Unmanned aerial vehicle undercarriage

By adopting structural designs such as slots and limit plates in the landing gear of the drone, the problem of inconvenience of user replacement of support legs is solved, rapid disassembly and replacement is achieved, and usage efficiency and safety are improved.

CN222496693UActive Publication Date: 2025-02-18CHANGSHU PUBLIC SECURITY BUREAU
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Patent Information

Application Number
CN202421272744.4
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-06-05
Publication Date
2025-02-18
Estimated Expiration
2034-06-05

AI Technical Summary

Technical Problem

The landing gear of existing toy drones is usually formed integrally with the fuselage or fixed by bolts, which makes it inconvenient for users to replace damaged support legs, requires professional tools, is cumbersome to operate, and takes a long time.

Method used

A drone landing gear is designed, with a structure of card slots, T-shaped slide slots, limit slots, limit plates and grooves, allowing users to quickly disassemble and replace support rods without professional tools.

Benefits of technology

It realizes users to quickly and easily replace support rods, reduces operation difficulty, saves maintenance time, and improves the efficiency and convenience of the drone. At the same time, through the design of special-shaped rods and short rods, the drone can be prevented from being uneven on the ground or The wind is affected by the dumping, ensuring the stability of the landing and the safety of use.

✦ Generated by Eureka AI based on patent content.

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Abstract

The undercarriage is arranged at the bottom of the unmanned aerial vehicle and comprises a supporting plate connected with the unmanned aerial vehicle, four clamping grooves are formed in the bottom of the supporting plate, four sets of limiting pieces matched with the clamping grooves are arranged at the bottom of the supporting plate, and each limiting piece comprises two pairs of T-shaped sliding grooves and two pairs of limiting grooves which are formed in the bottom of the supporting plate. The T-shaped sliding grooves are communicated with the limiting grooves, the limiting grooves are communicated with the clamping grooves, sliding blocks are arranged in the T-shaped sliding grooves in a sliding fit mode, limiting plates are connected to every two adjacent sliding blocks, and through the structural design of the clamping grooves, the T-shaped sliding grooves, the limiting grooves, the limiting plates and the grooves, when the supporting rod is accidentally damaged, a user can rapidly and conveniently disassemble and replace the supporting rod; no professional tool is needed, the operation difficulty of a user is reduced, the maintenance time is saved, and the use efficiency and convenience of the unmanned aerial vehicle are greatly improved.
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Description

Technical Field

[0001] The utility model relates to the technical field of landing gears, in particular to a landing gear for an unmanned aerial vehicle. Background Art

[0002] With the continuous development of drone technology, drones are increasingly used in various fields, especially toy drones, which are deeply loved by users for their portability and fun. During the use of toy drones, the landing gear, as an important component of the drone, its performance directly affects the stability and safety of the drone.

[0003] At present, the landing gear of toy drones on the market is usually made of plastic. Although this material has certain lightness and durability, the supporting legs of the landing gear are easily damaged under long-term use or accidental collision. Since the landing gear of traditional toy drones is mostly integrated with the fuselage or fixed by bolts, users usually need to use corresponding tools when replacing damaged supporting legs. The operation is cumbersome and time-consuming, which brings inconvenience to users. Therefore, a drone landing gear is proposed to address the above situation. Utility Model Content

[0004] The utility model aims to solve the shortcomings in the prior art that the landing gears of traditional toy drones are mostly integrally formed with the fuselage or fixed by bolts, which makes it inconvenient for users to replace the supporting legs, and proposes a drone landing gear.

[0005] In order to achieve the above purpose, the utility model adopts the following technical solutions:

[0006] A drone landing gear is arranged at the bottom of the drone;

[0007] The landing gear comprises a support plate connected to the UAV, four slots are arranged at the bottom of the support plate, and four groups of limiting members matching the slots are arranged at the bottom of the support plate.

