground can be increased, so that the base 1 can be placed more stably on the ground. By installing the water tank, the self-weight of the base 1 can be increased, making it more stable. By installing the insertion rod 7, it can penetrate into the sandbag 8, so that the sandbag 8 can be stably placed on the bearing plate 6, avoiding displacement of the sandbag 8, which may affect the stability of the base 1. The counterweight block 5 is made of lead to avoid rusting together due to long-term contact between the counterweight block 5 and the limit 4, facilitating the disassembly of the counterweight block 5. By installing the anti-slip plate 9, since the directions of each group of anti-slip plates 9 are opposite, the resistance between the base 1 and the ground when pushed by winds in multiple directions can be increased. Through the cooperation of the support plate 3 and the bearing plate 6, the contact area between the base 1 and the ground can be increased. With the self-weight of the base 1, stronger winds can be withstood, avoiding the displacement of the base 1 caused by the wind, and enabling the base 1 to be stably placed on the ground. The counterweight block (5) is made of lead to avoid rusting together due to long-term contact between the counterweight block 5 and the limiting rod 4, facilitating the disassembly of the counterweight block 5 and facilitating the subsequent movement of the base 1.

[0035] It should be noted that in this article, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variant thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements not only includes those elements, but also includes other elements not expressly listed, or elements inherent to such process, method, article or device. Without further limitation, an element defined by the statement "including a..." does not exclude the existence of additional identical elements in the process, method, article or device including the element.

[0036] Although embodiments of the present application have been shown and described, it will be understood by those of ordinary skill in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present application. The scope of the present application is defined by the appended claims and their equivalents.

Claims

1. Drone hangar base installation and fixing structure, including a base (1), characterized in that: The upper surface of the base (1) is provided with a plurality of mounting holes (2). The outer surface of the base (1) is fixedly connected with two support plates (3). The upper surfaces of the two support plates (3) are both welded with limiting rods (4). A plurality of the limiting rods (4) are all made of metal. A plurality of counterweight blocks (5) are sleeved on the outer surfaces of the plurality of limiting rods (4). The outer surface of the base (1) is fixedly connected with two bearing plates (6). A plurality of insertion rods (7) are fixedly connected to the upper surfaces of the two bearing plates (6). Sandbags (8) are arranged on the upper surfaces of the two bearing plates (6). A plurality of the insertion rods (7) all penetrate into the sandbags (8) adjacent to them.

2. The base mounting and fixing structure of the drone hangar according to claim 1, characterized in that: The base (1) is made of steel structure and undergoes an anti-rust treatment.

3. The base mounting and fixing structure of the drone hangar according to claim 1, characterized in that: The base (1) is designed with a hollow structure.

4. The base mounting and fixing structure of the drone hangar according to claim 1, wherein: Anti-slip plates (9) are installed on the bottom surfaces of the two support plates (3) and the two bearing plates (6).

5. The base mounting and fixing structure of the drone hangar according to claim 1, wherein: Stainless steel water tanks (10) are welded on the upper surfaces of the two support plates (3). The two stainless steel water tanks (10) are symmetrical to each other.

6. The base mounting and fixing structure of the drone hangar according to claim 1, wherein: A plurality of the counterweight blocks (5) are all made of lead blocks.

7. The base mounting and fixing structure of the drone hangar according to claim 1, characterized in that: A plurality of rubber pads (11) are fixedly connected to the upper surface of the base (1). The plurality of rubber pads (11) are distributed in a matrix.

8. The base mounting and fixing structure of the drone hangar according to claim 5, characterized in that: Water inlet pipes (12) are fixedly communicated with the upper surfaces of the two stainless steel water tanks (10). Valves (13) are installed on the outer surfaces of the two water inlet pipes (12).

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