Unmanned aerial vehicle landing platform with high stability

Abstract

The unmanned aerial vehicle landing platform with the high stability comprises a fixing table, laser sensors are arranged on the outer surfaces of the two sides of the top end of an abutting assembly, through grooves are formed in the two sides of the bottom end of the abutting assembly, and a plurality of sets of electric push rods are fixedly installed in the through grooves in the bottom end. According to the unmanned aerial vehicle landing control device, through detection of the pressure sensors, actions of the air cylinders and the electric push rods are automatically triggered, self-adaptive adjustment of the unmanned aerial vehicle landing process is achieved, laser sensors are introduced, and the unmanned aerial vehicle landing control device has the advantages that the unmanned aerial vehicle landing control device is simple in structure, convenient to operate and high in practicability. The landing platform can accurately measure the size and position of the unmanned aerial vehicle supporting piece, and then the bottom end supporting piece of the unmanned aerial vehicle is accurately clamped through the electric push rod. The accurate clamping ensures the stability of the unmanned aerial vehicle in the landing process, and the risk of shaking or inclination caused by external force interference such as wind power is reduced.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle landing platforms, in particular to a unmanned aerial vehicle landing platform with strong stability. Background Art

[0002] With the rapid development of drone technology, drones are increasingly used in various fields, including aerial photography, agricultural plant protection, logistics and transportation, rescue and disaster relief, etc. In these applications, the stable landing of drones is particularly important, especially in complex environmental conditions such as strong winds and uneven ground. The landing safety of drones faces severe challenges.

[0003] Currently, most drone landing platforms on the market are fixed in design, lacking sufficient stability and adaptability. Under complex environmental conditions, these landing platforms often fail to meet the requirements for safe landing of drones. For example, in strong winds, fixed landing platforms shake due to wind force, causing the drone to deviate or tilt during landing, and even causing accidents. Utility Model Content

[0004] (I) Purpose of the utility model

[0005] In view of this, the purpose of the utility model is to provide a UAV landing platform with strong stability, which solves the problems raised in the above background.

[0006] (II) Technical solution

[0007] A highly stable drone landing platform comprises a fixed platform, the top of the fixed platform is connected to a support seat, and the outer surface of the support seat is provided with a groove, multiple groups of cylinders are fixedly installed in the groove, and the tops of the multiple groups of cylinders are connected to abutment components, laser sensors are arranged on the outer surfaces of both sides of the top of the abutment components, and through grooves are provided on both sides of the bottom of the abutment components, multiple groups of electric push rods are fixedly installed in the through grooves at the bottom, and one end of the multiple groups of electric push rods is connected to a clamping plate, and multiple groups of pressure sensors are fixedly installed on the outer surface of the bottom end of the abutment components.

[0008] Preferably, a limiting groove is provided at the top of the fixed platform, and a plurality of groups of first circular plates are fixedly installed in the limiting groove, dampers are fixedly installed on the outer surfaces of the top ends of the plurality of groups of first circular plates, and the top ends of the dampers are connected to second circular plates, and the top ends of the second circular plates are connected to damping blocks. The damping system composed of the first circular plates, the dampers and the second circular plates can provide additional cushioning when the UAV lands, reduce the shaking of the UAV caused by uneven ground or wind, and thus enhance the landing stability.

[0009] Preferably, a spring is connected between the first circular plate and the second circular plate, and the combination of the spring and the damper can absorb and alleviate the impact force, reduce the risk of damage to the drone, and ensure the safety of landing.

[0010] Preferably, a light bar is provided on the outer surface of the top end of the support seat, which can improve the visibility of the UAV at night or in low-light environments, facilitate the UAV to accurately find the landing position, and reduce the risk of the UAV colliding with other obstacles during landing, thereby enhancing the safety of landing.

[0011] Preferably, a plurality of adjustment screws are provided on the outer surface of the bottom end of the fixed platform, and one end of the plurality of adjustment screws is connected with a ring. By combining the adjustment screws and the rings, the height and angle of the fixed platform can be conveniently adjusted to adapt to different ground conditions and UAV landing requirements.

[0012] Preferably, the outer surfaces of the abutment assembly and the clamping plate are both wrapped with rubber, which can reduce friction when in contact with the drone and avoid damage to the surface of the drone.

[0013] Preferably, the outer ends of the abutment assembly and the clamping plate are both arc-shaped, and the arc-shaped design can reduce the sharp edges when contacting the drone, thereby avoiding scratching or damaging the surface of the drone during the clamping or abutment process.

