Automatic main and standby synchronous monitoring equipment for air traffic control

Abstract

The utility model discloses an air traffic control automation main and standby synchronous monitoring device, which relates to the technical field of air traffic control monitoring server cabinets and comprises an air traffic control monitoring server cabinet and an air traffic control automation main and standby synchronous monitoring server, and a partition plate is fixedly connected inside the air traffic control monitoring server cabinet. According to the blank pipe automatic main and standby synchronous monitoring equipment, a motor drives a worm to rotate, the worm drives two elastic springs to rotate, a worm gear drives a screw to rotate, then a sliding block is driven to move towards the back face of a blank pipe monitoring server cabinet, a vertical rod is driven to move in the moving process, and meanwhile a rotating shaft rotates under the action of the elastic springs; the air filter screen is wound, all the spaces on the two sides of the air pipe monitoring server cabinet are exposed, air passes through the grid plate and the air filter screen to make contact with the air pipe automatic main and standby synchronous monitoring server, and compared with a traditional heat dissipation hole forming mode, the heat dissipation effect is good, the air contact face is large, and heat volatilization is fast.

Description

Technical Field

[0001] The utility model relates to the technical field of air traffic control monitoring server cabinets, in particular to an air traffic control automated main-standby synchronous monitoring device. Background Art

[0002] With the rapid development of civil aviation, the air traffic of civil aviation airports has been continuously increasing, which has put forward higher requirements for the stability and robustness of air traffic control automation systems. The main and standby synchronization of air traffic control automation systems is to realize the two-way real-time data interaction between the main and standby systems of air traffic control automation, including synchronization of system basic data information, flight plan information and track information, so that the target track flight situation and flight plan information of the standby system and the main system are consistent. Real-time data exchange is a key technology and an important foundation for realizing seamless switching and equivalent interoperability between the main and standby automation systems.

[0003] As the core equipment for the civil aviation traffic control department to implement air command, the air traffic control automation main and standby synchronization monitoring equipment provides the controller with the display of air flight situation and various flight conflicts and various abnormal alarms by processing radar signals and other monitoring data. By processing flight plans and dynamic telegrams, it provides the controller with flight plans and flight dynamics related information and management methods. It contains: automation system, main and standby automation system synchronization, which plays an important role in ensuring the safe implementation of civil aviation traffic control air command tasks. The air traffic control automation main and standby synchronization monitoring equipment is mainly realized by the air traffic control automation main and standby synchronization monitoring server. The air traffic control automation main and standby synchronization monitoring server is combined with the cabinet, and cooperates with the computer Computers are used to realize automatic master-standby synchronous monitoring of air traffic control. However, when the current automatic master-standby synchronous monitoring server cabinet for air traffic control is in use, the heat generated inside is high due to the large amount of operation. The heat dissipation holes opened on the existing server cabinet cannot effectively dissipate the internal heat, which will still cause the temperature inside the cabinet to be high. In the long run, the electronic components inside the cabinet will still be damaged and burned due to the high temperature. The long-term high temperature inside the cabinet will also affect the service life of the internal electronic components. Secondly, the traditional server cabinet is discharged from the back of the cabinet when arranging the cables, which is relatively messy and inconvenient to use. Therefore, we propose an automatic master-standby synchronous monitoring device for air traffic control. Utility Model Content

[0004] In view of the deficiencies in the prior art, the utility model provides an air traffic control automated main-standby synchronous monitoring device, which solves the problems raised in the above-mentioned background technology.

[0005] To achieve the above objectives, the utility model is implemented through the following technical solutions: an air traffic control automated main-standby synchronous monitoring device, comprising an air traffic control monitoring server cabinet and an air traffic control automated main-standby synchronous monitoring server, the air traffic control monitoring server cabinet is fixedly connected with a partition plate inside, an air traffic control automated main-standby synchronous monitoring server is arranged inside the air traffic control monitoring server cabinet and above the partition plate, a line fixing mechanism is arranged on the back of the air traffic control monitoring server cabinet, grid plates are installed on both sides of the inner cavity of the air traffic control monitoring server cabinet, the grid plates are connected to the partition plate, an air filter is connected to the inner cavity of the air traffic control monitoring server cabinet and on the outer side of the grid plate, and the air traffic control monitoring server cabinet is connected with an air filter. The cabinet is rotatably connected to a rotating shaft, and an elastic spring is provided between the rotating shaft and the air pipe monitoring server cabinet, a plastic soft board is fixedly connected to the rotating shaft, one end of the plastic soft board is fixedly connected to a vertical pole, and a sliding block is fixedly connected to the top of the vertical pole, the interior of the air pipe monitoring server cabinet is rotatably connected to screws on both sides, one end of the screw is fixedly connected to a worm gear, the interior of the air pipe monitoring server cabinet is rotatably connected to a worm, and the worm is meshed with the worm gear, the screw penetrates the sliding block and is threadedly connected to the sliding block, a cable trough is provided on the back of the air pipe monitoring server cabinet, a wiring mechanism is provided in the inner cavity of the cable trough, and a liquid cooling mechanism is installed on the air pipe monitoring server cabinet.

