Take-off and landing platform of unmanned aerial vehicle

Abstract

The landing platform of the unmanned aerial vehicle comprises a supporting plate, a plurality of height adjusting devices are arranged on the edge of the supporting plate, and each height adjusting device comprises a connecting part, an inner threaded pipe, a threaded rod and a foot margin. The unmanned aerial vehicle is simple in structure and reasonable in design, the height adjusting device and the foldable threaded rod structure are arranged, the round supporting plate, the anti-skid layer and the universal ground feet are combined, the height and the horizontal state of the supporting plate can be flexibly adjusted so as to adapt to uneven terrains, the stability of the unmanned aerial vehicle during taking-off and landing is ensured, and the unmanned aerial vehicle is convenient to use. The risk that the fuselage is unbalanced or the paddle touches the ground due to the inclination of the ground is avoided, meanwhile, a larger effective landing area and higher friction force are provided, the parking safety is enhanced, the portable storage is realized, the space is saved, and the use convenience is improved.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically to a UAV take-off and landing platform. Background Technology

[0002] Unmanned Aerial Vehicles (UAVs) are flight devices that do not require human piloting. Due to their flexibility and efficiency, they are widely used in various fields such as aerial photography, logistics delivery, agricultural monitoring, and emergency rescue. With the continuous development of UAV technology, their design and functions are becoming increasingly diversified, enabling them to perform a variety of tasks, from simple reconnaissance to complex transportation. In practical operation, the takeoff and landing of UAVs are critical links, directly affecting the success of the flight mission. To facilitate the use of UAVs in different environments, landing platforms are widely used as an auxiliary device. Their main function is to provide a stable takeoff and landing area for UAVs. They are usually made of lightweight and durable materials to meet the requirements of portability and practicality.

[0003] Traditional landing platforms typically employ a fixed structure design. While they can meet basic usage requirements well on flat ground, they often tilt when used on uneven terrain because they cannot adapt to changes in terrain. This tilting reduces platform stability, thereby increasing the risks during drone takeoff and landing. For example, platform tilting may cause the drone to tip over due to instability, or even cause the propellers to touch the ground and be damaged, leading to equipment failure. Utility Model Content

[0004] The purpose of this invention is to provide a take-off and landing platform for unmanned aerial vehicles (UAVs) to solve the problems mentioned in the background art.

[0005] To achieve the above objectives, the present invention provides the following technical solution: a landing platform for an unmanned aerial vehicle (UAV), comprising a support plate, wherein the edge of the support plate is provided with a plurality of height adjustment devices;

[0006] The height adjustment device includes:

[0007] The connecting portion is located at the edge of the support plate;

[0008] An internally threaded pipe, wherein the internally threaded pipe is rotatably connected to the connecting part;

[0009] A threaded rod is threadedly connected to the internally threaded pipe, and the end of the threaded rod is rotatably connected to a foot.

[0010] Preferably, the connecting portion includes an extension section and a connecting section, the internally threaded tube is rotatably connected to the connecting section, and the extension section is used to extend the connecting section above or below the horizontal plane of the support plate, such that the rotation axis of the connecting section and the internally threaded tube is not on the same horizontal plane as the support plate.

[0011] Preferably, the support plate is circular in shape.

[0012] Preferably, the foot is a universal foot.

[0013] Preferably, the surface of the support plate is provided with an anti-slip layer.

[0014] Preferably, the support plate has a beveled opening at its edge, and a retainer for fixing the UAV landing gear is rotatably connected inside the beveled opening.

[0015] Compared with the prior art, the beneficial effects of this utility model are:

[0016] 1. The take-off and landing platform of this UAV, by being equipped with a height adjustment device, including a connecting part, an internal threaded tube, a threaded rod and universal feet, can flexibly adjust the height and level of the support plate according to uneven terrain, ensuring the stability of the UAV during take-off and landing, and avoiding the risk of fuselage imbalance or propellers touching the ground due to ground tilt.

[0017] 2. The landing platform of this drone, by setting up a foldable threaded rod structure and a circular support plate design, combined with an anti-slip layer and omnidirectional feet, not only makes it easy to store and carry, saving space, but also provides a larger effective landing area and higher friction, further enhancing the parking safety and ease of use of the drone. Attached Figure Description

[0018] Figure 1 This is a perspective view of the present utility model;

[0019] Figure 2 This is the front view of the present invention;

[0020] Figure 3 This is a schematic diagram showing the connection between the internally threaded tube and the threaded rod of this utility model.

[0021] Figure 4 This is a schematic diagram of the present invention after folding;

[0022] Figure 5 This is a schematic diagram of the connecting part of this utility model;

[0023] Figure 6 This is a schematic diagram of the beveled portion of this utility model.

[0024] In the diagram: 1. Support plate; 2. Height adjustment device; 201. Connecting part; 2011. Extension section; 2012. Connecting section; 202. Internally threaded pipe; 203. Threaded rod; 204. Foot; 3. Anti-slip layer; 4. Bevel; 5. Clamping piece. Detailed Implementation

[0025] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0026] In the description of this utility model, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or component referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.

