A military airfield landing LED lighting system

Abstract

The utility model discloses a kind of military airport landing LED lighting systems, including luminaire module frame, the rotatable connection of connecting hinge is rotated in the upper end of luminaire module frame front and back side, and the other side fixedly connected with cover plate of connecting hinge, electrically connected between LED lamp, PLC controller, electric box, first servo motor, second servo motor.The kind of military airport landing LED lighting system can be stabilized by supporting base and support frame Support, and can be quickly moved and fixed by universal wheel Use, and can be carried out matrix illumination by LED lamp, can realize LED light intensity high, irradiation distance is far, and can be carried out up and down and left and right overturn and lifting adjustment by electric push rod, second servo motor, coupling mechanism, first servo motor, drive gear, transmission gear drive LED lamp, better adaptability, and can be independently disassembled by splicing block, splicing slot Conveniently LED lamp, and can be carried out light-transmitting cover combination by cover plate, and protection effect is good.

Description

Technical Field

[0001] This utility model relates to the technical field of waterproof landing lighting manholes for military airports and LED lighting fixtures for military airport landings, specifically a military airport landing LED lighting system. Background Technology

[0002] In practical applications, vehicle-mounted landing searchlights are installed on both sides of the landing area at military airports. When aircraft need landing lighting at night or in foggy weather, the military landing searchlight vehicles are driven to both sides of the runway to provide illumination, and then driven back to the hangar after use.

[0003] Existing searchlights are mostly gas discharge lamps, which have high power consumption and large size and weight. Vehicle-mounted landing searchlights are installed on vehicles, and the stability of the vehicle is not high after adding a lifting function. The size and height are also large, and the landing searchlight vehicle needs to be manually driven to a fixed position on both sides of the airport runway, which is not very automated. The searchlights used in the past were mostly floodlights or spotlights, which cannot be integrated into one. Furthermore, the electronic components are prone to failure, the equipment life is short, and the disassembly, replacement and protection are not good. Therefore, a military airport landing LED lighting system is needed to solve the above problems. Utility Model Content

[0004] The purpose of this utility model is to provide a military airport landing LED lighting system to solve the problems mentioned in the background art, which are mostly gas discharge lamps with high power and high power consumption, large lamp volume and heavy weight. The vehicle-mounted landing searchlight is installed on the vehicle, and the vehicle's stability is not high after adding the lifting function. The size and height are also large. The landing searchlight vehicle needs to be manually driven to a fixed position on both sides of the airport runway, and the automation performance is not high. The searchlights used in the past are mostly floodlights or spotlights, which cannot be integrated with the two. In addition, the electronic components are prone to failure, the equipment life is short, and the disassembly, replacement and protection effects are not good.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a military airport landing LED lighting system, comprising a lamp module frame, LED lights installed on the inner wall of the lamp module frame, and a pitch transmission box fixedly connected to one side of the lamp module frame. A coupling mechanism is rotatably connected to the inner wall of the lamp module frame, and a splicing slot is provided on the inner side of the coupling mechanism. A splicing block is inserted into the inner wall of the splicing slot, and the splicing block is fixedly connected to both sides of the LED lights. A second servo motor is fixedly connected to the inner wall of the pitch transmission box, and the output end of the second servo motor is fixedly connected to one end of the coupling mechanism. A support frame is slidably fitted onto the outer side of the lamp module frame, and a support bracket is fixedly connected to the rear edge of the support frame. The lower middle part of the support frame... A transmission gear is vertically fixedly connected, and a drive gear is meshed with the side of the transmission gear. A first servo motor is fixedly connected to one end of the drive gear, and a support base is sleeved on the outside of the first servo motor. A PLC controller is electrically connected to the front edge of the support base, and casters are fixedly connected to the lower corner of the support base and the lower end of the support frame. An electric push rod is inserted into the inner wall of the support frame, and the output end of the electric push rod is fixedly connected to both sides of the upper rear side of the lamp module frame. A connecting hinge is rotatably connected to the upper front and rear sides of the lamp module frame, and a cover plate is fixedly connected to the other side of the connecting hinge. An electrical box is electrically connected to one side of the support base. The LED lamp, PLC controller, electrical box, first servo motor, and second servo motor are electrically connected to each other.

