A landing gear for drones that stabilizes landing

Abstract

This utility model discloses a landing gear for a drone with stable landing, including a support structure consisting of two sets. Each support structure includes a rhomboid block and mounting tubes. Sleeves are fixedly connected to two opposite corners of the front face of the rhomboid block, and sleeves are fixedly connected to the other two opposite corners of the rear face of the rhomboid block. The four mounting tubes are arranged in an X-shape, with one end of each tube installed inside a sleeve and the other end fixedly connected to a mounting plate. A mounting cavity is formed at the center of the mounting plate. Two mounting plates at the bottom are equipped with anti-vibration structures. The X-shaped distribution of the rhomboid blocks and mounting tubes enhances the overall stability of the landing gear, allowing the drone to land more smoothly and reducing the risk of damage due to instability. Furthermore, the combination of mounting tubes and sleeves facilitates efficient assembly, and if one component is damaged, it can be replaced promptly, ensuring the overall service life.

Description

Technical Field

[0001] This utility model relates to the field of drone landing gear, specifically a drone landing gear for stable landing. Background Technology

[0002] The landing gear of a drone is a key component for takeoff and landing. Its main functions include: support, providing necessary support during parking, taxiing, takeoff and landing to ensure that the drone can be stably parked on the ground and bear the weight of the fuselage and impact loads during takeoff and landing; and cushioning, with shock-absorbing struts and other components in the landing gear absorbing the impact energy of the drone during landing, reducing damage to the fuselage and internal equipment, and protecting the overall structure of the drone.

[0003] Traditional landing gear is assembled using a one-piece molding method. When a certain area wears out, the entire landing gear must be replaced, which not only increases maintenance costs but also affects its normal service life. Utility Model Content

[0004] The purpose of this utility model is to provide a method for combining a mounting tube and a sleeve, which improves the overall assembly efficiency, allows for timely replacement of any damaged component, and ensures a stable landing gear for drones with a long service life. This can solve the problems mentioned in the background art.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a landing gear for a drone with stable landing, comprising a support structure, which consists of two sets. The support structure includes a rhomboid block and mounting tubes. Sleeves are fixedly connected to two opposite corners of the front face of the rhomboid block, and sleeves are fixedly connected to the other two opposite corners of the rear face of the rhomboid block. The four mounting tubes are distributed in an X-shape. One end of each mounting tube is installed inside a sleeve, and the other end is fixedly connected to a mounting plate. A mounting cavity is formed at the center of the mounting plate. Two anti-vibration structures are installed on the two mounting plates at the bottom.

[0006] Preferably, one end of the construction tube is slidably inserted into the inside of the sleeve, an inclined elastic plate is fixedly connected to the outer surface of the sleeve, an insertion rod is fixedly connected to the inner side of the elastic plate, the bottom end of the insertion rod slides through the sleeve, and a matching locking hole is opened on the outer side of the insertion end of the construction tube.

[0007] Preferably, an arc-shaped sliding rod is fixedly connected to the inner side wall of the sleeve, and an arc-shaped sliding groove is opened on the outer circular side wall of the insertion end of the building tube.

[0008] Preferably, the sleeve and the rhomboid block are integrally formed, and the construction pipe is welded to the mounting plate.

[0009] Preferably, the seismic-resistant structure includes a cylindrical sleeve and an elastic hemisphere. The cylindrical sleeve is slidably fitted onto the outside of the mounting plate. An oblong cavity is formed on the outer circular side wall of the cylindrical sleeve. The mounting cavity communicates with the oblong cavity. A bolt is inserted inside the oblong cavity. A nut is threaded to the other end of the bolt. An elastic hemisphere is fixedly connected to the bottom of the cylindrical sleeve.

[0010] Preferably, the outer circular sidewall of the cylindrical sleeve has two symmetrically arranged storage grooves, which are connected to the waist-shaped cavity, and the head of the bolt and the nut are both located in the storage grooves.

[0011] Compared with the prior art, the beneficial effects of this utility model are:

[0012] 1. The X-shaped distribution of diamond-shaped blocks and assembly tubes enhances the overall stability of the landing gear, making the drone land more smoothly and reducing the risk of damage caused by instability. The combination of assembly tubes and sleeves improves the overall assembly efficiency, and if one component is damaged, it can be replaced in time to ensure the overall service life.

[0013] 2. The flexible clamping plate allows the insertion rod to be easily inserted into or removed from the clamping hole, facilitating the installation or disassembly of the assembly tube and improving the assembly and maintenance efficiency of the landing gear. The arc-shaped sliding rod and arc-shaped sliding groove can limit and position the assembly tube, preventing it from rotating inside the sleeve and further improving assembly efficiency. Attached Figure Description

[0014] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0015] Figure 2 for Figure 1 Another perspective of the three-dimensional structure;

[0016] Figure 3 This is a schematic diagram of the three-dimensional structure of the exploded disassembly of both ends of the pipe in this utility model;

[0017] Figure 4 for Figure 3 A magnified schematic diagram of the structure at point A in the middle.