[0027] In the description of this patent, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "setting" should be interpreted broadly. For example, they can refer to a fixed connection or setting, a detachable connection or setting, or an integrated connection or setting. Those skilled in the art can understand the specific meaning of the above terms in this patent according to the specific circumstances.

[0028] Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of this utility model, "several" means two or more, unless otherwise explicitly specified.

[0029] Example

[0030] Please see Figure 1-5 As shown, the present invention provides a landing platform technical solution for a drone: a landing platform for a drone includes a support plate 1, and the edge of the support plate 1 is provided with a plurality of height adjustment devices 2;

[0031] The height adjustment device 2 includes a connecting part 201, an internal threaded tube 202, and a threaded rod 203. The connecting part 201 is installed on the edge of the support plate 1. The internal threaded tube 202 is rotatably connected to the connecting part 201. The threaded rod 203 is threadedly connected to the internal threaded tube 202. The end of the threaded rod 203 is rotatably connected to a foot 204.

[0032] When the drone takes off and lands on uneven ground, the operator must first place a dedicated landing platform on the ground. Due to the uneven ground, some feet 204 may be suspended in the air and not in contact with the ground, causing the support plate 1 to tilt. At this time, the operator drives the uncontacted feet 204 downward by rotating the adjusting threaded rod 203 until all feet 204 are in stable contact with the ground. Then, by continuing to adjust each threaded rod 203, the support plate 1 is brought to a relatively level state. After the adjustment is completed, the drone can take off and land safely on the level support plate 1, avoiding the risk of fuselage imbalance and propellers touching the ground due to the tilted terrain.

[0033] The connecting part 201 includes an extension section 2011 and a connecting section 2012. The internally threaded tube 202 is rotatably connected to the connecting section 2012. The extension section 2011 is used to extend the connecting section 2012 to above or below the horizontal plane of the support plate 1, so that the rotation axis of the connecting section 2012 and the internally threaded tube 202 is not on the same horizontal plane as the support plate 1.

[0034] During storage, the operator can adjust the angle between the threaded rod 203 and the support plate 1 by rotating it until the body of the threaded rod 203 rests against the support plate 1, thus achieving a folding effect, making it easy to carry and store, and saving space.

[0035] In this embodiment, the support plate 1 adopts a circular design to provide a larger effective landing area and ensure that the drone has enough space when landing.

[0036] The 204 feet are omnidirectional feet, a design that allows for flexible adjustments on uneven surfaces, ensuring platform stability. Furthermore, the omnidirectional feet also facilitate folding and storage of the platform.

[0037] The support plate 1 has an anti-slip layer 3 on its surface. This design can effectively increase friction, ensure the stability of the drone when it is parked, and prevent it from sliding.

[0038] A slanted opening 4 is provided at the edge of the support plate 1, and a retaining member 5 is rotatably connected within the slanted opening 4; specifically, the retaining member 5 is disposed in the slanted opening 4 via a damping pivot, and the structure of the slanted opening 4 and the retaining member 5 is as follows. Figure 6 As shown, the slanted opening 4 is used to accommodate the clamping component 5 and prevent the clamping component 5 from rotating excessively. The clamping component 5 has an arc-shaped structure to fix the drone landing gear, so as to prevent the drone from slipping during the platform adjustment process.

[0039] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. Those skilled in the art should understand that this utility model is not limited to the above embodiments. The embodiments and descriptions in the specification are merely preferred examples and are not intended to limit the utility model. Various changes and modifications can be made to this utility model without departing from its spirit and scope, and all such changes and modifications fall within the scope of the claimed utility model. The scope of protection of this utility model is defined by the appended claims and their equivalents.

Claims

1. A landing platform for an unmanned aerial vehicle (UAV), characterized in that: Includes a support plate (1), and the edge of the support plate (1) is provided with a plurality of height adjustment devices (2); The height adjustment device (2) includes: A connecting part (201) is provided at the edge of the support plate (1); An internally threaded tube (202) is rotatably connected to the connecting part (201); A threaded rod (203) is threadedly connected to the internally threaded tube (202), and a foot (204) is rotatably connected to the end of the threaded rod (203).

2. The landing platform for the unmanned aerial vehicle according to claim 1, characterized in that: The connecting part (201) includes an extension section (2011) and a connecting section (2012). The internally threaded tube (202) is rotatably connected to the connecting section (2012). The extension section (2011) is used to extend the connecting section (2012) above or below the horizontal plane of the support plate (1), such that the rotation axis of the connecting section (2012) and the internally threaded tube (202) is not on the same horizontal plane as the support plate (1).

3. The landing platform for the unmanned aerial vehicle according to claim 1, characterized in that: The support plate (1) is circular in shape.

4. The landing platform for the UAV according to claim 1, characterized in that: The foot (204) is a universal foot.

5. The landing platform for the unmanned aerial vehicle according to claim 1, characterized in that: The support plate (1) has an anti-slip layer (3) on its surface.

6. The landing platform for the unmanned aerial vehicle according to claim 1, characterized in that: The support plate (1) has a slanted opening (4) at its edge, and a clamp (5) for fixing the landing gear of the UAV is rotatably connected inside the slanted opening (4).

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