A half-moon shaped reflective tile for medium intensity aviation obstruction lights

Abstract

The utility model relates to the technical field of medium-intensity aviation obstruction light accessory devices, and in particular to a half-moon reflective tile for medium-intensity aviation obstruction lights, which is suitable for the half-moon reflective tile of medium-intensity aviation obstruction lights, so as to concentrate the divergent light, and concentrate the collected light again through a convex lens assembly, so as to form a narrower and more concentrated light beam, thereby reducing pollution and energy consumption, thereby enhancing the practicality of the half-moon reflective tile for medium-intensity aviation obstruction lights; the utility model comprises a medium-intensity aviation obstruction light body, a battery, a fixing block and a protective cover, a cover plate assembly is arranged at the top of the medium-intensity aviation obstruction light body, a mounting seat is arranged at the bottom of the medium-intensity aviation obstruction light body, a lamp holder is arranged at the top of the cover plate assembly, an LED lamp is arranged at the top of the lamp holder, and solar energy components are arranged on the front, back, left and right four groups of outer walls of the medium-intensity aviation obstruction light body respectively.

Description

Technical Field

[0001] The utility model relates to the technical field of medium-intensity aviation obstruction light accessory devices, in particular to a half-moon-shaped reflective tile used for medium-intensity aviation obstruction lights. Background Art

[0002] As we all know, in the field of modern aviation, aviation obstruction lights play a vital role, especially in high-rise buildings, communication towers, wind turbines and other facilities around airports and on routes. They are widely deployed to ensure the safe navigation of aircraft at night or in low visibility conditions. The main purpose of aviation obstruction lights is to remind pilots to pay attention to potential air obstacles, prevent collision accidents, and maintain air traffic order and flight safety.

[0003] Medium intensity aviation obstruction lights are usually installed on structures at a height between 45 meters and 150 meters. The light intensity level is between 2,000 and 20,000 candela (cd). The design of this type of obstruction light must not only meet the requirements of visibility and light intensity, but also consider energy efficiency, environmental adaptability and the impact of light pollution on the surrounding environment;

[0004] Traditional medium-intensity aviation obstruction lights mostly use spherical or conical reflectors to disperse and reflect the light generated by the light source. However, this design has the following problems: the spherical or conical reflector cannot effectively control the directionality of the light, resulting in a large amount of light scattering, reducing the lighting efficiency, while also increasing the light pollution to the surrounding environment. In addition, since the light cannot be effectively focused, a larger power is required to compensate for the loss caused by light scattering, which not only increases energy consumption, but may also aggravate the light pollution problem, resulting in poor practicality. Utility Model Content

[0005] In order to solve the above technical problems, the utility model provides a half-moon reflective tile suitable for medium-intensity aviation obstruction lights, so as to concentrate the divergent light and concentrate the collected light again through a convex lens assembly to form a narrower and more concentrated light beam, thereby reducing pollution and energy consumption, thereby enhancing the practicality of a half-moon reflective tile for medium-intensity aviation obstruction lights.

[0006] The utility model discloses a half-moon shaped reflective tile for a medium-intensity aviation obstruction light, comprising a medium-intensity aviation obstruction light body, a battery, a fixed block and a protective cover. A cover plate assembly is arranged at the top of the medium-intensity aviation obstruction light body, a mounting seat is arranged at the bottom of the medium-intensity aviation obstruction light body, a lamp holder is arranged at the top of the cover plate assembly, an LED lamp is arranged at the top of the lamp holder, solar energy components are arranged on four groups of outer walls of the front, back, left and right of the medium-intensity aviation obstruction light body, a chamber is arranged inside the medium-intensity aviation obstruction light body, the bottom of the chamber is connected to the battery, a control mainboard is arranged at the bottom of the cover plate assembly, the top of the cover plate assembly is connected to the fixed block, the top of the fixed block is arranged with a half-moon reflective tile assembly, a first thread is arranged on the outer wall of the fixed block, a second thread is arranged at the inner end of the protective cover, and the first thread is threadedly connected with the second thread.

