CN217994780U

CN217994780U - Airport airspace management and control device

Info

Publication number: CN217994780U
Application number: CN202221792130.XU
Authority: CN
Inventors: 盛匀
Original assignee: Civil Aviation Flight University of China
Current assignee: Civil Aviation Flight University of China
Priority date: 2022-07-12
Filing date: 2022-07-12
Publication date: 2022-12-09
Anticipated expiration: 2032-07-12

Abstract

The utility model discloses an airport airspace management and control device, which comprises a management and control patrol aircraft and a camera arranged on the management and control patrol aircraft; the bottom of aircraft is patrolled in management and control can be dismantled and be connected with the mounting panel, install on the mounting panel and be used for adjusting the rotation regulation subassembly of camera direction, rotation regulation subassembly's bottom has set firmly the connecting plate, the bottom of connecting plate is connected with the fixed plate through the telescopic link, camera demountable installation be in on the fixed plate, the connecting plate with still be equipped with the camera between the fixed plate and hide the rain subassembly. The utility model discloses an airport airspace management and control device, when the management and control patrol aircraft stops aloft, can carry out arbitrary regulation to the angle of camera, realize omnidirectional shooting, when meetting rainy day, can hide rain protection to the camera, avoid damaging the camera, reduced the cost of changing the camera.

Description

Airport airspace management and control device

Technical Field

The utility model relates to an airport airspace technical field especially relates to an airport airspace management and control device.

Background

At present, unmanned aerial vehicles are increasingly popular, the flight of the unmanned aerial vehicles is controlled by drivers of the unmanned aerial vehicles, but the control of the drivers at present is random and nonstandard, and some abnormal or black flying unmanned aerial vehicle flight activities appear near airport clearance airspace recently, so that a large number of airport flights are delayed in taking off and landing or are prepared for landing other airports, the safe flight of the airport flights is seriously influenced, and the hazard is very large. The problem to be solved urgently is to control the airspace of the airport and avoid the influence of abnormal or black flying unmanned aerial vehicles on the safe flight.

The utility model discloses a be CN 208828107U's utility model discloses a many unmanned aerial vehicle airport airspace management and control device, including management and control patrol aircraft and install the machine-carried data box on unmanned aerial vehicle, management and control patrol aircraft includes four-wing aircraft shell, four evenly distributed's of fixedly connected with main flight wing on the four-wing aircraft shell, fixedly connected with and main flight wing assorted bearer bar on the four-wing aircraft shell, a plurality of descending supports of lower extreme fixedly connected with of four-wing aircraft shell, the lower extreme fixedly connected with shock pad of descending support, the downside of four-wing aircraft shell is equipped with high definition digtal camera, can realize carrying out reasonable management and control to many unmanned aerial vehicle airports, the accessible installs machine-carried data box additional and realizes, the commonality is high, easily promote many unmanned aerial vehicle airports's safety and stability, and simultaneously, easily improve emergency's processing speed. However, the direction of the camera of the airport airspace management and control device is not adjustable, and when images in different directions need to be shot, the images can only be shot by controlling and controlling the flight of a patrol aircraft, so that the airport airspace management and control device is difficult to accurately control; in addition, when the bad weather such as rain appears, because the camera does not have corresponding safeguard procedures, also can cause the damage of camera, influence follow-up shooting effect, it is higher to change the camera cost.

Disclosure of Invention

To the problem that exists, the utility model aims at providing an airport airspace management and control device, when the management and control patrol aircraft stops aloft, can carry out arbitrary regulation to the angle of camera, realize omnidirectional shooting, when meetting rainy day, can hide rain protection to the camera, avoid damaging the camera.

In order to achieve the above object, the utility model adopts the following technical scheme:

an airport airspace management and control device comprises a management and control patrol aircraft and a camera installed on the management and control patrol aircraft; the method is characterized in that: the bottom of management and control patrol aircraft can be dismantled and be connected with the mounting panel, install on the mounting panel and be used for adjusting the rotation regulation subassembly of camera direction, rotation regulation subassembly's bottom has set firmly the connecting plate, the bottom of connecting plate is connected with the fixed plate through the telescopic link, camera demountable installation is in on the fixed plate, the connecting plate with still be equipped with the camera between the fixed plate and hide the rain subassembly.

Furthermore, the rotary adjusting assembly comprises a vertical adjusting assembly and a horizontal adjusting assembly, the vertical adjusting assembly comprises a first driving motor installed on the installation plate, the output end of the first driving motor is connected with a first rotating shaft, the first rotating shaft extends along the vertical direction, a U-shaped frame is fixedly arranged at the bottom of the installation plate, and the first rotating shaft penetrates through the bottom of the U-shaped frame in a rotating manner; the horizontal adjusting component is connected with the bottom end of the first rotating shaft.