[0006] Preferably, the lighting module frame is electrically lifted and lowered to the support frame via an electric push rod.

[0007] Preferably, the lamp module frame, LED lamp, and support frame are connected to the support base in a left-right meshing rotatable manner via drive gears and transmission gears.

[0008] Preferably, the LED light is connected to the lamp module frame via a coupling mechanism on the second servo motor in an up-down flip-up configuration.

[0009] Preferably, the LED lights are connected to the coupling mechanism in a limited-positioning splicing connection through splicing blocks in the splicing slot, and the LED lights are distributed in a matrix position on the inner wall of the lighting module frame. The cover plate is a transparent polycarbonate sheet, and the cover plate is connected to the lighting module frame in a flip-opening and closing connection through connecting hinges.

[0010] Preferably, the support frame is connected to the support base in a trapezoidal support structure via a support frame, and the casters are distributed in a matrix position on the support frame and the support base. The casters are self-locking structures, and the electrical box is an integrated exhaust and air inlet structure.

[0011] Compared with the prior art, the beneficial effects of this utility model are as follows: This military airport landing LED lighting system can be stably supported by a support base and support frame, and can be quickly moved and fixed for use by casters. Moreover, it can provide matrix lighting with LED lights, achieving high LED light intensity and long illumination distance. Furthermore, the LED lights can be rotated up, down, left, and right and adjusted in height and direction by an electric push rod, a second servo motor, a coupling mechanism, a first servo motor, a drive gear, and a transmission gear, resulting in better adaptability. In addition, the LED lights can be easily disassembled and assembled independently by splicing blocks and splicing slots, and can be covered by a cover plate for light transmission and excellent protection. Attached Figure Description

[0012] Figure 1 This is a front view of a military airport landing LED lighting system according to the present invention; Figure 2 This is a schematic diagram of the internal structure of a military airport landing LED lighting system according to the present invention; Figure 3 This is a side view of the internal structure of a military airport landing LED lighting system according to the present invention; Figure 4 This utility model relates to a military airport landing LED lighting system. Figure 2 Enlarged view of point A in the middle; Figure 5 This utility model relates to a military airport landing LED lighting system. Figure 2 Enlarged view at point B in the middle; Figure 6 This utility model relates to a military airport landing LED lighting system. Figure 3 Enlarged view of point C.

[0013] In the diagram: 1. Lighting module frame, 2. LED light, 3. Support frame, 4. Support base, 5. PLC controller, 6. Electrical box, 7. Pitch transmission box, 8. Casters, 9. First servo motor, 10. Second servo motor, 11. Support frame, 12. Electric push rod, 13. Coupling mechanism, 14. Splicing block, 15. Splicing slot, 16. Drive gear, 17. Transmission gear, 18. Cover plate, 19. Connecting hinge. Detailed Implementation