[0007] Preferably, the cover plate assembly includes a cover plate and screws, four groups of mounting threaded holes are arranged at the top of the medium-intensity aviation obstruction light body, four groups of mounting through holes are arranged at the top of the cover plate, the four groups of screws are threadedly connected to the mounting threaded holes through the mounting through holes respectively, the bottom end of the cover plate is connected to the control main board, and the top end of the cover plate is connected to the lamp holder and the fixing block.

[0008] Preferably, a sealing ring is provided at the bottom end of the cover plate.

[0009] Preferably, the half-moon reflective tile assembly includes four groups of half-moon reflective tiles and eight groups of first clamping blocks, the bottom ends of the four groups of half-moon reflective tiles are respectively connected to the two groups of first clamping blocks, the top of the fixing block is provided with eight groups of first clamping grooves, the eight groups of first clamping grooves are respectively clamped with the first clamping blocks, the four groups of half-moon reflective tiles are clamped and fixed by clamping assemblies, the tops of the four groups of half-moon reflective tiles are provided with convex lens fixing assemblies, and the inner ends of the four groups of half-moon reflective tiles are respectively provided with lens reflective films.

[0010] Preferably, the card-mounting components include four groups of second card-mounting blocks and four groups of third card-mounting blocks, the left ends of the four groups of half-moon reflective tiles are respectively connected to the second card-mounting blocks and the third card-mounting blocks, the right ends of the four groups of half-moon reflective tiles are respectively provided with second card-mounting grooves and third card-mounting grooves, the four groups of second card-mounting blocks are respectively card-mounted with the second card-mounting grooves, and the four groups of third card-mounting blocks are respectively card-mounted with the third card-mounting grooves.

[0011] Preferably, the outer walls of the four groups of half-moon reflective tiles are coated with fluorocarbon paint.

[0012] Preferably, the convex lens fixing assembly comprises four sets of fixing frames and convex lenses, the top ends of four sets of semicircular reflective tiles are respectively connected to the fixing frames, the inner ends of the four sets of fixing frames are respectively provided with lens clamping grooves, and the four sets of lens clamping grooves are all clamped with the convex lenses.

[0013] Preferably, the solar energy assembly includes four groups of solar panels, and the front, rear, left and right end faces of the medium-intensity aviation obstruction light body are respectively provided with a first mounting block and a second mounting block, the four groups of solar panels are respectively connected to the first mounting block and the second mounting block, and an inverter is provided in the chamber.

[0014] Compared with the prior art, the beneficial effects of the utility model are as follows: first, through the use of half-moon reflective tiles and convex lens assemblies, the originally divergent light can be re-gathered to form a more concentrated light beam, which not only improves the visibility of the obstacle light, but also makes the light more directional and reduces scattering. Moreover, since the light is better focused and utilized, the lamp does not need to excessively increase power to compensate for the brightness loss caused by light scattering, thereby significantly reducing energy consumption. Moreover, a more concentrated light beam means that only the necessary direction and range will be illuminated, reducing the irradiation of non-target areas, thereby reducing light pollution to the surrounding environment, and having less impact on the ecological environment and the quality of life of residents, thereby improving lighting efficiency and improving energy utilization efficiency, thereby enhancing practicality. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 It is a schematic diagram of the connection structure of the utility model;

[0016] Figure 2 It is a schematic diagram of the connection structure between the chamber and the battery of the utility model;

[0017] Figure 3 It is a schematic diagram of the connection structure between the half-moon reflective tile and the first clamping block of the utility model;

[0018] Figure 4 It is a schematic diagram of the enlarged structure of the A part of the utility model;

[0019] Markings in the attached drawings: 1. Medium-intensity aviation obstruction light body; 2. Mounting base; 3. Lamp holder; 4. LED lamp; 5. Chamber; 6. Battery; 7. Control main board; 8. Fixing block; 9. Protective cover; 10. Cover plate; 11. Screw; 12. Sealing ring; 13. Half-moon reflective tile; 14. First clamping block; 15. Lens reflective film; 16. Second clamping block; 17. Third clamping block; 18. Fixing bracket; 19. Convex lens; 20. First mounting block; 21. Second mounting block; 22. Solar panel; 23. Inverter. DETAILED DESCRIPTION

[0020] The following is a further detailed description of the specific implementation of the present invention in conjunction with the accompanying drawings and examples. The following examples are used to illustrate the present invention, but are not intended to limit the scope of the present invention.

