Unmanned aerial vehicle take-off and landing platform

Abstract

The unmanned aerial vehicle take-off and landing platform comprises a bottom plate, supporting feet, a threaded rod and a conical block, a lantern ring is fixedly installed on the outer side of the threaded rod, a reinforcing plate is fixedly installed on the inner wall of the lantern ring, the inner wall of the reinforcing plate is in threaded connection with a reinforcing rod, a damper is fixedly installed in the bottom plate, and the damper is fixedly connected with the conical block. A damping spring is arranged on the outer side of the damper, a movable rod is fixedly installed at the upper end of the damper, a base plate is fixedly installed at the upper end of the movable rod, and a limiting frame is arranged on the upper side of the base plate. The supporting legs, the threaded rods, the conical blocks and the reinforcing rods are used in cooperation, so that the unmanned aerial vehicle can be placed on the complex ground more stably, it is guaranteed that the situation that the unmanned aerial vehicle is damaged due to instability of the vehicle body is avoided, and use safety is guaranteed; and meanwhile, impact force generated in the falling process of the unmanned aerial vehicle is buffered through multiple layers of buffering mechanisms, and the situation that the unmanned aerial vehicle is damaged due to the impact force is reduced.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a take-off and landing platform for unmanned aerial vehicles. Background Art

[0002] Unmanned aerial vehicle, abbreviated as "UAV" in English, is an unmanned aircraft controlled by radio remote control equipment and self-contained program control device, or operated completely or intermittently autonomously by an on-board computer.

[0003] The existing UAV take-off and landing platforms have the following defects in daily use:

[0004] 1. When the existing UAV take-off and landing platform is used in some complex terrains, such as uneven terrain in the wild, it is easy to cause the body to become unstable during take-off and landing, causing damage to the UAV, and the safety of use is difficult to ensure;

[0005] 2. The existing UAV take-off and landing platform lacks a buffer mechanism. If the UAV lands directly on the take-off and landing platform, the UAV will be damaged due to excessive impact force during the falling process. Therefore, we propose a new type of UAV take-off and landing platform. Utility Model Content

[0006] The utility model provides a UAV take-off and landing platform to solve the problems raised in the above background technology.

[0007] In order to achieve the above purpose, the utility model adopts the following technical solutions:

[0008] A drone landing and taking-off platform comprises a base plate, the bottom of which is fixedly provided with a supporting foot, the inner wall of the supporting foot is threadedly connected to a threaded rod, the lower end of the threaded rod is fixedly provided with a conical block, the outer side of the threaded rod is fixedly provided with a collar, the inner wall of the collar is fixedly provided with a reinforcing plate, the inner wall of the reinforcing plate is threadedly connected to a reinforcing rod, a damper is fixedly provided inside the base plate, a shock-absorbing spring is arranged on the outer side of the damper, a movable rod is fixedly provided on the upper end of the damper, a base plate is fixedly provided on the upper end of the movable rod, a limit frame is arranged on the upper side of the base plate, a landing pad is fixedly provided on the inner wall of the limit frame, a positioning buckle is fixedly provided on the outer side of the limit frame, the inner wall of the positioning buckle is threadedly connected to the positioning rod, and a buffer column is fixedly provided on the lower side of the base plate.

[0009] As a further improvement of the technical solution: a stabilizing rod is fixedly installed on the inner side of the supporting foot.

[0010] As a further improvement of the technical solution: the conical block is made of stainless steel.

[0011] As a further improvement of the technical solution: the landing pad and the buffer column are both made of rubber material, wherein the buffer column is arranged between the base plate and the bottom plate.

[0012] As a further improvement of the technical solution: a positioning rod hole is opened inside the base plate, wherein the positioning rod is threadedly connected in the positioning rod hole.

[0013] As a further improvement of the technical solution: the lower end of the shock absorbing spring is fixedly installed inside the bottom plate, and the upper end of the shock absorbing spring is fixedly installed on the lower end of the movable rod.

[0014] Compared with the prior art, the beneficial effects of the utility model are:

[0015] 1. Adjust the extension length of the threaded rod according to the actual ground conditions, insert the conical block into the ground, and then rotate the reinforcement rod to insert it into the ground, so that the drone can be placed more firmly on the complex ground, ensuring that the drone will not be damaged due to body instability during take-off and landing, ensuring the safety of use;

[0016] 2. The landing pad will provide the first buffering for the impact force of the drone's fall, the damper and shock-absorbing spring will provide the second buffering for the impact force, and the buffer column will provide the third buffering for the impact force of the drone. The multi-layer buffer mechanism is used to buffer the impact force of the drone during its fall, reducing the possibility of damage to the drone due to the impact force.

