Multi-rotor unmanned aerial vehicle portable take-off and landing pad

By designing a portable multi-rotor drone takeoff and landing board, and adopting a semi-circular landing board and storage box structure, the problems of large size and easy deformation of drone takeoff and landing boards are solved, achieving the effect of portability and stable use.

CN224297480UActive Publication Date: 2026-05-29刘瑜奇

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
刘瑜奇
Filing Date
2025-08-14
Publication Date
2026-05-29

AI Technical Summary

Technical Problem

Existing drone takeoff and landing boards are bulky and inconvenient to carry, and the soft materials used in landing boards are easily deformed, affecting their use and making it impossible to effectively stabilize drone takeoff and landing.

Method used

A portable take-off and landing board for multi-rotor drones was designed. It adopts a semi-circular landing board structure and achieves folding through rotational connection and damping friction. Combined with the design of storage box and magnetic plate, the size is reduced and it is easy to carry. It is fixed by limit ring and ground nail to ensure stable use.

Benefits of technology

It achieves portability and stability of the landing plate, reduces the risk of deformation, improves the stability of drone takeoff and landing, and is easy to carry and store.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of unmanned plane, concretely is multi rotor unmanned plane portable take -off and landing board, including the parking board, the lower surface fixed gluing of parking board has the buffer board, and the lower surface fixed gluing of buffer board has ground plate, the side of parking board is provided with the storage box, and the front surface of storage box is provided with the box door, the side fixed mounting of storage box has no.
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Description

Technical Field

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

[0002] Unmanned aerial vehicles (UAVs) are unmanned aircraft controlled by radio remote control equipment or onboard computer program control systems. UAVs have a simple structure and low operating cost. They can not only perform the tasks that manned aircraft can perform, but are also suitable for tasks that manned aircraft cannot perform. They play a significant role in emergency response and early warning in some surveying and mapping fields. Multi-rotor UAVs occupy an important position as the main surveying and mapping tool.

[0003] When a drone takes off and lands, it needs a base point as a stable platform. Most existing drone take-off and landing boards are simple, regular board structures that are simply placed on the bottom surface for use in conjunction with drone take-off and landing.

[0004] However, the applicant believes that the shortcomings of the above-mentioned landing boards are: the simple board structure is mostly a fixed structure, which is large in size and inconvenient to carry; some landing boards are made of soft materials and are simply laid on the ground. They are usually stored by rolling them up. Long-term rolling up will cause them to deform and make their surface uneven, which will affect the take-off and landing of the drone.

[0005] To address these issues, we propose a portable take-off and landing pad for multi-rotor UAVs. Utility Model Content

[0006] The purpose of this invention is to provide a portable take-off and landing board for multi-rotor unmanned aerial vehicles (UAVs) to solve the problems mentioned in the background art.

[0007] To achieve the above objectives, this utility model provides the following technical solution: a portable take-off and landing board for a multi-rotor drone, including a landing board, a buffer plate fixedly glued to the lower surface of the landing board, and a ground panel fixedly glued to the lower surface of the buffer plate; a storage box is provided on the side of the landing board, and a door is provided on the front surface of the storage box; a second handle is fixedly installed on the side of the storage box.

[0008] Preferably, the landing plate, buffer plate, and ground plate form a semi-circular landing plate structure, and two sets of semi-circular landing plates form a set of circular landing plates. The two sets of semi-circular landing plates are rotatably connected, and there is a certain damping friction at the rotation point. The bottom surface of the ground plate is fixedly glued with a waterproof surface. The rotatable folding structure can effectively reduce the overall volume of the landing plate, thus making it easy to carry.

[0009] Preferably, four sets of limiting rings are evenly and fixedly distributed on the side of the ground panel, and two sets of No. 1 handles are symmetrically and fixedly distributed on the side of the ground panel. A ground spike is movably inserted in the middle of each set of limiting rings. The ground spikes allow the landing board to be placed more stably on the ground.

