Automatic unmanned aerial vehicle airport

Abstract

The utility model discloses an automatic unmanned aerial vehicle airport which comprises a shell, a first U-shaped cover plate and a second U-shaped cover plate are installed on the two sides of the top end of the shell respectively, and a first electric push rod is installed in the center of the bottom end in the shell. An unmanned aerial vehicle bearing assembly used for parking and wireless charging of an unmanned aerial vehicle is installed at the top end of the first electric push rod, and the first electric push rod is used for driving the unmanned aerial vehicle bearing assembly to move in the Y-axis direction and driving the first U-shaped cover plate and the second U-shaped cover plate to move in the X-axis direction. The unmanned aerial vehicle bearing assembly is provided with a first bearing plate used for parking of the unmanned aerial vehicle, and second bearing plates used for parking of the unmanned aerial vehicle are arranged on the two sides of the upper portion of the first bearing plate correspondingly. According to the unmanned aerial vehicle storage device, a plurality of unmanned aerial vehicles can be automatically stored at the same time, and the situation that external rainwater enters the shell from the joint between the first U-shaped cover plate and the second U-shaped cover plate, and consequently structures such as the unmanned aerial vehicles are eroded by the rainwater is avoided.

Description

Technical Field

[0001] The utility model relates to the technical field of UAV supporting equipment, in particular to an automatic UAV airport. Background Technique

[0002] In recent years, UAV technology has developed rapidly, and UAVs have been widely used in many fields, and many UAV-based job positions and job contents have also emerged. Traditional UAV applications mostly use manual operation near the site to control the UAV for flight operations. Although this method has high emergency response capabilities, it has great uncertainties, and the field labor cost is also relatively high. To solve the UAV field operation problem, in the field of UAV applications, a UAV derivative product - an automatic UAV airport has emerged. The automatic UAV airport can replace manual field flight work, enabling the UAV to achieve unmanned automated work. The operator only needs to send flight instructions and flight tasks on a remote computer, and the UAV can take off in the automatic airport, execute tasks, and automatically charge and upload data after returning and landing.

[0003] After retrieval, the patent publication number CN218949500U discloses a UAV airport and a UAV device. The UAV airport includes a bearing structure and a charging component. The charging component includes a power supply, a charging contact, and a wireless charging module. The power supply is arranged in the accommodation cavity. When the UAV is placed on the supporting platform, at least one of the charging contact and the wireless charging module is used to be electrically connected to the UAV and charge the UAV; the control module is signal-connected to the charging component. In the UAV airport of this embodiment, by setting the cooperation of the supporting platform and the cover body, the functions of waterproof and dustproof protection can be realized when charging the UAV. By setting the charging contact and the wireless charging module to cooperate with the UAV, the corresponding charging mode can be selected according to actual needs, and the use effect is good; at the same time, the UAV airport does not need to store a large number of batteries, and the cost and overall quality are also reduced, which is convenient for transportation and movement and easy to use.

[0004] In the actual use process of the above technical solution, it can only automatically store one UAV singly. When automatically storing multiple UAVs, multiple such devices are required, increasing the use cost. Therefore, an automatic UAV airport is designed. Content of the Utility Model

[0005] Aiming at the defects or deficiencies of the automatic UAV airport, the purpose of the utility model is to provide an automatic UAV airport, which can automatically store multiple UAVs at the same time, and avoid the situation that external rainwater enters the inside of the housing from the connection between the first U-shaped cover plate and the second U-shaped cover plate, resulting in the UAV and other structures being eroded by rainwater.

[0006] To achieve the above utility model purpose, the utility model adopts the following technical solutions:

[0007] An automatic UAV airport provided by the utility model comprises a housing. On both sides of the top end of the housing, a first U-shaped cover plate and a second U-shaped cover plate are respectively installed. At the central position of the bottom end inside the housing, a first electric push rod is installed. The top end of the first electric push rod is installed with a UAV bearing assembly for UAV parking and wireless charging, and the first electric push rod is used to drive the UAV bearing assembly to move in the Y-axis direction and the first U-shaped cover plate and the second U-shaped cover plate to move in the X-axis direction;

[0008] On the UAV bearing assembly, a first bearing plate for UAV parking is provided. On both sides above the first bearing plate, second bearing plates for UAV parking are provided, and between the first bearing plate and the second bearing plates, a second electric push rod for driving the second bearing plates to move in a certain direction is installed;

[0009] At one end wall of the first U-shaped cover plate, a sealing rubber block is installed. At one end wall of the second U-shaped cover plate, a sealing groove is formed.