[0017] The above description is only an overview of the technical solution of the utility model. In order to more clearly understand the technical means of the utility model and implement it according to the contents of the specification, the following is a detailed description of the preferred embodiment of the utility model with the accompanying drawings. The specific implementation method of the utility model is given in detail by the following embodiments and their drawings. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] The drawings described herein are used to provide a further understanding of the present invention and constitute a part of the present application. The exemplary embodiments of the present invention and their descriptions are used to explain the present invention and do not constitute an improper limitation on the present invention. In the drawings:

[0019] Figure 1 It is a structural schematic diagram of the utility model;

[0020] Figure 2 It is a schematic diagram of the structure of the shock absorbing spring of the utility model;

[0021] Figure 3 It is a schematic diagram of the positioning rod structure of the utility model.

[0022] In the accompanying drawings, the components represented by the reference numerals are listed as follows:

[0023] 1. Base plate; 2. Support feet; 3. Threaded rod; 4. Conical block; 5. Ring; 6. Reinforcement plate; 7. Reinforcement rod; 8. Damper; 9. Shock-absorbing spring; 10. Movable rod; 11. Base plate; 12. Limit frame; 13. Landing pad; 14. Positioning buckle; 15. Positioning rod; 16. Buffer column. DETAILED DESCRIPTION

[0024] The principles and features of the present invention are described below in conjunction with the accompanying drawings. The examples given are only used to explain the present invention and are not used to limit the scope of the present invention. The present invention is described in more detail in the following paragraphs by way of example with reference to the accompanying drawings. The advantages and features of the present invention will become clearer according to the following description and claims. It should be noted that the drawings are all in a very simplified form and are not in precise proportions, and are only used to conveniently and clearly assist in explaining the purpose of the embodiments of the present invention.

[0025] It should be noted that when a component is referred to as being "fixed to" another component, it may be directly on the other component or there may also be a component centered. When a component is considered to be "connected to" another component, it may be directly connected to the other component or there may also be a component centered. When a component is considered to be "set on" another component, it may be directly set on the other component or there may also be a component centered. The terms "vertical", "horizontal", "left", "right" and similar expressions used herein are for illustrative purposes only.

[0026] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as those commonly understood by those skilled in the art in the technical field of the present invention. The terms used herein in the specification of the present invention are only for the purpose of describing specific embodiments and are not intended to limit the present invention. The term "and / or" used herein includes any and all combinations of one or more related listed items.

[0027] See also Figures 1 to 3In the embodiment of the utility model, a UAV take-off and landing platform includes a base plate 1, a support foot 2 is fixedly installed at the bottom of the base plate 1, a threaded rod 3 is threadedly connected to the inner wall of the support foot 2, a conical block 4 is fixedly installed at the lower end of the threaded rod 3, a collar 5 is fixedly installed on the outer side of the threaded rod 3, a reinforcing plate 6 is fixedly installed on the inner wall of the collar 5, a reinforcing rod 7 is threadedly connected to the inner wall of the reinforcing plate 6, a damper 8 is fixedly installed inside the base plate 1, a shock-absorbing spring 9 is arranged on the outer side of the damper 8, a movable rod 10 is fixedly installed on the upper end of the damper 9, a base plate 11 is fixedly installed on the upper end of the movable rod 10, a limit frame 12 is arranged on the upper side of the base plate 11, a landing pad 13 is fixedly installed on the inner wall of the limit frame 12, a positioning buckle 14 is fixedly installed on the outer side of the limit frame 12, a positioning rod 15 is threadedly connected to the inner wall of the positioning buckle 14, and a buffer column 16 is fixedly installed on the lower side of the base plate 11.

[0028] See also Figure 1 A stabilizing rod is fixedly installed on the inner side of the support leg 2, and the stability of the UAV take-off and landing platform is enhanced by the stabilizing rod.

[0029] See also Figure 1 The conical block 4 is made of stainless steel. The conical block 4 made of stainless steel has good rust resistance and corrosion resistance, which can effectively improve the service life of the conical block 4.

[0030] See also Figure 1-2 The landing pad 13 and the buffer column 16 are both made of rubber material, wherein the buffer column 16 is arranged between the base plate 11 and the bottom plate 1. The landing pad 13 and the buffer column 16 buffer and reduce the impact force during the falling process of the drone, thereby ensuring the integrity of the drone.

