Heat dissipation ring for aviation obstruction beacon

Abstract

The utility model relates to the technical field of heat dissipation assemblies for aviation obstruction lights, in particular to a heat dissipation ring for an aviation obstruction light, which comprises an aviation obstruction light body and a heat dissipation ring, a heat dissipation mechanism is arranged on the heat dissipation ring, the heat dissipation mechanism comprises heat dissipation fins, the heat dissipation fins are arranged on the outer side of the heat dissipation ring, and the heat dissipation fins are arranged on the outer side of the heat dissipation ring. The multiple heat dissipation fins are arranged in an annular array mode, an assembling mechanism is arranged between the aviation obstruction beacon body and the heat dissipation ring, the assembling mechanism comprises a threaded ring and a threaded groove, and the threaded groove is formed in the bottom end of the inner wall of the heat dissipation ring. According to the structure, rapid and firm assembly of the heat dissipation ring and the aviation obstruction beacon body is achieved through the assembly mechanism, a user can complete installation only through simple operation, stable and reliable connection between the heat dissipation ring and the beacon body in the transportation and use process is guaranteed, and the loosening problem caused by vibration is avoided.

Description

Technical Field

[0001] The utility model relates to the technical field of heat dissipation components for aviation obstruction lights, in particular to a heat dissipation ring used for aviation obstruction lights. Background Art

[0002] As we all know, in the aviation field, aviation obstruction lights are important safety equipment and need to ensure continuous and stable operation. These lights are usually installed on high towers, building tops or hangars to indicate the presence of obstacles and prevent aircraft collisions. Aviation obstruction lights generate a lot of heat. If the heat cannot be effectively dissipated, it will directly affect the life and performance of the lights. Therefore, an efficient heat dissipation mechanism is crucial to ensure the reliability of aviation obstruction lights.

[0003] Traditional heat dissipation designs may use a simple heat sink structure or a heat sink ring with an insecure fixing method, which may lead to problems such as low heat dissipation efficiency, loose installation, and difficult maintenance. Therefore, it is necessary to propose a solution to this technical problem. Utility Model Content

[0004] 1. Technical issues to be solved

[0005] In view of the deficiencies of the prior art, the utility model provides a heat dissipation ring for an aviation obstruction light.

[0006] (II) Technical solution

[0007] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a heat dissipation ring for an aviation obstruction light, comprising an aviation obstruction light body and a heat dissipation ring, the heat dissipation ring being provided with a heat dissipation mechanism, the heat dissipation mechanism comprising heat dissipation fins, the heat dissipation fins being installed on the outside of the heat dissipation ring, the heat dissipation fins being provided in a plurality and being arranged in a ring array, an assembly mechanism being provided between the aviation obstruction light body and the heat dissipation ring, the assembly mechanism comprising a threaded ring and a threaded groove, the threaded groove being provided at the bottom end of the inner wall of the heat dissipation ring, a fastening groove being provided at the top end of the threaded groove, a fastening hole being provided between the fastening groove and the top end of the heat dissipation ring, a fastening column being provided on the fastening hole, a fastening plate being provided between the fastening column and the fastening groove, a toothed plate being provided at the bottom end of the fastening plate, a limiting mechanism and an elastic component being provided between the fastening plate and the fastening groove, the threaded ring being installed on the aviation obstruction light body, and an annular toothed groove being provided at the top end of the threaded ring.

[0008] Furthermore, the utility model is improved in that the heat dissipation mechanism also includes a heat dissipation hole, and the heat dissipation hole is opened on the heat dissipation fin, and there are a plurality of heat dissipation holes.

[0009] Furthermore, the utility model is improved in that the heat dissipation mechanism also includes a copper tube, and the copper tube passes through the plurality of heat dissipation fins.

[0010] Furthermore, the utility model is improved in that the copper tube is in an annular structure and a plurality of the copper tubes are provided.

[0011] Furthermore, the utility model is improved in that the limiting mechanism comprises a limiting groove, the limiting groove is opened on one side of the fastening groove, and a limiting block is provided between the fastening plate and the limiting groove.

[0012] Furthermore, the utility model is improved in that the limiting mechanisms are provided with two and are symmetrically arranged.

[0013] Furthermore, the utility model is improved in that a plurality of elastic components are provided.

[0014] Furthermore, the utility model is improved in that the elastic component is an alloy spring.