[0010] Preferably, a sixth connecting block is installed on the lower surface of the second bearing plate. The sixth connecting block is movably connected to an eighth connecting block through a movable pin shaft, and the eighth connecting block is installed at one end of the second electric push rod. At the other end of the second electric push rod, a seventh connecting block is installed. The seventh connecting block is movably connected to a fourth connecting block through a movable pin shaft, and the fourth connecting block is installed on both sides of the upper surface of the first bearing plate.

[0011] Preferably, fifth connecting blocks are installed at the four corners of the lower surface of the second bearing plate. The fifth connecting blocks are movably connected to one end of a third connecting rod through a movable pin shaft. The other end of the third connecting rod is movably connected to a third connecting block through a movable pin shaft, and the third connecting block is installed at the four corners of the upper surface of the first bearing plate.

[0012] Preferably, both sides of the front end wall and the rear end wall of the first bearing plate are respectively movably connected to one end of a first connecting rod and one end of a second connecting rod through a movable pin shaft. The other end of the first connecting rod is movably connected to a first connecting block through a movable pin shaft. The other end of the second connecting rod is movably connected to a second connecting block through a movable pin shaft, and the first connecting block and the second connecting block are respectively arranged at the inner tops of the first U-shaped cover plate and the second U-shaped cover plate.

[0013] Preferably, a first wireless charger is arranged at the central position of the upper surface of the first bearing plate, and a second wireless charger is arranged at the central position of the upper surface of the second bearing plate.

[0014] Preferably, T-shaped connecting blocks are installed on the front end walls and rear end walls inside the first U-shaped cover plate and the second U-shaped cover plate. The other ends of the T-shaped connecting blocks are installed in the T-shaped connecting grooves. There is a clearance connection between the outer walls of the T-shaped connecting blocks and the groove walls of the T-shaped connecting grooves. The T-shaped connecting grooves are opened above the front end walls and rear end walls of the housing.

[0015] Preferably, baffles are installed on the end walls at the other ends of the first U-shaped cover plate and the second U-shaped cover plate. Rain-proof louvers are provided on the outer walls on both sides of the housing.

[0016] Compared with the prior art, the above one or more technical solutions have the following beneficial effects:

[0017] 1. In the present utility model, through the cooperative setting of a series of structures, when the staff remotely controls the drone and flies it towards this device, the staff starts the first electric push rod on this device. When the first electric push rod expands and contracts, it will drive the drone bearing assembly to move in the Y-axis direction and the first U-shaped cover plate and the second U-shaped cover plate to move in the X-axis direction. Moreover, the moving directions of the first U-shaped cover plate and the second U-shaped cover plate are opposite. When the staff makes the drone bearing assembly move upward, the first U-shaped cover plate and the second U-shaped cover plate move along the outside in the X-axis direction of the housing. When the drone bearing assembly moves out of the housing to the outside, at this time, the vertical distance between the first U-shaped cover plate and the second U-shaped cover plate is greater than the overall length of the drone bearing assembly, so that the drone bearing assembly moves out of the housing. When the horizontal height of the upper surface of the first bearing plate on the drone bearing assembly is greater than the horizontal height of the first U-shaped cover plate or the second U-shaped cover plate, the staff starts the second electric push rod. When the second electric push rod contracts, it will drive the second bearing plates to move along the outside in the X-axis direction of the housing, and the moving directions of the two second bearing plates are opposite. When the distance between the two second bearing plates reaches a certain value, the staff can operate the drone to park on the first bearing plate and the second bearing plate. After the drone parks, the staff starts the second electric push rod and the first electric push rod again, so that the drone bearing assembly moves into the housing, and the first U-shaped cover plate and the second U-shaped cover plate are in a combined state. Therefore, the present utility model can automatically store multiple drones at the same time, reducing the use cost.

[0018] 2. In the present utility model, through the cooperative setting of a series of structures such as the first U-shaped cover plate, the second U-shaped cover plate, the sealing rubber, and the sealing groove, it can play a role in sealing the connection gap between the first U-shaped cover plate and the second U-shaped cover plate, avoiding the situation that external rainwater enters the housing through the connection gap between the first U-shaped cover plate and the second U-shaped cover plate and causes damage to electronic structures such as drones due to rain erosion. Description of the Drawings

[0019] The accompanying drawings of the specification, which form a part of the present utility model, are used to provide a further understanding of the present utility model. The schematic embodiments of the present utility model and their descriptions are used to explain the present utility model and do not constitute an improper limitation of the present utility model.