[0008] The limiting member includes two pairs of T-shaped slide grooves and two pairs of limiting grooves opened at the bottom of the support plate. The T-shaped slide grooves are connected with the limiting grooves, and the limiting grooves are connected with the card slots. Sliding blocks are slidably matched in the T-shaped slide grooves, and limiting plates are connected to two adjacent sliding blocks.

[0009] A top plate is clamped in the slot, the top plate is provided with a pair of grooves, the grooves cooperate with the limiting plate, a support rod is arranged at the bottom of the top plate, a special-shaped rod is arranged at the bottom of the support rod, and a pair of short rods inclined downward are arranged on the special-shaped rod.

[0010] Preferably, the sliding block is in an inverted "T" shape.

[0011] Preferably, an assembly groove is provided on the sliding block, a pair of springs are arranged in the assembly groove, and the pair of springs are fixedly connected to the limiting plate.

[0012] Preferably, a handle is provided at the bottom of the limiting plate.

[0013] Preferably, the special-shaped rod comprises a cross bar and arc-shaped rods arranged at both ends of the cross bar, a rubber sleeve is arranged on the surface of the cross bar, and the short rod is arranged on the arc-shaped rod.

[0014] Preferably, four annular grooves are formed through the surface of the support plate.

[0015] The utility model has the following beneficial effects:

[0016] 1. The utility model adopts the structural design of the card slot, T-shaped slide slot, limit slot, limit plate and groove. When the support rod is accidentally damaged, the user can quickly and conveniently disassemble and replace the support rod without using professional tools, which reduces the user's operating difficulty, saves maintenance time, and greatly improves the use efficiency and convenience of the drone.

[0017] 2. The utility model adopts the structural design of special-shaped rods and short rods. When the UAV lands, it can prevent the UAV from tipping over due to uneven ground or wind, ensure the stability of the UAV landing, thereby protecting the UAV and its internal equipment and ensuring the safety of the UAV use. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a schematic diagram of the structure of the landing gear;

[0019] Figure 2 It is a schematic diagram of the structure of the landing gear;

[0020] Figure 3 is a schematic diagram of the structure of the support rod;

[0021] Figure 4 for Figure 2 A schematic diagram of the structure with a partial enlargement at the center;

[0022] Figure 5 It is a structural schematic diagram of the sliding block.

[0023] In the figure: 1. UAV; 2. Landing gear; 3. Support plate; 301. Slot; 302. T-shaped slide; 303. Limiting slot; 4. Sliding block; 401. Assembly slot; 402. Spring; 5. Limiting plate; 6. Support rod; 601. Top plate; 6010. Groove; 602. Special-shaped rod; 603. Short rod. DETAILED DESCRIPTION

[0024] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.

[0025] Reference Figure 1-5 , a drone landing gear, the package is arranged at the bottom of the drone 1,

[0026] The landing gear 2 includes a support plate 3 connected to the drone 1 by bolts. Four annular grooves are formed on the surface of the support plate 3. The annular grooves serve as mounting grooves for the bolts. The bolts pass through the annular grooves and are connected to the screw holes on the shell of the drone 1. Four card slots 301 are formed at the bottom of the support plate 3. Four sets of limit members matching the card slots 301 are formed at the bottom of the support plate 3.

[0027] The limiting member includes two pairs of T-shaped slots 302 and two pairs of limiting slots 303 opened at the bottom of the support plate 3. The T-shaped slots 302 are connected to the limiting slots 303, and the limiting slots 303 are connected to the card slot 301. A sliding block 4 is slidably fitted in the T-shaped slots 302, and a limiting plate 5 is connected to two adjacent sliding blocks 4.

[0028] In order to make the sliding block 4 slide in the T-shaped sliding groove 302, as shown in FIG. Figure 4 and Figure 5 As shown, the sliding block 4 is in an inverted "T" shape.

