Control cabin with unmanned aerial vehicle take-off and landing platform

Abstract

The utility model relates to a control cabin with an unmanned aerial vehicle take-off and landing platform, and aims to solve the problems that the unmanned aerial vehicle cannot be centered on the take-off and landing platform when the unmanned aerial vehicle flies back and parks, so that the unmanned aerial vehicle is easy to damage when a cabin cover is closed, and the unmanned aerial vehicle is not easy to damage if dust is seriously raised in the environment in the trial task process. The technical problems that the unmanned aerial vehicle is contaminated with much dust if the unmanned aerial vehicle runs out of the control cabin, the unmanned aerial vehicle is difficult to dedust after executing a task and returning to the control cabin, and thus electrical elements in the control cabin are easily damaged by the dust are solved, and the unmanned aerial vehicle comprises the control cabin, and the two sides of the top of the control cabin are slidably provided with a left cabin cover and a right cabin cover correspondingly; the unmanned aerial vehicle parking device has the advantages that the unmanned aerial vehicle parked on the parking platform can be automatically centered, the unmanned aerial vehicle can be prevented from being damaged when the cover body is closed when the unmanned aerial vehicle is parked obliquely, and the situation that the unmanned aerial vehicle is contaminated with more dust, and consequently electrical elements in the control cabin are damaged is avoided.

Description

Technical Field

[0001] The utility model relates to the field of unmanned aerial vehicle control cabins, in particular to a control cabin with an unmanned aerial vehicle take-off and landing platform. Background Art

[0002] The drone control cabin is a platform for remote and precise take-off and landing of drones. It is a stable "home" for drones that can withstand severe weather such as strong winds and heavy rains. The machine nest is interconnected with the smart inspection fleet operation control center to realize automatic storage of drones, intelligent automatic charging, real-time status monitoring, and automatic data transmission.

[0003] When traditional drones fly back to park, they cannot be centered on the take-off and landing platform, which can easily cause damage to the drone when the hatch is closed. This requires personnel to manually adjust the position of the drone, which is inconvenient. In addition, during the trial mission of the drone, if the dust in the environment is serious, the drone will be contaminated with a lot of dust. After the drone completes the mission and returns to the control cabin, it is difficult to remove the dust, so the dust can easily damage the electrical components in the control cabin. For this reason, a new technical solution needs to be designed to solve this problem. Utility Model Content

[0004] The purpose of the utility model is to overcome the shortcomings of the prior art, meet the actual needs, and provide a control cabin with a UAV take-off and landing platform to solve the problem that the current UAV cannot be centered on the take-off and landing platform when it flies back to park, so that the UAV is easily damaged when the cabin cover is closed, so that personnel need to manually adjust the position of the UAV, which is inconvenient. In addition, during the trial mission of the UAV, if the dust in the environment is relatively serious, the UAV will be contaminated with a lot of dust. After the UAV completes the mission and returns to the control cabin, it is difficult to remove the dust, so that the dust easily damages the electrical components in the control cabin.

[0005] In order to achieve the purpose of the utility model, the technical solution adopted by the utility model is: designing a control cabin with a drone take-off and landing platform, including a control cabin, a left cabin cover and a right cabin cover are slidably installed on both sides of the top of the control cabin, a parking platform is arranged in the middle of the inner cavity of the control cabin, and two first adjustment grooves and two second adjustment grooves are arranged on the surface of the parking platform, the two first adjustment grooves and the two second adjustment grooves are symmetrically distributed, a first bidirectional screw rod is rotatably connected between the two sides of the inner cavity of the two first adjustment grooves, two first adjustment blocks are slidably connected in the two first adjustment grooves, and the four first adjustment blocks are respectively threadedly sleeved on the two first bidirectional screw rods. On the outer sides of the rod, a first clamping plate is fixedly connected between the first adjusting blocks in the two first adjusting grooves, and a second bidirectional screw rod is rotatably connected between the two sides of the inner cavity of the two second adjusting grooves, and two second adjusting blocks are slidably connected in the two second adjusting grooves, and the four second adjusting blocks are respectively threadedly sleeved on the outer sides of the two second bidirectional screw rods, and a second clamping plate is fixedly connected between the second adjusting blocks in the two second adjusting grooves; the first clamping plate is attached to the top of the second clamping plate, and the first clamping plate and the second clamping plate are both hollow structures, and the surfaces of the first clamping plate and the second clamping plate are provided with multiple air injection holes, and the first clamping plate and the second clamping plate are connected with air blowing pipes.

