Buffering type takeoff and landing assembly of unmanned aerial vehicle

Abstract

The utility model relates to the field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle buffer type landing assembly which comprises a mounting plate and a connecting plate, the two sides of the lower end of the mounting plate are each fixedly connected with two supporting rods, the lower ends of the multiple supporting rods are each fixedly connected with a mounting box, and the inner walls of the two mounting boxes are each provided with a bidirectional threaded rod; the two ends of the outer walls of the two bidirectional threaded rods are both sleeved with threaded sleeves, and the two sides of the outer walls of the multiple threaded sleeves are both rotationally connected with first rotating rods. According to the unmanned aerial vehicle, the design of the unfolding plate effectively increases the contact area with the ground, the overall weight of the unmanned aerial vehicle can be dispersed in the landing process, the pressure intensity on the ground can be reduced, potential damage to the ground is reduced, meanwhile, toppling or rolling caused by too small pressure intensity in the landing process can be effectively avoided, the landing stability is improved, and meanwhile the unmanned aerial vehicle is convenient to use. The wider landing area enables the unmanned aerial vehicle to absorb landing impact energy more effectively when making contact with the ground, and therefore the structure of the unmanned aerial vehicle and sensitive assemblies in the unmanned aerial vehicle are further protected against damage.

Description

Technical Field

[0001] The utility model relates to the field of unmanned aerial vehicles (UAVs), and in particular to a buffered landing assembly for UAVs. Background Art

[0002] A drone cushioned landing assembly is a specially designed device installed on a drone to reduce impact force during landing and protect the drone from damage. This assembly is commonly used on fixed-wing and rotary-wing drones.

[0003] However, the contact area of ​​traditional drone cushioning landing components is small, resulting in greater pressure on the ground when the drone lands, which may cause dents, cracks or other damage to the ground, and may cause the drone to easily tip over or roll over when landing. At the same time, traditional landing components are limited in their effectiveness in absorbing landing impact energy, which can easily cause damage to the drone's structure and internal components.

[0004] Therefore, those skilled in the art provide a cushioned landing assembly for a UAV to solve the problems raised in the above background technology. Utility Model Content

[0005] The purpose of the present invention is to solve the shortcomings of the prior art and to propose a cushioned landing assembly for drones. The design of the unfolding plate effectively increases the contact area with the ground, which helps to disperse the overall weight of the drone during landing, significantly reduces the pressure on the ground, and reduces potential damage to the ground. At the same time, it can effectively avoid tipping or rolling during landing due to too little pressure, and improve landing stability. Through the mutual cooperation between the spring, sliding ring, sliding rod, second rotating rod, slider, and slide groove, the drone fixed on the upper end of the mounting plate can be effectively cushioned when it is subjected to vibration, thereby effectively reducing the damage to the internal components of the drone caused by vibration and increasing the service life of the drone.

[0006] To achieve the above objectives, the present invention provides the following technical solutions:

[0007] The two lever of the upper right corner is connected with the up-down knob on the top end of the hinge connector and the two lock holes on the hinge parts of each said frame, and the lock holes on the upper right corner are connected with the chest of said frame, and the upper right corner is connected with the chest of said frame.

[0008] Through the above technical solution, the design of the deployment plate effectively increases the contact area with the ground, which helps to disperse the overall weight of the drone during landing, significantly reduces the pressure on the ground, and reduces potential damage to the ground. At the same time, it can effectively avoid tipping or rolling during landing due to too little pressure, improve landing stability, and through the mutual cooperation between the spring, sliding ring, sliding rod, second rotating rod, slider, and slide groove, the drone fixed on the upper end of the mounting plate can be effectively buffered when it is subjected to vibration, thereby effectively reducing the damage to the internal components of the drone caused by vibration and increasing the service life of the drone.

[0009] Furthermore, the plurality of guide rods all slide inside the guide hole;

[0010] Through the above technical solution, this design helps to maintain the stability of the landing gear during landing.

[0011] Furthermore, the lower ends of the outer walls of the two sliding rings are rotatably connected to the second rotating rod;

[0012] Through the above technical solution, the rotating connection allows the sliding ring to rotate flexibly on the second rotating rod, so that the angle and position of the landing gear can be adjusted according to different landing conditions, thereby increasing the adjustment range of the landing gear.

[0013] Furthermore, the rear ends of the two installation boxes are fixedly connected to a protection box;

[0014] The above technical solution helps to dissipate heat from the servo motor, prevent overheating, and extend the service life of the servo motor.

[0015] Furthermore, the front ends of the two inner walls of the protection box are fixedly connected to the servo motor;

[0016] Through the above technical solution, the protection box helps to maintain the performance of the servo motor by protecting the servo motor from damage.

[0017] Furthermore, both ends of the two bidirectional threaded rods are rotatably connected to the installation box;

[0018] Through the above technical solution, the friction between the threaded rod and the installation box is reduced, the wear is reduced, and the service life of the component is extended.

[0019] Furthermore, rectangular grooves are provided at both ends of the two installation boxes;

[0020] Through the above technical solution, the rectangular groove provides a positioning and fixing position for the first rotating rod.