[0018] In the diagram: 1. Support structure; 11. Rhombus block; 12. Construction tube; 13. Mounting plate; 14. Sleeve; 15. Mounting cavity; 16. Elastic clamping plate; 17. Insert rod; 18. Arc-shaped slide rod; 101. Arc-shaped slide groove; 102. Locking hole; 2. Seismic structure; 21. Cylindrical sleeve; 22. Storage groove; 23. Elastic hemisphere; 24. Waist-shaped cavity; 25. Bolt; 26. Nut. Detailed Implementation

[0019] 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.

[0020] Please see Figure 1-4 The diagram shows a landing gear for a drone that ensures stable landing. It includes a support structure 1, which consists of two sets. The two sets of support structures 1 can be installed on both sides of the drone body. Each support structure 1 includes a rhomboid block 11 and four mounting tubes 12. Sleeves 14 are fixedly connected to two opposite corners of the front face of the rhomboid block 11 and to the other two opposite corners of the rear face of the rhomboid block 11. The four mounting tubes 12 are arranged in an X-shape. One end of each mounting tube 12 is installed inside the sleeve 14, and the other end is fixedly connected to a mounting plate 13. A mounting cavity 15 is opened at the center of the mounting plate 13. The two mounting plates 13 at the bottom are equipped with anti-vibration structures 2, and the mounting plate 13 at the top can be installed on the drone body with screws.

[0021] It is worth noting that the X-shaped distribution of the rhomboid blocks 11 and the mounting tubes 12 enhances the overall stability of the landing gear, making the drone land more smoothly and reducing the risk of damage caused by instability. Furthermore, the combination of the mounting tubes 12 and the sleeves 14 improves the overall assembly efficiency. If one component is damaged, it can be replaced in time to ensure the overall service life.

[0022] Please see Figure 1 , Figure 2 , Figure 3 and Figure 4 One end of the construction tube 12 is slidably inserted into the inside of the sleeve 14. An inclined elastic clamping plate 16 is fixedly connected to the outer circular surface of the sleeve 14. An insertion rod 17 is fixedly connected to the inner side of the elastic clamping plate 16. The bottom end of the insertion rod 17 slides through the sleeve 14. A matching locking hole 102 is opened on the outer circular side of the insertion end of the construction tube 12.

[0023] Before the assembly tube 12 is fully inserted into the sleeve 14, manually lift the elastic clamp 16. The insertion rod 17, under the elastic force of the elastic clamp 16, is precisely inserted into the clamp hole 102, fixing the assembly tube 12 and the sleeve 14. This prevents the impact force generated when the UAV lands from causing the assembly tube 12 and the sleeve 14 to loosen or fall off, further enhancing the stability of the landing gear. At the same time, the setting of the elastic clamp 16 allows the insertion rod 17 to be easily inserted into or removed from the clamp hole 102, facilitating the installation or disassembly of the assembly tube 12 and improving the assembly and maintenance efficiency of the landing gear.

[0024] Please refer to Figure 4 An arc-shaped sliding rod 18 is fixedly connected to the inner wall of the sleeve 14. An arc-shaped sliding groove 101 is provided on the outer circular side wall of the insertion end of the assembly tube 12. The arc-shaped sliding rod 18 is slidably engaged inside the arc-shaped sliding groove 101. When the insertion rod 17 is engaged in the locking hole 102 to fix the assembly tube 12, the arc-shaped sliding rod 18 and the arc-shaped sliding groove 101 can limit and position the assembly tube 12, preventing the assembly tube 12 from rotating inside the sleeve 14, thus further improving the assembly efficiency. The sliding cooperation of the arc-shaped sliding rod 18 and the arc-shaped sliding groove 101 facilitates the quick installation or disassembly of the assembly tube 12 and the sleeve 14, further improving the assembly and maintenance efficiency of the landing gear.

[0025] See Figure 3 The sleeve 14 and the rhombus block 11 are integrally formed, and the mounting tube 12 is welded to the mounting plate 13, which enhances the connection strength between the sleeve 14 and the rhombus block 11, as well as the structural strength between the mounting tube 12 and the mounting plate 13, ensuring the overall stability of the landing gear. The setting of the rhombus block 11 makes the connection between the landing gear and the UAV body more stable, which can effectively disperse the impact force generated when the UAV lands and avoid damage to the UAV body. The rhombus block 11 and the sleeve 14 are made of plastic materials, and the mounting tube 12 is made of aluminum alloy materials. Plastic materials have the characteristics of light weight, corrosion resistance, and easy processing and molding, which can effectively reduce the overall weight of the landing gear. Aluminum alloy materials have the characteristics of low density, high strength, and good corrosion resistance, which allows the mounting tube 12 to have sufficient load-bearing capacity while adopting a lightweight design, which helps to improve the flight performance and endurance of the UAV.