[0014] It can be seen from the above technical solutions that the present application has the following beneficial effects:

[0015] 1. The utility model automatically triggers the action of the cylinder and the electric push rod through the detection of the pressure sensor, and realizes the adaptive adjustment of the landing process of the UAV. The introduction of the laser sensor enables the landing platform to accurately measure the size and position of the UAV support, and then accurately clamp the bottom support of the UAV through the electric push rod. This precise clamping ensures the stability of the UAV during the landing process and reduces the risk of shaking or tilting caused by external forces such as wind.

[0016] 2. The utility model can ensure that the drone remains stable during landing through adaptive adjustment and precise clamping, thereby reducing the risk of damage to the drone or personal injury caused by unstable landing. The arc-shaped design of the abutment components and the splint further reduces friction and damage when in contact with the drone, improving landing safety. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 This is a schematic diagram of the first three-dimensional structure of the utility model;

[0018] Figure 2 This is a schematic diagram of the second three-dimensional structure of the utility model;

[0019] Figure 3 This is a schematic diagram of the cross-sectional structure of the utility model;

[0020] Figure 4 This is a schematic diagram of the structure of the abutment assembly of the utility model;

[0021] Figure 5 For this utility model Figure 3 The enlarged schematic diagram at A in the middle;

[0022] Figure 6 For this utility model Figure 3 Enlarged schematic diagram of point B in the middle.

[0023] In the figure: 1. fixing table; 2. supporting seat; 3. light bar; 4. abutting assembly; 5. damping block; 6. adjusting screw; 7. circular ring; 8. cylinder; 9. spring; 411. electric push rod; 412. clamping plate; 413. laser sensor; 414. pressure sensor; 911. first circular plate; 912. damper; 913. second circular plate. DETAILED DESCRIPTION

[0024] The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, and use. It should be understood that in all of these figures, the same or similar reference numerals indicate the same or similar parts and features. The various drawings only schematically represent the concepts and principles of the embodiments of the present disclosure, and do not necessarily show the specific dimensions and proportions of the various embodiments of the present disclosure. Specific parts in specific drawings may be exaggerated to illustrate the relevant details or structures of the embodiments of the present disclosure.

[0025] See also Figure 1-6 , an embodiment provided by the utility model:

[0026] A highly stable drone landing platform comprises a fixed platform 1, the top of the fixed platform 1 is connected to a support seat 2, and the outer surface of the support seat 2 is provided with a groove, multiple groups of cylinders 8 are fixedly installed in the groove, and the tops of the multiple groups of cylinders 8 are connected to abutment components 4, laser sensors 413 are arranged on the outer surfaces of both sides of the top of the abutment components 4, and through grooves are provided on both sides of the bottom end of the abutment components 4, multiple groups of electric push rods 411 are fixedly installed in the bottom through grooves, and one end of the multiple groups of electric push rods 411 is connected to a clamping plate 412, and multiple groups of pressure sensors 414 are fixedly installed on the outer surface of the bottom end of the abutment components 4.

[0027] Furthermore, a limiting groove is provided at the top of the fixed platform 1, and a plurality of groups of first circular plates 911 are fixedly installed in the limiting groove, a damper 912 is fixedly installed on the outer surface of the top of the plurality of groups of first circular plates 911, and the top of the damper 912 is connected to a second circular plate 913, and the top of the second circular plate 913 is connected to a damping block 5. The damping system composed of the first circular plate 911, the damper 912 and the second circular plate 913 can provide additional cushioning when the UAV lands, reduce the shaking of the UAV caused by uneven ground or wind, and thus enhance the landing stability.

[0028] Furthermore, a spring 9 is connected between the first circular plate 911 and the second circular plate 913. The combination of the spring 9 and the damper 912 can absorb and alleviate the impact force, reduce the risk of damage to the drone, and ensure the safety of landing.

[0029] Furthermore, a light bar 3 is provided on the top outer surface of the support base 2, which can improve the visibility of the UAV at night or in low-light environments, facilitate the UAV to accurately find the landing position, and reduce the risk of the UAV colliding with other obstacles during landing, thereby enhancing the safety of landing.

[0030] Furthermore, a plurality of adjusting screws 6 are provided on the outer surface of the bottom end of the fixed platform 1, and a ring 7 is connected to one end of the plurality of adjusting screws 6. By combining the adjusting screws 6 and the ring 7, the height and angle of the fixed platform 1 can be conveniently adjusted to adapt to different ground conditions and UAV landing requirements.