[0021] like Figures 1 to 4As shown, the utility model is a half-moon-shaped reflective tile for a medium-intensity aviation obstruction light, comprising a medium-intensity aviation obstruction light body 1, a battery 6, a fixing block 8 and a protective cover 9. A cover plate 10 assembly is arranged at the top of the medium-intensity aviation obstruction light body 1, a mounting seat 2 is arranged at the bottom of the medium-intensity aviation obstruction light body 1, a lamp holder 3 is arranged at the top of the cover plate 10 assembly, and an LED lamp 4 is arranged at the top of the lamp holder 3. Solar energy components are arranged on the front, back, left and right four groups of outer walls of the medium-intensity aviation obstruction light body 1 respectively. A chamber 5 is arranged inside the medium-intensity aviation obstruction light body 1, and the bottom end of the chamber 5 is connected to the battery 6. A control main board 7 is arranged at the bottom end of the cover plate 10 assembly, and the top of the cover plate 10 assembly is connected to the fixing block 8. A half-moon reflective tile 13 assembly is arranged on the top of the fixing block 8, and a There is a first thread, and the inner end of the protective cover 9 is provided with a second thread, and the first thread is threadedly connected to the second thread; firstly, through the use of the half-moon reflective tile and the convex lens assembly, the originally divergent light can be re-gathered to form a more concentrated light beam, which not only improves the visibility of the obstacle light, but also makes the light more directional and reduces scattering. Moreover, since the light is better focused and utilized, the lamp does not need to excessively increase power to compensate for the brightness loss caused by light scattering, thereby significantly reducing energy consumption. Moreover, a more concentrated light beam means that only the necessary direction and range will be illuminated, reducing the irradiation of non-target areas, thereby reducing light pollution to the surrounding environment, and having less impact on the ecological environment and the quality of life of residents, thereby improving lighting efficiency and improving energy utilization efficiency, thereby enhancing practicality.

[0022] As a preferred embodiment of the above embodiment, the cover plate 10 assembly includes a cover plate 10 and screws 11. The top of the medium-intensity aviation obstruction light body 1 is provided with four groups of mounting threaded holes, and the top of the cover plate 10 is provided with four groups of mounting through holes. The four groups of screws 11 are threadedly connected with the mounting threaded holes through the mounting through holes respectively. The bottom end of the cover plate 10 is connected to the control main board 7, and the top end of the cover plate 10 is connected to the lamp holder 3 and the fixing block 8. The chamber of the medium-intensity aviation obstruction light body can be opened and closed by the cover plate and the four groups of screws, thereby facilitating the repair and maintenance of the parts in the chamber, thereby enhancing practicality.

[0023] As a preferred embodiment of the above embodiment, a sealing ring 12 is provided at the bottom end of the cover plate 10; the sealing ring can enhance the sealing between the cover plate and the medium-intensity aviation obstruction light body, thereby enhancing practicality.

[0024] As a preferred embodiment of the above embodiment, the half-moon reflective tile 13 assembly includes four groups of half-moon reflective tiles 13 and eight groups of first clamping blocks 14, the bottom ends of the four groups of half-moon reflective tiles 13 are respectively connected to the two groups of first clamping blocks 14, the top of the fixing block 8 is provided with eight groups of first clamping grooves, the eight groups of first clamping grooves are respectively clamped with the first clamping blocks 14, the four groups of half-moon reflective tiles 13 are clamped and fixed by the clamping assembly, the top of the four groups of half-moon reflective tiles 13 is provided with a convex lens 19 fixing assembly, and the inner ends of the four groups of half-moon light-emitting tiles are respectively provided with lens reflective films 15; when installing the four groups of half-moon reflective tiles, the four groups of half-moon reflective tiles are assembled by the clamping assembly, and then the four groups of half-moon reflective tiles are clamped and fixed by the eight groups of first clamping blocks, so that the light is refracted by the four groups of half-moon reflective tiles, thereby enhancing practicality.