[0006] Preferably, a motor is installed on one side of the air traffic control monitoring server cabinet, and the output shaft of the motor is fixedly connected to the worm gear.

[0007] Preferably, the wiring mechanism includes a wiring seat, a wiring cover and a rubber pad, a wiring cover is provided above the wiring seat, guide columns are fixedly connected to the lower sides of the wiring cover, both sides of the upper surface of the wiring seat are connected to limiting holes, and the guide columns are sleeved into the inner cavity of the limiting holes, the wiring cover and the inner cavity of the wiring seat are connected to the rubber pad, and one end of the wiring cover is provided with an arc corner.

[0008] Preferably, a slide groove is provided at the bottom of the inner cavity of the cable trough, and a compression pad is fixedly connected to the bottom of the inner cavity of the cable trough.

[0009] Preferably, a slider is connected to the bottom of the wiring seat, and the slider is slidably connected to the inner cavity of the slide groove.

[0010] Preferably, the liquid cooling mechanism includes a coolant tank, a semiconductor cooling fin, a water pump and a cooling copper tube. The coolant tank is installed on the top of the empty pipe monitoring server cabinet. The inner cavity of the coolant tank is provided with coolant. The inner cavity of the coolant tank is installed with a water pump. The output end of the water pump is connected to the cooling copper tube. The cooling copper tube extends to the inner cavity of the partition and is arranged in a serpentine shape. The other end of the cooling copper tube is connected to the inner cavity of the coolant tank. Semiconductor cooling fins are connected to both sides of the coolant tank.

[0011] The utility model provides an automatic main-standby synchronous monitoring device for air traffic control, which has the following beneficial effects:

[0012] 1. The automatic main and standby synchronous monitoring equipment for air traffic control is driven by a motor to rotate the worm, which drives two elastic springs to rotate, and the worm wheel drives the screw to rotate, thereby driving the sliding block to move to the back of the air traffic control monitoring server cabinet, and driving the vertical pole to move during the movement. At the same time, the shaft rotates under the action of the elastic spring, thereby reeling the air filter, exposing all the space on both sides of the air traffic control monitoring server cabinet. The air contacts the automatic main and standby synchronous monitoring server through the mesh plate and the air filter. Compared with the traditional method of opening heat dissipation holes, the heat dissipation effect is good, the air contact surface is large, the heat evaporates quickly, and the mesh plate and air The filter can protect the air traffic control automation main and standby synchronous monitoring server to prevent dust and some animals from entering the inner cavity of the air traffic control monitoring server cabinet. When the air traffic control automation main and standby synchronous monitoring server is running at high speed, the heat is greater. Start the water pump to inject the coolant in the coolant tank cavity into the cooling copper tube cavity. The coolant flows in the cooling copper tube cavity and then is discharged into the coolant tank cavity to achieve circulation. At the same time, the cooling surface of the semiconductor cooling plate is in contact with the coolant tank. When the coolant temperature rises or the coolant tank has been running for a period of time, start the semiconductor cooling plate to force cooling of the coolant in the coolant tank to ensure the cooling effect and improve the equipment operation stability.

[0013] 2. The automatic main and standby synchronous monitoring equipment for air pipes uses a wiring seat, a wiring cover and a rubber pad in coordination. The wiring seat is pulled outward to move the wiring cover out of the inner cavity of the air pipe monitoring server cabinet, and then the wiring cover is lifted upward to disengage the guide column from the inner cavity of the limiting hole. The lines that need to be discharged on the automatic main and standby synchronous monitoring server of the air pipe are passed through the cable trough and placed on the surface of the rubber pad in the inner cavity of the wiring seat. The wiring cover is then placed on the wiring seat, and the guide column is sleeved into the inner cavity of the limiting hole. The wiring cover is then pressed down to deform the rubber pad to wrap the wiring harness. The wiring seat and the wiring cover are then pushed to be sleeved into the inner cavity of the cable trough to fix the lines and arrange the lines uniformly for greater convenience. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 It is a schematic diagram of the structure of the utility model in cross section;