[0014] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0015] Please see Figure 1-6This utility model provides a technical solution: a military airport landing LED lighting system, including a lamp module frame 1, LED lights 2, a support frame 3, a support base 4, a PLC controller 5, an electrical box 6, a pitch transmission box 7, casters 8, a first servo motor 9, a second servo motor 10, a support frame 11, an electric push rod 12, a coupling mechanism 13, a splicing block 14, a splicing slot 15, a drive gear 16, a transmission gear 17, a cover plate 18, and a connecting hinge 19. LED lights 2 are installed on the inner wall of the lamp module frame 1, and the pitch transmission box 7 is fixedly connected to one side of the lamp module frame 1. The lamp module frame 1 is electrically connected to the support frame 3 via the electric push rod 12, allowing the lamp module frame 1 to be adjusted for height adaptation. The lighting module frame 1, LED lamp 2, and support frame 3 are connected to the support base 4 via drive gear 16 and transmission gear 17 in a left-right meshing rotatable manner. This allows the lighting module frame 1, LED lamp 2, and support frame 3 to be adjusted left and right rotationally, providing excellent adaptability. The LED lamp 2 is connected to the lighting module frame 1 via a coupling mechanism 13 on a second servo motor 10 in a vertical flipping manner. This allows the LED lamp 2 to independently flip up and down, ensuring stable and reliable rotational operation. The LED lamp 2 is connected to the coupling mechanism 13 via splicing blocks 14 in splicing slots 15 in a limited insertion splicing manner. The LED lamps 2 are distributed in a matrix position on the inner wall of the lighting module frame 1. The cover plate 18 is made of transparent polycarbonate sheet and is connected to the lighting fixture via connecting hinges 19. The module frame 1 has a flip-open / closed connection, which facilitates matrix installation of the LED lights 2 and allows for independent insertion and disassembly. It also allows light transmission and protection through the cover plate 18, resulting in excellent performance. A coupling mechanism 13 is rotatably connected to the inner wall of the module frame 1, and a splicing slot 15 is provided on the inner side of the coupling mechanism 13. A splicing block 14 is inserted into the inner wall of the splicing slot 15 and is fixedly connected to both sides of the LED lights 2. A second servo motor 10 is fixedly connected to the inner wall of the pitch transmission box 7, and the output end of the second servo motor 10 is fixedly connected to one end of the coupling mechanism 13. A support frame 3 is slidably fitted onto the outer side of the module frame 1, and a support bracket 11 is fixedly connected to the rear edge of the support frame 3. The support frame 3 is connected to the support base via the support bracket 11. The base 4 is connected in a trapezoidal shape, and the casters 8 are distributed in a matrix position on the support frame 11 and the support base 4. The casters 8 have a self-locking structure. The electrical box 6 has an integrated exhaust and air inlet structure. This allows the support frame 3 to be stably supported by the support frame 11 and to be stably moved and fixed by the casters 8, making it more stable to use. A transmission gear 17 is vertically fixedly connected to the middle of the lower end of the support frame 3, and a drive gear 16 is meshed with the side of the transmission gear 17. A first servo motor 9 is fixedly connected to one end of the drive gear 16, and the support base 4 is sleeved on the outside of the first servo motor 9. A PLC controller 5 is electrically connected to the front edge of the support base 4, and casters 8 are fixedly connected to the lower corner of the support base 4 and the lower end of the support frame 11.An electric push rod 12 is inserted and connected to the inner wall of the support frame 11, and the output end of the electric push rod 12 is fixedly connected to both sides of the upper rear end of the lamp module frame 1. A connecting hinge 19 is rotatably connected to the upper front and rear sides of the lamp module frame 1, and a cover plate 18 is fixedly connected to the other side of the connecting hinge 19. An electrical box 6 is electrically connected to one side of the support base 4. The LED light 2, PLC controller 5, electrical box 6, first servo motor 9, and second servo motor 10 are electrically connected.

[0016] Working principle: When using this military airport landing LED lighting system, the device is first assembled and installed, then electrically connected to the electrical box 6, and then controlled by the PLC controller 5. When structural adjustment is required, the entire unit can be raised and lowered using the electric push rod 12. Then, the entire unit is rotated left and right using the first servo motor 9, drive gear 16, and transmission gear 17. Then, the second servo motor 10 and coupling mechanism 13 drive a row of LED lights 2 to independently flip up and down for more flexible adjustment. When temporary movement adjustment is required, the universal wheels 8 can be used for pushing and pulling, and then the universal wheels 8 are self-locking and fixed, and supported by the support frame 11. When the LED lights 2 need to be replaced or repaired, the cover plate 18 can be flipped open, and then the splicing blocks 14 and splicing slots 15 can be used for independent disassembly and replacement. This is the usage process of this military airport landing LED lighting system.

