Unmanned aerial vehicle air traffic control monitoring equipment

Abstract

The utility model relates to the technical field of dynamic information monitoring, in particular to an unmanned aerial vehicle air traffic control monitoring device which comprises a functional module box, a detection block and a bearing assembly, the bearing assembly comprises a spherical fixing base, a supporting cylinder, a driving piece, a lead screw, a lifting rod, a guiding piece, a supporting base and a rotating piece, and according to the air traffic control monitoring requirement of the detection block on the functional module box, the detection block is arranged on the functional module box. A lead screw is driven to rotate through a driving piece in a supporting cylinder, the lead screw rotates to drive a lifting rod to stretch out and draw back in the supporting cylinder through guiding of a guiding piece, the blank pipe monitoring height of a function module box and a detection block is adjusted, and therefore the problem that according to existing blank pipe monitoring equipment for same-field operation of an unmanned aerial vehicle and a manned aerial vehicle, due to the fact that the length of a connecting column is fixed, the working efficiency is high is solved. Therefore, after the spherical fixing seat is buried in the soil, the monitoring height positions of the functional module box and the detection block cannot be adjusted according to different monitoring conditions, and the problem of poor monitoring effect is further caused.

Description

TECHNICAL FIELD

[0001] The utility model relates to dynamic information monitoring technical field especially relates to a unmanned plane air traffic control monitoring equipment. BACKGROUND

[0002] Because of the influence of different regions, the setting and operation of base airspace are different, and there may be a situation of joint operation of unmanned aerial vehicles and manned aircraft in the same place, so air traffic control monitoring equipment is needed for air control, and the existing air traffic control monitoring equipment cannot meet the operation requirements of the activities between manned aircraft and unmanned aerial vehicles.

[0003] The prior art (CN217543695U) discloses an air traffic control monitoring equipment for unmanned aerial vehicles and manned aircraft in the same field, which comprises a device main body, a functional module box, a connecting column and a spherical fixed bottom which are connected in sequence from top to bottom inside the device main body; a detection block is electrically connected to the functional module box, and a trajectory detector, an error judge, an interval distance identifier and an environment detector are arranged in the detection block in parallel from top to bottom and are electrically connected to the detection block, so that the functional module box can timely find the trajectory contradiction between unmanned and manned aircraft during operation, and meet the operation requirements of the activities between unmanned aerial vehicles and manned aircraft in the airport.

[0004] However, since the length of the connecting column is fixed, after the spherical fixed seat is buried in the soil, the monitoring height position of the functional module box and the detection block cannot be adjusted according to different monitoring conditions, which leads to poor monitoring effect. UTILITY MODEL CONTENT

[0005] The utility model aims at providing a unmanned plane air traffic control monitoring equipment, and aims at solving the problems that the existing air traffic control monitoring equipment for unmanned aerial vehicles and manned aircraft in the same field cannot adjust the monitoring height position of the functional module box and the detection block according to different monitoring conditions after the spherical fixed seat is buried in the soil, which leads to poor monitoring effect.

[0006] To achieve the above purpose, the utility model provides a unmanned plane air traffic control monitoring equipment, which comprises a functional module box, a detection block, two light-shielding sheets and a bearing assembly, the detection block is arranged on one side of the functional module box, two light-shielding sheets are arranged on both sides of the functional module box respectively,

[0007] The bearing assembly comprises a spherical fixed seat, a supporting cylinder, a driving piece, a lead screw, a lifting rod, a guide piece, a supporting seat and a rotating piece;

[0008] The support cylinder is fixedly connected with the spherical fixing base and is located on one side of the spherical fixing base; the driving part is arranged in the support cylinder; the lead screw is fixedly connected with the driving part and is located on one side of the driving part; the lifting rod is threadedly connected with the lead screw and is located on one side of the lead screw; the guide part is arranged on one side of the spherical fixing base; the support base is fixedly connected with the lifting rod and is located on one side of the lifting rod; and the rotating part is arranged between the support base and the functional module box.

[0009] The driving part comprises a driving motor and a rotating rod, the driving motor is fixedly connected with the support cylinder and is located in the support cylinder; the rotating rod is fixedly connected with the output end of the driving motor, is fixedly connected with the lead screw, and is located on one side of the driving motor.

[0010] The guide part comprises a guide frame, a guide rod and a guide block, the guide frame is fixedly connected with the spherical fixing base and is located on one side of the spherical fixing base; the guide rod is fixedly connected with the guide frame and is located on one side of the guide frame; the guide block is slidingly connected with the guide rod, is fixedly connected with the support base, and is located on one side of the guide rod.

[0011] The rotating part comprises a rotating base, a rotating motor and a rotating disc, the rotating base is fixedly connected with the support base and is located on one side of the support base; the rotating motor is fixedly connected with the rotating base and is located on one side of the rotating base; the rotating disc is fixedly connected with the output end of the rotating motor, is fixedly connected with the functional module box, and is located on one side of the rotating motor.

[0012] The bearing assembly further comprises a scale table, the scale table is fixedly connected with the lifting rod and is located on one side of the lifting rod.