[0015] Figure 2 For this utility model Figure 1 The structural diagram at A in the middle;

[0016] Figure 3 It is a structural schematic diagram of the wiring mechanism of the utility model;

[0017] Figure 4It is a structural schematic diagram of the front side of the utility model;

[0018] Figure 5 It is a schematic diagram of the cross-sectional structure of the utility model when viewed from above;

[0019] Figure 6 It is a schematic structural diagram of the utility model in another cross-section view.

[0020] In the figure: 1. ATC monitoring server cabinet; 2. Cable duct; 3. Slider; 4. Slide; 5. Wiring seat; 6. Rubber cushion; 7. Extrusion cushion; 8. Coolant tank; 9. Water pump; 10. Semiconductor cooling plate; 11. Cooling copper tube; 12. Partition; 13. Grid plate; 14. Air filter; 15. Vertical pole; 16. Wiring cover; 17. Rotating shaft; 18. Elastic spring; 19. Worm; 20. Screw; 21. Sliding block; 22. ATC automation master-slave synchronous monitoring server; 23. Plastic soft board; 24. Motor; 25. Worm gear. DETAILED DESCRIPTION

[0021] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.

[0022] Example 1: Reference Figure 1-Figure 6 The utility model provides an air traffic control automated main-standby synchronous monitoring device, including an air traffic control monitoring server cabinet 1 and an air traffic control automated main-standby synchronous monitoring server 22. A partition 12 is fixedly connected inside the air traffic control monitoring server cabinet 1. An air traffic control automated main-standby synchronous monitoring server 22 is arranged inside the air traffic control monitoring server cabinet 1 and above the partition 12. A line fixing mechanism is arranged on the back of the air traffic control monitoring server cabinet 1. Grid plates 13 are installed on both sides of the inner cavity of the air traffic control monitoring server cabinet 1. The grid plates 13 are connected to the partition 12. An air filter 14 is connected to the inner cavity of the air traffic control monitoring server cabinet 1 and located on the outer side of the grid plate 13. A rotating shaft 17 is rotatably connected to the inner cavity of the air traffic control monitoring server cabinet 1. An elastic spring 18 is provided between the rotating shaft 17 and the air pipe monitoring server cabinet 1, a plastic soft board 23 is fixedly connected to the rotating shaft 17, one end of the plastic soft board 23 is fixedly connected to the vertical rod 15, and a sliding block 21 is fixedly connected to the top of the vertical rod 15. The inner sides of the air pipe monitoring server cabinet 1 are rotatably connected with screws 20, and one end of the screw 20 is fixedly connected with a worm gear 25. The inner part of the air pipe monitoring server cabinet 1 is rotatably connected with a worm 19, and the worm 19 is meshed with the worm gear 25. The screw 20 penetrates the sliding block 21 and is threadedly connected with the sliding block 21. A cable trough 2 is opened on the back of the air pipe monitoring server cabinet 1, and a wiring mechanism is provided in the inner cavity of the cable trough 2. A liquid cooling mechanism is installed on the air pipe monitoring server cabinet 1.

[0023] A motor 24 is installed on one side of the air traffic control monitoring server cabinet 1 , and the output shaft of the motor 24 is fixedly connected to the worm 19 .

[0024] The wiring mechanism includes a wiring seat 5, a wiring cover 16 and a rubber pad 6. A wiring cover 16 is provided above the wiring seat 5. Guide columns are fixedly connected to the lower sides of the wiring cover 16. Both sides of the upper surface of the wiring seat 5 are connected with limiting holes, and the guide columns are sleeved into the inner cavity of the limiting holes. The wiring cover 16 and the inner cavity of the wiring seat 5 are connected with the rubber pad 6. One end of the wiring cover 16 is provided with an arc corner.

[0025] A slide groove 4 is provided at the bottom of the inner cavity of the cable trough 2 , and a pressing pad 7 is fixedly connected to the bottom of the inner cavity of the cable trough 2 .

[0026] The bottom of the wiring seat 5 is connected with a slider 3 , and the slider 3 is slidably connected to the inner cavity of the slide groove 4 .