[0020] Figure 1 It is a schematic three-dimensional structure diagram of the whole of the present utility model.

[0021] Figure 2 It is a cross-sectional view of the present utility model.

[0022] Figure 3 It is a schematic connection structure between the drone carrying assembly of the present utility model, the first U-shaped cover plate and the second U-shaped cover plate Figure 1 .

[0023] Figure 4 It is a schematic connection structure between the drone carrying assembly of the present utility model, the first U-shaped cover plate and the second U-shaped cover plate Figure 2 .

[0024] Figure 5 It is a schematic structure diagram of the drone carrying assembly of the present utility model.

[0025] Figure 6 It is a cross-sectional view of the drone carrying assembly of the present utility model.

[0026] Figure 7 It is a schematic structure diagram of the first U-shaped cover plate of the present utility model.

[0027] Figure 8 It is a schematic structure diagram of the second U-shaped cover plate of the present utility model.

[0028] Figure 9 It is a schematic structure diagram of the housing of the present utility model.

[0029] In the figure:

[0030] 100, the first U-shaped cover plate; 110, the baffle; 120, the T-shaped connecting block; 130, the first connecting block; 140, the sealing rubber block;

[0031] 200, the drone carrying assembly; 210, the first carrier plate; 211, the first wireless charger; 212, the third connecting block; 213, the fourth connecting block; 220, the second carrier plate; 221, the second wireless charger; 222, the fifth connecting block; 223, the sixth connecting block; 230, the third connecting rod; 240, the second electric push rod; 241, the seventh connecting block; 242, the eighth connecting block;

[0032] 300, the second U-shaped cover plate; 310, the second connecting block; 320, the sealing groove;

[0033] 400, housing; 410, T-shaped connection groove; 420, rainproof louvers;

[0034] 500, first electric push rod;

[0035] 600, first connecting rod;

[0036] 700, second connecting rod. Detailed implementation mode

[0037] The present utility model will be further described below in conjunction with the drawings and embodiments.

[0038] It should be noted that the following detailed description is exemplary and is intended to provide further illustration of the present utility model. Unless otherwise specified, all technical and scientific terms used herein have the same meaning as commonly understood by those of ordinary skill in the technical field to which the present utility model belongs.

[0039] It should be noted that the terms used herein are only for describing specific implementation modes and are not intended to limit the exemplary implementation modes according to the present invention. As used herein, unless the context clearly indicates otherwise, the singular form is also intended to include the plural form. In addition, it should be understood that when the terms "comprising" and / or "including" are used in this specification, they indicate the presence of features, steps, operations, devices, components, and / or combinations thereof.

[0040] As Figures 1 - 9 shown, an automatic UAV airport includes a housing 400. On both sides of the top end of the housing 400, a first U-shaped cover plate 100 and a second U-shaped cover plate 300 are respectively installed. At the center position of the bottom end inside the housing 400, a first electric push rod 500 is installed. At the top end of the first electric push rod 500, a UAV bearing assembly 200 for UAV parking and wireless charging is installed, and the first electric push rod 500 is used to drive the UAV bearing assembly 200 to move in the Y-axis direction and the first U-shaped cover plate 100 and the second U-shaped cover plate 300 to move in the X-axis direction;

[0041] On the UAV bearing assembly 200, a first bearing plate 210 for UAV parking is provided. On both sides above the first bearing plate 210, second bearing plates 220 for UAV parking are provided, and between the first bearing plate 210 and the second bearing plate 220, a second electric push rod 240 for driving the second bearing plate 220 to move in a certain direction is installed;

[0042] A sealing rubber block 140 is installed on the end wall at one end of the first U-shaped cover plate 100, and a sealing groove 320 is formed on the end wall at one end of the second U-shaped cover plate 300. When the first U-shaped cover plate 100 and the second U-shaped cover plate 300 are in a combined state and the sealing rubber block 140 on the first U-shaped cover plate 100 moves into the sealing groove 320 on the second U-shaped cover plate 300, at this time, the sealing rubber block 140 can seal the connection gap between the first U-shaped cover plate 100 and the second U-shaped cover plate 300, avoiding the situation that external rainwater enters the interior of the housing 400 from the connection gap between the first U-shaped cover plate 100 and the second U-shaped cover plate 300, resulting in damage to electronic structures such as drones due to rain erosion.