Furthermore, a rotating groove is formed in the bottom end of the first rotating shaft, the rotating groove penetrates through the front side face and the rear side face of the first rotating shaft, the horizontal adjusting assembly comprises a second rotating shaft which is rotatably connected in the rotating groove, the second rotating shaft extends along the horizontal direction, one end of the second rotating shaft rotatably penetrates through the first rotating shaft, the bottom of the U-shaped frame is rotatably connected with an L-shaped plate, a second driving motor is mounted on the L-shaped plate, and one end of the second rotating shaft, which penetrates through the first rotating shaft, is connected with the output end of the second driving motor; and the bottom of the second rotating shaft in the rotating groove is fixedly provided with a connecting rod, and the connecting plate is fixedly arranged at the bottom of the connecting rod.

Further, the camera hides rain subassembly includes swing joint and is in a plurality of movable rods of connecting plate periphery, it is a plurality of the movable rod symmetry sets up, the periphery activity of fixed plate be equipped with a plurality of with the bracing piece that the movable rod corresponds each other, swing joint between bracing piece and the movable rod that corresponds each other is a plurality of it hides the rain cloth to have set firmly between the top of movable rod.

Furthermore, every the movable rod is close to the sliding tray has all been seted up to a side of telescopic link, slide in the sliding tray be equipped with sliding tray matched with sliding block, sliding block and mutual correspondence the bracing piece tip swing joint.

Furthermore, the control patrol aircraft comprises a fuselage, a control antenna, support legs, supports and rotors, wherein the control antenna is positioned at the top of the fuselage, the plurality of supports are symmetrically arranged on the periphery of the fuselage, and the rotors are arranged at the end parts of the supports; the support legs are fixedly arranged at the bottom of the machine body.

The utility model has the advantages that: compared with the prior art, the utility model has the improvement that,

1. the utility model discloses a camera is installed in the bottom of management and control patrol aircraft to airport airspace management and control device, can rotate camera horizontal direction and vertical direction through the rotation regulation subassembly and adjust, thereby make management and control patrol aircraft stop when aerial, can adjust wantonly to the angle of camera, realize the shooting of airport airspace interior omnidirectional, the result of shooing through the camera carries out reasonable management and control, when the service function, management and control patrol aircraft can carry out corresponding shooting operation outside airport headroom district, can not influence taking off and descending of normal flight.

2. The utility model discloses an airport airspace management and control device is provided with camera rain-shading component at the top of camera, and in rainy day, the position of camera is promoted upwards to the accessible length that shortens the telescopic link, when telescopic link length shortens, also can drive the bracing piece and strut the movable rod, and the cloth that hides at movable rod top forms umbrella shape, can play the effect of keeping out the rain to the camera, avoids the rainwater to damage the camera, has reduced the cost of changing the camera; under the condition that does not have rain, movable rod, bracing piece and rain-proof cloth are the contraction status, and the camera is located the camera and hides the below of rain subassembly, can not influence the shooting of camera.

Drawings

Fig. 1 is the utility model discloses airport airspace management and control device structural schematic.

Fig. 2 is the utility model discloses connection structure schematic diagram between camera and the management and control patrol aircraft.

Fig. 3 is a partial enlarged view of a portion a of fig. 2 according to the present invention.

Fig. 4 is the utility model discloses the camera hides rain subassembly open mode structure schematic diagram.

Wherein: 1-control patrol aircraft, 101-fuselage, 102-control antenna, 103-support foot, 104-bracket, 105-rotor, 2-camera, 3-mounting plate, 4-connecting plate, 5-telescopic rod, 6-fixing plate, 7-first driving motor, 8-first rotating shaft, 9-U-shaped frame, 10-rotating groove, 11-second rotating shaft, 12-L-shaped plate, 13-second driving motor, 14-connecting rod, 15-movable rod, 16-supporting rod, 17-sliding groove and 18-sliding block.

Detailed Description

In order to make those skilled in the art better understand the technical solution of the present invention, the following describes the technical solution of the present invention with reference to the accompanying drawings and embodiments.

Example (b):

referring to fig. 1-4, an airport airspace management and control device includes a management and control patrol aircraft 1 and a camera 2 installed on the management and control patrol aircraft 1; the bottom of aircraft 1 is patrolled in management and control can be dismantled through the bolt and be connected with mounting panel 3, install on the mounting panel 3 and be used for adjusting the rotation regulation subassembly of 2 directions of camera, rotation regulation subassembly's bottom has set firmly connecting plate 4, the bottom of connecting plate 4 is connected with fixed plate 6 through

telescopic link

5, 2 demountable installation of camera are in on the fixed plate 6, connecting plate 4 with it hides the rain subassembly still to be equipped with the camera between the fixed plate 6.