[0027] The liquid cooling mechanism includes a coolant tank 8, a semiconductor cooling sheet 10, a water pump 9 and a cooling copper tube 11. The coolant tank 8 is installed on the top of the air pipe monitoring server cabinet 1. The inner cavity of the coolant tank 8 is provided with coolant. The water pump 9 is installed in the inner cavity of the coolant tank 8. The output end of the water pump 9 is connected to the cooling copper tube 11. The cooling copper tube 11 extends to the inner cavity of the partition 12 and is arranged in a serpentine shape. The other end of the cooling copper tube 11 is connected to the inner cavity of the coolant tank 8. Semiconductor cooling sheets 10 are connected to both sides of the coolant tank 8.

[0028] In summary, when the air traffic control automation main and standby synchronization monitoring equipment is used, the air traffic control automation main and standby synchronization monitoring server 22 adopts the existing technology to realize the two-way real-time data interaction between the air traffic control automation main system and the standby system, including synchronization of system basic data information, flight plan information and track information, etc., so that the standby system and the main system target track flight situation and flight plan information maintain consistency, real-time data exchange and other functions,

[0029] When the air traffic control automation main and standby synchronous monitoring server 22 is running, the starting motor 24 drives the worm 19 to rotate, and the worm 19 drives the two worm wheels 25 to rotate, and the worm wheel 25 drives the screw 20 to rotate, thereby driving the sliding block 21 to move to the back of the air traffic control monitoring server cabinet 1, and driving the vertical rod 15 to move during the movement. At the same time, the rotating shaft 17 rotates under the action of the elastic spring 18, thereby reeling the air filter 14, exposing all the space on both sides of the air traffic control monitoring server cabinet 1. The air contacts the air traffic control automation main and standby synchronous monitoring server 22 through the grid plate 13 and the air filter 14. Compared with the traditional method of opening heat dissipation holes, the heat dissipation effect is good, the air contact surface is large, and the heat evaporates quickly. In addition, the grid plate 13 and the air filter 14 can protect the air traffic control automation main and standby synchronous monitoring server 22 to prevent dust and some animals from entering the inner cavity of the air traffic control monitoring server cabinet 1.

[0030] When the air traffic control automation main and standby synchronous monitoring server 22 runs at high speed, the heat is greater at this time, and the water pump 9 is started to inject the coolant in the inner cavity of the coolant tank 8 into the inner cavity of the cooling copper tube 11. The coolant flows in the inner cavity of the cooling copper tube 11 and then is discharged into the inner cavity of the coolant tank 8 to realize circulation. At the same time, the cooling surface of the semiconductor cooling plate 10 is in contact with the coolant tank 8. When the coolant temperature rises or the coolant tank 8 has been running for a period of time, the semiconductor cooling plate 10 is started to forcefully cool the coolant in the coolant tank 8 to ensure the cooling effect and improve the stability of equipment operation.

[0031] When wiring, first pull the wiring seat 5 outward to move the wiring cover 16 out of the inner cavity of the air conditioning monitoring server cabinet 1, then lift the wiring cover 16 upward to disengage the guide column from the inner cavity of the limiting hole, and then pass the lines that need to be discharged on the air conditioning automation main and standby synchronous monitoring server 22 through the cable trough 2 and place them on the surface of the rubber pad 6 in the inner cavity of the wiring seat 5, then cover the wiring cover 16 on the wiring seat 5, and at the same time, sleeve the guide column into the inner cavity of the limiting hole, and then press down the wiring cover 16 to deform the rubber pad 6 to wrap the wiring harness, and then push the wiring seat 5 and the wiring cover 16 to sleeve the wiring seat 5 and the wiring cover 16 into the inner cavity of the cable trough 2, and at the same time, the wiring cover 16 contacts the extrusion pad 7 and squeezes the extrusion pad 7 to deform, thereby limiting the wiring cover 16 to prevent the wiring cover 16 and the wiring seat 5 from moving randomly, thereby improving the stability of equipment operation.

[0032] When the air traffic control automation main and standby synchronous monitoring server 22 is not in use, the motor 24 is started to rotate in the reverse direction, thereby pulling the plastic soft board 23 to move and shield the two sides of the air traffic control monitoring server cabinet 1.