[0043] A sixth connection block 223 is installed on the lower surface of the second bearing plate 220. The sixth connection block 223 is movably connected to an eighth connection block 242 through a movable pin shaft, and the eighth connection block 242 is installed at one end of a second electric push rod 240. The other end of the second electric push rod 240 is installed with a seventh connection block 241. The seventh connection block 241 is movably connected to a fourth connection block 213 through a movable pin shaft, and the fourth connection block 213 is installed on both sides of the upper surface of the first bearing plate 210. Fifth connection blocks 222 are installed at the four corners of the lower surface of the second bearing plate 220. The fifth connection blocks 222 are movably connected to one end of a third connecting rod 230 through a movable pin shaft. The other end of the third connecting rod 230 is movably connected to a third connection block 212 through a movable pin shaft, and the third connection block 212 is installed at the four corners of the upper surface of the first bearing plate 210. With the coordinated setting of structures such as the sixth connection block 223, the eighth connection block 242, the seventh connection block 241, the fourth connection block 213, the fifth connection block 222, the third connecting rod 230, the third connection block 212, and the second electric push rod 240, when the second electric push rod 240 expands and contracts, it will drive the second bearing plate 220 to move in a certain direction.

[0044] Both sides of the front end wall and the rear end wall of the first bearing plate 210 are respectively movably connected to one end of a first connecting rod 600 and one end of a second connecting rod 700 through movable pin shafts. The other end of the first connecting rod 600 is movably connected to a first connection block 130 through a movable pin shaft. The other end of the second connecting rod 700 is movably connected to a second connection block 310 through a movable pin shaft, and the first connection block 130 and the second connection block 310 are respectively arranged at the inner tops of the first U-shaped cover plate 100 and the second U-shaped cover plate 300. With the coordinated setting of structures such as the first connection block 130, the second connection block 310, the first connecting rod 600, and the second connecting rod 700, when the first electric push rod 500 expands and contracts, it will drive the first U-shaped cover plate 100 and the second U-shaped cover plate 300 to move in the X-axis direction.

[0045] At the center position of the upper surface of the first carrier plate 210, a first wireless charger 211 is provided. At the center position of the upper surface of the second carrier plate 220, a second wireless charger 221 is provided. The first wireless charger 211 and the second wireless charger 221 can wirelessly charge the drone.

[0046] T-shaped connection blocks 120 are installed on the front end walls and the rear end walls inside the first U-shaped cover plate 100 and the second U-shaped cover plate 300. The other ends of the T-shaped connection blocks 120 are installed in the T-shaped connection grooves 410. There is a clearance connection between the outer walls of the T-shaped connection blocks 120 and the groove walls of the T-shaped connection grooves 410. And the T-shaped connection grooves 410 are opened above the front end walls and the rear end walls of the housing 400. Because there is a clearance connection between the outer walls of the T-shaped connection blocks 120 and the groove walls of the T-shaped connection grooves 410, it can play a role in limiting and guiding the movement of the first U-shaped cover plate 100 and the second U-shaped cover plate 300.

[0047] Baffles 110 are installed on the end walls at the other ends of the first U-shaped cover plate 100 and the second U-shaped cover plate 300. The setting of the baffles 110 can prevent rainwater from entering the interior of the housing from both sides of the top of the housing 400. Rainproof louvers 420 are provided on the outer walls on both sides of the housing 400. The setting of the rainproof louvers 420 can not only play a role in protecting the housing 400 from rain, but also play a role in natural ventilation and heat dissipation for the interior of the housing 400.

[0048] When the staff remotely controls the drone and it flies towards this device, the staff activates the first electric push rod 500 on this device. When the first electric push rod 500 expands and contracts, it will drive the drone bearing assembly 200 to move in the Y-axis direction and the first U-shaped cover plate 100 and the second U-shaped cover plate 300 to move in the X-axis direction. Moreover, the moving directions of the first U-shaped cover plate 100 and the second U-shaped cover plate 300 are opposite. When the staff makes the drone bearing assembly 200 move upward, the first U-shaped cover plate 100 and the second U-shaped cover plate 300 move along the outside of the housing 400 in the X-axis direction. When the drone bearing assembly 200 moves out of the housing 400 to the outside, at this time, the vertical distance between the first U-shaped cover plate 100 and the second U-shaped cover plate 300 is greater than the overall length of the drone bearing assembly 200, so that the drone bearing assembly 200 moves out of the housing 400. When the horizontal height of the upper surface of the first bearing plate 210 on the drone bearing assembly 200 is greater than the horizontal height of the first U-shaped cover plate 100 or the second U-shaped cover plate 300, the staff activates the second electric push rod 240. When the second electric push rod 240 contracts, it will drive the second bearing plates 220 to move along the outside of the housing 400 in the X-axis direction, and the moving directions of the two second bearing plates 220 are opposite. When the distance between the two second bearing plates 220 reaches a certain value, the staff can operate the drone to park on the first bearing plate 210 and the second bearing plates 220. After the drone has parked, the staff activates the second electric push rod 240 and the first electric push rod 500 again, so that the drone bearing assembly 200 moves into the housing 400, and the first U-shaped cover plate 100 and the second U-shaped cover plate 300 are in a combined state. Thus, the utility model can automatically store multiple drones at the same time, reducing the use cost.