[0015] (III) Beneficial effects

[0016] Compared with the prior art, the utility model provides a heat dissipation ring for aviation obstruction lights, which has the following beneficial effects:

[0017] The heat dissipation ring used in the aviation obstruction light realizes the fast and firm assembly of the heat dissipation ring and the aviation obstruction light body through the assembly mechanism. The user only needs to perform simple operations to complete the installation and ensure that the connection between the heat dissipation ring and the lamp body is stable and reliable during transportation and use, avoiding the problem of looseness caused by vibration. Through multiple heat dissipation fins, the surface area can be effectively increased, and the heat transfer from the lamp body to the air can be accelerated, thereby improving the heat dissipation performance and extending the service life of the lamp. It is particularly suitable for high-power, long-running aviation obstruction lights to ensure that they are always within a safe operating temperature range;

[0018] When the heat dissipation fins accumulate dust due to long-term use and affect the heat dissipation efficiency, the quick disassembly mechanism provided by the utility model becomes a highlight. The user only needs to pull the fastening column and rotate the heat dissipation ring to easily separate the heat dissipation ring for cleaning or replacement, which greatly simplifies the maintenance process, reduces maintenance costs, and ensures that the lamp maintains a good heat dissipation state for a long time. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 This is a schematic diagram of the structure of the utility model Figure 1 ;

[0020] Figure 2 This is a schematic diagram of the structure of the utility model Figure 2 ;

[0021] Figure 3 This is a half-section view of the structure of the utility model;

[0022] Figure 4It is a top view of the structure of the utility model in half section.

[0023] In the figure: 1. Aviation obstruction light body; 2. Heat dissipation ring; 3. Heat dissipation fins; 4. Threaded ring; 5. Fastening column; 6. Fastening plate; 7. Tooth plate; 8. Elastic component; 9. Annular tooth groove; 10. Heat dissipation hole; 11. Copper tube; 12. Limit block. DETAILED DESCRIPTION

[0024] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0025] See also Figure 1-4The utility model is a heat dissipation ring for an aviation obstruction light, comprising an aviation obstruction light body 1 and a heat dissipation ring 2, wherein the heat dissipation ring 2 is provided with a heat dissipation mechanism, wherein the heat dissipation mechanism comprises heat dissipation fins 3, wherein the heat dissipation fins 3 are mounted on the outside of the heat dissipation ring 2, wherein the heat dissipation fins 3 are provided with a plurality of heat dissipation fins 3 and are arranged in an annular array, wherein an assembly mechanism is provided between the aviation obstruction light body 1 and the heat dissipation ring 2, wherein the assembly mechanism comprises a threaded ring 4 and a threaded groove, wherein the threaded groove is provided at the bottom end of the inner wall of the heat dissipation ring 2, wherein a fastening groove is provided at the top end of the threaded groove, wherein the fastening groove is fastened to the top of the heat dissipation ring 2 A fastening hole is provided between the ends, a fastening column 5 is provided on the fastening hole, a fastening plate 6 is provided between the fastening column 5 and the fastening groove, a tooth plate 7 is provided at the bottom end of the fastening plate 6, a limiting mechanism and an elastic component 8 are provided between the fastening plate 6 and the fastening groove, the threaded ring 4 is installed on the aviation obstruction light body 1, and an annular tooth groove 9 is provided at the top of the threaded ring 4. In this embodiment, the fastening column 5 on the heat dissipation ring 2 is pulled, and the fastening column 5 drives the fastening plate 6 to move, so that the elastic component 8 is squeezed by the fastening plate 6 and shrinks and deforms in the fastening groove. At this time, the tooth plate 7 moves into the fastening groove and is fixed by the heat dissipation ring 2 passes through the aviation obstruction light body 1, and then is threadedly connected with the threaded ring 4 of the aviation obstruction light body 1 through the threaded groove, so that the heat dissipation ring 2 is assembled on the aviation obstruction light body 1, and then the fastening column 5 is loosened to fine-tune the angle of the heat dissipation ring 2. When the tooth plate 7 is aligned with the annular tooth groove 9 opened at the top of the threaded ring 4, the fastening plate 6 is supported by the elastic component 8 so that the tooth plate 7 and the annular tooth groove 9 are meshed together, so that the heat dissipation ring 2 is firmly fixed in the aviation obstruction light body 1. When it is subjected to external shaking during transportation, etc., there will be no loosening between the threaded ring 4 and the threaded groove, ensuring that the heat dissipation ring 2 is firmly fixed to the aviation obstruction light body 1. The installation firmness between the aviation obstruction light body 1, when the aviation obstruction light body 1 is in use, the heat generated by the aviation obstruction light body 1 during operation is absorbed by the heat dissipation ring 2, and the multiple heat dissipation fins 3 in the heat dissipation mechanism can absorb the heat and then volatilize it into the outside air to achieve heat dissipation of the aviation obstruction light body 1. After long-term use, dust and foreign matter will accumulate on the heat dissipation fins 3, affecting the heat dissipation efficiency of the heat dissipation ring 2. At this time, by pulling the fastening column 5, the toothed plate 7 leaves the annular tooth groove 9, and then rotating the heat dissipation ring 2 to make the threaded ring 4 leave the threaded groove, thereby realizing quick disassembly of the heat dissipation ring 2, which is convenient for cleaning or replacement of the heat dissipation ring 2.