[0033] Finally, a few points should be explained: First, in the description of this application, it should be noted that, unless otherwise specified and limited, the terms "installed", "connected", and "connected" should be understood in a broad sense, which may refer to mechanical connection or electrical connection, or internal communication between two components, or direct connection. "upper", "lower", "left", "right", etc. are only used to indicate relative positional relationships. When the absolute position of the object being described changes, the relative positional relationship may change;

[0034] Secondly: In the drawings of the embodiments disclosed in the present utility model, only the structures related to the embodiments disclosed in the present utility model are involved, and other structures can refer to the general design. In the absence of conflict, the same embodiment and different embodiments of the present utility model can be combined with each other;

[0035] Finally: The above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present utility model should be included in the protection scope of the present utility model.

Claims

1. An air traffic control automation master-slave synchronous monitoring device, comprising an air traffic control monitoring server cabinet (1) and an air traffic control automation master-slave synchronous monitoring server (22), characterized in that: The air traffic control monitoring server cabinet (1) is fixedly connected to a partition (12) inside, an air traffic control automated master-slave synchronous monitoring server (22) is arranged inside and above the partition (12), a line fixing mechanism is arranged on the back of the air traffic control monitoring server cabinet (1), grid plates (13) are installed on both sides of the inner cavity of the air traffic control monitoring server cabinet (1), the grid plates (13) are connected to the partition (12), an air filter (14) is connected to the inner cavity of the air traffic control monitoring server cabinet (1) and located on the outer side of the grid plates (13), a rotating shaft (17) is rotatably connected inside the air traffic control monitoring server cabinet (1), an elastic spring (18) is arranged between the rotating shaft (17) and the air traffic control monitoring server cabinet (1), and the rotating shaft (1 7) is fixedly connected with a plastic soft board (23), one end of the plastic soft board (23) is fixedly connected with a vertical rod (15), the top of the vertical rod (15) is fixedly connected with a sliding block (21), the inner sides of the air pipe monitoring server cabinet (1) are rotatably connected with screw rods (20), one end of the screw rods (20) is fixedly connected with a worm gear (25), the inner part of the air pipe monitoring server cabinet (1) is rotatably connected with a worm gear (19), and the worm gear (19) is meshed with the worm gear (25), the screw rod (20) passes through the sliding block (21) and is threadedly connected with the sliding block (21), the back of the air pipe monitoring server cabinet (1) is provided with a cable tray (2), the inner cavity of the cable tray (2) is provided with a wiring mechanism, and a liquid cooling mechanism is installed on the air pipe monitoring server cabinet (1).

2. The automatic main-standby synchronous monitoring equipment for air traffic control according to claim 1 is characterized in that: A motor (24) is installed on one side of the air traffic control monitoring server cabinet (1), and the output shaft of the motor (24) is fixedly connected to the worm (19).

3. The automatic main-standby synchronous monitoring equipment for air traffic control according to claim 1 is characterized in that: The wiring mechanism comprises a wiring seat (5), a wiring cover (16) and a rubber cushion (6); a wiring cover (16) is provided above the wiring seat (5); guide columns are fixedly connected to the lower sides of the wiring cover (16); both sides of the upper surface of the wiring seat (5) are connected to limiting holes, and the guide columns are sleeved into the inner cavity of the limiting holes; the wiring cover (16) and the inner cavity of the wiring seat (5) are both connected to the rubber cushion (6); and one end of the wiring cover (16) is provided with an arc angle.

4. The automatic main-standby synchronous monitoring equipment for air traffic control according to claim 1 is characterized in that: A sliding groove (4) is provided at the bottom of the inner cavity of the cable tray (2), and a pressing pad (7) is fixedly connected to the bottom of the inner cavity of the cable tray (2).

5. The automatic main-standby synchronous monitoring equipment for air traffic control according to claim 3 is characterized in that: The bottom of the wiring seat (5) is connected to a slider (3), and the slider (3) is slidably connected to the inner cavity of the slide groove (4).

6. The automatic main-standby synchronous monitoring equipment for air traffic control according to claim 1 is characterized by: The liquid cooling mechanism comprises a cooling liquid tank (8), a semiconductor cooling fin (10), a water pump (9) and a cooling copper tube (11); the cooling liquid tank (8) is installed on the top of the air pipe monitoring server cabinet (1); the inner cavity of the cooling liquid tank (8) is provided with cooling liquid; the inner cavity of the cooling liquid tank (8) is installed with a water pump (9); the output end of the water pump (9) is connected to the cooling copper tube (11); the cooling copper tube (11) extends to the inner cavity of the partition (12) and is arranged in a serpentine shape; the other end of the cooling copper tube (11) is connected to the inner cavity of the cooling liquid tank (8); and both sides of the cooling liquid tank (8) are connected to semiconductor cooling fins (10).

Images