[0025] As a preferred embodiment of the above embodiment, the card-mounting components include four groups of second card-mounting blocks 16 and four groups of third card-mounting blocks 17. The left ends of the four groups of half-moon reflective tiles 13 are respectively connected to the second card-mounting blocks 16 and the third card-mounting blocks 17. The right ends of the four groups of half-moon reflective tiles 13 are respectively provided with second card-mounting grooves and third card-mounting grooves. The four groups of second card-mounting blocks 16 are respectively card-mounted with the second card-mounting grooves, and the four groups of third card-mounting blocks 17 are respectively card-mounted with the third card-mounting grooves. The second card-mounting blocks and the third card-mounting blocks at the left ends of the four groups of half-moon reflective tiles can be card-mounted and fixed with the second card-mounting grooves and the third card-mounting grooves at their right ends, thereby facilitating later installation and thus enhancing practicality.

[0026] As a preferred embodiment of the above embodiment, the outer walls of the four groups of half-moon reflective tiles 13 are coated with fluorocarbon paint; fluorocarbon paint has good light and color retention, weather resistance, corrosion resistance and other effects, so that the outer walls of the half-moon reflective tiles have the effect of preventing ultraviolet oxidation, thereby enhancing practicality.

[0027] As a preferred embodiment of the above, the convex lens 19 fixing assembly comprises four groups of fixing frames 18 and convex lenses 19, the top ends of the four groups of semicircular reflective tiles are respectively connected to the fixing frames 18, the inner ends of the four groups of fixing frames 18 are respectively provided with lens clamping grooves, and the four groups of lens clamping grooves are all clamped with the convex lenses 19; the convex lenses can be fixed and clamped by the four groups of fixing frames to gather the reflected light, thereby reducing light pollution and enhancing practicality.

[0028] As a preferred embodiment of the above, the solar energy assembly includes four groups of solar panels 22, and the front, rear, left and right end surfaces of the medium-intensity aviation obstruction light body 1 are respectively provided with a first mounting block 20 and a second mounting block 21, and the four groups of solar panels 22 are respectively connected to the first mounting block 20 and the second mounting block 21, and an inverter 23 is provided in the chamber 5; the medium-intensity aviation obstruction light body can be self-sufficient in energy through the four groups of solar panels, inverters and batteries, thereby enhancing practicality.

[0029] The utility model is a half-moon shaped reflective tile for medium-intensity aviation obstruction lights. Its working principle is that when it is working, the medium-intensity aviation obstruction light is first installed in a suitable position through a mounting seat, and then the battery is powered by the solar panel and the inverter, so as to power the control mainboard and the LED lamp through the battery, and then the LED light is refracted through four groups of half-moon reflective tiles, and the divergent light is collected through the convex lens, and the light is irradiated through the color of the protective cover, and then the half-moon reflector or the LED lamp is needed. When replacing, the protective cover is unscrewed through the first thread and the second thread, and then the four groups of half-moon reflective tiles that are installed are removed, and then the bulb can be replaced, and then the four groups of half-moon reflective tiles that are installed are contact-installed, and then the convex lens is removed for maintenance, and then if the four groups of half-moon reflective tiles are damaged, they can be replaced, and then the convex lens is re-installed and the four groups of half-moon reflective tiles are fixed by the second and third clamping blocks, and then reinstalled by the eight groups of first clamping blocks, and then the protective cover is screwed on and the medium-intensity aviation obstruction light can continue to be used.

[0030] The terms "vertical," "horizontal," "left," "right," and the like are used herein for illustrative purposes only.

[0031] The “first”, “second” and “third” mentioned in the present invention do not represent specific quantities and orders, but are merely used to distinguish names.

[0032] The above is only a preferred embodiment of the present invention. It should be pointed out that for ordinary technicians in this technical field, several improvements and modifications can be made without departing from the technical principle of the present invention. These improvements and modifications should also be regarded as the protection scope of the present invention.