[0029] In order to make the limiting plate 5 limit the top plate 601, as shown in FIG. Figure 4 and Figure 5 As shown, a mounting groove 401 is provided on the sliding block 4, a pair of springs 402 is provided in the mounting groove 401, the pair of springs 402 is fixedly connected to the limiting plate 5, and a handle is provided at the bottom of the limiting plate 5.

[0030] A top plate 601 is clamped in the slot 301, and a pair of grooves 6010 are provided on the top plate 601, and the grooves 6010 cooperate with the limiting plate 5. A support rod 6 is provided at the bottom of the top plate 601, and a special-shaped rod 602 is provided at the bottom of the support rod 6. The special-shaped rod 602 is provided with a pair of short rods 603 inclined downward.

[0031] When the support rod 6 is accidentally damaged, the user pulls the handle downwards, and the handle drives the limit plate 5 to stretch the spring 402, so that the limit plate 5 moves out of the groove 6010, releasing the limit on the top plate 601, and then slides the limit plate 5 to one side. After loosening the limit plate 5, the top plate 601 can be removed from the slot 301 for replacement, so that the user can quickly and conveniently disassemble and replace the support rod without using professional tools, which reduces the user's operating difficulty, saves maintenance time, and greatly improves the use efficiency and convenience of the drone 1.

[0032] Furthermore, if Figure 3 As shown, the special-shaped rod 602 includes a cross bar and arc-shaped rods arranged at both ends of the cross bar, a rubber sleeve is arranged on the surface of the cross bar, and a short rod 603 is arranged on the arc-shaped rod.

[0033] When the drone 1 tilts forward or backward due to uneven ground during landing, as the angle of the arc rod changes, the short rod 603 will contact the ground in advance, thereby supporting the entire device. Therefore, after the drone 1 lands, it can prevent the drone 1 from tipping over due to uneven ground or wind, ensuring the stability of the drone 1 landing, thereby protecting the drone 1 and its internal equipment, and ensuring the safety of the drone 1.

[0034] The above description is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes within the technical scope disclosed by the present invention according to the technical scheme and the utility model concept of the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A drone landing gear, arranged at the bottom of a drone (1), characterized in that: The landing gear (2) comprises a support plate (3) connected to the drone (1), the bottom of the support plate (3) is provided with four slots (301), and the bottom of the support plate (3) is provided with four groups of limit members matching the slots (301); The limiting member comprises two pairs of T-shaped slide grooves (302) and two pairs of limiting grooves (303) arranged at the bottom of the support plate (3); the T-shaped slide grooves (302) are connected to the limiting grooves (303); the limiting grooves (303) are connected to the clamping grooves (301); a sliding block (4) is slidably fitted in the T-shaped slide grooves (302); and a limiting plate (5) is connected to two adjacent sliding blocks (4); A top plate (601) is clamped in the clamping slot (301), and a pair of grooves (6010) are provided on the top plate (601), and the grooves (6010) cooperate with the limiting plate (5). A support rod (6) is provided at the bottom of the top plate (601), and a special-shaped rod (602) is provided at the bottom of the support rod (6), and a pair of short rods (603) inclined downward are provided on the special-shaped rod (602).

2. The UAV landing gear according to claim 1, characterized in that: The sliding block (4) is in an inverted "T" shape.

3. The UAV landing gear according to claim 1 or 2, characterized in that: The sliding block (4) is provided with an assembly groove (401), a pair of springs (402) are arranged in the assembly groove (401), and the pair of springs (402) are fixedly connected to the limiting plate (5).

4. The UAV landing gear according to claim 1, characterized in that: A handle is provided at the bottom of the limiting plate (5).

5. The UAV landing gear according to claim 1, characterized in that: The special-shaped rod (602) comprises a crossbar and arc-shaped rods arranged at both ends of the crossbar, a rubber sleeve is arranged on the surface of the crossbar, and the short rod (603) is arranged on the arc-shaped rod.

6. The UAV landing gear according to claim 1, characterized in that: Four annular grooves are formed through the surface of the support plate (3).