Specifically, management and control patrol aircraft 1 includes fuselage 101, control antenna 102, stabilizer blade 103, support 104 and rotor 105, control antenna 102 is located fuselage 101's top, fuselage 101's periphery symmetry is equipped with a plurality of supports 104, every the tip of support 104 all is equipped with rotor 105, and a power device is constituteed with the rotor 105 that corresponds to every support 104, and four are no less than to power device's quantity, stabilizer blade 103 fixed mounting be in fuselage 101's bottom, landing leg 103 adopts the trapezium structure, just landing leg 103's bottom fixed mounting has the gasket for unmanned aerial vehicle places more stably, and landing leg 103 is difficult for wearing and tearing.

The rotary adjusting assembly comprises a vertical adjusting assembly and a horizontal adjusting assembly, the vertical adjusting assembly comprises a first driving motor 7 installed on the installation plate 3, the output end of the first driving motor 7 is connected with a first rotating shaft 8, the first rotating shaft 8 extends along the vertical direction, a U-shaped frame 9 is fixedly arranged at the bottom of the installation plate 3, the top of the U-shaped frame 9 is of an open structure, and the first rotating shaft 8 penetrates through the bottom of the U-shaped frame 9 through a bearing in a rotating mode; the horizontal adjusting component is connected with the bottom end of the first rotating shaft 8. When the first driving motor 7 works, the first rotating shaft 8 and the whole horizontal adjusting assembly are driven to rotate in the vertical direction.

A rotating groove 10 is formed in the bottom end of the first rotating shaft 8, the rotating groove 10 penetrates through the front side face and the rear side face of the first rotating shaft 8, the horizontal adjusting assembly comprises a second rotating shaft 11 which is rotatably connected in the rotating groove 10, the second rotating shaft 11 extends in the horizontal direction, one end of the second rotating shaft 11 rotatably penetrates through the first rotating shaft 8 through a bearing, the other end of the second rotating shaft 11 is rotatably connected with the side wall of the rotating groove 10 through a bearing, the bottom of the U-shaped frame 9 is rotatably connected with an L-shaped plate 12, a second driving motor 13 is installed on the L-shaped plate 12, and one end, penetrating through the first rotating shaft 8, of the second rotating shaft 11 is connected with the output end of the second driving motor 13; and a connecting rod 14 is fixedly arranged at the bottom of the second rotating shaft 11 positioned in the rotating groove 10, and the connecting plate 4 is fixedly arranged at the bottom of the connecting rod 14. The L-shaped plate 12 is rotatably connected with the bottom surface of the U-shaped frame 9, so that the whole horizontal adjusting assembly can synchronously rotate along with the first rotating shaft 8 when the first driving motor 7 works, the second rotating shaft 11 is driven to rotate in the horizontal direction when the second driving motor 13 works, the connecting rod 14 and the connecting plate 4 connected with the connecting rod 14 are further driven to rotate in the horizontal direction, and the telescopic rod 5, the fixed plate 6 and the camera 2 can be further driven to rotate in the horizontal direction by the rotation of the connecting plate 4; that is when management and control patrol aircraft 1 stops in aerial certain position, can drive camera 2 through starting first driving motor 7 and take place to rotate in the vertical direction, drive camera 2 through starting second driving motor 13 and take place to rotate in the horizontal direction to realize the omnidirectional shooting of camera 2 multi-angle.

The utility model discloses a theory of operation: the utility model discloses when using, use the bolt earlier to install camera 2 on fixed plate 6, adjusted camera 2's height through telescopic link 5, telescopic link 5 adopts electric telescopic handle, can carry out long-range expansion control. Start management and control patrol aircraft 1, make its peripheral department that moves the peripheral airspace control in airport stop in the air, start first driving motor 7, it takes place to rotate at the vertical direction to drive camera 2, it takes place to rotate at the horizontal direction to start second driving motor 13 to drive camera 2, thereby realize 2 multi-angle omnidirectional shootings of camera, the result accessible wireless transmission that camera 2 was shot is to ground management and control tower and operation remote control center, be convenient for in time handle economic conditions, detect the management and control to the peripheral environment in airport. The camera hides rain subassembly can hide rain to camera 2 when rainy day, avoids the camera to drench the damage by the rainwater. In this embodiment, the camera hides rain subassembly adopts the current structure that can play the effect of hiding rain can.

Example two:

on the basis of embodiment one, the camera hides the rain subassembly and connects including articulated a plurality of movable rod 15 in 4 peripheries of connecting plate, the quantity of movable rod 15 is 4 at least, and is a plurality of the 15 symmetry of movable rod set up, the periphery of fixed plate 6 articulated be connected with a plurality ofly with the bracing piece 16 that the movable rod 15 corresponds each other, swing joint between bracing piece 16 and the movable rod 15 that corresponds each other is a plurality of set firmly the cloth of keeping out the rain (not shown in the figure) between the top of movable rod 15. Every the movable rod 15 is close to sliding tray 17 has all been seted up to one side of telescopic link 5, slide tray 17 in slide tray 17 slide be equipped with sliding tray 17 assorted sliding block 18, sliding block 18 with mutual correspondence 16 end swing joint of bracing piece.