[0006] Preferably, the air blowing pipe is a hose, and the bottom ends of the inner cavities of the first regulating groove and the second regulating groove are both provided with rectangular holes, and the air blowing pipe is placed in the rectangular holes.

[0007] Preferably, rubber pads are fixedly connected to the outer sides of the first clamping plate and the second clamping plate.

[0008] Preferably, a hatch is provided at the front end of the control cabin, a drone console is installed at the bottom of the inner cavity of the hatch, slide grooves are provided on both sides of the inner cavity of the hatch, sliders are slidably connected in the two slide grooves, a cabin door is provided between the two sliders, connecting shafts are rotatably connected on both sides of the cabin door, and the two connecting shafts are rotatably connected to the two sliders respectively, and support blocks are fixedly connected to the inner walls of the hatch below the two slide grooves.

[0009] Preferably, a wind speed meter is installed on the top of the left cabin cover, and a rain sensor is installed on the left cabin cover on one side of the wind speed meter.

[0010] Preferably, the width of the rectangular hole is matched to the outer diameter of the blowing tube.

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

[0012] The utility model combines the first adjusting slot, the second adjusting slot, the first adjusting block, the second adjusting block, the first bidirectional screw rod, the second bidirectional screw rod, the first clamping plate, the second clamping plate, the air jet hole and the air blowing pipe. When the drone returns to the parking platform after performing the task, the first bidirectional screw rod is driven to rotate by the motor, and the first adjusting block is guided to move in the first adjusting slot, thereby driving the two first clamping plates to move synchronously towards each other and contact the drone bracket and push the drone to be centered in the middle of the parking platform. Then, the second bidirectional screw rod is driven to rotate by the motor, thereby cooperating with the second clamping plate to contact the other two sides of the drone to fix the drone, thereby automatically aligning the drone parked on the parking platform, thereby avoiding damage to the drone when the cover body is closed when the drone is parked and tilted, which is more convenient. When the drone is centered, the air pump cooperates with the air blowing pipe to spray high-pressure airflow from the air jet hole to clean the dust adsorbed on the surface of the drone, thereby avoiding that more dust will be contaminated on the drone and easily damage the electrical components in the control cabin. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0014] Figure 2 This is a schematic diagram of the control cabin structure of the utility model;

[0015] Figure 3 It is the front view of the utility model;

[0016] Figure 4 This is a top view of the parking platform of the utility model;

[0017] Figure 5 It is an enlarged view of point A of the utility model;

[0018] Figure 6 This is a schematic diagram of the hatch structure of the utility model;

[0019] Figure 7 It is the front view of the hatch of the present utility model.

[0020] In the figure: 1. control cabin; 11. left hatch; 12. right hatch; 2. anemometer; 21. rain sensor; 3. hatch; 31. hatch door; 32. slide; 33. slider; 34. support block; 35. connecting shaft; 4. parking platform; 5. second splint; 51. jet hole; 52. first splint; 53. first adjustment slot; 54. air blowing pipe; 55. first adjustment block; 56. second adjustment block; 57. second bidirectional screw rod; 58. first bidirectional screw rod; 59. rectangular hole; 510. second adjustment slot; 6. rubber pad; 7. drone control console. DETAILED DESCRIPTION

[0021] The utility model is further described below in conjunction with the accompanying drawings and embodiments:

[0022] Example 1: A control cabin with a drone take-off and landing platform, see Figures 1 to 5 , including a control cabin 1, the control cabin 1 has an external size of 6 meters * 3 meters and a height of 2.7 meters. A left hatch cover 11 and a right hatch cover 12 are slidably installed on both sides of the top of the control cabin 1, and a parking platform 4 is arranged in the middle of the inner cavity of the control cabin 1. The surface of the parking platform 4 is provided with two first adjustment grooves 53 and two second adjustment grooves 510. The two first adjustment grooves 53 and the two second adjustment grooves 510 are symmetrically distributed. A first bidirectional screw rod 58 is rotatably connected between both sides of the inner cavity of the two first adjustment grooves 53, and two first adjustment blocks 55 are slidably connected in the two first adjustment grooves 53. , four first adjustment blocks 55 are respectively threadedly sleeved on both sides of the outside of the two first bidirectional screw rods 58, a first clamping plate 52 is fixedly connected between the first adjustment blocks 55 in the two first adjustment grooves 53, a second bidirectional screw rod 57 is rotatably connected between both sides of the inner cavity of the two second adjustment grooves 510, two second adjustment blocks 56 are slidably connected in the two second adjustment grooves 510, four second adjustment blocks 56 are respectively threadedly sleeved on both sides of the outside of the two second bidirectional screw rods 57, and a second clamping plate 5 is fixedly connected between the second adjustment blocks 56 in the two second adjustment grooves 510; the first clamping plate 5 2 is attached to the top of the second clamping plate 5, the first clamping plate 52 and the second clamping plate 5 are both hollow structures, and the surfaces of the first clamping plate 52 and the second clamping plate 5 are both provided with a plurality of air injection holes 51, the first clamping plate 52 and the second clamping plate 5 are both connected with an air blowing pipe 54, and the other end of the air blowing pipe 54 is connected with an air pump. When the UAV returns to the parking platform 4 after completing the mission, the first bidirectional screw rod 58 is driven by the motor to rotate, and the first adjusting block 55 is guided to move in the first adjusting groove 53, thereby driving the two first clamping plates 52 to move synchronously towards each other and contact the UAV bracket and push the UAV to be centered. The middle part of the parking platform 4 is then driven by the motor to rotate the second bidirectional screw rod 57, thereby cooperating with the second clamping plate 5 to contact the other two sides of the drone to fix the drone, so that the drone parked on the parking platform 4 can be automatically centered, thereby avoiding damage to the drone when the cover is closed when the drone is parked and tilted, which is more convenient. When the drone is centered, the air pump cooperates with the air pipe 54 to spray high-pressure air from the jet hole 51 to clean the dust adsorbed on the surface of the drone, so as to avoid more dust on the drone, which may easily damage the electrical components in the control cabin 1.

[0023] For details, see Figure 1The air blowing pipe 54 is a hose, and a rectangular hole 59 is opened at the bottom of the inner cavity of the first adjusting groove 53 and the second adjusting groove 510. The air blowing pipe 54 is placed in the rectangular hole 59. The width of the rectangular hole 59 is adapted to the outer diameter of the air blowing pipe 54. The air blowing pipe 54 is a hose, and the air blowing pipe 54 can move in the first adjusting groove 53 and the second adjusting groove 510, so as to provide high-pressure airflow when the first clamping plate 52 and the second clamping plate 5 move.

[0024] For further information, see Figure 5 The outer sides of the first clamping plate 52 and the second clamping plate 5 are fixedly connected with rubber pads 6. The rubber pads 6 can prevent the first clamping plate 52 and the second clamping plate 5 from directly contacting with the UAV bracket and causing damage, and can increase the friction between the first clamping plate 52 and the second clamping plate 5 and the UAV bracket, thereby improving the stability of the first clamping plate 52 and the second clamping plate 5 in fixing the UAV.

[0025] It is worth noting that see Figure 1 , Figure 5 and Figure 6 A hatch 3 is provided at the front end of the control cabin 1, and a drone console 7 is installed at the bottom of the inner cavity of the hatch 3. Slide grooves 32 are provided on both sides of the inner cavity of the hatch 3, and sliders 33 are slidably connected in the two slide grooves 32. A hatch 31 is provided between the two sliders 33, and connecting shafts 35 are rotatably connected on both sides of the hatch 31, and the two connecting shafts 35 are rotatably connected to the two sliders 33 respectively, and the inner wall of the hatch 3 below the two slide grooves 32 is fixedly connected with a supporting block 34. The hatch 31 can be rotated and placed horizontally by pulling the hatch 31 outward to cooperate with the connecting shaft 35, and then the slider 33 slides in the slide groove 32, so that the opened hatch 31 can be pushed into the hatch 3 and the hatch 31 can be supported by the supporting block 34, so as to facilitate the storage of the opened hatch 31 in the hatch 3, so as to avoid the opened hatch 31 occupying space and affecting the use.