[0013] The utility model discloses an unmanned plane air traffic control monitoring equipment, the spherical fixing base is buried in the land, then according to the air traffic control monitoring demand of detection block on the functional module box, through the driving part in the support cylinder drive the rotation of the lead screw, the lead screw rotation drives the lifting rod in the support cylinder, through the guidance of the guide part telescopic, adjust the air traffic control monitoring height of functional module box and detection block, then when needing to adjust the monitoring angle of air traffic control monitoring in the air traffic control monitoring process, through the rotating part drive the rotation of functional module box adjust the monitoring angle of detection block, thereby solve the existing unmanned plane and manned plane same field operation's air traffic control monitoring equipment, because the length of connecting column is fixed, when the spherical fixing base is buried in the earth, the monitoring height position of functional module box and detection block cannot be adjusted according to different monitoring conditions, and further lead to the problem of poor monitoring effect. BRIEF DESCRIPTION OF DRAWINGS

[0014] In order to more clearly illustrate the technical solutions in the embodiments of the present application or the prior art, the drawings needed to be used in the embodiments or prior art description will be briefly introduced.

[0015] Figure 1 is the overall structure schematic diagram of the utility model.

[0016] Figure 2 is the side view of the utility model's whole.

[0017] Figure 3 is the front view of the utility model's whole.

[0018] Figure 4 is the section view of the utility model's support cylinder, driving part, screw rod and lifting rod.

[0019] 101-function module box, 102-detection block, 103-spherical fixed seat, 104-support cylinder, 105-driving part, 106-screw rod, 107-lifting rod, 108-guiding part, 109-supporting seat, 110-rotating part, 111-driving motor, 112-rotating rod, 113-guiding frame, 114-guiding rod, 115-guiding block, 116-rotating seat, 117-rotating motor, 118-rotating disc, 119-dial, 120-photofilter. DETAILED DESCRIPTION

[0020] The embodiments of the utility model will be described in detail below, the examples of the embodiments are shown in the drawings, the embodiments described below by referring to the drawings are exemplary, and are intended to explain the utility model, and can not be understood as the limitation of the utility model

[0021] Please refer to Figures 1-4 , wherein, Figure 1 is the overall structure schematic diagram of the utility model, Figure 2 is the side view of the utility model's whole, Figure 3 is the front view of the utility model's whole, Figure 4 is the section view of the utility model's support cylinder, driving part, screw rod and lifting rod.

[0022] The utility model provides a kind of unmanned aerial vehicle air traffic control monitoring equipment: including functional module box 101, detection block 102, two light-shielding sheets 120 and bearing assembly, the bearing assembly includes spherical fixed seat 103, support cylinder 104, driving part 105, screw rod 106, lifting rod 107, guide piece 108, support seat 109, rotating part 110 and scale table 119, the driving part 105 includes driving motor 111 and rotating lever 112, the guide piece 108 includes guide frame 113, guide rod 114 and guide block 115, the rotating part 110 includes rotating seat 116, rotating motor 117 and turntable 118, by the foregoing scheme, the existing air traffic control monitoring equipment facing unmanned aerial vehicle and manned aircraft same field operation has been solved, since the length of connecting column is fixed, when spherical fixed seat is buried in soil, the monitoring height position of functional module box and detection block cannot be adjusted according to different monitoring conditions, in turn lead to the problem of poor monitoring effect.

[0023] For this specific implementation, the detection block 102 is placed on one side of the functional module box 101, and two light-shielding sheets 120 are placed on both sides of the functional module box 101. The detection block 102 cooperates with the functional module box 101 to monitor unmanned aerial vehicles. The two light-shielding sheets 120 are used to shield light on both sides of the detection block 102. The functional module box 101, the detection block 102, and the light-shielding sheets 120 are prior art, and their specific structures and usage are described in detail in the patent document CN217543695U. Therefore, further description is not provided here.

[0024] The support cylinder 104 is fixedly connected with the spherical fixing seat 103 and located on one side of the spherical fixing seat 103; the driving part 105 is arranged inside the support cylinder 104; the lead screw 106 is fixedly connected with the driving part 105 and located on one side of the driving part 105; the lifting rod 107 is threadedly connected with the lead screw 106 and located on one side of the lead screw 106; the guide part 108 is arranged on one side of the spherical fixing seat 103; the support seat 109 is fixedly connected with the lifting rod 107 and located on one side of the lifting rod 107; the rotating part 110 is arranged between the support seat 109 and the functional module box 101, the spherical fixing seat 103 is buried in the land, then according to the air pipe monitoring requirement of the detection block 102 on the functional module box 101, the lead screw 106 is driven to rotate by the driving part 105 in the support cylinder 104, the lifting rod 107 is driven to rotate in the support cylinder 104 by the lead screw 106, the support seat 109 is telescoped by the guide of the guide part 108, the monitoring height of the functional module box 101 and the detection block 102 is adjusted, then when the monitoring angle of the air pipe monitoring needs to be adjusted in the air pipe monitoring process, the monitoring angle of the detection block 102 is adjusted by rotating the functional module box 101 through the rotating part 110, thereby solving the problem that the existing air pipe monitoring equipment faces unmanned aerial vehicles and manned aircrafts running in the same field, because the length of the connecting column is fixed, after the spherical fixing seat is buried in the soil, the monitoring height position of the functional module box and the detection block cannot be adjusted according to different monitoring conditions, and the monitoring effect is poor.