[0026] See Figure 2 and Figure 4 The seismic-resistant structure 2 includes a cylindrical sleeve 21 and an elastic hemisphere 23. The cylindrical sleeve 21 is slidably fitted onto the outside of the mounting plate 13. An oblong cavity 24 is formed on the outer sidewall of the cylindrical sleeve 21. The mounting cavity 15 communicates with the oblong cavity 24, and a bolt 25 is inserted inside it. The other end of the bolt 25 is threaded with a nut 26. The elastic hemisphere 23 is fixedly connected to the bottom of the cylindrical sleeve 21. The elastic hemisphere 23 absorbs the vibrations generated during the landing of the UAV, further enhancing the seismic performance of the landing gear. The sliding fit between the cylindrical sleeve 21 and the mounting plate 13 allows the seismic-resistant structure 2 to adjust according to the... The drone's landing status is adaptively adjusted, improving the adaptability and stability of the landing gear. This allows for fine-tuning of the height of the cylindrical sleeve 21. The height adjustment is achieved through the cooperation of the waist-shaped cavity 24 and the bolt 25. The operator can loosen the nut 26, then move the bolt 25 up and down within the waist-shaped cavity 24 to adjust to the appropriate height. After that, the nut 26 is tightened again to fix the bolt 25, thus achieving precise fine-tuning of the height of the cylindrical sleeve 21. This design not only improves the flexibility and applicability of the landing gear but also helps ensure the smoothness of the drone's landing.

[0027] Please refer to Figure 2 The cylindrical sleeve 21 has two symmetrically arranged storage slots 22 on its outer circular sidewall. The storage slots 22 are connected to the waist-shaped cavity 24. The head of the bolt 25 and the nut 26 are both located in the storage slots 22. This design allows the bolt 25 and nut 26 to be stored in the storage slots 22 when not in use, avoiding the bolt 25 and nut 26 from protruding. The design of the storage slots 22 also keeps the landing gear appearance clean and smooth, which helps to reduce air resistance and ensure the flight efficiency of the UAV.

[0028] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A landing gear for a drone that provides stable landing, comprising a support structure (1), characterized in that, The support structure (1) consists of two sets. The support structure (1) includes a rhombus block (11) and a building tube (12). The front end face of the rhombus block (11) is fixedly connected to two opposite corners with a sleeve (14). The rear end face of the rhombus block (11) is fixedly connected to two other opposite corners with a sleeve (14). The four building tubes (12) are distributed in an X shape. One end of the building tube (12) is installed inside the sleeve (14), and the other end is fixedly connected to an installation plate (13). An installation cavity (15) is opened in the center of the installation plate (13). The two installation plates (13) at the bottom are both equipped with an anti-seismic structure (2).

2. The landing gear for a drone with stable landing as described in claim 1, characterized in that: One end of the construction tube (12) is slidably inserted into the inside of the sleeve (14). An inclined elastic plate (16) is fixedly connected to the outer circular surface of the sleeve (14). An insertion rod (17) is fixedly connected to the inner side of the elastic plate (16). The bottom end of the insertion rod (17) slides through the sleeve (14). A matching locking hole (102) is opened on the outer circular side of the insertion end of the construction tube (12).

3. The landing gear for a drone with stable landing as described in claim 2, characterized in that: The inner wall of the sleeve (14) is fixedly connected with an arc-shaped sliding rod (18), and the outer circular side wall of the insertion end of the building tube (12) is provided with an arc-shaped sliding groove (101).

4. The landing gear for a drone with stable landing as described in claim 1, characterized in that: The sleeve (14) and the rhombus block (11) are integrally formed, and the building pipe (12) is welded to the mounting plate (13).

5. The landing gear for a drone with stable landing as described in claim 1, characterized in that: The seismic structure (2) includes a cylindrical sleeve (21) and an elastic hemisphere (23). The cylindrical sleeve (21) is slidably sleeved on the outside of the mounting plate (13). The outer side wall of the cylindrical sleeve (21) is provided with a waist-shaped cavity (24). The mounting cavity (15) is connected to the waist-shaped cavity (24). A bolt (25) is inserted inside the cavity. The other end of the bolt (25) is threaded with a nut (26). The bottom of the cylindrical sleeve (21) is fixedly connected to the elastic hemisphere (23).

6. The landing gear for a drone with stable landing as described in claim 5, characterized in that: The cylindrical sleeve (21) has two symmetrically arranged storage grooves (22) on its outer circular sidewall. The storage grooves (22) are connected to the waist-shaped cavity (24). The head of the bolt (25) and the nut (26) are both located in the storage grooves (22).

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