[0010] Preferably, one end of the box door is hinged to the side of the storage box, and the other end of the box door is connected to the other side of the storage box by a buckle. The box door can be used to seal the storage box to prevent the items stored inside from falling out.

[0011] Preferably, the outer dimensions of the storage box are larger than the outer dimensions of the semi-circular landing plate structure, and a partition is fixedly installed in the middle of the interior of the storage box to separate the landing plate and the ground stake for storage.

[0012] Preferably, a magnetic plate is fixedly attached to the inner bottom surface of the storage box. The design of the magnetic plate can attract and fix the iron ground nails, thereby reducing the possibility of ground nails being lost.

[0013] This utility model provides a portable take-off and landing board for multi-rotor drones, which has the following advantages:

[0014] The landing plate, equipped with a rotating structure, can be folded, consisting of two semi-circular landing plates, a buffer plate, and a ground plate, thus reducing its overall size. It also includes a storage box for storing the folded landing plate. The storage box's double-layer structure allows for separate storage of the iron ground spikes from the landing plate. A magnetic layer secures the ground spikes, preventing direct contact and damage, and reducing the risk of loss. The combination of the landing plate and storage box results in a compact and portable device. Attached Figure Description

[0015] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0016] Figure 1 This is a three-dimensional front view of the structure of this utility model;

[0017] Figure 2 This is a schematic diagram showing the separation structure of the stop plate, buffer plate, and ground plate of this utility model;

[0018] Figure 3 This is a schematic diagram of the folded structure of the stop plate, buffer plate and ground plate of this utility model after being pressed together;

[0019] Figure 4 This is a three-dimensional front view of the storage box structure of this utility model.

[0020] In the diagram: 1. Stop plate; 2. Buffer plate; 3. Ground plate; 4. Limit ring; 5. Handle No. 1; 6. Ground nail; 7. Storage box; 8. Box door; 9. Handle No. 2; 10. Partition; 11. Magnetic plate. Detailed Implementation

[0021] 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.

[0022] This embodiment proposes a portable takeoff and landing board for multi-rotor unmanned aerial vehicles.

[0023] Example 1: As Figures 1 to 4 As shown, this embodiment proposes a portable take-off and landing board for multi-rotor drones, including a landing board 1, a buffer board 2 fixedly glued to the lower surface of the landing board 1, and a ground board 3 fixedly glued to the lower surface of the buffer board 2; a storage box 7 is provided on the side of the landing board 1, and a box door 8 is provided on the front surface of the storage box 7, and a second handle 9 is fixedly installed on the side of the storage box 7.

[0024] The stop plate 1, buffer plate 2, and ground plate 3 form a semi-circular landing plate structure, and two sets of semi-circular landing plates form a circular landing plate. The two sets of semi-circular landing plates are rotatably connected, and there is a certain damping friction at the rotation point. The bottom surface of the ground plate 3 is fixedly glued with a waterproof surface. One end of the box door 8 is hinged to the side of the storage box 7, and the other end of the box door 8 is connected to the other side of the storage box 7 by a buckle. The outer dimension of the storage box 7 is larger than the outer dimension of the semi-circular landing plate structure. A partition 10 is fixedly installed in the middle of the interior of the storage box 7. A magnetic plate 11 is fixedly attached to the bottom surface of the interior of the storage box 7.

[0025] In the above embodiment, hold the two sets of No. 1 handles 5 respectively and fold them toward the landing plate 1 so that the circular landing plate is folded into a semi-circular structure. Due to the existence of friction, the folded or unfolded landing plate has a certain self-fixing effect, and the volume of the folded landing plate is greatly reduced.

[0026] The buffer plate 2 installed in the landing plate is made of elastic material, which gives the landing plate itself a certain elastic cushioning effect, thereby reducing the inertial force caused by the drone flying straight down. At the same time, the waterproof surface at the bottom of the ground plate 3 is supported by plastic-coated canvas, which has a high waterproof performance, thus effectively preventing ground water from penetrating into the landing plate.