[0017] It should be noted that this utility model is a military airport landing LED lighting system. All components are standard parts or components known to those skilled in the art. Their structure and principle can be learned by those skilled in the art through technical manuals or conventional experimental methods. Furthermore, all electrical components mentioned above refer to power elements, electrical components, and the matching monitoring computer and power supply connected by wires. The specific connection method should refer to the working principle described above, and the electrical connection between each electrical component should be completed in the order of operation. The detailed connection method is a well-known technology in the field.

[0018] In the description of this utility model, it should also be noted that, unless otherwise explicitly specified and limited, the terms "set up," "install," "connect," and "link" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or a connection through an intermediate medium; and they can refer to the internal communication between two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model according to the specific circumstances.

[0019] Although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present invention should be included within the protection scope of the present invention.

Claims

1. A military airport landing LED lighting system, comprising a lamp module frame (1), wherein LED lamps (2) are installed on the inner wall of the lamp module frame (1), and a pitch transmission box (7) is fixedly connected to one side of the lamp module frame (1), characterized in that: The inner wall of the lamp module frame (1) is rotatably connected to a coupling mechanism (13), and a splicing slot (15) is provided on the inner side of the coupling mechanism (13). A splicing block (14) is inserted into the inner wall of the splicing slot (15), and the splicing block (14) is fixedly connected to both sides of the LED lamp (2). A second servo motor (10) is fixedly connected to the inner wall of the pitch transmission box (7), and the output end of the second servo motor (10) is fixedly connected to one end of the coupling mechanism (13). A support frame (3) is slidably fitted onto the outer side of the lamp module frame (1), and a support frame (11) is fixedly connected to the rear edge of the support frame (3). A transmission gear (17) is vertically fixedly connected to the middle position of the lower end of the support frame (3), and a drive gear (16) is meshed with the side of the transmission gear (17). One end of the drive gear (16) is fixedly connected to a... The first servo motor (9) is fitted with a support base (4) on its outer side. The front edge of the support base (4) is electrically connected to a PLC controller (5). The lower corner of the support base (4) and the lower end of the support frame (11) are fixedly connected to casters (8). The inner wall of the support frame (11) is fitted with an electric push rod (12). The output end of the electric push rod (12) is fixedly connected to the upper rear side of the lamp module frame (1). The upper front and rear sides of the lamp module frame (1) are rotatably connected to a connecting hinge (19). The other side of the connecting hinge (19) is fixedly connected to a cover plate (18). The support base (4) is electrically connected to an electrical box (6). The LED lamp (2), PLC controller (5), electrical box (6), first servo motor (9), and second servo motor (10) are electrically connected to each other.

2. The military airport landing LED lighting system according to claim 1, characterized in that: The lighting module frame (1) is electrically lifted and lowered to the support frame (3) via an electric push rod (12).

3. The military airport landing LED lighting system according to claim 2, characterized in that: The lamp module frame (1), LED lamp (2), and support frame (3) are connected to the support base (4) in a left-right meshing and rotating manner through the drive gear (16) and transmission gear (17).

4. A military airport landing LED lighting system according to claim 3, characterized in that: The LED lamp (2) is connected to the lamp module frame (1) via a coupling mechanism (13) on the second servo motor (10) in an up-down flipping manner.

5. A military airport landing LED lighting system according to claim 4, characterized in that: The LED lamp (2) is connected to the coupling mechanism (13) in a limited insertion splicing connection through the splicing block (14) in the splicing slot (15), and the LED lamp (2) is distributed in a matrix position on the inner wall of the lamp module frame (1). The cover plate (18) is a transparent polycarbonate sheet, and the cover plate (18) is connected to the lamp module frame (1) in a flip-opening and closing connection through the connecting hinge (19).

6. A military airport landing LED lighting system according to claim 5, characterized in that: The support frame (3) is connected to the support base (4) in a trapezoidal support structure through the support frame (11), and the casters (8) are distributed in a matrix position on the support frame (11) and the support base (4). The casters (8) are self-locking structures, and the electrical box (6) is an integrated exhaust and air inlet structure.

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