Claims

1. A half-moon reflective tile for medium-intensity aviation obstruction lights, characterized in that: The medium-intensity aviation obstruction light comprises a main body (1), a storage battery (6), a fixing block (8) and a protective cover (9); a cover plate (10) component is arranged at the top of the main body (1); a mounting seat (2) is arranged at the bottom of the main body (1); a lamp holder (3) is arranged at the top of the cover plate (10) component; an LED lamp (4) is arranged at the top of the lamp holder (3); and solar panels (5) are arranged on the front, rear, left and right outer walls of the main body (1). The medium-intensity aviation obstruction light body (1) is provided with a chamber (5) inside, the bottom end of the chamber (5) is connected to a battery (6), the bottom end of the cover plate (10) assembly is provided with a control main board (7), the top end of the cover plate (10) assembly is connected to a fixed block (8), the top end of the fixed block (8) is provided with a half-moon reflective tile (13) assembly, the outer wall of the fixed block (8) is provided with a first thread, the inner end of the protective cover (9) is provided with a second thread, and the first thread is threadedly connected to the second thread.

2. A half-moon shaped reflective tile for medium intensity aviation obstruction lights as claimed in claim 1, characterized in that: The cover plate (10) assembly comprises a cover plate (10) and screws (11); the top of the medium-intensity aviation obstruction light body (1) is provided with four groups of mounting threaded holes; the top of the cover plate (10) is provided with four groups of mounting through holes; the four groups of screws (11) are respectively threadedly connected to the mounting threaded holes through the mounting through holes; the bottom end of the cover plate (10) is connected to the control main board (7); the top end of the cover plate (10) is connected to the lamp holder (3) and the fixing block (8).

3. A half-moon shaped reflective tile for medium intensity aviation obstruction lights as claimed in claim 2, characterized in that: A sealing ring (12) is provided at the bottom end of the cover plate (10).

4. A half-moon shaped reflective tile for medium intensity aviation obstruction lights as claimed in claim 3, characterized in that: The half-moon reflective tile (13) assembly comprises four groups of half-moon reflective tiles (13) and eight groups of first clamping blocks (14). The bottom ends of the four groups of half-moon reflective tiles (13) are respectively connected to the two groups of first clamping blocks (14). The top end of the fixing block (8) is provided with eight groups of first clamping grooves. The eight groups of first clamping grooves are respectively clamped with the first clamping blocks (14). The four groups of half-moon reflective tiles (13) are clamped and fixed by the clamping assembly. The top ends of the four groups of half-moon reflective tiles (13) are provided with convex lens (19) fixing assemblies. The inner ends of the four groups of half-moon reflective tiles are respectively provided with lens reflective films (15).

5. The half-moon-shaped reflective tile for medium-intensity aviation obstruction lights as claimed in claim 4, characterized in that: The clamping assembly comprises four groups of second clamping blocks (16) and four groups of third clamping blocks (17); the left ends of the four groups of half-moon reflective tiles (13) are respectively connected to the second clamping blocks (16) and the third clamping blocks (17); the right ends of the four groups of half-moon reflective tiles (13) are respectively provided with second clamping grooves and third clamping grooves; the four groups of second clamping blocks (16) are respectively clamped to the second clamping grooves; and the four groups of third clamping blocks (17) are respectively clamped to the third clamping grooves.

6. The half-moon-shaped reflective tile for medium-intensity aviation obstruction lights as claimed in claim 5, characterized in that: The outer walls of the four groups of half-moon reflective tiles (13) are coated with fluorocarbon paint.

7. A half-moon shaped reflective tile for a medium-intensity aviation obstruction light as claimed in claim 6, characterized in that: The convex lens (19) fixing assembly comprises four groups of fixing frames (18) and convex lenses (19), the top ends of the four groups of semicircular reflective tiles are respectively connected to the fixing frames (18), the inner ends of the four groups of fixing frames (18) are respectively provided with lens clamping grooves, and the four groups of lens clamping grooves are all clamped with the convex lenses (19).

8. The half-moon-shaped reflective tile for medium-intensity aviation obstruction lights as claimed in claim 7, characterized in that: The solar energy assembly comprises four groups of solar panels (22); four groups of end faces, front, back, left and right, of a medium-intensity aviation obstruction light body (1) are respectively provided with a first mounting block (20) and a second mounting block (21); the four groups of solar panels (22) are respectively connected to the first mounting block (20) and the second mounting block (21); and an inverter (23) is provided in the chamber (5).

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