[0049] The above are only the preferred embodiments of the utility model and are not used to limit the present invention. For those skilled in the art, various changes and modifications can be made to the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention shall be included within the protection scope of the present invention.

Claims

1. An automatic drone airport, comprising a housing (400), characterized in that: A first U-shaped cover plate (100) and a second U-shaped cover plate (300) are respectively installed on both sides of the top end of the shell (400); a first electric push rod (500) is installed at the center of the bottom end of the shell (400); a drone carrying assembly (200) for parking and wireless charging of the drone is installed on the top end of the first electric push rod (500); and the first electric push rod (500) is used to drive the drone carrying assembly (200) to move in the Y-axis direction and the first U-shaped cover plate (100) and the second U-shaped cover plate (300) to move in the X-axis direction; The drone bearing assembly (200) is provided with a first bearing plate (210) for parking the drone, and second bearing plates (220) for parking the drone are provided on both sides above the first bearing plate (210), and a second electric push rod (240) for driving the second bearing plate (220) to move in a certain direction is installed between the first bearing plate (210) and the second bearing plate (220); A sealing rubber block (140) is installed on the end wall of one end of the first U-shaped cover plate (100), and a sealing groove (320) is opened on the end wall of one end of the second U-shaped cover plate (300).

2. The automatic drone airport according to claim 1, characterized in that: A sixth connecting block (223) is installed on the lower surface of the second supporting plate (220), and the sixth connecting block (223) is movably connected to the eighth connecting block (242) through a movable pin shaft, and the eighth connecting block (242) is installed on one end of the second electric push rod (240), and a seventh connecting block (241) is installed on the other end of the second electric push rod (240), and the seventh connecting block (241) is movably connected to the fourth connecting block (213) through a movable pin shaft, and the fourth connecting block (213) is installed on both sides of the upper surface of the first supporting plate (210).

3. The automatic drone airport according to claim 1, characterized in that: A fifth connecting block (222) is installed at the four corners of the lower surface of the second supporting plate (220), and the fifth connecting block (222) is movably connected to one end of the third connecting rod (230) through a movable pin, and the other end of the third connecting rod (230) is movably connected to the third connecting block (212) through a movable pin, and the third connecting block (212) is installed at the four corners of the upper surface of the first supporting plate (210).

4. The automatic drone airport according to claim 1, characterized in that: Both sides of the front end wall and the rear end wall of the first bearing plate (210) are movably connected to one end of the first connecting rod (600) and one end of the second connecting rod (700) through a movable pin shaft, respectively; the other end of the first connecting rod (600) is movably connected to the first connecting block (130) through a movable pin shaft, and the other end of the second connecting rod (700) is movably connected to the second connecting block (310) through an active pin shaft, and the first connecting block (130) and the second connecting block (310) are respectively arranged on the inner top of the first U-shaped cover plate (100) and the second U-shaped cover plate (300).

5. The automatic drone airport according to claim 1, characterized in that: A first wireless charger (211) is arranged at the center of the upper surface of the first carrying plate (210), and a second wireless charger (221) is arranged at the center of the upper surface of the second carrying plate (220).

6. The automatic drone airport according to claim 1, characterized in that: A T-shaped connection block (120) is installed on the front end wall and the rear end wall of the inner side of the first U-shaped cover plate (100) and the second U-shaped cover plate (300); the other end of the T-shaped connection block (120) is installed in the T-shaped connection groove (410); the outer wall of the T-shaped connection block (120) and the groove wall of the T-shaped connection groove (410) are connected with a gap, and the T-shaped connection groove (410) is opened above the front end wall and the rear end wall of the shell (400).

7. The automatic drone airport according to claim 1, characterized in that: The end walls of the other ends of the first U-shaped cover plate (100) and the second U-shaped cover plate (300) are both installed with baffles (110), and the outer walls on both sides of the shell (400) are both provided with rainproof shutters (420).

Images