[0026] It is worth noting that see Figure 1 A wind speed meter 2 is installed on the top of the left cabin cover 11, and a rain sensor 21 is installed on the left cabin cover 11 on one side of the wind speed meter 2. The wind speed of the drone when performing a mission can be monitored in real time through the wind speed meter 2, and the rain sensor 21 can monitor the rainfall when it rains.

[0027] In addition, the components designed in the present invention are all universal standard parts or components known to technical personnel in the field. Their structures and principles can be known to technical personnel through technical manuals or through conventional experimental methods. They can be fully implemented by technical personnel in the field, and there is no need to elaborate. The content protected by the present invention does not involve improvements to internal structures and methods.

[0028] The embodiments of the present invention disclose preferred embodiments, but are not limited thereto. A person skilled in the art can easily understand the spirit of the present invention based on the above embodiments and make different extensions and changes. However, as long as they do not deviate from the spirit of the present invention, they are all within the protection scope of the present invention.

Claims

1. A control cabin with a take-off and landing platform for an unmanned aerial vehicle, comprising a control cabin (1), characterized in that: A left hatch cover (11) and a right hatch cover (12) are slidably mounted on both sides of the top of the control cabin (1), a parking platform (4) is arranged in the middle of the inner cavity of the control cabin (1), two first adjustment grooves (53) and two second adjustment grooves (510) are arranged on the surface of the parking platform (4), the two first adjustment grooves (53) and the two second adjustment grooves (510) are symmetrically distributed, a first bidirectional screw rod (58) is rotatably connected between the two sides of the inner cavity of the two first adjustment grooves (53), two first adjustment blocks (55) are slidably connected in the two first adjustment grooves (53), and the four first adjustment blocks (55) are respectively The first adjusting grooves (53) are provided with a first clamping plate (52) fixedly connected between the first adjusting blocks (55) in the two first adjusting grooves (53); the second bidirectional screw rods (57) are rotatably connected between the inner cavities of the two second adjusting grooves (510); the two second adjusting blocks (56) are slidably connected in the two second adjusting grooves (510); the four second adjusting blocks (56) are respectively threadedly mounted on the outer sides of the two second bidirectional screw rods (57); the second clamping plate (5) is fixedly connected between the second adjusting blocks (56) in the two second adjusting grooves (510); The first clamping plate (52) is attached to the top of the second clamping plate (5); the first clamping plate (52) and the second clamping plate (5) are both hollow structures, and a plurality of air injection holes (51) are provided on the surfaces of the first clamping plate (52) and the second clamping plate (5); and the first clamping plate (52) and the second clamping plate (5) are both connected to an air blowing pipe (54).

2. A control cabin with a UAV take-off and landing platform as claimed in claim 1, characterized in that: The air blowing pipe (54) is a hose, and the bottom ends of the inner cavities of the first regulating groove (53) and the second regulating groove (510) are both provided with rectangular holes (59), and the air blowing pipe (54) is placed in the rectangular holes (59).

3. A control cabin with a UAV take-off and landing platform as claimed in claim 1, characterized in that: The outer sides of the first clamping plate (52) and the second clamping plate (5) are both fixedly connected with rubber pads (6).

4. The control cabin with a UAV take-off and landing platform as claimed in claim 1, characterized in that: The front end of the control cabin (1) is provided with a hatch (3), the bottom end of the inner cavity of the hatch (3) is equipped with a drone console (7), both sides of the inner cavity of the hatch (3) are provided with slide grooves (32), two slide grooves (32) are slidably connected with sliders (33), a cabin door (31) is arranged between the two sliders (33), both sides of the cabin door (31) are rotatably connected with connecting shafts (35), and the two connecting shafts (35) are rotatably connected with the two sliders (33) respectively, and the inner wall of the hatch (3) below the two slide grooves (32) is fixedly connected with support blocks (34).

5. The control cabin with a UAV take-off and landing platform as claimed in claim 1, characterized in that: A wind speed meter (2) is installed on the top of the left hatch cover (11), and a rain sensor (21) is installed on the left hatch cover (11) on one side of the wind speed meter (2).

6. A control cabin with a UAV take-off and landing platform as claimed in claim 2, characterized in that: The width of the rectangular hole (59) is adapted to the outer diameter of the blowing tube (54).

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