[0025] Secondly, the driving motor 111 is fixedly connected with the support cylinder 104 and located inside the support cylinder 104; the rotating rod 112 is fixedly connected with the output end of the driving motor 111 and fixedly connected with the lead screw 106 and located on one side of the driving motor 111, the rotating rod 112 is driven to rotate by the driving motor 111, and the lead screw 106 is driven to rotate by the rotating rod 112.

[0026] Meanwhile, the guide frame 113 is fixedly connected with the spherical fixing seat 103 and located on one side of the spherical fixing seat 103; the guide rod 114 is fixedly connected with the guide frame 113 and located on one side of the guide frame 113; the guide block 115 is slidingly connected with the guide rod 114 and fixedly connected with the support seat 109 and located on one side of the guide rod 114, the guide frame 113 is used for supporting the assembly of the guide rod 114, when the support seat 109 is telescoped by the lifting rod 107, the support seat 109 is limited by the guide block 115 sliding on the guide rod 114, so that the support seat 109 vertically ascends and descends.

[0027] In addition, the rotating seat 116 is fixedly connected with the supporting seat 109 and located at one side of the supporting seat 109; the rotating motor 117 is fixedly connected with the rotating seat 116 and located at one side of the rotating seat 116; the rotating disc 118 is fixedly connected with an output end of the rotating motor 117, fixedly connected with the functional module box 101 and located at one side of the rotating motor 117; the rotating seat 116 is used for assembling the rotating motor 117; the rotating disc 118 and the functional module box 101 are driven to rotate by the rotating motor 117; and the position of the detection block 102 for air pipe monitoring is adjusted.

[0028] Furthermore, the scale table 119 is fixedly connected with the lifting rod 107 and located at one side of the lifting rod 107; and the scale table 119 is used for facilitating observation of the height position of the lifting rod 107 during lifting of the lifting rod 107.

[0029] In use of the utility model, the spherical fixing seat 103 is buried in the land; then, according to the air pipe monitoring requirement of the detection block 102 on the functional module box 101, the rotating disc 118 and the functional module box 101 are driven to rotate by the rotating motor 117; the rotating disc 118 and the functional module box 101 are driven to rotate by the rotating motor 117; and the position of the detection block 102 for air pipe monitoring is adjusted.

[0030] The above only discloses one or more preferred embodiments of the present application, and cannot limit the scope of rights of the present application; and a person skilled in the art can understand that all or part of the processes of the above embodiments are implemented, and equivalent changes made according to the claims of the present application still belong to the scope covered by the present application.

Claims

1. An unmanned aerial vehicle (UAV) air traffic control surveillance device, comprising a functional module box, a detection block, and two light-shielding plates, wherein the detection block is disposed on one side of the functional module box; and the two light-shielding plates are respectively disposed on both sides of the functional module box; characterized in that, It also includes the carrier component; The load-bearing assembly includes a spherical fixed seat, a support cylinder, a driving component, a lead screw, a lifting rod, a guide component, a support seat, and a rotating component; The support cylinder is fixedly connected to the spherical fixed seat and located on one side of the spherical fixed seat; the driving component is disposed inside the support cylinder; the lead screw is fixedly connected to the driving component and located on one side of the driving component; the lifting rod is threadedly connected to the lead screw and located on one side of the lead screw; the guide component is disposed on one side of the spherical fixed seat; the support seat is fixedly connected to the lifting rod and located on one side of the lifting rod; the rotating component is disposed between the support seat and the functional module box.

2. The UAV air traffic control monitoring device as described in claim 1, characterized in that, The driving component includes a drive motor and a rotating rod. The drive motor is fixedly connected to the support cylinder and located inside the support cylinder. The rotating rod is fixedly connected to the output end of the drive motor and to the lead screw, and is located on one side of the drive motor.

3. The UAV air traffic control monitoring device as described in claim 2, characterized in that, The guide component includes a guide frame, a guide rod, and a guide block. The guide frame is fixedly connected to the spherical fixed seat and is located on one side of the spherical fixed seat. The guide rod is fixedly connected to the guide frame and is located on one side of the guide frame. The guide block is slidably connected to the guide rod and fixedly connected to the support seat, and is located on one side of the guide rod.

4. The UAV air traffic control monitoring device as described in claim 3, characterized in that, The rotating component includes a rotating base, a rotating motor, and a turntable. The rotating base is fixedly connected to the support base and is located on one side of the support base. The rotating motor is fixedly connected to the rotating base and is located on one side of the rotating base. The turntable is fixedly connected to the output end of the rotating motor and to the functional module box, and is located on one side of the rotating motor.

5. The UAV air traffic control monitoring device as described in claim 4, characterized in that, The load-bearing component also includes a scale, which is fixedly connected to the lifting rod and located on one side of the lifting rod.

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