[0031] See also Figure 1 and Figure 3 A positioning rod hole is provided inside the base plate 11, wherein the positioning rod 15 is threadedly connected in the positioning rod hole. The base plate 11 can be fixed to the bottom plate 1 by using the positioning rod 15 in conjunction with the positioning buckle 14.

[0032] See also Figure 1-2 The lower end of the shock-absorbing spring 9 is fixedly installed inside the bottom plate 1, and the upper end of the shock-absorbing spring 9 is fixedly installed on the lower end of the movable rod 10. The shock-absorbing spring 9 and the damper 8 are used in combination to buffer the impact force during the landing of the drone.

[0033] The working principle of the utility model is as follows: when installing the UAV take-off and landing platform on a complex terrain, the extension length of the threaded rod 3 is adjusted directly according to the actual ground conditions, the supporting foot 2 is held by one hand, the threaded rod 3 is held by the other hand, the threaded rod 3 is rotated, the extension length thereof is adjusted, and then the conical block 4 is inserted into the ground, the reinforcing rod 7 is rotated, so that the reinforcing rod 7 is inserted into the ground, so that the UAV can be placed more firmly on the complex ground, and the UAV body will not be damaged due to instability during the take-off and landing process, and the safety of use is ensured. When the UAV lands, the UAV directly lands on the landing pad 13, and the landing pad 13 will buffer the impact force of the UAV falling for the first time. At the same time, the movable rod 10 and the base plate 11 will move downward under the pressure to compress the shock absorbing spring 9, the damper 8 and the shock absorbing spring 9 will buffer the impact force for the second time, and the buffer column 16 will buffer the impact force of the UAV for the third time, and the multi-layer buffer mechanism is used to buffer the impact force of the UAV during the falling process, so as to reduce the damage of the UAV due to the impact force.

[0034] The above description is only a preferred embodiment of the utility model and does not impose any form of limitation on the utility model. Any ordinary technician in the industry can smoothly implement the utility model as shown in the drawings of the specification and described above. However, any equivalent changes, modifications and evolutions made by technicians familiar with the profession without departing from the scope of the technical solution of the utility model using the technical content disclosed above are all equivalent embodiments of the utility model. At the same time, any equivalent changes, modifications and evolutions made to the above embodiments based on the essential technology of the utility model are still within the protection scope of the technical solution of the utility model.

Claims

1. A UAV take-off and landing platform, characterized in that: The invention comprises a base plate (1), wherein a support foot (2) is fixedly installed at the bottom of the base plate (1), a threaded rod (3) is threadedly connected to the inner wall of the support foot (2), a conical block (4) is fixedly installed at the lower end of the threaded rod (3), a collar (5) is fixedly installed on the outer side of the threaded rod (3), a reinforcing plate (6) is fixedly installed on the inner wall of the collar (5), a reinforcing rod (7) is threadedly connected to the inner wall of the reinforcing plate (6), a damper (8) is fixedly installed inside the base plate (1), and a A shock absorbing spring (9), a movable rod (10) is fixedly mounted on the upper end of the damper (8), a base plate (11) is fixedly mounted on the upper end of the movable rod (10), a limit frame (12) is arranged on the upper side of the base plate (11), a landing pad (13) is fixedly mounted on the inner wall of the limit frame (12), a positioning buckle (14) is fixedly mounted on the outer side of the limit frame (12), a positioning rod (15) is threadedly connected to the inner wall of the positioning buckle (14), and a buffer column (16) is fixedly mounted on the lower side of the base plate (11).

2. The UAV take-off and landing platform according to claim 1, characterized in that: A stabilizing rod is fixedly mounted on the inner side of the supporting foot (2).

3. The UAV take-off and landing platform according to claim 1, characterized in that: The conical block (4) is made of stainless steel.

4. The UAV take-off and landing platform according to claim 1, characterized in that: The landing pad (13) and the buffer column (16) are both made of rubber material, wherein the buffer column (16) is arranged between the base plate (11) and the bottom plate (1).

5. The UAV take-off and landing platform according to claim 1, characterized in that: A positioning rod hole is provided inside the base plate (11), wherein the positioning rod (15) is threadedly connected in the positioning rod hole.

6. The UAV take-off and landing platform according to claim 1, characterized in that: The lower end of the shock absorbing spring (9) is fixedly mounted inside the bottom plate (1), and the upper end of the shock absorbing spring (9) is fixedly mounted on the lower end of the movable rod (10).

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