[0021] Furthermore, the output ends of the two servo motors are fixedly connected to one end of the bidirectional threaded rod;

[0022] Through the above technical solution, the automated motor drive reduces the need for manual adjustment of the landing gear.

[0023] The utility model has the following beneficial effects:

[0024] 1. The utility model proposes a cushioned landing assembly for drones. The design of the deployable plate effectively increases the contact area with the ground, helps to disperse the overall weight of the drone during landing, can reduce the pressure on the ground, and reduce potential damage to the ground. At the same time, it can effectively avoid tipping or rolling during landing due to insufficient pressure, thereby improving landing stability. At the same time, the wider landing area enables the drone to more effectively absorb landing impact energy when it contacts the ground, thereby further protecting the drone's structure and its internal sensitive components from damage.

[0025] 2. The utility model proposes a cushioned landing assembly for drones, which cooperates with each other among a spring, a sliding ring, a sliding rod, a second rotating rod, a slider, and a sliding groove, so that when a drone fixed on the upper end of a mounting plate is subjected to vibration, it can effectively cushion the vibration, thereby effectively reducing the damage to the internal components of the drone and increasing the service life of the drone. BRIEF DESCRIPTION OF THE DRAWINGS

[0026] Figure 1 This is an axonometric diagram of a cushioned landing assembly for a UAV proposed in the present invention;

[0027] Figure 2 This is an exploded view of a cushioned landing assembly for a UAV proposed in the present invention;

[0028] Figure 3 This is a front view of a cushioned landing assembly for a UAV proposed in the present invention;

[0029] Figure 4 This is a partial structural diagram of a cushioned landing assembly for a UAV proposed in the present invention;

[0030] Figure 5 This is a partial exploded view of a cushioned landing assembly for a UAV proposed in the present invention.

[0031] Legend:

[0032] 1. Mounting plate; 2. Support rod; 3. Mounting box; 4. Servo motor; 5. Bidirectional threaded rod; 6. Threaded sleeve; 7. First rotating rod; 8. Expanding plate; 9. Protective box; 10. Rectangular groove; 11. Slide groove; 12. Slider; 13. Second rotating rod; 14. Sliding ring; 15. Spring; 16. Slide rod; 17. Connecting plate; 18. Guide rod; 19. Guide hole. DETAILED DESCRIPTION

[0033] The following will be combined with the drawings in the specific embodiments of the present invention to clearly and completely describe the technical solutions in the specific embodiments of the present invention. Obviously, the specific embodiments described are only part of the specific embodiments of the present invention, not all of the specific embodiments. Based on the specific embodiments of the present invention, all other specific embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0034] Reference Figure 1-5 , a specific implementation method provided by the utility model:

[0035] A cushioned landing assembly for a drone comprises a mounting plate 1 and a connecting plate 17. Two support rods 2 are fixedly connected to both sides of the lower end of the mounting plate 1. The lower ends of the multiple support rods 2 are fixedly connected to mounting boxes 3. The inner walls of the two mounting boxes 3 are provided with bidirectional threaded rods 5. Both ends of the outer walls of the two bidirectional threaded rods 5 are sleeved with threaded sleeves 6. Both sides of the outer walls of the multiple threaded sleeves 6 are rotatably connected to first rotating rods 7. One end of the multiple first rotating rods 7 is rotatably connected to an expansion plate 8. The rear ends of the two mounting boxes 3 are provided with Servo motor 4, multiple guide holes 19 are provided at the four corners of the upper end of the mounting plate 1, a slide groove 11 is provided in the middle of the upper end of the mounting plate 1, sliders 12 are slidably connected to both sides of the inner wall of the slide groove 11, and the upper ends of the two sliders 12 are rotatably connected to the second rotating rod 13, a plurality of guide rods 18 are fixedly connected to the four corners of the lower end of the connecting plate 17, a slide rod 16 is fixedly connected to the middle of the inner wall of the connecting plate 17, and sliding rings 14 are slidably connected to both sides of the outer wall of the slide rod 16, and a spring 15 is fixedly connected between the two sliding rings 14;

[0036] The design of the unfolding plate 8 effectively increases the contact area with the ground, which helps to disperse the overall weight of the drone during landing, significantly reduces the pressure on the ground, and reduces potential damage to the ground. At the same time, it can effectively avoid tipping or rolling during landing due to too little pressure, thereby improving landing stability. Through the mutual cooperation between the spring 15, the sliding ring 14, the sliding rod 16, the second rotating rod 13, the slider 12, and the slide groove 11, the drone fixed at the upper end of the mounting plate 1 can be effectively buffered when subjected to vibration, thereby effectively reducing the damage to the internal components of the drone caused by vibration and increasing the service life of the drone.