The camera in this embodiment hides rain subassembly when using, shorten through control telescopic link 5, can promote the height of fixed plate 6, when 6 high lifts of fixed plate, drive 16 rebound of bracing piece and rotate round the articulated shaft, the movable rod 15 who will correspond struts, the cloth that hides the rain at movable rod 15 top is in the expansion state, at this moment, 2 rebound of camera to the inside that the camera sheltered the rain subassembly, as shown in figure 4, can avoid camera 2 to be drenched the damage by the rainwater, when not using, movable rod 15 is in the shrink state, camera 2 is located the camera and hides the below of rain subassembly, can not influence the shooting of camera 2.

The foregoing shows and describes the general principles, essential features, and advantages of the invention. It should be understood by those skilled in the art that the present invention is not limited to the above embodiments, and the above embodiments and descriptions are only illustrative of the principles of the present invention, and that various changes and modifications may be made without departing from the spirit and scope of the present invention, and all such changes and modifications fall within the scope of the present invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. An airport airspace management and control device comprises a management and control patrol aircraft (1) and a camera (2) installed on the management and control patrol aircraft (1); the method is characterized in that: the bottom of management and control patrol aircraft (1) can be dismantled and be connected with mounting panel (3), install on mounting panel (3) and be used for adjusting the rotation regulation subassembly of camera (2) direction, rotation regulation subassembly's bottom has set firmly connecting plate (4), the bottom of connecting plate (4) is connected with fixed plate (6) through telescopic link (5), camera (2) demountable installation be in on fixed plate (6), connecting plate (4) with it hides the rain subassembly still to be equipped with the camera between fixed plate (6).

2. The airport airspace management and control device of claim 1, wherein: the rotary adjusting assembly comprises a vertical adjusting assembly and a horizontal adjusting assembly, the vertical adjusting assembly comprises a first driving motor (7) installed on the installation plate (3), the output end of the first driving motor (7) is connected with a first rotating shaft (8), the first rotating shaft (8) extends along the vertical direction, a U-shaped frame (9) is fixedly arranged at the bottom of the installation plate (3), and the first rotating shaft (8) penetrates through the bottom of the U-shaped frame (9) in a rotating mode; the horizontal adjusting component is connected with the bottom end of the first rotating shaft (8).

3. The airport airspace management and control device according to claim 2, wherein: a rotating groove (10) is formed in the bottom end of the first rotating shaft (8), the rotating groove (10) penetrates through the front side face and the rear side face of the first rotating shaft (8), the horizontal adjusting assembly comprises a second rotating shaft (11) which is rotatably connected into the rotating groove (10), the second rotating shaft (11) extends in the horizontal direction, one end of the second rotating shaft (11) rotatably penetrates through the first rotating shaft (8), the bottom of the U-shaped frame (9) is rotatably connected with an L-shaped plate (12), a second driving motor (13) is mounted on the L-shaped plate (12), and one end, penetrating through the first rotating shaft (8), of the second rotating shaft (11) is connected with the output end of the second driving motor (13); and a connecting rod (14) is fixedly arranged at the bottom of the second rotating shaft (11) positioned in the rotating groove (10), and the connecting plate (4) is fixedly arranged at the bottom of the connecting rod (14).

4. The airport airspace management and control device of claim 1, wherein: the camera hides rain subassembly includes swing joint and is in a plurality of movable rod (15) of connecting plate (4) periphery, and is a plurality of movable rod (15) symmetry sets up, the periphery activity of fixed plate (6) be equipped with a plurality of with bracing piece (16) that movable rod (15) correspond each other, swing joint between bracing piece (16) and the movable rod (15) that correspond each other is a plurality of it hides the rain cloth to have set firmly between the top of movable rod (15).

5. The airport airspace management and control device of claim 4, wherein: every movable rod (15) are close to sliding tray (17) have all been seted up to a side of telescopic link (5), slide in sliding tray (17) be equipped with sliding tray (17) assorted sliding block (18), sliding block (18) and mutual correspondence bracing piece (16) tip swing joint.

6. The airport airspace management and control device of claim 1, wherein: the management and control patrol aircraft (1) comprises an aircraft body (101), a control antenna (102), support legs (103), brackets (104) and rotors (105), wherein the control antenna (102) is positioned at the top of the aircraft body (101), the plurality of brackets (104) are symmetrically arranged on the periphery of the aircraft body (101), and the end part of each bracket (104) is provided with a rotor (105); the supporting feet (103) are fixedly arranged at the bottom of the machine body (101).