[0027] The folded landing board can be placed in the upper space of the storage box 7, then stored by closing the box door 8, and the storage box 7 can be carried and moved around by the second handle 9. The design of the storage box 7 greatly facilitates the overall carrying of the device.

[0028] Example 2: Figure 1 and Figure 2 As shown, based on the same concept as the above embodiment, this embodiment also proposes that: four sets of limiting rings 4 are evenly and fixedly distributed on the side of the ground panel 3, and two sets of No. 1 handles 5 are symmetrically and fixedly distributed on the side of the ground panel 3, and a ground nail 6 is movably inserted in the middle position of each set of limiting rings 4.

[0029] In the above embodiment, when the landing plate is deployed, the landing plate is placed in a designated suitable position, and then the ground spikes 6 are passed through the limiting ring 4 in sequence. The ground spikes 6 are driven into the ground with the help of external force to fix the landing plate, thereby preventing the landing plate from being misaligned and ensuring the take-off or landing of the drone. It should be noted that the ground spikes 6 are not suitable for hard materials such as cement.

[0030] Finally, several points should be noted: First, in the description of this application, it should be noted that, unless otherwise specified and limited, the terms "installation," "connection," and "linkage" should be interpreted broadly, and can refer to mechanical or electrical connections, or internal connections between two components, or direct connections. Terms such as "upper," "lower," "left," and "right" are only used to indicate relative positional relationships. When the absolute position of the described object changes, the relative positional relationship may change. Second, the accompanying drawings of the embodiments disclosed in this utility model only involve structures related to the embodiments disclosed in this utility model. Other structures can refer to common designs. In the absence of conflict, the same embodiment and different embodiments of this utility model can be combined with each other. Finally, the above are only preferred embodiments of this utility model and are not intended to limit this utility model. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this utility model should be included within the protection scope of this utility model.

Claims

1. A portable take-off and landing board for a multi-rotor unmanned aerial vehicle, including a landing board (1), characterized in that: The lower surface of the stop plate (1) is fixedly glued with a buffer plate (2), and the lower surface of the buffer plate (2) is fixedly glued with a ground panel (3); a storage box (7) is provided on the side of the stop plate (1), and a box door (8) is provided on the front surface of the storage box (7), and a second handle (9) is fixedly installed on the side of the storage box (7).

2. The portable takeoff and landing board for multi-rotor unmanned aerial vehicles according to claim 1, characterized in that: The stop plate (1), buffer plate (2) and ground plate (3) form a semi-circular landing plate structure, and the two sets of semi-circular landing plates form a set of circular landing plates. The two sets of semi-circular landing plates are rotatably connected, and there is a certain damping friction at the rotation point. The bottom surface of the ground plate (3) is fixedly glued with a waterproof surface.

3. The portable takeoff and landing board for multi-rotor unmanned aerial vehicles according to claim 1, characterized in that: Four sets of limiting rings (4) are evenly and fixedly distributed on the side of the ground panel (3), and two sets of No. 1 handles (5) are symmetrically and fixedly distributed on the side of the ground panel (3). A ground nail (6) is movably inserted in the middle position of each set of limiting rings (4).

4. The portable takeoff and landing board for multi-rotor unmanned aerial vehicles according to claim 1, characterized in that: One end of the box door (8) is hinged to the side of the storage box (7) by a hinge, and the other end of the box door (8) is connected to the other side of the storage box (7) by a buckle.

5. The portable takeoff and landing board for multi-rotor unmanned aerial vehicles according to claim 2, characterized in that: The outer dimensions of the storage box (7) are larger than the outer dimensions of the semi-circular landing plate structure, and a partition (10) is fixedly installed in the middle of the interior of the storage box (7).

6. The portable takeoff and landing board for multi-rotor unmanned aerial vehicles according to claim 1, characterized in that: A magnetic plate (11) is fixedly attached to the bottom of the inner surface of the storage box (7).