[0026] In this embodiment, the heat dissipation mechanism also includes a heat dissipation hole 10, and the heat dissipation hole 10 is opened on the heat dissipation fin 3. There are multiple heat dissipation holes 10. Through the multiple heat dissipation holes 10 opened on the heat dissipation fin 3, air passes through the heat dissipation holes 10, which can improve the efficiency of heat dissipation of the heat dissipation fin 3.

[0027] In this solution, the heat dissipation mechanism also includes a copper tube 11, which passes through the multiple heat dissipation fins 3. By passing the copper tube 11 through the multiple heat dissipation fins 3, the heat of the heat dissipation fins 3 can be evenly dispersed to each heat dissipation fin 3 through the copper tube 11, thereby achieving more uniform and efficient heat dissipation.

[0028] In this solution, the copper tube 11 is in an annular structure, and a plurality of the copper tubes 11 are provided. The plurality of annular copper tubes 11 can better conduct heat and disperse the heat to the heat sink fins 3 more efficiently.

[0029] In the present embodiment, the limiting mechanism includes a limiting groove, which is opened on one side of the fastening groove. A limiting block 12 is provided between the fastening plate 6 and the limiting groove. The limiting block 12 between the fastening plate 6 and the limiting groove can limit the fastening plate 6. When the heat dissipation ring 2 is removed, the fastening plate 6 is effectively limited to prevent the fastening plate 6 from being separated from the fastening groove.

[0030] In this solution, two limiting mechanisms are provided and are symmetrically arranged. By providing two limiting mechanisms that are symmetrically arranged, the fastening plate 6 can be limited more stably, so that the fastening plate 6 can be limited more stably.

[0031] In this solution, a plurality of elastic components 8 are provided, and the plurality of elastic components 8 can provide better elastic support to the fastening plate 6 .

[0032] In this solution, the elastic component 8 is an alloy spring. The alloy spring has the characteristic of good elastic effect, so it can have a stable elastic supporting force in this structure.

[0033] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A heat dissipation ring for an aviation obstruction light, comprising an aviation obstruction light body (1) and a heat dissipation ring (2), wherein the heat dissipation ring (2) is provided with a heat dissipation mechanism, characterized in that: The heat dissipation mechanism comprises heat dissipation fins (3), the heat dissipation fins (3) are mounted on the outer side of the heat dissipation ring (2), a plurality of the heat dissipation fins (3) are provided and arranged in a ring array, an assembly mechanism is provided between the aviation obstruction light body (1) and the heat dissipation ring (2), the assembly mechanism comprises a threaded ring (4) and a threaded groove, the threaded groove is provided at the bottom end of the inner wall of the heat dissipation ring (2), a fastening groove is provided at the top end of the threaded groove, a fastening hole is provided between the fastening groove and the top end of the heat dissipation ring (2), a fastening column (5) is provided on the fastening hole, a fastening plate (6) is provided between the fastening column (5) and the fastening groove, a toothed plate (7) is provided at the bottom end of the fastening plate (6), a limiting mechanism and an elastic component (8) are provided between the fastening plate (6) and the fastening groove, the threaded ring (4) is mounted on the aviation obstruction light body (1), and an annular toothed groove (9) is provided at the top end of the threaded ring (4).

2. A heat dissipation ring for an aviation obstruction light according to claim 1, characterized in that: The heat dissipation mechanism further comprises a heat dissipation hole (10), wherein the heat dissipation hole (10) is provided on the heat dissipation fin (3), and a plurality of the heat dissipation holes (10) are provided.

3. The heat dissipation ring for aviation obstruction lights according to claim 2, characterized in that: The heat dissipation mechanism further comprises a copper tube (11), wherein the copper tube (11) passes through the plurality of heat dissipation fins (3).

4. The heat dissipation ring for aviation obstruction lights according to claim 3, characterized in that: The copper tube (11) is in an annular structure, and a plurality of the copper tubes (11) are provided.

5. The heat dissipation ring for aviation obstruction lights according to claim 4, characterized in that: The limiting mechanism comprises a limiting groove, the limiting groove is arranged on one side of the fastening groove, and a limiting block (12) is arranged between the fastening plate (6) and the limiting groove.

6. The heat dissipation ring for aviation obstruction lights according to claim 5, characterized in that: The limiting mechanisms are provided with two and are symmetrically arranged.

7. The heat dissipation ring for aviation obstruction lights according to claim 6, characterized in that: The elastic component (8) is provided in plurality.

8. The heat dissipation ring for aviation obstruction lights according to claim 7, characterized in that: The elastic component (8) is an alloy spring.

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