[0037] Multiple guide rods 18 all slide inside the guide holes 19. This design helps to maintain the stability of the landing gear during landing. The lower ends of the outer walls of the two sliding rings 14 are rotatably connected to the second rotating rod 13. The rotating connection allows the sliding rings 14 to flexibly rotate on the second rotating rod 13, so that the angle and position of the landing gear can be adjusted according to different landing conditions, increasing the adjustment range of the landing gear. The rear ends of the two mounting boxes 3 are fixedly connected to the protective box 9, which helps to dissipate heat from the servo motor 4, prevent overheating, and extend the service life of the servo motor 4. The front ends of the inner walls of the two protective boxes 9 are fixedly connected to the servo motor 4. By protecting the servo motor 4 from damage, the protective box 9 helps to maintain the performance of the motor. Both ends of the two bidirectional threaded rods 5 are rotatably connected to the mounting box 3, reducing the friction between the bidirectional threaded rods 5 and the mounting box 3, reducing wear and extending the service life of the components. Rectangular grooves 10 are provided at both ends of the two mounting boxes 3. The rectangular grooves 10 provide a positioning and fixing position for the first rotating rod 7. The output ends of the two servo motors 4 are fixedly connected to one end of the bidirectional threaded rod 5. The automated motor drive reduces the need for manual adjustment of the landing gear.

[0038] Working principle: It is used by connecting the mounting plate 1 to the lower end of the drone. When the drone is ready to land, the servo motor 4 starts and drives the bidirectional threaded rod 5 to rotate. This rotational motion is transmitted to the first rotating rod 7 through the threaded sleeve 6, causing the deployment plate 8 to deploy outward, thereby increasing the contact area with the ground. This design helps to disperse the weight of the drone, reduce the pressure on the ground, and effectively absorb the impact force during landing. At the same time, it can effectively avoid tipping or rolling during landing due to too little pressure, thereby improving landing stability. At the same time, the guide rod 18 slides smoothly inside the guide hole 19, and the slider 12 is slidably connected in the slide groove 11, and the lower end of the outer wall of the sliding ring 14 is rotatably connected to the second rotating rod 13, so that the landing gear can effectively reduce the vibration caused by ground impact during landing. When the drone is ready to take off, the servo motor 4 rotates in the opposite direction to drive the bidirectional threaded rod 5 to rotate, driving the deployment plate 8 to retract.

[0039] Finally, it should be noted that the above is only a preferred specific implementation method of the present invention and is not intended to limit the present invention. Although the present invention has been described in detail with reference to the aforementioned specific implementation methods, those skilled in the art can still modify the technical solutions described in the aforementioned specific implementation methods or make equivalent replacements for some of the technical features therein. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of protection of the present invention.

Claims

1. A cushioned landing assembly for an unmanned aerial vehicle, comprising a mounting plate (1) and a connecting plate (17), characterized in that: Two support rods (2) are fixedly connected to both sides of the lower end of the mounting plate (1), and the lower ends of the plurality of support rods (2) are fixedly connected to mounting boxes (3). The inner walls of the two mounting boxes (3) are provided with bidirectional threaded rods (5), and both ends of the outer walls of the two bidirectional threaded rods (5) are sleeved with threaded sleeves (6). Both sides of the outer walls of the plurality of threaded sleeves (6) are rotatably connected to first rotating rods (7), and one end of the plurality of first rotating rods (7) is rotatably connected to an expansion plate (8). The rear ends of the two mounting boxes (3) are provided with servo motors (4). The upper end of the mounting plate (1) is provided with a servo motor (4). A plurality of guide holes (19) are provided at the four corners, a slide groove (11) is provided in the middle of the upper end of the mounting plate (1), sliders (12) are slidably connected to both sides of the inner wall of the slide groove (11), and the upper ends of the two sliders (12) are rotatably connected to the second rotating rod (13), a plurality of guide rods (18) are fixedly connected at the four corners of the lower end of the connecting plate (17), a slide rod (16) is fixedly connected to the middle of the inner wall of the connecting plate (17), and slide rings (14) are slidably connected to both sides of the outer wall of the slide rod (16), and a spring (15) is fixedly connected between the two slide rings (14).

2. The cushioned landing assembly for a drone according to claim 1, characterized in that: The plurality of guide rods (18) all slide inside the guide holes (19).

3. The cushioned landing assembly for a drone according to claim 1, characterized in that: The lower ends of the outer walls of the two sliding rings (14) are both rotatably connected to the second rotating rod (13).

4. The cushioned landing assembly for a drone according to claim 1, characterized in that: The rear ends of the two installation boxes (3) are both fixedly connected with a protection box (9).

5. The cushioned landing assembly for a drone according to claim 4, characterized in that: The front ends of the inner walls of the two protection boxes (9) are fixedly connected to the servo motor (4).

6. The cushioned landing assembly for a UAV according to claim 1, characterized in that: Both ends of the two bidirectional threaded rods (5) are rotatably connected to the installation box (3).

7. The cushioned landing assembly for a UAV according to claim 1, characterized in that: Rectangular grooves (10) are provided at both ends of the two installation boxes (3).

8. The cushioned landing assembly for a UAV according to claim 1, characterized in that: The output ends of the two servo motors (4) are both fixedly connected to one end of the bidirectional threaded rod (5).

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