[0031] Furthermore, the outer surfaces of the abutting component 4 and the clamping plate 412 are both wrapped with rubber, which can reduce friction when in contact with the drone and prevent the surface of the drone from being damaged.

[0032] Furthermore, the outer ends of the abutment component 4 and the clamping plate 412 are both arc-shaped. The arc-shaped design can reduce the sharp edges when contacting the drone, thereby avoiding scratching or damaging the surface of the drone during the clamping or abutment process.

[0033] Working principle: When the drone is ready to land on the top of the support base 2, first, the drone contacts the top surface of the support base 2, at which time, the pressure sensor 414 at the bottom of the abutment assembly 4 will immediately sense the weight of the drone. Once the pressure sensor 414 detects that the drone has landed, it will send a signal to the control system to activate the multiple groups of cylinders 8 corresponding to the contact position of the drone.

[0034] After receiving the control signal, the cylinder 8 starts to move downward, driving the abutment assembly 4 to descend as a whole to adapt to the support at the bottom of the drone. During the descent, the laser sensors 413 on the outer surfaces of both sides of the abutment assembly 4 start to work and quickly scan the support at the bottom of the drone. The laser sensor 413 can accurately measure the size and position of the drone support by emitting a laser beam and receiving a reflected signal.

[0035] According to the measurement data of the laser sensor 413, the control system calculates the precise position of the drone support that needs to be clamped, and sends instructions to multiple sets of electric push rods 411. After receiving the instructions, the electric push rods 411 start to telescope, and by adjusting their telescopic length, the clamping plate 412 can tightly clamp the bottom support of the drone.

[0036] In this way, the drone landing platform can ensure the stability and safety of the drone during the landing process. Regardless of whether the ground is flat or there is wind interference, the landing platform can provide a stable and reliable landing environment for the drone through adaptive adjustment and precise clamping.

[0037] It is obvious to those skilled in the art that the present invention is not limited to the details of the exemplary embodiments described above, and that the present invention can be implemented in other specific forms without departing from the spirit or essential features of the present invention. Therefore, the embodiments should be regarded as exemplary and non-limiting from any point of view, and the scope of the present invention is defined by the appended claims rather than the above description, and it is intended that all changes falling within the meaning and scope of the equivalent elements of the claims are included in the present invention. Any reference numeral in a claim should not be regarded as limiting the claim to which it relates.

Claims

1. A highly stable drone landing platform, comprising a fixed platform (1), characterized in that: The top of the fixed platform (1) is connected to a support base (2), and a groove is provided on the outer surface of the support base (2), a plurality of groups of cylinders (8) are fixedly installed in the groove, and the tops of the plurality of groups of cylinders (8) are connected to abutment components (4), laser sensors (413) are provided on the outer surfaces of both sides of the top of the abutment components (4), and through grooves are provided on both sides of the bottom of the abutment components (4), a plurality of groups of electric push rods (411) are fixedly installed in the through grooves at the bottom, and one end of the plurality of groups of electric push rods (411) is connected to a clamping plate (412), and a plurality of groups of pressure sensors (414) are fixedly installed on the outer surface of the bottom of the abutment components (4).

2. A highly stable UAV landing platform according to claim 1, characterized in that: A limiting groove is provided at the top of the fixed platform (1), and a plurality of groups of first circular plates (911) are fixedly installed in the limiting groove; dampers (912) are fixedly installed on the outer surfaces of the top ends of the plurality of groups of first circular plates (911); the top ends of the dampers (912) are connected to second circular plates (913), and the top ends of the second circular plates (913) are connected to damping blocks (5).

3. A highly stable UAV landing platform according to claim 2, characterized in that: A spring (9) is connected between the first circular plate (911) and the second circular plate (913).

4. The UAV landing platform with strong stability according to claim 1, characterized in that: A light bar (3) is provided on the outer surface of the top end of the support seat (2).

5. The UAV landing platform with high stability according to claim 1, characterized in that: The outer surface of the bottom end of the fixed platform (1) is provided with a plurality of sets of adjusting screws (6), and one end of the plurality of sets of adjusting screws (6) is connected to a circular ring (7).

6. The UAV landing platform with strong stability according to claim 1, characterized in that: The outer surfaces of the abutment component (4) and the clamping plate (412) are both wrapped with rubber.

7. The UAV landing platform with high stability according to claim 1, characterized in that: The outer ends of the abutment assembly (4) and the clamping plate (412) are both arc-shaped.

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